METHOD FOR FORMING A TUBE

[0001] The present application claims priority on United States Provisional Application serial No. 63//226,289 filed July 28, 2021, which is incorporated herein by reference.

[0002] The invention relates generally to medical devices and medical device applications.

SUMMARY OF THE INVENTION

[0003] The present invention is direct to a medical device that is at least partially made of a biomedical material. The biomedical material can be fully or partially formed of a novel alloy having improved properties as compared to past medical devices. As defined herein, biomedical material is a material that is suitable for use in partially or fully forming an implant or other type of medical device. The biomedical material is not a biological agent as defined herein. The biomedical material can be partially or fully formed of a metal alloy, bone, cartilage, ceramic material, and/or composite materials (e.g., material containing one or more carbon fibers, boron fibers glass fibers, aramid fibers [Kevlar, Twaron, etc.], basalt fibers, etc.).

[0004] In one non-limiting aspect of the present disclosure, the biomedical material is partially or fully formed of a novel metal alloy, which novel metal alloy is used to at least partially form a medical device, which medical device has one or more improved properties (e.g., strength, durability, hardness, biostability, bendability, coefficient of friction, radial strength, flexibility, tensile strength, tensile elongation, longitudinal lengthening, stress-strain properties, improved recoil properties, radiopacity, heat sensitivity, biocompatibility, improved fatigue life, crack resistance, crack propagation resistance, etc.) of such medical device. These one or more improved physical properties of the novel alloy can be achieved in the medical device without having to increase the bulk, volume and/or weight of the medical device, and in some instances these improved physical properties can be obtained even when the volume, bulk and/or weight of the medical device is reduced as compared to medical devices that are at least partially formed from traditional stainless steel or cobalt and chromium alloy materials. However, it will be appreciated that the novel alloy can include metals such as stainless steel, cobalt and chromium, etc.

[0005] The novel alloy that is used to at least partially form the medical device can thus 1) increase the radiopacity of the medical device, 2) increase the radial strength of the medical device, 3) increase the yield strength and/or ultimate tensile strength of the medical device, 4) improve the stress-strain properties of the medical device, 5) improve the crimping and/or expansion properties of the medical device, 6) improve the bendability and/or flexibility of the medical device, 7) improve the strength and/or durability of the medical device, 8) increase the hardness of the medical device, 9) improve the longitudinal lengthening properties of the medical device, 10) improve the recoil properties of the medical device, 11) improve the friction coefficient of the medical device, 12) improve the heat sensitivity properties of the medical device, 13) improve the biostability and/or biocompatibility properties of the medical device, 14) increase fatigue resistance of the medical device, 15) resist cracking in the medical device and resist propagation of crack, and/or 16) enable smaller, thinner and/or lighter weight medical devices to be made. The medical device generally includes one or more materials that impart the desired properties to the medical device so as to withstand the manufacturing processes that are needed to produce the medical device. These manufacturing processes can include, but are not limited to, laser cutting, etching, crimping, annealing, drawing, pilgering, electroplating, electro-polishing, machining, plasma coating, 3D printing, 3D printed coatings, chemical vapor deposition, chemical polishing, cleaning, pickling, ion beam deposition or implantation, sputter coating, vacuum deposition, etc. In one non-limiting embodiment, the medical device is partially or fully formed by a 3D printing process.

[0006] In another non-limiting aspect of the present invention, a medical device that can include the novel alloy is an orthopedic device; PFO (patent foramen ovale) device; stent; valve (e.g., heart valve, TAVR valve, etc.); spinal implant; frame and other structures for use with a spinal implant; vascular implant; graft; guide wire; sheath; catheter; needle; stent catheter; electrophysiology catheter; hypotube; staple; cutting device; any type of implant; pacemaker; dental implant; dental crown; dental braces; wire for used in medical procedures; bone implant; prosthetic implant or device to repair, replace and/or support a bone (e.g., acromion, atlas, axis, calcaneus, carpus, clavicle, coccyx, epicondyle, epitrochlea, femur, fibula, frontal bone, greater trochanter, humerus, ilium, ischium, mandible, maxilla, metacarpus, metatarsus, occipital bone, olecranon, parietal bone, patella, phalanx, radius, ribs, sacrum, scapula, sternum, talus, tarsus, temporal bone, tibia, ulna, zygomatic bone, etc.) and/or cartilage; nail; rod; screw; post; cage; plate; pedicle screw; cap; hinge; joint system; anchor; spacer; shaft; anchor; disk; ball; tension band; locking connector other structural assembly that is used in a body to support a structure, mount a structure and/or repair a structure in a body such as, but not limited to, a human body. In one non-limiting application, the medical device is a spinal implant. In another non-limiting application, the medical device is a prosthetic device. In another non-limiting application, the medical device is a stent. In another non-limiting application, the medical device is a TAVR valve. [0007] Although the present invention will be described with particular reference to medical devices, it will be appreciated that the novel alloy can be used in other components that are subjected to stresses that can lead to cracking and fatigue failure (e.g., automotive parts, springs, aerospace parts, industrial machinery and parts, tools (e.g., medical tools, industrial tools, household tools), etc.).

[0008] In another and/or alternative non-limiting aspect of the present invention, the novel alloy has a generally uniform density throughout the novel alloy, and also results in the desired yield and ultimate tensile strengths of the novel alloy. The density of the novel alloy is generally at least about 5 gm/cc (e.g., 5 gm/cc-20 gm/cc and all values and ranges therebetween; 12-20 gm/cc; etc.), and typically at least about 13-13.5 gm/cc. This substantially uniform high density of the novel alloy significantly improves the radiopacity of the novel alloy.

[0009] In another and/or alternative non-limiting aspect of the present invention, the novel alloy includes a certain amount of carbon and oxygen; however, this is not required. These two elements have been found to affect the forming properties and brittleness of the novel alloy. The controlled atomic ratio of carbon and oxygen of the novel alloy also can be used to minimize the tendency of the novel alloy to form micro-cracks during the forming of the novel alloy into a medical device, and/or during the use and/or expansion of the medical device in a body passageway. The control of the atomic ratio of carbon to oxygen in the novel alloy allows for the redistribution of oxygen in the novel alloy so as to minimize the tendency of micro-cracking in the novel alloy during the forming of the novel alloy into a medical device, and/or during the use and/or expansion of the medical device in a body passageway. The atomic ratio of carbon to oxygen in the novel alloy is believed to be important to minimize the tendency of micro-cracking in the novel alloy and improve the degree of elongation of the novel alloy, both of which can affect one or more physical properties of the novel alloy that are useful or desired in forming and/or using the medical device. The carbon to oxygen atomic ratio can be as low as about 0.2:1 (e.g., 0.2:1 to 50:1 and all values and ranges therebetween). In one non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally at least about 0.4: 1 (i.e., weight ratio of about 0.3:1). In another non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally at least about 0.5:1 (i.e., weight ratio of about 0.375:1). In still another non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally at least about 1 : 1 (i.e., weight ratio of about 0.75: 1). In yet another non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally at least about 2: 1 (i.e., weight ratio of about 1.5:1). In still yet another non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally at least about 2.5:1 (i.e., weight ratio of about 1.88:1). In still another non limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally at least about 3:1 (i.e., weight ratio of about 2.25: 1). In yet another non-limiting formulation, the carbon to oxygen atomic ratio of the novel alloy is generally at least about 4: 1 (i.e., weight ratio of about 3: 1). In still yet another non-limiting formulation, the carbon to oxygen atomic ratio of the novel alloy is generally at least about 5: 1 (i.e., weight ratio of about 3.75: 1). In still another non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally about 2.5-50: 1 (i.e., weight ratio of about 1.88-37.54:1). In a further non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally about 2.5-20:1 (i.e., weight ratio of about 1.88-15:1). In a further non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally about 2.5-13.3:1 (i.e., weight ratio of about 1.88-10:1). In still a further non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally about 2.5-10: 1 (i.e., weight ratio of about 1.88-7.5:1). In yet a further non-limiting formulation, the carbon to oxygen atomic ratio in the novel alloy is generally about 2.5-5: 1 (i.e., weight ratio of about 1.88-3.75:1). As can be appreciated, other atomic ratios of the carbon to oxygen in the novel alloy can be used. The carbon to oxygen ratio can be adjusted by intentionally adding carbon to the novel alloy until the desired carbon to oxygen ratio is obtained. Typically the carbon content of the novel alloy is less than about 0.2 wt.% (e.g., 0 wt.% to 0.1999999 wt.% and all values and ranges therebetween). Carbon contents that are too large can adversely affect the physical properties of the novel alloy. In one non-limiting formulation, the carbon content of the novel alloy is less than about 0.1 wt.% of the novel alloy. In another non-limiting formulation, the carbon content of the novel alloy is less than about 0.05 wt.% of the novel alloy of the novel alloy. In still another non-limiting formulation, the carbon content of the novel alloy is less than about 0.04 wt.% of the novel alloy. When carbon is not intentionally added to the novel alloy of the novel alloy, the novel alloy can include up to about 150 ppm carbon, typically up to about 100 ppm carbon, and more typically less than about 50 ppm carbon. The oxygen content of the novel alloy can vary depending on the processing parameters used to form the novel alloy of the novel alloy. Generally, the oxygen content is to be maintained at very low levels. In one non-limiting formulation, the oxygen content is less than about 0.1 wt.% of the novel alloy (e.g., 0 wt. to 0.0999999 wt.% and all values and ranges therebetween). In another non-limiting formulation, the oxygen content is less than about 0.05 wt.% of the novel alloy. In still another non-limiting formulation, the oxygen content is less than about 0.04 wt.% of the novel alloy. In yet another non-limiting formulation, the oxygen content is less than about 0.03 wt.% of the novel alloy. In still yet another non-limiting formulation, the novel alloy includes up to about 100 ppm oxygen. In a further non-limiting formulation, the novel alloy includes up to about 75 ppm oxygen. In still a further non-limiting formulation, the novel alloy includes up to about 50 ppm oxygen. In yet a further non-limiting formulation, the novel alloy includes up to about 30 ppm oxygen. In still yet a further non-limiting formulation, the novel alloy includes less than about 20 ppm oxygen. In yet a further non-limiting formulation, the novel alloy includes less than about 10 ppm oxygen. As can be appreciated, other amounts of carbon and/or oxygen in the novel alloy can exist. It is believed that the novel alloy will have a very low tendency to form micro-cracks during the formation of the medical device and after the medical device has been inserted into a patient by closely controlling the carbon to oxygen ration when the oxygen content exceeds a certain amount in the novel alloy. In one non- limiting arrangement, the carbon to oxygen atomic ratio in the novel alloy is at least about 2.5:1 when the oxygen content is greater than about 100 ppm in the novel alloy of the novel alloy. [0010] In another and/or alternative non-limiting aspect of the present invention, the novel alloy includes a controlled amount of nitrogen; however, this is not required. Large amounts of nitrogen in the novel alloy can adversely affect the ductility of the novel alloy of the novel alloy. This can in turn adversely affect the elongation properties of the novel alloy. A too high nitrogen content in the novel alloy can begin to cause the ductility of the novel alloy to unacceptably decrease, thus adversely affect one or more physical properties of the novel alloy that are useful or desired in forming and/or using the medical device. In one non-limiting formulation, the novel alloy includes less than about 0.001 wt.% nitrogen (e.g., 0 wt.% to 0.0009999 wt.% and all values and ranges therebetween). In another non-limiting formulation, the novel alloy includes less than about 0.0008 wt.% nitrogen. In still another non-limiting formulation, the novel alloy includes less than about 0.0004 wt.% nitrogen. In yet another non-limiting formulation, the novel alloy includes less than about 30 ppm nitrogen. In still yet another non-limiting formulation, the novel alloy includes less than about 25 ppm nitrogen. In still another non-limiting formulation, the novel alloy includes less than about 10 ppm nitrogen. In yet another non-limiting formulation, the novel alloy of the novel alloy includes less than about 5 ppm nitrogen. As can be appreciated, other amounts of nitrogen in the novel alloy can exist. The relationship of carbon, oxygen and nitrogen in the novel alloy is also believed to be important. It is believed that the nitrogen content should be less than the content of carbon or oxygen in the novel alloy. In one non-limiting formulation, the atomic ratio of carbon to nitrogen is at least about 1.5:1 (e.g., 1.5: 1 to 400: 1 and all values and ranges therebetween). In another non-limiting formulation, the atomic ratio of carbon to nitrogen is at least about 1:1.71. In another non-limiting formulation, the atomic ratio of carbon to nitrogen is at least about 2: 1 (i.e., weight ratio of about 2.57: 1). In another non-limiting formulation, the atomic ratio of carbon to nitrogen is at least about 3:1 (i.e., weight ratio of about 3.43-85.7:1, weight ratio of about 3.43-64.3: 1, weight ratio of about 3.43-42.85: 1). In still another non-limiting formulation, the atomic ratio of carbon to nitrogen is about 3-100: 1. In yet another non-limiting formulation, the atomic ratio of carbon to nitrogen is about 3-75:1. In still another non-limiting formulation, the atomic ratio of carbon to nitrogen is about 3-50:1. In yet another non-limiting formulation, the atomic ratio of carbon to nitrogen is about 3-35: 1 (i.e., weight ratio of about 3.43- 30: 1). In still yet another non-limiting formulation, the atomic ratio of carbon to nitrogen is about 3-25: 1 (i.e., weight ratio of about 3.43-21.43: 1). In a further non-limiting formulation, the atomic ratio of oxygen to nitrogen is at least about 1.2:1 (e.g., 1.2:1 to 150:1 and all value and ranges therebetween). In another non-limiting formulation, the atomic ratio of oxygen to nitrogen is at least about 1.37:1. In another non-limiting formulation, the atomic ratio of oxygen to nitrogen is at least about 2: 1 (i.e., weight ratio of about 2.28: 1). In still another non-limiting formulation, the atomic ratio of oxygen to nitrogen is about 3-100:1 (i.e., weight ratio of about 3.42-114.2:1). In yet another non-limiting formulation, the atomic ratio of oxygen to nitrogen is at least about 3- 75:1 (i.e., weight ratio of about 3.42-85.65:1, weight ratio of about 3.42-57.1:1, weight ratio of about 3.42-62.81:1). In still yet another non-limiting formulation, the atomic ratio of oxygen to nitrogen is at least about 3-55:1. In yet another non-limiting formulation, the atomic ratio of oxygen to nitrogen is at least about 3-50: 1.

[0011] In another non-limiting aspect of the present invention, carbon nanotubes (CNT) can optionally be incorporated into a metal material that is used to at least partially form the medical device. The one or more metals used in the novel alloy generally have an alloy matrix and the CNT can be optionally incorporated within the grain structure of the alloy matrix. It is believed that certain portions of the CNT (when used) will cross the grain boundary of the metal material and embed into the neighboring grains, thus forming an additional linkage between the grains. When a novel alloy is employed in dynamic application, a cyclic stress is applied on the alloy. At some point at a number of cycles, the novel alloy will crack due to fatigue failure that initiates and propagates along the grain boundaries. It is believed that the attachment of CNT across the grains will prevent or prolong crack propagation and fatigue failure. Further, when the grain size is large, the CNT gets completely embedded into a grain. The twinning of the grains is limited by the presence of CNT either fully embedded or partially embedded within the grain structure. Additionally, the CNT offers better surface erosion resistance. The novel alloy that includes the CNT can be made by powder metallurgy by adding the CNT to the metal powder or mixture of various metal powders to make a multicomponent alloy. The mixture can then be compressed under high isostatic pressure into a preform where the particles of the powder fuse together and thereby trap the CNT into the matrix of the novel alloy. The preform can then be sintered under inert atmosphere or reducing atmosphere and at temperatures that will allow the metallic components to fuse and solidify. Depending on the desired grain structure, the fused metal can then be annealed or further processed into the final shape and then annealed. At no point should the novel alloy be heated above 300°C without enclosing the novel alloy in an inert or reducing atmosphere and/or under vacuum. The material can also be processed in several other conventional ways. One in particular will be by metal injection molding or metal molding technique in which the metal and CNT are mixed with a binder to form a slurry. The slurry is then injected under pressure into a mold of desired shape. The slurry sets in the mold and is then removed. The binder is then sintered off in multiple steps, leaving behind the densified metal- CNT composite. The alloy may be heated up to 1500°C in an inert or reducing atmosphere and/or under vacuum. Most elemental metals and alloys have a fatigue life which limits its use in a dynamic application where cyclic load is applied during its use. The novel alloy prolongs the fatigue life of the medical device. The novel alloy is believed to have enhanced fatigue life, enhancing the bond strength between grain boundaries of the metal in the novel alloy, thus inhibiting, preventing or prolonging the initiation and propagation of cracking that leads to fatigue failure. For example, in an orthopedic spinal application, the spinal rod implant undergoes repeated cycles throughout the patient’s life and can potentially cause the spinal rod to crack. Titanium is commonly used in such devices; however, titanium has low fatigue resistance. The fatigue resistance can be improved by alloying the titanium metal with CNT in the manner described above. With the addition of at least about 0.05 wt.% (e.g., 0.05 wt.% to 10 wt.% and all values and ranges therebetween), typically at least about 0.5 wt.%, and more typically about 0.5-5% wt.% of CNT to the metal material of the novel alloy, the novel alloy can exhibit enhanced fatigue life.

[0012] In another and/or alternative non-limiting aspect of the present invention, the medical device is generally designed to include at least about 5 weight percent of the novel metal alloy (e.g., 5 wt.% to 100 wt.% and all values and ranges therebetween); however, this is not required. In one non-limiting embodiment of the invention, the medical device includes at least about 40 weight percent of the novel metal alloy. In another and/or alternative non-limiting embodiment of the invention, the medical device includes at least about 50 weight percent of the novel metal alloy. In still another and/or alternative non-limiting embodiment of the invention, the medical device includes at least about 60 weight percent of the novel metal alloy. In yet another and/or alternative non-limiting embodiment of the invention, the medical device includes at least about 70 weight percent of the novel metal alloy. In still yet another and/or alternative non-limiting embodiment of the invention, the medical device includes at least about 85 weight percent of the novel metal alloy. In a further and/or alternative non-limiting embodiment of the invention, the medical device includes at least about 90 weight percent of the novel metal alloy. In still a further and/or alternative non-limiting embodiment of the invention, the medical device includes at least about 95 weight percent of the novel metal alloy. In yet a further and/or alternative non-limiting embodiment of the invention, the medical device includes about 100 weight percent of the novel metal alloy.

[0013] In another and/or alternative non-limiting aspect of the present invention, the novel metal alloy that is used to form all or part of the medical device 1) is not clad, metal sprayed, plated and/or formed (e.g., cold worked, hot worked, etc.) onto another metal, or 2) does not have another metal or metal alloy metal sprayed, plated, clad and/or formed onto the novel metal alloy. It will be appreciated that in some applications, the novel metal alloy of the present invention may be clad, metal sprayed, plated and/or formed onto another metal, or another metal or metal alloy may be plated, metal sprayed, clad and/or formed onto the novel metal alloy when forming all or a portion of a medical device. [0014] In another and/or alternative non-limiting aspect of the present invention, the novel alloy (when used) can be used to form a coating on a portion of all of a medical device. For example, the novel alloy can be used as a coating on a polymer or base metal that is used to form all or a portion of a medical device (e.g., medical device for articulation points of artificial joints, etc.). Such a coating can provide the benefit of improved wear, improved scratch resistance, improved hardness, and/or eliminate leaching of harmful metallic ions (i.e., Co, Cr, etc.) from the medical device (e.g., medical devices having articulating surfaces when they undergo fretting (i.e., scratching during relative motion)). As can be appreciated, the novel alloy can have other or additional advantages. As can also be appreciated, the novel alloy can be coated on other or additional types of medical devices. The coating process on a base metal (e.g., Ti or Ti alloy, Co or Co alloy, Cr alloy, CoCr alloy, stainless steel, Fe and Fe alloys, Ni alloy, W alloy, Mo or Mo alloy, Re or Re alloy, etc.) or polymer can be by plasma coating, chemical vapor deposition, and/or 3D printing of the coating on the base metal or polymer. The coating thickness of the novel alloy is non-limiting (e.g., 0.000001-0.5 inches and all values and ranges therebetween). In one non- limiting example, there is provided a medical device in the form of a clad rod wherein in the core of the rod is formed of a metal or ceramic or composite material or polymer, and the outer layer of the rod is formed of the novel alloy that was coated by a plasma coating process, a chemical vapor deposition process, or 3D printing process. The core and the outer coated layer of the rod can each form 50-99% (and all values and ranges therebetween) of the overall cross section of the rod. As can also be appreciated, the novel alloy can form the outer layer of other or additional types of medical devices or devices other than medical devices (e.g., automotive parts, springs, aerospace parts, industrial machinery and parts, tools (e.g., medical tools, industrial tools, household tools, etc.), etc.). The coating can be used to create a hard surface on the medical or devices or than medical devices at specific locations as well as all over the surface. The base hardness of novel alloy can be as low as 300 Vickers and/or as high as 500 Vickers (e.g., 300-500 Vickers and all values and ranges therebetween). However, at high hardness the properties may not be desirable. In instances where the properties of fully annealed material is desired, but only the surface requires to be hardened as in this invention, the present invention includes a method that can provide benefits of both a softer metal alloy with a harder outer surface or shell. A non- limiting example is an orthopedic screw where a softer iron alloy is desired for high ductility as well as ease of machinability. Simultaneously, a hard shell is desired of the finished screw. While the inner hardness can range from 250 Vickers to 550 Vickers (and all values and ranges therebetween), the outer hardness can vary from 350 Vickers to 1000 Vickers (and all values and ranges therebetween) when using novel alloy.

[0015] In another and/or alternative non-limiting aspect of the present invention, the novel alloy can be used to form a core of a portion or all of a medical device. For example, a medical device can be in the form of a rod. The core of the rod can be formed of the novel alloy and then the outside of the core can then be coated with one or more other materials (e.g., another type of metal, polymer coating, ceramic coating, composite material coating, etc.). Such a rod can be used, for example, for orthopedic applications such as, but not limited to, spinal rods and/or pedicle screw systems. Non-limiting benefits to using the novel alloy in the core of a medical device can reducing the size of the medical device, increasing the strength of the medical device, and/or maintaining or reducing the cost of the medical device. As can be appreciated, the novel alloy can have other or additional advantages. As can also be appreciated, the novel alloy can form the core of other or additional types of medical devices. The core size and/or thickness of the novel alloy are non-limiting. In one non-limiting example, there is provided a medical device in the form of a clad rod wherein in the core of the rod is formed of a novel alloy, and the other layer of the clad rod is formed of a metal or novel alloy. The core and the other layer of the rod can each form 50-99% (and all values and ranges therebetween) of the overall cross section of the rod. As can also be appreciated, the novel alloy can form the core of other or additional types of medical devices.

[0016] In another and/or alternative non-limiting aspect of the present invention, the novel alloy has several physical properties that positively affect the medical device when the medical device is at least partially formed of the novel alloy of the present invention. In one non-limiting embodiment of the invention, the average Vickers hardness of novel alloy of the present invention used to form the medical device is generally at least about 234 DHP (Vickers) (i.e., Rockwell A hardness of at least about 60 at 77°F, Rockwell C hardness of at least about 19 at 77°F) (e.g., 234 DPH to 700 DPH and all values and ranges therebetween; Rockwell C hardness of 19-60 at 77°F and all values and ranges therebetween); however, this is not required. In one non-limiting aspect of this embodiment, the average hardness of the novel alloy of the present invention used to form the medical device is generally at least about 248 DHP (i.e., Rockwell A hardness of at least about 62 at 77°F, Rockwell C hardness of at least about 22 at 77°F). In another and/or additional non- limiting aspect of this embodiment, the average hardness of the novel alloy of the present invention used to form the medical device is generally about 248-513 DHP (i.e., Rockwell A hardness of about 62-76 at 77°F, Rockwell C hardness of about 22-50 at 77°F). In still another and/or additional non-limiting aspect of this embodiment, the average hardness of the novel alloy of the present invention used to form the medical device is generally about 272-458 DHP (i.e., Rockwell A hardness of about 64-74 at 77°F, Rockwell C hardness of about 26-46 at 77°F). The novel alloy of the present invention generally has an average hardness that is greater than stainless steel. In another and/or alternative non-limiting embodiment of the invention, the average ultimate tensile strength of the novel alloy of the present invention is generally at least about 60 UTS (ksi); however, this is not required. In one non-limiting aspect of this embodiment, the average ultimate tensile strength of the novel alloy of the present invention is generally at least about 70 UTS (ksi) (e.g., 70 UTS to 850 UTS and all values and ranges therebetween), and typically about 80-550 UTS (ksi). The average ultimate tensile strength of the novel alloy of the present invention may vary somewhat when the novel alloy is in the form of a tube or a solid wire. When the novel alloy of the present invention is in the form of a tube, the average ultimate tensile strength of the novel alloy of the present invention is generally about 80-550 UTS (ksi) (and all values and ranges therebetween), typically at least about 110 UTS (ksi), and more typically 110- 150 UTS (ksi). When the novel alloy of the present invention is in the form of a solid wire, the average ultimate tensile strength of the novel alloy of the present invention wire is generally about 120-650 UTS (ksi) (and all values and ranges therebetween). In still another and/or alternative non-limiting embodiment of the invention, the average yield strength of the novel alloy of the present invention is at least about 70 ksi (e.g., 70-150 ksi and all values and ranges therebetween); however, this is not required. In one non-limiting aspect of this embodiment, the average yield strength of the novel alloy of the present invention used to form the medical device is at least about 80 ksi, and typically about 100-150 (ksi). In yet another and/or alternative non-limiting embodiment of the invention, the average grain size of the novel alloy of the present invention used to form the medical device is no greater than about 4 ASTM (e.g., 4 ASTM to 20 ASTM using ASTM El 12 and all values and ranges therebetween, e.g., 0.35 micron to 90 micron, and all values and ranges therebetween); however, this is not required. The grain size as small as about 14-15 ASTM can be achieved; however, the grain size is typically larger than 15 ASTM. The small grain size of the novel alloy of the present invention enables the medical device to have the desired elongation and ductility properties that are useful in enabling the medical device to be formed, crimped and/or expanded. In one non-limiting aspect of this embodiment, the average grain size of the novel alloy of the present invention used to form the medical device is about 5.2- 10 ASTM, typically about 5.5-9 ASTM, more typically about 6-9 ASTM, still more typically about 6-9 ASTM, even more typically about 6.6-9 ASTM, and still even more typically about 7- 8.5 ASTM; however, this is not required.

[0017] In another and/or alternative non-limiting embodiment of the invention, the average tensile elongation of the novel alloy of the present invention used to form the medical device is at least about 25% (e.g., 25%-50% average tensile elongation and all values and ranges therebetween). An average tensile elongation of at least 25% for the novel alloy is important to enable the medical device to be properly expanded when positioned in the treatment area of a body passageway. A medical device that does not have an average tensile elongation of at least about 25% can form micro-cracks and/or break during the forming, crimping and/or expansion of the medical device. In one non-limiting aspect of this embodiment, the average tensile elongation of the novel alloy of the present invention used to form the medical device is about 25-35%. The unique combination of the metals in the novel alloy of the present invention in combination with achieving the desired purity and composition of the alloy and the desired grain size of the novel alloy results in 1) a medical device having the desired high ductility at about room temperature, 2) a medical device having the desired amount of tensile elongation, 3) a homogeneous or solid solution of a novel alloy having high radiopacity, 4) a reduction or prevention of micro-crack formation and/or breaking of the novel alloy of the present invention tube when the tube is sized and/or cut to form the medical device, 5) a reduction or prevention of micro-crack formation and/or breaking of the medical device when the medical device is crimped onto a balloon and/or other type of medical device for insertion into a body passageway, 6) a reduction or prevention of micro-crack formation and/or breaking of the medical device when the medical device is bent and/or expanded in a body passageway, 7) a medical device having the desired ultimate tensile strength and yield strength, 8) a medical device that can have very thin wall thicknesses and still have the desired radial forces needed to retain the body passageway on an open state when the medical device has been expanded, and/or 9) a medical device that exhibits less recoil when the medical device is crimped onto a delivery system and/or expanded in a body passageway.

[0018] The present disclosure is direct to a medical device that is at least partially made of a refractory metal alloy, and more particularly to a prosthetic heart valve that is at least partially formed of the refractory metal alloy. As defined herein, a refractory metal alloy is a metal alloy that includes at least 20 wt.% of one or more of Mo, Re, Nb, Ta or W. Non-limiting refractory metal alloys include MoRe alloy, ReW alloy, MoReCr alloy, MoReTa alloy, MoReTi alloy, WCu alloy, Mo alloy, Re alloy, W alloy, Ta alloy, Nb alloy, etc.

[0019] In another non-limiting aspect of the present invention, the metals that are used to form the novel alloy include, a refractory metal (e.g., Mo, Re, Nb, Ta or W) and one or more alloying agents such as, but are not limited to, calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iron, lanthanum oxide, lead, magnesium, nickel, niobium, osmium, platinum, rare earth metals, rhenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components (e.g., MoHfC, M0Y2O3, M0CS2O, MoW, MoTa, MoZrC , MoLa203, MoRe alloy, MoReW alloy, etc ). In one non-limiting formulation, the novel alloy includes 40 wt.% to 99.9 wt.% molybdenum (and all values and ranges therebetween) (e.g., 40 wt.%, 40.01 wt.%, 40.02 wt.% ... 99.88 wt.%, 99.89 wt.%, 99.9 wt.%). Although the novel alloy is described as including one or more metals and/or metal oxides, it can be appreciated that some or all of the metal and/or metal oxide in the novel alloy can be substituted for one or more materials selected form the group of ceramics, plastics, thermoplastics, thermosets, rubbers, laminates, non-wovens, etc. The addition of controlled amounts of the alloying agents to the molybdenum alloy has been found to form a novel alloy that has improved physical properties. For instance, the addition of controlled amounts of carbon, cerium oxide, hafnium, lanthanum oxide, rhenium, tantalum, tungsten, yttrium oxide, zirconium oxide to the molybdenum alloy can result in 1) an increase in yield strength of the alloy, 2) an increase in tensile elongation of the alloy, 3) an increase in ductility of the alloy, 4) a reduction in grain size of the alloy, 5) a reduction in the amount of free carbon, oxygen and/or nitrogen in the alloy, and/or 6) a reduction in the tendency of the alloy to form micro-cracks during the forming of the alloy into a medical device.

[0020] In another and/or alternative non-limiting aspect of the present invention, the novel alloy that is used to form all or a portion of the medical device is a novel alloy that includes 40 wt.% to 99.9 wt.% molybdenum (and all values and ranges therebetween) (e.g., 40 wt.%, 40.01 wt.%, 40.02 wt.% ... 99.88 wt.%, 99.89 wt.%, 99.9 wt.%) and optionally 0.01-5 wt.% CNT (and all values and ranges therebetween) (e.g., 0.01 wt.%, 0.011 wt.%, 0.012 wt.% ... 4.998 wt.%, 4.999 wt.%, 5 wt.%).

[0021 ] Another and/or alternative non-limiting object of the present invention, the novel alloy includes a duplex stainless steel. The duplex stainless steel includes an austenite phase and ferrite phase, about 40-60% (and all values and ranges therebetween) of the duplex stainless steel includes the austenite phase, about 40-60% (and all values and ranges therebetween) of the duplex stainless steel includes the ferrite phase, the duplex stainless steel includes less than 0.05 wt.% C (e.g., 0-0.049999 wt.% and all values and ranges therebetween), less than 1 wt.% Si (e.g., 0- 0.9999999 and all values and ranges therebetween), less than 6 wt.% Mn (e.g., 0-5.999999 wt.% and all values and ranges therebetween), 17-30 wt.% Cr (and all values and ranges therebetween), no more than 3 wt.% Cu (0-3 wt.% and all values and ranges therebetween), no more than 5 wt.% Mo (0-5 wt.% and all values and ranges therebetween), and 0.9-9 wt.% Ni (and all values and ranges therebetween), and greater than 50 wt.% Fe (e.g., 50.0000001-82.1 wt.% and all values and ranges therebetween), the duplex stainless steel has an ultimate tensile strength of 600-1000 MPa (European Standard EN 10088-3 (2014)) (and all values and ranges therebetween), and an elongation of 24-32% (and all values and ranges therebetween).

[0022] In another and/or alternative non-limiting aspect of the present invention, the novel copper and tungsten alloy is used to form all or a portion of the medical device. In particular, a novel alloy includes tungsten and copper and optionally one or more metal agents such as, but are not limited to, calcium, carbon, cerium oxide, chromium, cobalt, gold, hafnium, iron, lanthanum oxide, lead, magnesium, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhenium, silver, tantalum, technetium, titanium, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components. The one or more metal agents may or may not alloy with the tungsten and/or copper in the novel alloy. In one non- limiting formulation, the novel alloy includes 1-99.9 wt.% tungsten (and all values and ranges therebetween) (e.g., 1 wt.%, 1.01 wt.%, 1.02 wt.% ... 99.88 wt.%, 99.89 wt.%, 99.9 wt.%), and 0.1-99 wt.% copper (and all values and ranges therebetween) (e.g., 0.1 wt.%, 0.101 wt.%, 0.102 wt.% ... 98.998 wt.%, 98.999 wt.%, 99 wt.%). In another non-limiting formulation, the tungsten constitutes the greatest weight percent in the novel alloy and the copper constitutes the second greatest weight percent in the novel alloy. In another non-limiting formulation, the tungsten constitutes the largest weight percent of any component that forms the novel alloy. In another non-limiting formulation, the tungsten constitutes greater than 50 wt.% of the novel alloy. [0023] In another and/or alternative non-limiting aspect of the present invention, the novel alloy is used to form all or a portion of the medical device. In particular, a novel alloy includes rhenium and tungsten and optionally one or more alloying agents such as, but not limited to, calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iron, lanthanum oxide, lead, magnesium, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components (e.g., WRe, WReMo, etc.). Although the novel alloy is described as including one or more metals and/or metal oxides, it can be appreciated that some of the metals and/or metal oxides in the novel alloy can be substituted for one or more materials selected from the group of ceramics, plastics, thermoplastics, thermosets, rubbers, laminates, non-wovens, etc. In one non-limiting formulation, the novel alloy includes 1-40 wt.% rhenium (and all values and ranges therebetween) (e.g., 1 wt.%, 1.01 wt.%, 1.02 wt.% ... 39.98 wt.%, 39.99 wt.%, 40 wt.%) and 60-99 wt.% tungsten (and all values and ranges therebetween) (e.g., 60 wt.%, 60.01 wt.%, 60.02 wt.% ... 98.98 wt.%, 98.99 wt.%, 99 wt.%). The total weight percent of the tungsten and rhenium in the tungsten-rhenium alloy is at least about 99 wt.%, typically at least about 99.5 wt.%, more typically at least about 99.9 wt.%, and still more typically at least about 99.99 wt.%. In another non-limiting formulation, the novel alloy includes 1-47.5 wt.% rhenium (and all values and ranges therebetween) (e.g., 1 wt.%, 1.01 wt.%, 1.02 wt.% ... 47.48 wt.%, 47.49 wt.%, 47.5 wt.%) and 20-80 wt.% tungsten (and all values and ranges therebetween) (e.g., 20 wt.%, 20.01 wt.%, 20.02 wt.% ... 79.98 wt.%, 79.99 wt.%, 80 wt.%) and 1-47.5 wt.% molybdenum (and all values and ranges therebetween) (e.g., 1 wt.%, 1.01 wt.%, 1.02 wt.% ... 47.48 wt.%, 47.49 wt.%, 47.5 wt.%). The total weight percent of the tungsten, rhenium and molybdenum in the tungsten-rhenium-molybdenum alloy is at least about 99 wt.%, typically at least about 99.5 wt.%, more typically at least about 99.9 wt.%, and still more typically at least about 99.99 wt.%. In one non-limiting specific tungsten-rhenium- molybdenum alloy, the weight percent of the tungsten is greater than a weight percent of rhenium and also the weight percent of molybdenum. In another non-limiting specific tungsten-rhenium- molybdenum alloy, the weight percent of the tungsten is greater than 50 wt.% of the tungsten- rhenium-molybdenum alloy. In another non-limiting specific tungsten-rhenium-molybdenum alloy, the weight percent of the tungsten is greater than a weight percent of rhenium, but less than a weigh percent of molybdenum. In another non-limiting specific tungsten-rhenium-molybdenum alloy, the weight percent of the tungsten is greater than a weight percent of molybdenum, but less than a weigh percent of rhenium. In another non-limiting specific tungsten-rhenium-molybdenum alloy, the weight percent of the tungsten is less than a weight percent of rhenium and also less than the weight percent of molybdenum.

[0024] In another and/or alternative non-limiting aspect of the present invention, the novel cobalt alloy is used to form all or a portion of the medical device. In one non-limiting embodiment, the novel cobalt alloy includes 50.01-72 wt.% cobalt (and all values and ranges therebetween), 25-35 wt.% chromium (and all values and ranges therebetween), 3-7 wt.% tungsten (and all values and ranges therebetween), 0.2-2 wt.% carbon (and all values and ranges therebetween, 0-2.2 wt.% molybdenum (and all values and ranges therebetween), 0-4.5 wt.% nickel (and all values and ranges therebetween), 0-2.8 wt.% manganese (and all values and ranges therebetween), 0-4.5 wt. % iron (and all values and ranges therebetween), 0-2 wt.% silicon (and all values and ranges therebetween, and 0-0.18 wt.% impurities (and all values and ranges therebetween). In another non-limiting embodiment, the total weight percent of cobalt, chromium, tungsten and carbon in the novel cobalt alloy constitutes at least 90 wt.% of the novel cobalt alloy. In another non-limiting embodiment, the total weight percent of cobalt, chromium, tungsten and carbon in the novel cobalt alloy constitutes at least 95 wt.% of the novel cobalt alloy.

[0025] In another and/or alternative non-limiting aspect of the present invention, the novel alloy includes less than about 5 wt.% (e.g., 0-4.999999 wt.% and all values and ranges therebetween) other metals and/or impurities. A high purity level of the novel alloy results in the formation of a more homogeneous alloy, which in turn results in a more uniform density throughout the novel alloy, and also results in the desired yield and ultimate tensile strengths of the novel alloy. In one non-limiting composition, the novel alloy includes less than about 1 weight percent other metals and/or impurities. In another and/or alternative non-limiting composition, the novel alloy includes less than about 0.5 weight percent other metals and/or impurities. In still another and/or alternative non-limiting composition, the novel alloy includes less than about 0.4 weight percent other metals and/or impurities. In yet another and/or alternative non-limiting composition, the novel alloy includes less than about 0.2 weight percent other metals and/or impurities. In still yet another and/or alternative non-limiting composition, the novel alloy includes less than about 0.1 weight percent other metals and/or impurities. In a further and/or alternative non-limiting composition, the novel alloy includes less than about 0.05 weight percent other metals and/or impurities. In still a further and/or alternative non-limiting composition, the novel alloy includes less than about 0.02 weight percent other metals and/or impurities. In yet a further and/or alternative non-limiting composition, the novel alloy includes less than about 0.01 weight percent other metals and/or impurities. As can be appreciated, other weight percentages of the amount of other metals and/or impurities in the novel alloy can exist.

[0026] In another and/or alternative non-limiting aspect of the present invention, the novel alloy is at least partially formed by a swaging process; however, this is not required. In one non- limiting embodiment, swaging is performed on the metal alloy to at least partially or fully achieve final dimensions of one or more portions of the medical device. The swaging dies can be shaped to fit the final dimension of the medical device; however, this is not required. Where there are undercuts of hollow structures in the medical device, which is not required, a separate piece of metal can be placed in the undercut to at least partially fill the gap. The separate piece of metal, when used, can be designed to be later removed from the undercut; however, this is not required. The swaging operation can be performed on the medical device in the areas to be hardened. For a round or curved portion of a medical device, the swaging can be rotary. For non-round portion of the medical device, the swaging of the non-round portion of the medical device can be performed by non-rotating swaging dies. The dies can optionally be made to oscillate in radial and/or longitudinal directions instead of or in addition to rotating. The medical device can optionally be swaged in multiple directions in a single operation or in multiple operations to achieve a hardness in desired location and/or direction of the medical device. The swaging temperature for a particular novel alloy (e.g., MoRe alloy, ReW alloy, etc.) can vary. For a refractory alloy (e.g., MoRe alloy, ReW alloy, Mo alloy, Re alloy, W alloy, etc.), the swaging temperature can be from room temperature (RT) (e.g., 10-27°C and all values and ranges therebetween) to about 400°C (e.g., 10-400°C and all values and ranges therebetween) if the swaging is conducted in air or an oxidizing environment. As defined herein, a refractory alloy is an alloy that includes at least 1 wt.% Mo, Re and/or W. The swaging temperature can be increased to up to about 1500°C (e.g., 10-1500°C and all values and ranges therebetween) if the swaging process is performed in a controlled neutral or non-reducing environment (e.g., inert environment). The swaging process can be conducted by repeatedly hammering the medical device at the location to be hardened at the desired swaging temperature. In one non-limiting embodiment, during the swaging process ions of boron and/or nitrogen are allowed to impinge upon rhenium atoms in the MoRe alloy so as to form ReB2, ReN2 and/or ReN3; however, this is not required. It has been found that ReE , ReN2 and/or ReN3 are ultra-hard compounds. As can be appreciated, other refractory alloys that include Re and that are subjected to a swaging process can also form ReB2, ReN2 and/or ReN3. In one non-limiting process, the metal for the medical device can be machined and shape into the medical device when the metal is in a less hardened state. As such, the raw starting material can be first annealed to soften and then machined into the metal into a desired shape. After the novel alloy is shaped, the novel alloy can be re-hardened. The hardening of the metal material of the medical device can improve the wear resistance and/or shape retention of the medical device. The metal material of the medical generally cannot be re hardened by annealing, thus a special rehardening processes is required. Such rehardening can be achieved by the swaging process of the present invention.

[0027] In accordance with another and/or alternative non-limiting aspect of the present disclosure, at least 30 wt.% (e.g., 30-100 wt.% and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, niobium, rhenium, tantalum, or tungsten. In another non-limiting embodiment, at least 40 wt.% of the refractory metal alloy includes one or more of molybdenum, niobium, rhenium, tantalum, or tungsten. In another non- limiting embodiment, at least 50 wt.% of the refractory metal alloy includes one or more of molybdenum, niobium, rhenium, tantalum, or tungsten.

[0028] In another non-limiting embodiment, at least 50 wt.% (e.g., 50-100 wt.% and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, niobium, rhenium, tantalum, or tungsten, and 0-40 wt.% (and all values and ranges therebetween) of the refractory alloy includes one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, nickel, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, technetium, titanium, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide. In another non-limiting embodiment, at least 50 wt.% (e.g., 50-99.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, niobium, rhenium, tantalum, or tungsten, and 0.1-40 wt.% (and all values and ranges therebetween) of the refractory alloy includes one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, nickel, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, technetium, titanium, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide. In another non-limiting embodiment, at least 50 wt.% (e.g., 50-100 wt.% and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, niobium, rhenium, tantalum, or tungsten, and 0-40 wt.% (and all values and ranges therebetween) of the refractory alloy includes one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, nickel, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, technetium, titanium, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory alloy includes 0-2 wt.% (and all values and ranges therebetween) of a combination of other metals, carbon, oxygen and nitrogen. In another non-limiting embodiment, at least 50 wt.% (e.g., 50-99.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, niobium, rhenium, tantalum, or tungsten, and 0.1-40 wt.% (and all values and ranges therebetween) of the refractory alloy includes one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, nickel, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, technetium, titanium, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory alloy includes 0-2 wt.% (and all values and ranges therebetween) of a combination of other metals, carbon, oxygen and nitrogen. In another non-limiting embodiment, at least 55 wt.% of the refractory metal alloy includes one or more of molybdenum, niobium, rhenium, tantalum, or tungsten, and 0-40 wt.% of the refractory alloy includes one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, nickel, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, technetium, titanium, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory alloy includes 0-0.1 wt.% of a combination of other metals, carbon, oxygen and nitrogen. In another non-limiting embodiment, at least 55 wt.% of the refractory metal alloy includes one or more of molybdenum, niobium, rhenium, tantalum, or tungsten, and 0.1-40 wt.% of the refractory alloy includes one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, nickel, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, technetium, titanium, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory alloy includes 0-0.1 wt.% of a combination of other metals, carbon, oxygen and nitrogen. [0029] In accordance with another and/or alternative non-limiting aspect of the present disclosure, the refractory metal alloy includes at least 30 wt.% (e.g., 30-99 wt.% and all values and ranges therebetween) rhenium and one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide. In another non-limiting embodiment, the refractory metal alloy includes at least 30 wt.% (e.g., 30-99 wt.% and all values and ranges therebetween) rhenium and one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory metal alloy includes 0-2 wt.% (and all values and ranges therebetween) of a combination of other metals, carbon, oxygen, and nitrogen. In another non-limiting embodiment, the refractory metal alloy includes at least 30 wt.% (e.g., 30-99 wt.% and all values and ranges therebetween) rhenium and one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory metal alloy includes 0-0.1 wt.% (and all values and ranges therebetween) of a combination of other metals, carbon, oxygen, and nitrogen. In another non- limiting embodiment, the refractory metal alloy includes at least 35 wt.% (e.g., 35-99 wt.% and all values and ranges therebetween) rhenium and 0.1-65 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide. In another non-limiting embodiment, the refractory metal alloy includes at least 35 wt.% (e.g., 35-99 wt.% and all values and ranges therebetween) rhenium and 0.1-65 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory metal alloy includes 0-2 wt.% (and all values and ranges therebetween) of a combination of other metals, carbon, oxygen, and nitrogen. In another non limiting embodiment, the refractory metal alloy includes at least 35 wt.% (e.g., 35-99.9 wt.% and all values and ranges therebetween) rhenium and 0.1-65 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory metal alloy includes 0-0.1 wt.% (and all values and ranges therebetween) of a combination of other metals, carbon, oxygen, and nitrogen. In another non-limiting embodiment, the refractory metal alloy includes at least 40 wt.% (e.g., 40-99.9 wt.% and all values and ranges therebetween) rhenium and 0.1-60 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide. In another non limiting embodiment, the refractory metal alloy includes at least 40 wt.% (e.g., 40-99.9 wt.% and all values and ranges therebetween) rhenium and 0.1-60 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory metal alloy includes 0-2 wt.% (and all values and ranges therebetween) of a combination of other metals, carbon, oxygen, and nitrogen. In another non-limiting embodiment, the refractory metal alloy includes at least 40 wt.% (e.g., 40-99.9 wt.% and all values and ranges therebetween) rhenium and 0.1-60 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, or zirconium oxide, and the refractory metal alloy includes 0-0.1 wt.% (and all values and ranges therebetween) of a combination of other metals, carbon, oxygen, and nitrogen.

[0030] In accordance with another and/or alternative non-limiting aspect of the present disclosure, there is provided a refractory metal alloy wherein at least 20 wt.% (e.g., 20-99 wt.% and all values and ranges therebetween) of the refractory metal alloy includes rhenium. In one non-limiting embodiment, the refractory metal alloy includes at least 20 wt.% (e.g., 20-99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-80 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components. In another non-limiting embodiment, the refractory metal alloy includes at least 20 wt.% (e.g., 30-99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-80 wt.% (and all values and ranges therebetween) of one or more of copper, chromium, hafnium, iridium, manganese, molybdenum, niobium, osmium, rhodium, ruthenium, tantalum, technetium, titanium, tungsten, vanadium, zirconium, and and/or alloys of one or more of such components. In another non-limiting embodiment, the refractory metal alloy includes at least 30 wt.% (e.g., 30-99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-70 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components. In another non-limiting embodiment, the refractory metal alloy includes at least 30 wt.% (e.g., 30- 99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-70 wt.% (and all values and ranges therebetween) of one or more of copper, chromium, hafnium, iridium, manganese, molybdenum, niobium, osmium, rhodium, ruthenium, tantalum, technetium, titanium, tungsten, vanadium, zirconium, and and/or alloys of one or more of such components. In another non- limiting embodiment, the refractory metal alloy includes at least 35 wt.% (e.g., 35-99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-65 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components. In another non-limiting embodiment, the refractory metal alloy includes at least 35 wt.% (e.g., 35-99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-65 wt.% (and all values and ranges therebetween) of one or more of copper, chromium, hafnium, iridium, manganese, molybdenum, niobium, osmium, rhodium, ruthenium, tantalum, technetium, titanium, tungsten, vanadium, zirconium, and and/or alloys of one or more of such components. In another non-limiting embodiment, In another non-limiting embodiment, the refractory metal alloy includes 35-60 wt.% (and all values and ranges therebetween) rhenium, and 40-65 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components. In another non-limiting embodiment, the refractory metal alloy includes 35-60 wt.% (and all values and ranges therebetween) rhenium, and 40-65 wt.% (and all values and ranges therebetween) of one or more of copper, chromium, hafnium, iridium, manganese, molybdenum, niobium, osmium, rhodium, ruthenium, tantalum, technetium, titanium, tungsten, vanadium, zirconium, and and/or alloys of one or more of such components. In another non-limiting embodiment, the refractory metal alloy includes at least 40 wt.% (e.g., 40-99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-60 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components. In another non-limiting embodiment, the refractory metal alloy includes at least 40 wt.% (e.g., 40-99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-60 wt.% (and all values and ranges therebetween) of one or more of copper, chromium, hafnium, iridium, manganese, molybdenum, niobium, osmium, rhodium, ruthenium, tantalum, technetium, titanium, tungsten, vanadium, zirconium, and and/or alloys of one or more of such components. In one non-limiting embodiment, the refractory metal alloy includes at least 50 wt.% (e.g., 50-99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-50 wt.% (and all values and ranges therebetween) of one or more of calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iridium, iron, lanthanum, lanthanum oxide, lead, magnesium, manganese, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhodium, ruthenium, silver, tantalum, technetium, titanium, tungsten, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components. In another non-limiting embodiment, the refractory metal alloy includes at least 50 wt.% (e.g., 50- 99.9 wt.% and all values and ranges therebetween) rhenium, and 0.1-50 wt.% (and all values and ranges therebetween) of one or more of copper, chromium, hafnium, iridium, manganese, molybdenum, niobium, osmium, rhodium, ruthenium, tantalum, technetium, titanium, tungsten, vanadium, zirconium, and and/or alloys of one or more of such components.

[0031] In another non-limiting aspect of the present disclosure, the metals used to form the refractory metal alloy includes rhenium and tungsten and optionally one or more alloying agents such as, but not limited to, calcium, carbon, cerium oxide, chromium, cobalt, copper, gold, hafnium, iron, lanthanum oxide, lead, magnesium, molybdenum, nickel, niobium, osmium, platinum, rare earth metals, rhenium, silver, tantalum, technetium, titanium, vanadium, yttrium, yttrium oxide, zinc, zirconium, zirconium oxide, and/or alloys of one or more of such components (e.g., WRe, WReMo, etc.). Although the refractory metal alloy is described as including one or more metals and/or metal oxides, it can be appreciated that some of the metals and/or metal oxides in the refractory metal alloy can be substituted for one or more materials selected from the group of ceramics, plastics, thermoplastics, thermosets, rubbers, laminates, non-wovens, etc. In one non-limiting formulation, the refractory metal alloy includes 1-40 wt.% rhenium (and all values and ranges therebetween) and 60-99 wt.% tungsten (and all values and ranges therebetween). In one non-limiting embodiment, the total weight percent of the tungsten and rhenium in the tungsten-rhenium alloy is at least about 95 wt.%, typically at least about 99 wt.%, more typically at least about 99.5 wt.%, yet more typically at least about 99.9 wt.%, and still more typically at least about 99.99 wt.%. In another non-limiting formulation, the refractory metal alloy includes 1-47.5 wt.% rhenium (and all values and ranges therebetween) and 20-80 wt.% tungsten (and all values and ranges therebetween) and 1-47.5 wt.% molybdenum (and all values and ranges therebetween). The total weight percent of the tungsten, rhenium, and molybdenum in the tungsten-rhenium-molybdenum alloy is at least about 95 wt.%, typically at least about 99 wt.%, more typically at least about 99.5 wt.%, yet more typically at least about 99.9 wt.%, and still more typically at least about 99.99 wt.%. In one non-limiting specific tungsten-rhenium-molybdenum alloy, the weight percent of the tungsten is greater than a weight percent of rhenium and also greater than the weight percent of molybdenum. In another non-limiting specific tungsten- rhenium-molybdenum alloy, the weight percent of the tungsten is greater than 50 wt.% of the tungsten-rhenium-molybdenum alloy. In another non-limiting specific tungsten-rhenium- molybdenum alloy, the weight percent of the tungsten is greater than a weight percent of rhenium, but less than a weigh percent of molybdenum. In another non-limiting specific tungsten-rhenium- molybdenum alloy, the weight percent of the tungsten is greater than a weight percent of molybdenum, but less than a weigh percent of rhenium. In another non-limiting specific tungsten- rhenium-molybdenum alloy, the weight percent of the tungsten is less than a weight percent of rhenium and also less than the weight percent of molybdenum.

[0032] In accordance with another and/or alternative non-limiting aspect of the present disclosure, there is provided a refractory metal alloy wherein at least 30 wt.% (e.g., 30-99 wt.% and all values and ranges therebetween) of the refractory metal alloy includes rhenium. In another non-limiting embodiment, at least 35 wt.% of the refractory metal alloy includes rhenium. In another non-limiting embodiment, at least 35 wt.% (e.g., 35-99.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes rhenium, and 0.1-65 wt.% (and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, niobium, tantalum, tantalum, titanium, vanadium, chromium, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and/or iridium. In another non-limiting embodiment, 35-60 wt.% (and all values and ranges therebetween) of the refractory metal alloy includes rhenium, and 40-65 wt.% (and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, niobium, tantalum, tungsten, titanium, vanadium, chromium, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and/or iridium. In another non-limiting embodiment, 35-60 wt.% (e.g., and all values and ranges therebetween) of the refractory metal alloy includes rhenium, and 40-65 wt.% (and all values and ranges therebetween) of the refractory metal alloy includes two or more of molybdenum, niobium, tantalum, tantalum, titanium, vanadium, chromium, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and/or iridium. In another non-limiting embodiment, 35-60 wt.% (e.g., and all values and ranges therebetween) of the refractory metal alloy includes rhenium, and 40-65 wt.% (and all values and ranges therebetween) of the refractory metal alloy includes three or more of molybdenum, niobium, tantalum, tantalum, titanium, vanadium, chromium, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and/or iridium.

[0033] In another non-limiting aspect of the present disclosure, the metals used to form the refractory metal alloy include at least 35 wt.% rhenium (e.g., 35-99.9 wt.% and all values and ranges therebetween) and one or more alloying agents such as, but are not limited to, molybdenum, niobium, tantalum, tantalum, titanium, vanadium, chromium, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and/or iridium, and/or alloys of one or more of such components. In one non-limiting formulation, the refractory metal alloy includes 40-99.9 wt.% rhenium and one or more molybdenum, niobium, tantalum, tantalum, titanium, vanadium, chromium, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and/or iridium. In one non-limiting formulation, the refractory metal alloy includes rhenium and one or more molybdenum, niobium, tantalum, tantalum, titanium, vanadium, chromium, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and/or iridium.

[0034] In another non-limiting aspect of the present disclosure, the metals used to form the refractory metal alloy include rhenium, molybdenum, and one or more alloying metals selected from the group consisting of bismuth, chromium, copper, hafnium, iridium, manganese, niobium, osmium, rhodium, ruthenium, tantalum, technetium, titanium, tungsten, vanadium, yttrium, and zirconium. In one non-limiting embodiment, a combined weight percentage of rhenium and alloy metals in the refractory metal alloy is greater than or equal to the weight percent of molybdenum in the refractory metal alloy. In another non-limiting embodiment, a combined weight percentage of rhenium and alloy metals in the refractory metal alloy is greater than the weight percent of molybdenum in the refractory metal alloy. In another non-limiting embodiment, a weight percent of molybdenum in the refractory metal alloy is at least 10 wt.% and less than 60 wt.% (and all values and ranges therebetween). In another non-limiting embodiment, a weight percent of rhenium in the refractory metal alloy is 35-60 wt.% (and all values and ranges therebetween). In another non-limiting embodiment, a combined weight percent of the alloying metals is 5-45 wt.% (and all values and ranges therebetween) of the refractory metal alloy. In another non-limiting embodiment, a weight percent of the rhenium in the refractory metal alloy is greater than a combined weight percent of the alloying metals. In another non-limiting embodiment, a combined weight percent of the rhenium, molybdenum, and the one or more alloying metals in the refractory metal alloy is at least 99.9 wt.%. In another non-limiting embodiment, alloy metal includes chromium. In another non-limiting embodiment, the alloying metal includes chromium and one or more metals selected from the group consisting of bismuth, zirconium, iridium, niobium, tantalum, titanium, and yttrium. In another non-limiting embodiment, the alloying metal includes chromium and one or more metals selected from the group consisting of bismuth, zirconium, iridium, niobium, tantalum, titanium, and yttrium; and wherein an atomic ratio of chromium to an atomic ratio of each or all of the metals selected from the group consisting of bismuth, chromium, iridium, niobium, tantalum, titanium, and yttrium is 0.4:1 to 2.5:1 (and all values and ranges therebetween). In another non-limiting embodiment, the alloying metal includes chromium and one or more metals selected from the group consisting of zirconium, niobium, and tantalum. In another non-limiting embodiment, the alloying metal includes a first metal selected from the group consisting of bismuth, chromium, iridium, niobium, tantalum, titanium, yttrium and zirconium, and a second metal selected from the group consisting of bismuth, chromium, iridium, niobium, tantalum, titanium, yttrium and zirconium; and wherein the first and second metals are different; and wherein an atomic ratio of the first metal to the second metal is 0.4: 1 to 2.5:1 (and all values and ranges therebetween). In another non-limiting embodiment, the alloying metal a first metal selected from the group consisting of chromium, niobium, tantalum, and zirconium, and a second metal selected from the group consisting of chromium, niobium, tantalum, and zirconium; and wherein the first and second metals are different; and wherein an atomic ratio of the first metal to the second metal is 0.4:1 to 2.5:1 (and all values and ranges therebetween).

[0035] In accordance with another and/or alternative non-limiting aspect of the present disclosure, the weight percent of rhenium plus the weigh percent of the combined weight percentage of bismuth, niobium, tantalum, tungsten, titanium, vanadium, chromium, manganese, yttrium, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and iridium is greater than the weight percent of molybdenum in the refractory metal alloy. In one specific non- limiting formulation, the weight percent of rhenium plus the weigh percent of the combined weight percentage of bismuth, chromium, iridium, niobium, tantalum, titanium, yttrium, and zirconium is greater than the weight percent of molybdenum in the refractory metal alloy. In another specific non-limiting formulation, the weight percent of rhenium plus the weigh percent of the combined weight percentage of chromium, niobium, tantalum, and zirconium is greater than the weight percent of molybdenum in the refractory metal alloy. In another non-limiting specific non-limiting formulation, the weight percent of molybdenum in the refractory metal alloy is at least 10 wt.% and less than 50 wt.% (and all values and ranges therebetween). In another non- limiting specific non-limiting formulation, the weight percent of rhenium in the refractory metal alloy is 41-58.5 wt.% (and all values and ranges therebetween), the weight percent of molybdenum in the refractory metal alloy is at least 15-45 wt.% (and all values and ranges therebetween), and the combined weight percent of bismuth, niobium, tantalum, tungsten, titanium, vanadium, chromium, manganese, yttrium, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and iridium in the refractory metal alloy is 11-41 wt.% (and all values and ranges therebetween). In another non-limiting specific non-limiting formulation, the weight percent of rhenium in the refractory metal alloy is 41-58.5 wt.% (and all values and ranges therebetween), the weight percent of molybdenum in the refractory metal alloy is at least 15-45 wt.% (and all values and ranges therebetween), and the combined weight percent of bismuth, chromium, iridium, niobium, tantalum, titanium, yttrium, and zirconium in the refractory metal alloy is 11- 41 wt.% (and all values and ranges therebetween). In another non-limiting specific non-limiting formulation, the weight percent of rhenium in the refractory metal alloy is 41-58.5 wt.% (and all values and ranges therebetween), the weight percent of molybdenum in the refractory metal alloy is at least 15-45 wt.% (and all values and ranges therebetween), and the combined weight percent of chromium, niobium, tantalum, and zirconium in the refractory metal alloy is 11-41 wt.% (and all values and ranges therebetween). In another non-limiting embodiment of the invention, the weight percent of rhenium in the refractory metal alloy is greater than the combined weight percent of bismuth, chromium, iridium, niobium, tantalum, titanium, yttrium, and zirconium in the refractory metal alloy. In another non-limiting specific non-limiting formulation, the weight percent of rhenium in the refractory metal alloy is greater than the combined weight percent of chromium, niobium, tantalum, and zirconium in the refractory metal alloy.

[0036] In accordance with another and/or alternative non-limiting aspect of the present disclosure, the atomic weight percent of rhenium to the atomic weight percent of the combination of bismuth, niobium, tantalum, tungsten, titanium, vanadium, chromium, manganese, yttrium, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and iridium in the refractory metal alloy is 0.7:1 to 1.5:1 (and all values and ranges therebetween), typically 0.8:1 to 1.4:1, more typically 0.8:1 to 1.25:1, and still more typically about 0.9:1 to 1.1:1 (e.g., 1:1). In one specific non-limiting formulation, the atomic weight percent of rhenium to the atomic weight percent of the combination of bismuth, chromium, iridium, niobium, tantalum, titanium, yttrium, and zirconium is 0.7:1 to 5.1:1 (and all values and ranges therebetween), typically 0.8:1 to 1.5:1, more typically 0.8:1 to 1.25:1, and still more typically about 0.9:1 to 1.1:1 (e.g., 1:1). In one specific non-limiting formulation, the atomic weight percent of rhenium to the atomic weight percent of the combination of chromium, niobium, tantalum, and zirconium is 0.7:1 to 5.1:1 (and all values and ranges therebetween), typically 0.8:1 to 1.5:1, more typically 0.8:1 to 1.25:1, and still more typically about 0.9:1 to 1.1:1 (e.g., 1:1).

[0037] In accordance with another and/or alternative non-limiting aspect of the present disclosure, when the refractory metal alloy includes two of bismuth, niobium, tantalum, tungsten, titanium, vanadium, chromium, manganese, yttrium, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, and iridium, the atomic ratio of the two metals is 0.4: 1 to 2.5: 1 (and all values and ranges therebetween), and typically 0.5:1 to 2:1. In one specific non-limiting formulation, when the refractory metal alloy includes two of bismuth, chromium, iridium, niobium, tantalum, titanium, yttrium, and zirconium, the atomic ratio of the two metals is 0.4: 1 to 2.5:1 (and all values and ranges therebetween), and typically 0.5: 1 to 2: 1. In another specific non- limiting formulation, when the refractory metal alloy includes two of chromium, niobium, tantalum, and zirconium, the atomic ratio of the two metals is 0.4:1 to 2.5:1 (and all values and ranges therebetween), and typically 0.5:1 to 2:1.

[0038] In accordance with another and/or alternative non-limiting aspect of the present disclosure, at least 35 wt.% (e.g., 35-75 wt.% and all values and ranges therebetween) of the refractory metal alloy includes rhenium, and the refractory metal alloy also includes chromium. In one non-limiting embodiment, at least 25 wt.% (e.g., 25-49.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes chromium. In another non-limiting embodiment, at least 30 wt.% of the refractory metal alloy includes chromium. In another non- limiting embodiment, at least 33 wt.% of the refractory metal alloy includes chromium. In another non-limiting embodiment, at least 50 wt.% (e.g., 50-74.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes rhenium, at least 25 wt.% (e.g., 25-49.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes chromium, and 0.1- 25 wt.% (and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, bismuth, niobium, tantalum, titanium, vanadium, tungsten, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, yttrium, zirconium, and/or iridium. In another non-limiting embodiment, at least 55 wt.% (e.g., 55-69.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes rhenium, at least 30 wt.% (e.g., 30-44.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes chromium, and 0.1-15 wt.% (and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, bismuth, niobium, tantalum, titanium, vanadium, tungsten, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, yttrium, zirconium, and/or iridium. In another non-limiting embodiment, at least 60 wt.% (e.g., 60-69.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes rhenium, at least 30 wt.% (e.g., 30-39.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes chromium, and 0.1-10 wt.% (and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, bismuth, niobium, tantalum, titanium, vanadium, tungsten, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, yttrium, zirconium, and/or iridium. In another non-limiting embodiment, at least 62 wt.% (e.g., 62-67.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes rhenium, at least 32 wt.% (e.g., 32-32.9 wt.% and all values and ranges therebetween) of the refractory metal alloy includes chromium, and 0.1-6 wt.% (and all values and ranges therebetween) of the refractory metal alloy includes one or more of molybdenum, bismuth, niobium, tantalum, titanium, vanadium, tungsten, manganese, zirconium, technetium, ruthenium, rhodium, hafnium, osmium, copper, yttrium, zirconium, and/or iridium.

[0039] In accordance with another and/or alternative non-limiting aspect of the present disclosure, the refractory metal alloy includes less than about 5 wt.% (e.g., 0-4.999999 wt.% and all values and ranges therebetween) other metals and/or impurities. A high purity level of the refractory metal alloy results in the formation of a more homogeneous alloy, which in turn results in a more uniform density throughout the refractory metal alloy, and also results in the desired yield and ultimate tensile strengths of the refractory metal alloy. In one non-limiting embodiment, the refractory metal alloy includes less than about 0.5 wt.% other metals and/or impurities. In another non-limiting embodiment, the refractory metal alloy includes less than about 0.2 wt.% other metals and/or impurities. In another non-limiting embodiment, the refractory metal alloy includes less than about 0.1 wt.% other metals and/or impurities. In another non-limiting embodiment, the refractory metal alloy includes less than about 0.05 wt.% other metals and/or impurities. In another non-limiting embodiment, the refractory metal alloy includes less than about 0.01 wt.% other metals and/or impurities.

[0040] In another and/or alternative non-limiting aspect of the present invention, the metal alloy can be nitrided; however, this is not required. The nitride layer on the metal alloy can function as a lubricating surface during the optional drawing of the metal alloy when partially or fully forming the medical device. After the metal alloy is nitrided, the metal alloy is typically cleaned; however, this is not required. During the nitride process, the surface of the metal alloy is modified by the present of nitrogen. The nitriding process can be by gas nitriding, salt bath nitriding, or plasma nitriding. In gas nitriding, the nitrogen diffuses onto the surface of the metal alloy, thereby creating a nitride layer. The thickness and phase constitution of the resulting nitriding layers can be selected and the process optimized for the particular properties required. During gas nitriding, the metal alloy is generally nitrided in the presence of nitrogen gas or a nitrogen gas mixture (e.g., 90-99% vol.% N and 1-10 vol.% H, etc.) for at least 10 seconds a temperature of at least about 400°C (e.g., 400-1000°C and all values and ranges therebetween). In one non-limiting nitriding process, the metal alloy is heated in the presence of nitrogen or a nitrogen-hydrogen mixture to a temperature of at least 400°C, and generally about 400-800°C (and all values and ranges therebetween) for at least 10 seconds (e.g., 10 seconds to 60 minutes and all values and ranges therebetween), and generally about 1-30 minutes. In salt bath nitriding, a nitrogen-containing salt such as cyanide salt is used. During the salt bath nitriding, the metal alloy is generally exposed to temperatures of about 520-590°C. In plasma nitriding, the gas used for plasma nitriding is usually pure nitrogen. Plasma nitriding is often coupled with physical vapor deposition (PVD) process; however, this is not required. Plasma nitriding of the metal alloy generally occurs at a temperature of 220-630°C (and all values and ranges therebetween). The metal alloy can optionally be exposed to argon and/or hydrogen gas prior to the nitriding process to clean and/or preheat the metal alloy. These gasses can be optionally used to clean oxide layers and/or solvents from the surface of the metal alloy. During the nitriding process, the metal alloy can optionally be exposed to hydrogen gas so as to inhibit or prevent the formation of oxides on the surface of the metal alloy. The thickness of the nitride surface layer is less than about 1 mm. In one non-limiting embodiment, the thickness of the nitride surface layer is at least about 50 nanometer and less than about 1 mm (and all values and ranges therebetween). In another non limiting embodiment, the thickness of the nitride surface layer is at least about 50 nanometer and less than about 0.1 mm. When a MoRe alloy is nitride, the weight percent of the nitrogen in the nitride surface layer is less than a weight percent of the molybdenum in the nitride surface layer. Also, the weight percent of nitrogen in the nitride surface layer is less than a weight percent of the rhenium in the nitride surface layer. In one non-limiting composition of the nitride surface layer on a MoRe alloy (e.g., 40-99 wt.% Mo, 1-40 wt.% Re), the nitride surface layer comprises 40-99 wt.% molybdenum (and all values and ranges therebetween), 1-40 wt.% rhenium (and all values and ranges therebetween), and 0.0001-5 wt.% nitrogen (and all values and ranges therebetween). In another non-limiting composition of the nitride surface layer, the nitride surface layer comprises 40-99 wt.% molybdenum, 1-40 wt.% rhenium, and 0.001-1 wt.% nitrogen. As can be appreciated, other refractory alloys can be nitrided. In one non-limiting embodiment of the invention, the surface of the metal alloy is nitrided prior to at least one drawing step for the metal alloy. In another non-limiting aspect of this invention, after the metal alloy has been annealed, the metal alloy is nitrided prior to being drawn. In another and/or alternative non-limiting embodiment, the metal alloy is cleaned to remove nitride compounds on the surface of the metal alloy prior to annealing the metal alloy. The nitride compounds can be removed by a variety of steps such as, but not limited to, grit blasting, polishing, etc. After the metal alloy has been annealed, the metal alloy can be again nitrided prior to one or more drawing steps; however, this is not required. As can be appreciated, the complete outer surface of the metal alloy can be nitrided or a portion of the outer surface of the metal alloy can be nitrided. Nitriding only selected portions of the outer surface of the metal alloy can be used to obtain different surface characteristics of the metal alloy; however, this is not required. As can be appreciated, the final formed metal alloy can include a nitride outer surface. The nitriding process for the metal alloy can be used to increase surface hardness and/or wear resistance of the medical device, and/or to inhibit or prevent discoloration of the metal alloy (e.g., discoloration by oxidation, etc.). For example, the nitriding process can be used to increase the wear resistance of articulation surfaces or surfaces wear on the metal alloy used in the medical device to extend the life of the medical device, and/or to increase the wear life of mating surfaces on the medical device (e.g., polyethylene liners of joint implants like knees, hips, shoulders, etc.), and/or to reduce particulate generation from use of the medical device, and/or to maintain the outer surface appearance of the metal alloy on the medical device.

[0041] In another and/or alternative non-limiting aspect of the present invention, the metal alloy, just prior to or after being partially or fully formed into the desired medical device, can be cleaned, polished, sterilized, nitrided, etc. for final processing of the metal alloy. In one non- limiting embodiment of the invention, the metal alloy is electropolished. In one non-limiting aspect of this embodiment, the metal alloy is cleaned prior to being exposed to the polishing solution; however, this is not required. The cleaning process (when used) can be accomplished by a variety of techniques such as, but not limited to, 1) using a solvent (e.g., acetone, methyl alcohol, etc.) and wiping the metal alloy with a Kimwipe or other appropriate towel, and/or 2) by at least partially dipping or immersing the metal alloy in a solvent and then ultrasonically cleaning the metal alloy. As can be appreciated, the metal alloy can be cleaned in other or additional ways. In another and/or alternative non-limiting aspect of this embodiment, the polishing solution can include one or more acids. One non-limiting formulation of the polishing solution includes about 10-80 percent by volume sulfuric acid (and all values and ranges therebetween). As can be appreciated, other polishing solution compositions can be used. In still another and/or alternative non-limiting aspect of this embodiment, about 5-12 volts (and all values and ranges therebetween) are directed to the metal alloy during the electropolishing process; however, other voltage levels can be used. In yet another and/or alternative non-limiting aspect of this embodiment, the metal alloy is rinsed with water and/or a solvent and allowed to dry to remove polishing solution on the metal alloy.

[0042] Several non-limiting examples of the refractory metal alloy in accordance with the present disclosure are set forth below:

Ex 1 Ex 2 Ex 3 Ex 4

40-80% 40-80% 40-80% 40-80% 0.01-0.3% 0-0.3% 0-0.3% 0-0.3% <0.002% <0.002% <0.002% <0.002% 0-0.2% 0-0.2% 0.01-0.2% 0-0.2% <0.02% <0.02% <0.02% <0.02% <0.002% <0.002% <0.002% <0.002% 0.1 -2.5% 0-2.5% 0-2.5% 0-2.5% <0.06% <0.06% <0.06% <0.06% <1% <1% <1% <1%

0-2% 0.1-2% 0-2% 0-2% <20 ppm <20 ppm <20 ppm <20 ppm <0.01% <0.01% <0.01% <0.01% Pt <1% <1% <1% <1%

Re 20-49% 20-49% 20-49% 20-49%

S <0.008% <0.008% <0.008% <0.008%

Sn <0.002% <0.002% <0.002% <0.002%

Ta 0-50% 0-50% 0-50% 0-50%

Tc <1% <1% <1% <1%

Ti <1% <1% <1% <1%

V <1% <1% <1% <1% w 0-50% 0-50% 0-50% 0.5-50%

Y ₂ C>3 0-1% 0-1% 0.1-1% 0-1%

Zr <1% <1% <1% <1%

Zr0 ₂ 0-3% 0-3% 0-3% 0-3%

CNT 0-10% 0-10% 0-10% 0-10%

Ex 5 Ex 6 Ex 7 40-80% 40-80% 40-80% 0-0.3% 0-0.3% 0-0.3% <0.002% <0.002% <0.002% 0-0.2% 0-0.2% 0-0.2% <0.002% <0.002% <0.002% 0-2.5% 0-2.5% 0-2.5% <0.06% <0.06% <0.06% <1% <1% <1% 0-2% 0-2% 0-2% <20 ppm <20 ppm <20 ppm <0.01% <0.01% <0.01% <1% <1% <1% 20-49% 20-49% 20-49% <0.008% <0.008% <0.008% <0.002% <0.002% <0.002% 0-50% 0.5-50% 0-50% <1% <1% <1% <1% <1% <1% <1% <1% <1% 0-50% 0-50% 0-50% 0-1% 0-1% 0-1% 0.1-3% 0-3% 0-3% 0-10% 0-10% 0-10%

Metal/Wt. % Ex 8 Ex 9 Ex 10

Mo 45-78% 45-75% 45-70%

C 0-0.3% 0-0.3% 0-0.3%

Co <0.002% <0.002% <0.002%

Cs ₂ 0 0-0.2% 0-0.2% 0-0.2%

H <0.002% <0.002% <0.002%

Hf 0-2.5% 0-2.5% 0-2.5% O <0.06% <0.06% <0.06%

Os <1% <1% <1%

La ₂ 0 ₃ 0-2% 0-2% 0-2%

N <20 ppm <20 ppm <20 ppm

Nb <0.01% <0.01% <0.01%

Pt <1% <1% <1%

Re 22-49% 25-49% 30-49%

S <0.008% <0.008% <0.008%

Sn <0.002% <0.002% <0.002%

Ta 0-50% 0.5-50% 0-50%

Tc <1% <1% <1%

Ti <1% <1% <1%

V <1% <1% <1%

W 0-50% 0-50% 0-50%

Y ₂ 0 ₃ 0-1% 0-1% 0-1%

Zr0 ₂ 0.1-3% 0-3% 0-3%

CNT 0-10% 0-10% 0-10%

Ex 11 Ex 12 Ex 13 Ex 14 35-80% 35-80% 35-70% 35-65% 0.05-0.15% 0-0.15% 0-0.15% 0-0.15% 0-0.2% 0-0.2% 0.04-0.1% 0-0.2% 0.8-1.4% 0-2% 0-2.5% 0-2.5% 0-2% 0.3 -0.7% 0-2% 0-2% 20-49% 20-49% 30-49% 35-49% 0-2% 0-2% 0-50% 0-50%

0-2% 0-2% 0-50% 20-50%

0-1% 0-1% 0.3-0.5% 0-1% 0-3% 0-3% 0-3% 0-3%

Metal/Wt. % Ex 15 Ex 16 Ex 17

Mo 40-60% 35-60% 30-60%

C 0-0.15% 0-0.15% 0-0.15%

Cs ₂ 0 0-0.2% 0-0.2% 0-0.2%

Hf 0-2.5% 0-2.5% 0-2.5%

La ₂ 0 ₃ 0-2% 0-2% 0-2%

Re 40-60% 40-65% 40-70%

Ta 0-3% 10-50% 0-40%

W 0-3% 0-50% 0-40%

Y ₂ 0 ₃ 0-1% 0-1% 0-1%

Zr0 ₂ 1.2-1.8% 0-3% 0-3%

Metal/Wt. % Ex 18 Ex 19 Ex 20

W 20-80% 60-80% 20-78%

Re 20-47.5% 20-40% 22-47.5%

Mo 0-47.5% <0.5% 1-47.5% <0.5% <0.5% <0.5%

<0.15% <0.15% <0.15%

<0.002% <0.002% <0.002%

<0.2% <0.2% <0.2%

<0.02% <0.02% <0.02%

<0.002% <0.002% <0.002%

<0.5% <0.5% <0.5%

<0.5% <0.5% <0.5%

<0.06% <0.06% <0.06%

<0.5% <0.5% <0.5%

<20 ppm <20 ppm <20 ppm

<0.01% <0.01% <0.01%

<0.5% <0.5% <0.5%

<0.008% <0.008% <0.008%

<0.002% <0.002% <0.002%

<0.5% <0.5% <0.5%

<0.5% <0.5% <0.5%

<0.5% <0.5% <0.5%

<0.5% <0.5% <0.5%

<0.5% <0.5% <0.5%

<0.5% <0.5% <0.5%

<0.5% <0.5% <0.5% 0-10% 0-10% <0.5%.

Metal/Wt. % Ex 21 Ex 22 Ex 23

W 20-80% 60-80% 20-75%

Re 20-47.5% 20-40% 25-47.5%

Mo 0-47.5% <0.5% 1-47.5%

Metal/Wt. % Ex 24 Ex 25 Ex 26

W 50.1-80% 65-80% 50.1-79%

Re 20-40% 20-35% 20-40%

Mo 0-40% <0.5% 1-30%

Metal/Wt. % Ex 27 Ex 28 Ex 29

W 20-49% 20-49% 20-49%

Re 20-60% 30-60% 40-60%

Mo 0-40% 0-40% 0-39%

Metal/Wt. % Ex 30 Ex 31 Ex 32 Re 20-98% 60-95% 80-90% Mo 0-80% 0-40% 0-20% W 0-80% 0-40% 0-20%

Metal/Wt. % Ex 33 Ex 34 Ex 35 W 20-49% 20-49% 20-49% Re 20-40% 20-40% 22-39%

Mo 20-60% 30-60% 40-60%

Metal/Wt. % Ex. 36 Ex 37 Ex 38

W 20-40% 20-35% 20-30%

Re 20-40% 20-40% 31-40%

Mo 0-40% 10-40% 31-40%

Wt. % Ex 39 Ex 40 Ex 41 Ex 42

Re 30-60% 35-60% 35-60% 35-60%

Mo 0-55% 10-55% 10-55% 10-55%

Bi 1-42 0-32 0-32 0-32

Cr 0-32 1-42 0-32 0-32

Ir 0-32 0-32 1-42 0-32

Nb 0-32 0-32 0-32 1-42

Ta 0-32 0-32 0-32 0-32

Ti 0-32 0-32 0-32 0-32

Y 0-32 0-32 0-32 0-32

Zr 0-32 0-32 0-32 0-32

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06

Wt. % Ex 43 Ex 44 Ex 45 Ex 46

Re 30-60% 35-60% 35-60% 35-60%

Mo 15-55% 15-55% 15-55% 15-55%

Bi 0-32 0-32 0-32 0-32

Cr 0-32 0-32 0-32 0-32

Ir 0-32 0-32 0-32 0-32

Nb 0-32 0-32 0-32 0-32

Ta 1-42 0-32 0-32 0-32

Ti 0-32 1-42 0-32 0-32

Y 0-32 0-32 1-42 0-32

Zr 0-32 0-32 0-32 1-42

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06

Wt. % Ex 47 Ex 48 Ex 49 Ex 50

Re 41-59% 41-59% 41-59% 41-59%

Mo 18-45% 18-45% 18-45% 18-45%

Bi 1-42 0-32 0-32 0-32

Cr 0-32 1-42 0-32 0-32

Ir 0-32 0-32 1-42 0-32

Nb 0-32 0-32 0-32 1-42

Ta 0-32 0-32 0-32 0-32 Ti 0-32 0-32 0-32 0-32

Y 0-32 0-32 0-32 0-32

Zr 0-32 0-32 0-32 0-32

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06

Wt. % Ex 51 Ex 52 Ex 53 Ex 54

Re 41-59% 41-59% 41-59% 41-59%

Mo 18-45% 18-45% 18-45% 18-45%

Bi 0-32 0-32 0-32 0-32

Cr 0-32 0-32 0-32 0-32

Ir 0-32 0-32 0-32 0-32

Nb 0-32 0-32 0-32 0-32

Ta 1-42 0-32 0-32 0-32

Ti 0-32 1-42 0-32 0-32

Y 0-32 0-32 1-42 0-32

Zr 0-32 0-32 0-32 1-42

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06 wt. % Ex 55 Ex 56 Ex 57 Ex 58

Re 41-59% 41-59% 41-59% 41-59%

Mo 18-45% 18-45% 18-45% 18-45%

Bi 0-15 0-15 1-36 0-15

Cr 1-20 1-20 1-20 1-20

Ir 0-15 0-15 0-15 0-15

Nb 1-36 0-15 0-15 0-15

Ta 0-15 1-36 0-15 0-15

Ti 0-15 0-15 0-15 0-15

Y 0-15 0-15 0-15 0-15

Zr 0-15 0-15 0-15 1-36

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06

Wt. % Ex 59 Ex 60 Ex 61 Ex 62

Re 41-59% 41-59% 41-59% 41-59%

Mo 18-45% 18-45% 18-45% 18-45%

Bi 1-36 0-15 0-15 0-15

Cr 1-20 1-20 1-20 1-20

Ir 0-15 1-36 0-15 0-15

Nb 0-15 0-15 0-15 0-15

Ta 0-15 0-15 0-15 0-15

Ti 0-15 0-15 1-36 0-15 Y 0-15 0-15 0-15 1-36

Zr 0-15 0-15 0-15 0-15

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06

Wt. % Ex 63 Ex 64 Ex 65 Ex 66

Re 41-59% 41-59% 41-59% 41-59%

Mo 18-45% 18-45% 18-45% 18-45%

Bi 1-34 0-15 0-15 0-15

Cr 0-15 0-15 0-15 0-15

Ir 0-15 0-15 0-15 1-34

Nb 3-27 3-27 3-27 3-27

Ta 0-42 1-34 0-15 0-15

Ti 0-15 0-15 0-15 0-15

Y 0-15 0-15 0-15 0-15

Zr 0-15 0-15 3-27 0-15

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06 wt. % Ex 67 Ex 68 Ex 69 Ex 70

Re 41-59% 41-59% 41-59% 41-59%

Mo 18-45% 18-45% 18-45% 18-45%

Bi 0-15 0-15 0-15 0-15

Cr 0-15 0-15 0-15 0-15

Ir 0-15 1-34 0-15 0-15

Nb 0-15 0-15 0-15 0-15

Ta 1-34 0-15 3-27 0-15

Ti 0-15 0-15 0-15 0-15

Y 0-15 0-15 0-15 3-27

Zr 3-27 3-27 3-27 3-27

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06

Wt. % Ex 71 Ex 72 Ex 73 Ex 74

Re 41-59% 41-59% 41-59% 41-59%

Mo 18-45% 18-45% 18-45% 18-45%

Bi 0-15 0-15 0-15 0-15

Cr 0-15 0-15 0-15 1-10

Ir 1-34 0-25 3-27 0-15

Nb 0-15 3-27 0-15 0-15

Ta 0-15 0-15 1-34 0-15

Ti 0-15 0-15 0-15 0-15

Y 3-27 3-27 0-15 0-15 Zr 0-15 0-15 3-27 1-12

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06

Element/Wt. % Ex 75 Ex 76 Ex 77 Ex 78

Re 50-75% 55-75% 60-75% 65-75%

Cr 25-50% 25-45% 25-40% 25-35%

Mo 0-25% 0-25% 0-25% 0-25%

Bi 0-25% 0-25% 0-25% 0-25%

Cr 0-25% 0-25% 0-25% 0-25%

Ir 0-25% 0-25% 0-25% 0-25%

Nb 0-25% 0-25% 0-25% 0-25%

Ta 0-25% 0-25% 0-25% 0-25%

V 0-25% 0-25% 0-25% 0-25% w 0-25% 0-25% 0-25% 0-25%

Mn 0-25% 0-25% 0-25% 0-25%

Tc 0-25% 0-25% 0-25% 0-25%

Ru 0-25% 0-25% 0-25% 0-25%

Rh 0-25% 0-25% 0-25% 0-25%

Hf 0-25% 0-25% 0-25% 0-25%

Os 0-25% 0-25% 0-25% 0-25%

Cu 0-25% 0-25% 0-25% 0-25%

Ir 0-25% 0-25% 0-25% 0-25%

Ti 0-25% 0-25% 0-25% 0-25%

Y 0-25% 0-25% 0-25% 0-25% Zr 0-25% 0-25% 0-25% 0-25% C <0.06 <0.06 <0.06 <0.06 N <0.06 <0.06 <0.06 <0.06 O <0.06 <0.06 <0.06 <0.06

Element/Wt. % Ex 79 Ex 80 Ex 81 Ex 82

Re 50-72% 55-72% 60-72% 65-72%

Cr 28-50% 28-45% 28-40% 28-35%

Mo 0-25% 0-25% 0-25% 0-25%

Bi 0-10% 0-10% 0-10% 0-10%

Cr 0-10% 0-10% 0-10% 0-10%

Ir 0-10% 0-10% 0-10% 0-10%

Nb 0-10% 0-10% 0-10% 0-10%

Ta 0-10% 0-10% 0-10% 0-10%

V 0-10% 0-10% 0-10% 0-10%

W 0-10% 0-10% 0-10% 0-10%

Mn 0-10% 0-10% 0-10% 0-10%

Tc 0-10% 0-10% 0-10% 0-10%

Ru 0-10% 0-10% 0-10% 0-10%

Rh 0-10% 0-10% 0-10% 0-10% Hf 0-10% 0-10% 0-10% 0-10%

Os 0-10% 0-10% 0-10% 0-10%

Cu 0-10% 0-10% 0-10% 0-10%

Ir 0-10% 0-10% 0-10% 0-10%

Ti 0-10% 0-10% 0-10% 0-10%

Y 0-10% 0-10% 0-10% 0-10%

Zr 0-10% 0-10% 0-10% 0-10%

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06

Element/Wt. % Ex 83 Ex 84 Ex 85 Ex 86

Re 50-70% 55-70% 60-70% 65-70%

Cr 30-50% 30-45% 30-40% 30-35%

Mo 0-10% 0-10% 0-10% 0-10%

Bi 0-10% 0-10% 0-10% 0-10%

Cr 0-10% 0-10% 0-10% 0-10%

Ir 0-10% 0-10% 0-10% 0-10%

Nb 0-10% 0-10% 0-10% 0-10%

Ta 0-10% 0-10% 0-10% 0-10%

Y 0-10% 0-10% 0-10% 0-10%

W 0-10% 0-10% 0-10% 0-10%

Mn 0-10% 0-10% 0-10% 0-10%

Tc 0-10% 0-10% 0-10% 0-10%

Ru 0-10% 0-10% 0-10% 0-10%

Rh 0-10% 0-10% 0-10% 0-10%

Hf 0-10% 0-10% 0-10% 0-10%

Os 0-10% 0-10% 0-10% 0-10%

Cu 0-10% 0-10% 0-10% 0-10%

Ir 0-10% 0-10% 0-10% 0-10%

Ti 0-10% 0-10% 0-10% 0-10%

Y 0-10% 0-10% 0-10% 0-10%

Zr 0-10% 0-10% 0-10% 0-10%

C <0.06 <0.06 <0.06 <0.06

N <0.06 <0.06 <0.06 <0.06

O <0.06 <0.06 <0.06 <0.06

Element/Wt. % Ex 87 Ex 88 Ex 89 Ex 90

Re 50-67.5% 55-67.5% 60-67.5% 65-67.5%

Cr 32.5-50% 32.5-45% 32.5-40% 32.5-35%

Mo 0-10% 0-10% 0-10% 0-10%

Bi 0-10% 0-10% 0-10% 0-10%

Cr 0-10% 0-10% 0-10% 0-10%

Ir 0-10% 0-10% 0-10% 0-10%

Nb 0-10% 0-10% 0-10% 0-10%

Ta 0-10% 0-10% 0-10% 0-10% V 0-10% 0-10% 0-10% 0-10% W 0-10% 0-10% 0-10% 0-10% Mn 0-10% 0-10% 0-10% 0-10% Tc 0-10% 0-10% 0-10% 0-10% Ru 0-10% 0-10% 0-10% 0-10% Rh 0-10% 0-10% 0-10% 0-10% Hf 0-10% 0-10% 0-10% 0-10% Os 0-10% 0-10% 0-10% 0-10% Cu 0-10% 0-10% 0-10% 0-10% Ir 0-10% 0-10% 0-10% 0-10% Ti 0-10% 0-10% 0-10% 0-10%

Y 0-10% 0-10% 0-10% 0-10% Zr 0-10% 0-10% 0-10% 0-10% C <0.06 <0.06 <0.06 <0.06 N <0.06 <0.06 <0.06 <0.06 O <0.06 <0.06 <0.06 <0.06

Element/Wt. % Ex 91 Ex 92 Ex 93 Ex 94

Re 50-67.5% 55-67.5% 60-67.5% 65-67.5%

Cr 32.5-50% 32.5-45% 32.5-40% 32.5-35%

Mo 0-5% 0-5% 0-5% 0-5%

Bi 0-5% 0-5% 0-5% 0-5%

Cr 0-5% 0-5% 0-5% 0-5%

Ir 0-5% 0-5% 0-5% 0-5%

Nb 0-5% 0-5% 0-5% 0-5%

Ta 0-5% 0-5% 0-5% 0-5%

V 0-5% 0-5% 0-5% 0-5% w 0-5% 0-5% 0-5% 0-5%

Mn 0-5% 0-5% 0-5% 0-5%

Tc 0-5% 0-5% 0-5% 0-5%

Ru 0-5% 0-5% 0-5% 0-5%

Rh 0-5% 0-5% 0-5% 0-5%

Hf 0-5% 0-5% 0-5% 0-5%

Os 0-5% 0-5% 0-5% 0-5%

Cu 0-5% 0-5% 0-5% 0-5%

Ir 0-5% 0-5% 0-5% 0-5%

Ti 0-5% 0-5% 0-5% 0-5%

Y 0-5% 0-5% 0-5% 0-5% Zr 0-5% 0-5% 0-5% 0-5% C <0.06 <0.06 <0.06 <0.06 N <0.06 <0.06 <0.06 <0.06 O <0.06 <0.06 <0.06 <0.06

Metal/Wt. % Ex 95 Ex 96 Ex 97 Ex 98 Mo 40-99.98% 40-99.9% 40-99.8% 40-99.5% 0.01-0.3% 0-0.3% 0-0.3% 0-0.3% <0.002% <0.002% <0.002% <0.002% 0-0.2% 0-0.2% 0.01-0.2% 0-0.2% <0.02% <0.02% <0.02% <0.02% <0.002% <0.002% <0.002% <0.002% 0.1 -2.5% 0-2.5% 0-2.5% 0-2.5% <0.06% <0.06% <0.06% <0.06% <1% <1% <1% <1%

0-2% 0.1-2% 0-2% 0-2%

<20 ppm <20 ppm <20 ppm <20 ppm <0.01% <0.01% <0.01% <0.01% <1% <1% <1% <1% 0-40% 0-40% 0-40% 0-40% <0.008% <0.008% <0.008% <0.008% <0.002% <0.002% <0.002% <0.002% 0-50% 0-50% 0-50% 0-50% <1% <1% <1% <1%

<1% <1% <1% <1%

<1% <1% <1% <1%

0-50% 0-50% 0-50% 0.5-50%

0-1% 0-1% 0.1-1% 0-1%

<1% <1% <1% <1%

0-3% 0-3% 0-3% 0-3% 0-10% 0-10% 0-10% 0-10%

Metal/Wt. % Ex 99 Ex 100 Ex 101

Mo 40-99.9% 40-99.5% 40-99.5%

C 0-0.3% 0-0.3% 0-0.3%

Co <0.002% <0.002% <0.002%

Cs ₂ 0 0-0.2% 0-0.2% 0-0.2%

H <0.002% <0.002% <0.002%

Hf 0-2.5% 0-2.5% 0-2.5%

O <0.06% <0.06% <0.06%

Os <1% <1% <1%

La ₂ 0 ₃ 0-2% 0-2% 0-2%

N <20 ppm <20 ppm <20 ppm

Nb <0.01% <0.01% <0.01%

Pt <1% <1% <1%

Re 0-40% 0-40% 0.5-40%

S <0.008% <0.008% <0.008%

Sn <0.002% <0.002% <0.002%

Ta 0-50% 0.5-50% 0-50%

Tc <1% <1% <1%

Ti <1% <1% <1%

V <1% <1% <1%

W 0-50% 0-50% 0-50% Y2O3 0-1% 0-1% 0-1%

Zr0 ₂ 0.1-3% 0-3% 0-3%

CNT 0-10% 0-10% 0-10%

Ex 102 Ex 103 Ex 104

60-99% 60-95% 60-90% 0-0.3% 0-0.3% 0-0.3% <0.002% <0.002% <0.002% 0-0.2% 0-0.2% 0-0.2% <0.002% <0.002% <0.002% 0-2.5% 0-2.5% 0-2.5% <0.06% <0.06% <0.06% <1% <1% <1% 0-2% 0-2% 0-2% <20 ppm <20 ppm <20 ppm <0.01% <0.01% <0.01% <1% <1% <1% 1-40% 5-40% 10-40% <0.008% <0.008% <0.008% <0.002% <0.002% <0.002% 0-50% 0.5-50% 0-50% <1% <1% <1% <1% <1% <1% <1% <1% <1% 0-50% 0-50% 0-50% 0-1% 0-1% 0-1% 0.1-3% 0-3% 0-3% 0-10% 0-10% 0-10%

Metal/Wt. % Ex 105 Ex 106 Ex 107 Ex 108

Mo 98-99.15% 98-99.7% 50-99.66% 40-80%

C 0.05-0.15% 0-0.15% 0-0.15% 0-0.15%

Cs ₂ 0 0-0.2% 0-0.2% 0.04-0.1% 0-0.2%

Hf 0.8-1.4% 0-2% 0-2.5% 0-2.5%

La ₂ 0 ₃ 0-2% 0.3 -0.7% 0-2% 0-2%

Re 0-2% 0-2% 0-40% 0-40%

Ta 0-2% 0-2% 0-50% 0-50%

W 0-2% 0-2% 0-50% 20-50%

Y ₂ 0 ₃ 0-1% 0-1% 0.3-0.5% 0-1%

Zr0 ₂ 0-3% 0-3% 0-3% 0-3%

Metal/Wt. % Ex 109 Ex 110 Ex 111

Mo 97-98.8% 50-90% 60-99.5%

C 0-0.15% 0-0.15% 0-0.15%

Cs ₂ 0 0-0.2% 0-0.2% 0-0.2%

Hf 0-2.5% 0-2.5% 0-2.5% La ₂ 0 ₃ 0-2% 0-2% 0-2%

Re 0-3% 0-40% 0.5-40%

Ta 0-3% 10-50% 0-40%

W 0-3% 0-50% 0-40%

Y ₂ 0 ₃ 0-1% 0-1% 0-1%

Zr0 ₂ 1.2-1.8% 0-3% 0-3%

Ex 112 Ex 113 Ex 114

20-99% 60-99% 20-80% 1-47.5% 1-40% 1-47.5% 0-47.5% <0.5% 1-47.5% <0.5% <0.5% <0.5% <0.15% <0.15% <0.15% <0.002% <0.002% <0.002% <0.2% <0.2% <0.2% <0.02% <0.02% <0.02% <0.002% <0.002% <0.002% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.06% <0.06% <0.06% <0.5% <0.5% <0.5% <20 ppm <20 ppm <20 ppm <0.01% <0.01% <0.01% <0.5% <0.5% <0.5% <0.008% <0.008% <0.008% <0.002% <0.002% <0.002% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% 0-10% 0-10% <0.5%.

Metal/Wt. % Ex 115 Ex 116 Ex 117 Ex 118

W 1-99.9% 1-99.9% 1-99.9% 10-99%

Cu 0.1-99% 0.1-99% 0.1-99% 1-90%

C 0.01-0.3% 0-0.3% 0-0.3% 0-0.3%

Co <0.002% <0.002% <0.002% <0.002%

Cs ₂ 0 0-0.2% 0-0.2% 0.01-0.2% 0-0.2%

Fe <0.02% <0.02% <0.02% <0.02%

H <0.002% <0.002% <0.002% <0.002%

Hf 0.1 -2.5% 0-2.5% 0-2.5% 0-2.5%

O <0.06% <0.06% <0.06% <0.06%

Os <1% <1% <1% <1% La203 0-2% 0.1-2% 0-2% 0-2%

Mo 0-5% 0.1-3% 0-2% 0-3%

N <20 ppm <20 ppm <20 ppm <20 ppm

Nb <0.01% <0.01% <0.01% <0.01%

Pt <1% <1% <1% <1%

Re 0-40% 0-40% 0-40% 0-40%

S <0.008% <0.008% <0.008% <0.008%

Sn <0.002% <0.002% <0.002% <0.002%

Ta 0-50% 0-50% 0-50% 0-50%

Tc <1% <1% <1% <1%

Ti <1% <1% <1% <1%

V <1% <1% <1% <1%

Y2O3 0-1% 0-1% 0.1-1% 0-1%

Zr <1% <1% <1% <1%

Zr0 ₂ 0-3% 0-3% 0-3% 0-3%

CNT 0-10% 0-10% 0-10% 0-10%

Ex 119 Ex 120 Ex 121

20-98% 25-98% 30-95%

2-80% 2-75% 5-70%

0-0.3% 0-0.3% 0-0.3%

<0.002% <0.002% <0.002%

0-0.2% 0-0.2% 0-0.2%

<0.002% <0.002% <0.002%

0-2.5% 0-2.5% 0-2.5%

<0.06% <0.06% <0.06%

<1% <1% <1%

0-2% 0-2% 0-2%

0-3% 0-2% 0-1%

<20 ppm <20 ppm <20 ppm <0.01% <0.01% <0.01% <1% <1% <1% 0-40% 0-40% 0.5-40% <0.008% <0.008% <0.008% <0.002% <0.002% <0.002% 0-50% 0.5-50% 0-50% <1% <1% <1% <1% <1% <1% <1% <1% <1% 0-1% 0-1% 0-1% 0.1-3% 0-3% 0-3% 0-10% 0-10% 0-10%

Metal/Wt. % Ex 122 Ex 123 Ex 124 Ex 125

W 25-95% 35-95% 40-95% 50-95%

Cu 5-75% 5-65% 5-60% 5-50% 0.05-0.15% 0-0.15% 0-0.15% 0-0.15%

0-0.2% 0-0.2% 0.04-0.1% 0-0.2%

0.8-1.4% 0-2.5% 0-2.5% 0-2.5%

0-2% 0.3 -0.7% 0-2% 0-2%

0-40% 0-40% 0-40% 0-40%

0-50% 0-50% 0-50% 0-50%

0-1% 0-1% 0.3-0.5% 0-1% 0-3% 0-3% 0-3% 0-3%

Metal/Wt. % Ex 126 Ex 127 Ex 128 W 55-99% 60-99% 70-99% Cu 1-45% 1-40% 1-30% C 0-0.15% 0-0.15% 0-0.15%

Cs ₂ 0 0-0.2% 0-0.2% 0-0.2%

Hf 0-2.5% 0-2.5% 0-2.5%

La ₂ 0 ₃ 0-2% 0-2% 0-2%

Re 0-40% 0-40% 5-40%

Ta 0-50% 10-50% 0-50%

W 0-50% 0-50% 0-50%

Y ₂ 0 ₃ 0-1% 0-1% 0-1%

Zr0 ₂ 1.2-1.8% 0-3% 0-3%

Metal/Wt. % Ex 129 Ex 130 Ex 131

Ti 55-80% 65-80% 70-80%

Mo 20-30% 20-30% 20-25%

Re <0.5% <0.5% <0.5%

Yt <0.5% <0.5% <0.5%

Nb <0.5% <0.5% <0.5%

Co <0.5% <0.5% <0.5%

Cr <0.5% <0.5% <0.5%

Zr <0.5% <0.5% <0.5%

C <0.15% <0.15% <0.15%

O <0.06% <0.06% <0.06%

N <20 ppm <20 ppm <20 ppm

Metal/Wt. % Ex 132 Ex 133 Ex 134

W 20-99% 60-99% 20-80%

Re 1-47.5% 1-40% 1-47.5%

Mo 0-47.5% <0.5% 1-47.5%

Metal/Wt. % Ex 135 Ex 136 Ex 137

W 50.1-99% 65-99% 70-99%

Re 1-40% 1-35% 1-30%

Mo 0-40% <0.5% 1-30%

Metal/Wt. % Ex 138 Ex 139 Ex 140 W 20-49% 20-49% 20-49%

Re 1-40% 1-40% 1-39%

Mo 20-60% 30-60% 40-60%

Metal/Wt. % Ex. 141 Ex 142 Ex 143

W 20-40% 20-35% 20-30%

Re 1-40% 10-40% 25-40%

Mo 0-40% 10-40% 25-40%

Ex 144 Ex 145 Ex 146

20-99% 60-99% 20-80% 1-47.5% 1-40% 1-47.5% 0-47.5% <0.5% 1-47.5% <0.5% <0.5% <0.5% <0.15% <0.15% <0.15% <0.002% <0.002% <0.002% <0.2% <0.2% <0.2% <0.02% <0.02% <0.02% <0.002% <0.002% <0.002% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.06% <0.06% <0.06% <0.5% <0.5% <0.5% <20 ppm <20 ppm <20 ppm <0.01% <0.01% <0.01% <0.5% <0.5% <0.5% <0.008% <0.008% <0.008% <0.002% <0.002% <0.002% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% <0.5% 0-10% 0-10% <0.5%.

[0043] In Examples 1-146, it will be appreciated that all of the above ranges include any value between the range and any other range that is between the ranges set forth above. Any of the above values that include the < symbol includes the range from 0 to the stated value and all values and ranges therebetween.

[0044] In the above refractory metal alloys, the average grain size of the refractory metal alloy can be about 4-20 ASTM, the tensile elongation of the refractory metal alloy can be about 25- 50%, the average density of the refractory metal alloy can be at least about 5 gm/cc, the average yield strength of the refractory metal alloy can be about 70-250 (ksi), the average ultimate tensile strength of the refractory metal alloy can be about 80-550 UTS (ksi), and an average Vickers hardness can be 234 DPH to 700 DPH or a Rockwell C hardness of 19-60 at 77°F; however, this is not required.

[0045] In another and/or alternative non-limiting aspect of the present invention, the use of the novel metal alloy to partially or fully form the medical device can be used to increase the strength and/or hardness and/or durability of the medical device as compared with stainless steel or chromium-cobalt alloys; thus, less quantity of novel metal alloy can be used in the medical device to achieve similar strengths as compared to medical devices formed of different metals. As such, the resulting medical device can be made smaller and less bulky by use of the novel metal alloy without sacrificing the strength and durability of the medical device. Such a medical device can have a smaller profile, thus can be inserted in smaller areas, openings and/or passageways. The novel metal alloy also can increase the radial strength of the medical device. For instance, the thickness of the walls of the medical device and/or the wires used to form the medical device can be made thinner and achieve a similar or improved radial strength as compared with thicker walled medical devices formed of stainless steel or cobalt and chromium alloy. The novel metal alloy also can improve stress-strain properties, bendability and flexibility of the medical device, thus increase the life of the medical device. For instance, the medical device can be used in regions that subject the medical device to bending. Due to the improved physical properties of the medical device from the novel metal alloy, the medical device has improved resistance to fracturing in such frequent bending environments. In addition or alternatively, the improved bendability and flexibility of the medical device due to the use of the novel metal alloy can enable the medical device to be more easily inserted into various regions of a body. The novel metal alloy can also reduce the degree of recoil during the crimping and/or expansion of the medical device. For example, the medical device better maintains its crimped form and/or better maintains its expanded form after expansion due to the use of the novel metal alloy. As such, when the medical device is to be mounted onto a delivery device when the medical device is crimped, the medical device better maintains its smaller profile during the insertion of the medical device into various regions of a body. Also, the medical device better maintains its expanded profile after expansion so as to facilitate in the success of the medical device in the treatment area. In addition to the improved physical properties of the medical device by use of the novel metal alloy, the novel metal alloy has improved radiopaque properties as compared to standard materials such as stainless steel or cobalt-chromium alloy, thus reducing or eliminating the need for using marker materials on the medical device. For instance, the novel metal alloy is believed to at least about 10-20% more radiopaque than stainless steel or cobalt-chromium alloy. Specifically, the novel metal alloy (e.g., novel refractory alloys) is believed to be at least about 33% more radiopaque than cobalt-chromium alloy and is believed to be at least about 40% more radiopaque than stainless steel.

[0046] In yet another and/or alternative non-limiting aspect of the present invention, the medical device can include, contain and/or be coated with one or more agents that facilitate in the success of the medical device and/or treated area. The term “agent” includes, but is not limited to a substance, pharmaceutical, biologic, veterinary product, drug, and analogs or derivatives otherwise formulated and/or designed to prevent, inhibit and/or treat one or more clinical and/or biological events, and/or to promote healing. Non-limiting examples of clinical events that can be addressed by one or more agents include, but are not limited to, viral, fungus and/or bacterial infection; vascular diseases and/or disorders; digestive diseases and/or disorders; reproductive diseases and/or disorders; lymphatic diseases and/or disorders; cancer; implant rejection; pain; nausea; swelling; arthritis; bone diseases and/or disorders; organ failure; immunity diseases and/or disorders; cholesterol problems; blood diseases and/or disorders; lung diseases and/or disorders; heart diseases and/or disorders; brain diseases and/or disorders; neuralgia diseases and/or disorders; kidney diseases and/or disorders; ulcers; liver diseases and/or disorders; intestinal diseases and/or disorders; gallbladder diseases and/or disorders; pancreatic diseases and/or disorders; psychological disorders; respiratory diseases and/or disorders; gland diseases and/or disorders; skin diseases and/or disorders; hearing diseases and/or disorders; oral diseases and/or disorders; nasal diseases and/or disorders; eye diseases and/or disorders; fatigue; genetic diseases and/or disorders; bums; scarring and/or scars; trauma; weight diseases and/or disorders; addiction diseases and/or disorders; hair loss; cramps; muscle spasms; tissue repair; nerve repair; neural regeneration and/or the like. Non-limiting examples of agents that can be used include, but are not limited to, 5-fluorouracil and/or derivatives thereof; 5-phenylmethimazole and/or derivatives thereof; ACE inhibitors and/or derivatives thereof; acenocoumarol and/or derivatives thereof; acyclovir and/or derivatives thereof; actilyse and/or derivatives thereof; adrenocorticotropic hormone and/or derivatives thereof; adriamycin and/or derivatives thereof; agents that modulate intracellular Ca2+ transport such as L-type (e.g., diltiazem, nifedipine, verapamil, etc.) or T-type Ca2+ channel blockers (e.g., amiloride, etc.); alpha-adrenergic blocking agents and/or derivatives thereof; alteplase and/or derivatives thereof; amino glycosides and/or derivatives thereof (e.g., gentamycin, tobramycin, etc.); angiopeptin and/or derivatives thereof; angiostatic steroid and/or derivatives thereof; angiotensin II receptor antagonists and/or derivatives thereof; anistreplase and/or derivatives thereof; antagonists of vascular epithelial growth factor and/or derivatives thereof; antibiotics; anti-coagulant compounds and/or derivatives thereof; anti-fibrosis compounds and/or derivatives thereof; antifungal compounds and/or derivatives thereof; anti inflammatory compounds and/or derivatives thereof; anti -invasive factor and/or derivatives thereof; anti-metabolite compounds and/or derivatives thereof (e.g., staurosporin, trichothecenes, and modified diphtheria and ricin toxins, pseudomonas exotoxin, etc.); anti -matrix compounds and/or derivatives thereof (e.g., colchicine, tamoxifen, etc.); anti-microbial agents and/or derivatives thereof; anti-migratory agents and/or derivatives thereof (e.g., caffeic acid derivatives, nilvadipine, etc.); anti-mitotic compounds and/or derivatives thereof; anti -neoplastic compounds and/or derivatives thereof; anti-oxidants and/or derivatives thereof; anti -platelet compounds and/or derivatives thereof; anti-proliferative and/or derivatives thereof; anti-thrombogenic agents and/or derivatives thereof; argatroban and/or derivatives thereof; ap-1 inhibitors and/or derivatives thereof (e.g., for tyrosine kinase, protein kinase C, myosin light chain kinase, Ca2+/calmodulin kinase II, casein kinase II, etc.); aspirin and/or derivatives thereof; azathioprine and/or derivatives thereof; b-estradiol and/or derivatives thereof; b-1-anticollagenase and/or derivatives thereof; calcium channel blockers and/or derivatives thereof; calmodulin antagonists and/or derivatives thereof (e.g., H7, etc.); CAPTOPRIL and/or derivatives thereof; cartilage- derived inhibitor and/or derivatives thereof; ChIMP-3 and/or derivatives thereof; cephalosporin and/or derivatives thereof (e.g., cefadroxil, cefazolin, cefaclor, etc.); chloroquine and/or derivatives thereof; chemotherapeutic compounds and/or derivatives thereof (e.g., 5-fluorouracil, vincristine, vinblastine, cisplatin, doxyrubicin, adriamycin, tamocifen, etc.); chymostatin and/or derivatives thereof; CILAZAPRIL and/or derivatives thereof; clopidigrel and/or derivatives thereof; clotrimazole and/or derivatives thereof; colchicine and/or derivatives thereof; cortisone and/or derivatives thereof; coumadin and/or derivatives thereof; curacin-A and/or derivatives thereof; cyclosporine and/or derivatives thereof; cytochalasin and/or derivatives thereof (e.g., cytochalasin A, cytochalasin B, cytochalasin C, cytochalasin D, cytochalasin E, cytochalasin F, cytochalasin G, cytochalasin H, cytochalasin J, cytochalasin K, cytochalasin L, cytochalasin M, cytochalasin N, cytochalasin O, cytochalasin P, cytochalasin Q, cytochalasin R, cytochalasin S, chaetoglobosin A, chaetoglobosin B, chaetoglobosin C, chaetoglobosin D, chaetoglobosin E, chaetoglobosin F, chaetoglobosin G, chaetoglobosin J, chaetoglobosin K, deoxaphomin, proxiphomin, protophomin, zygosporin D, zygosporin E, zygosporin F, zygosporin G, aspochalasin B, aspochalasin C, aspochalasin D, etc.); cytokines and/or derivatives thereof; desirudin and/or derivatives thereof; dexamethazone and/or derivatives thereof; dipyridamole and/or derivatives thereof; eminase and/or derivatives thereof; endothelin and/or derivatives thereof endothelial growth factor and/or derivatives thereof; epidermal growth factor and/or derivatives thereof; epothilone and/or derivatives thereof; estramustine and/or derivatives thereof; estrogen and/or derivatives thereof; fenoprofen and/or derivatives thereof; fluorouracil and/or derivatives thereof; flucytosine and/or derivatives thereof; forskolin and/or derivatives thereof; ganciclovir and/or derivatives thereof; glucocorticoids and/or derivatives thereof (e.g., dexamethasone, betamethasone, etc.); glycoprotein Ilb/IIIa platelet membrane receptor antibody and/or derivatives thereof; GM-CSF and/or derivatives thereof; griseofulvin and/or derivatives thereof; growth factors and/or derivatives thereof (e.g., VEGF; TGF; IGF; PDGF; FGF, etc.); growth hormone and/or derivatives thereof; heparin and/or derivatives thereof; hirudin and/or derivatives thereof; hyaluronate and/or derivatives thereof; hydrocortisone and/or derivatives thereof; ibuprofen and/or derivatives thereof; immunosuppressive agents and/or derivatives thereof (e.g., adrenocorticosteroids, cyclosporine, etc.); indomethacin and/or derivatives thereof; inhibitors of the sodium/calcium antiporter and/or derivatives thereof (e.g., amiloride, etc.); inhibitors of the IP3 receptor and/or derivatives thereof; inhibitors of the sodium/hydrogen antiporter and/or derivatives thereof (e.g., amiloride and derivatives thereof, etc.); insulin and/or derivatives thereof; interferon a-2-macroglobulin and/or derivatives thereof; ketoconazole and/or derivatives thereof; lepirudin and/or derivatives thereof; LISINOPRIL and/or derivatives thereof; LOVASTATIN and/or derivatives thereof; marevan and/or derivatives thereof; mefloquine and/or derivatives thereof; metalloproteinase inhibitors and/or derivatives thereof; methotrexate and/or derivatives thereof; metronidazole and/or derivatives thereof; miconazole and/or derivatives thereof; monoclonal antibodies and/or derivatives thereof; mutamycin and/or derivatives thereof; naproxen and/or derivatives thereof; nitric oxide and/or derivatives thereof; nitroprusside and/or derivatives thereof; nucleic acid analogues and/or derivatives thereof (e.g., peptide nucleic acids, etc.); nystatin and/or derivatives thereof; oligonucleotides and/or derivatives thereof; paclitaxel and/or derivatives thereof; penicillin and/or derivatives thereof; pentamidine isethionate and/or derivatives thereof; phenindione and/or derivatives thereof; phenylbutazone and/or derivatives thereof; phosphodiesterase inhibitors and/or derivatives thereof; plasminogen activator inhibitor- 1 and/or derivatives thereof; plasminogen activator inhibitor-2 and/or derivatives thereof; platelet factor 4 and/or derivatives thereof; platelet derived growth factor and/or derivatives thereof; plavix and/or derivatives thereof; POSTMI 75 and/or derivatives thereof; prednisone and/or derivatives thereof; prednisolone and/or derivatives thereof; probucol and/or derivatives thereof; progesterone and/or derivatives thereof; prostacyclin and/or derivatives thereof; prostaglandin inhibitors and/or derivatives thereof; protamine and/or derivatives thereof; protease and/or derivatives thereof; protein kinase inhibitors and/or derivatives thereof (e.g., staurosporin, etc.); quinine and/or derivatives thereof; radioactive agents and/or derivatives thereof (e.g., Cu-64, Ca-67, Cs-131, Ga- 68, Zr-89, Ku-97, Tc-99m, Rh-105, Pd-103, Pd-109, In-111, 1-123, 1-125, 1-131, Re-186, Re-188, Au-198, Au-199, Pb-203, At-211, Pb-212, Bi-212, H3P32O4, etc.); rapamycin and/or derivatives thereof; receptor antagonists for histamine and/or derivatives thereof; refludan and/or derivatives thereof; retinoic acids and/or derivatives thereof; revasc and/or derivatives thereof; rifamycin and/or derivatives thereof; sense or anti-sense oligonucleotides and/or derivatives thereof (e.g., DNA, RNA, plasmid DNA, plasmid RNA, etc.); seramin and/or derivatives thereof; steroids; seramin and/or derivatives thereof; serotonin and/or derivatives thereof; serotonin blockers and/or derivatives thereof; streptokinase and/or derivatives thereof; sulfasalazine and/or derivatives thereof; sulfonamides and/or derivatives thereof (e.g., sulfamethoxazole, etc.); sulphated chitin derivatives; Sulphated Polysaccharide Peptidoglycan Complex and/or derivatives thereof; TH1 and/or derivatives thereof (e.g., Interleukins-2, -12, and -15, gamma interferon, etc.); thioprotese inhibitors and/or derivatives thereof; taxol and/or derivatives thereof (e.g., taxotere, baccatin, 10- deacetyltaxol, 7-xylosyl-lO-deacetyltaxol, cephalomannine, 10-deacetyl-7-epitaxol, 7 epitaxol, 10-deacetylbaccatin III, 10-deacetylcephaolmannine, etc.); ticlid and/or derivatives thereof; ticlopidine and/or derivatives thereof; tick anti-coagulant peptide and/or derivatives thereof; thioprotese inhibitors and/or derivatives thereof; thyroid hormone and/or derivatives thereof; tissue inhibitor of metalloproteinase- 1 and/or derivatives thereof; tissue inhibitor of metalloproteinase-2 and/or derivatives thereof; tissue plasma activators; TNF and/or derivatives thereof, tocopherol and/or derivatives thereof; toxins and/or derivatives thereof; tranilast and/or derivatives thereof; transforming growth factors alpha and beta and/or derivatives thereof; trapidil and/or derivatives thereof; triazolopyrimidine and/or derivatives thereof; vapiprost and/or derivatives thereof; vinblastine and/or derivatives thereof; vincristine and/or derivatives thereof; zidovudine and/or derivatives thereof. As can be appreciated, the agent can include one or more derivatives of the above listed compounds and/or other compounds. In one non-limiting embodiment, the agent includes, but is not limited to, trapidil, trapidil derivatives, taxol, taxol derivatives (e.g., taxotere, baccatin, 10-deacetyltaxol, 7-xylosyl-lO-deacetyltaxol, cephalomannine, 10-deacetyl-7-epitaxol, 7 epitaxol, 10-deacetylbaccatin III, 10- deacetylcephaolmannine, etc.), cytochalasin, cytochalasin derivatives (e.g., cytochalasin A, cytochalasin B, cytochalasin C, cytochalasin D, cytochalasin E, cytochalasin F, cytochalasin G, cytochalasin H, cytochalasin J, cytochalasin K, cytochalasin L, cytochalasin M, cytochalasin N, cytochalasin O, cytochalasin P, cytochalasin Q, cytochalasin R, cytochalasin S, chaetoglobosin A, chaetoglobosin B, chaetoglobosin C, chaetoglobosin D, chaetoglobosin E, chaetoglobosin F, chaetoglobosin G, chaetoglobosin J, chaetoglobosin K, deoxaphomin, proxiphomin, protophomin, zygosporin D, zygosporin E, zygosporin F, zygosporin G, aspochalasin B, aspochalasin C, aspochalasin D, etc.), paclitaxel, paclitaxel derivatives, rapamycin, rapamycin derivatives, 5- phenylmethimazole, 5-phenylmethimazole derivatives, GM-CSF (granulo-cytemacrophage colony-stimulating-factor), GM-CSF derivatives, statins or HMG-CoA reductase inhibitors forming a class of hypolipidemic agents, combinations, or analogs thereof, or combinations thereof. The type and/or amount of agent included in the device and/or coated on the device can vary. When two or more agents are included in and/or coated on the device, the amount of two or more agents can be the same or different. The type and/or amount of agent included on, in and/or in conjunction with the device are generally selected to address one or more clinical events. [0047] Typically, the amount of agent included on, in and/or used in conjunction with the device is about 0.01-100ug per mm ² and/or at least about 0.00001 wt.% of device; however, other amounts can be used. In one non-limiting embodiment of the invention, the device can be partially or fully coated and/or impregnated with one or more agents to facilitate in the success of a particular medical procedure. The amount of two of more agents on, in and/or used in conjunction with the device can be the same or different. The one or more agents can be coated on and/or impregnated in the device by a variety of mechanisms such as, but not limited to, spraying (e.g., atomizing spray techniques, etc.), flame spray coating, powder deposition, dip coating, flow coating, dip-spin coating, roll coating (direct and reverse), sonication, brushing, plasma deposition, depositing by vapor deposition, MEMS technology, and rotating mold deposition. In another and/or alternative non-limiting embodiment of the invention, the type and/or amount of agent included on, in and/or in conjunction with the device is generally selected for the treatment of one or more clinical events. Typically, the amount of agent included on, in and/or used in conjunction with the device is about 0.01-100ug per mm ² (and all values and ranges wherein between); however, other amounts can be used. The amount of two of more agents on, in and/or used in conjunction with the device can be the same or different. As such, the medical device, when it includes, contains, and/or is coated with one or more agents, can include one or more agents to address one or more medical needs. In one non-limiting embodiment of the invention, the medical device can be partially or fully coated with one or more agents and/or impregnated with one or more agents to facilitate in the success of a particular medical procedure. The one or more agents can be coated on and/or impregnated in the medical device by a variety of mechanisms such as, but not limited to, spraying (e.g., atomizing spray techniques, etc.), dip coating, roll coating, sonication, brushing, plasma deposition, depositing by vapor deposition. In another and/or alternative non-limiting embodiment of the invention, the type and/or amount of agent included on, in and/or in conjunction with the medical device is generally selected for the treatment of one or more medical treatments. The amount of two or more agents on, in and/or used in conjunction with the medical device can be the same or different.

[0048] In a further and/or alternative non-limiting aspect of the present invention, the one or more agents on and/or in the medical device, when used on the medical device, can be released in a controlled manner so the area in question to be treated is provided with the desired dosage of agent over a sustained period of time. As can be appreciated, controlled release of one or more agents on the medical device is not always required and/or desirable. As such, one or more of the agents on and/or in the medical device can be uncontrollably released from the medical device during and/or after insertion of the medical device in the treatment area. It can also be appreciated that one or more agents on and/or in the medical device can be controllably released from the medical device and one or more agents on and/or in the medical device can be uncontrollably released from the medical device. It can also be appreciated that one or more agents on and/or in one region of the medical device can be controllably released from the medical device and one or more agents on and/or in the medical device can be uncontrollably released from another region on the medical device. As such, the medical device can be designed such that 1) all the agent on and/or in the medical device is controllably released, 2) some of the agent on and/or in the medical device is controllably released and some of the agent on the medical device is non-controllably released, or 3) none of the agent on and/or in the medical device is controllably released. The medical device can also be designed such that the rate of release of the one or more agents from the medical device is the same or different. The medical device can also be designed such that the rate of release of the one or more agents from one or more regions on the medical device is the same or different. Non-limiting arrangements that can be used to control the release of one or more agents from the medical device include 1) at least partially coat one or more agents with one or more polymers, 2) at least partially incorporate and/or at least partially encapsulate one or more agents into and/or with one or more polymers, and/or 3) insert one or more agents in pores, passageway, cavities, etc. in the medical device and at least partially coat or cover such pores, passageway, cavities, etc. with one or more polymers. As can be appreciated, other or additional arrangements can be used to control the release of one or more agents from the medical device. [0049] The one or more polymers used to at least partially control the release of one or more agents from the medical device can be porous or non-porous. The one or more agents can be inserted into and/or applied to one or more surface structures and/or micro-structures on the medical device, and/or be used to at least partially form one or more surface structures and/or micro-structures on the medical device. As such, the one or more agents on the medical device can be 1) coated on one or more surface regions of the medical device, 2) inserted and/or impregnated in one or more surface structures and/or micro-structures, etc. of the medical device, and/or 3) form at least a portion or be included in at least a portion of the structure of the medical device. When the one or more agents are coated on the medical device, the one or more agents can 1) be directly coated on one or more surfaces of the medical device, 2) be mixed with one or more coating polymers or other coating materials and then at least partially coated on one or more surfaces of the medical device, 3) be at least partially coated on the surface of another coating material that has been at least partially coated on the medical device, and/or 4) be at least partially encapsulated between a) a surface or region of the medical device and one or more other coating materials and/or b) two or more other coating materials.

[0050] As can be appreciated, many other coating arrangements can be additionally or alternatively used. When the one or more agents are inserted and/or impregnated in one or more internal structures, surface structures and/or micro-structures of the medical device, 1) one or more other coating materials can be applied at least partially over the one or more internal structures, surface structures and/or micro-structures of the medical device, and/or 2) one or more polymers can be combined with one or more agents. As such, the one or more agents can be 1) embedded in the structure of the medical device; 2) positioned in one or more internal structures of the medical device; 3) encapsulated between two polymer coatings; 4) encapsulated between the base structure and a polymer coating; 5) mixed in the base structure of the medical device that includes at least one polymer coating; or 6) one or more combinations of 1, 2, 3, 4 and/or 5. In addition or alternatively, the one or more coating of the one or more polymers on the medical device can include 1) one or more coatings of non-porous polymers; 2) one or more coatings of a combination of one or more porous polymers and one or more non-porous polymers; 3) one or more coating of porous polymer, or 4) one or more combinations of options 1, 2, and 3.

[0051] As can be appreciated different agents can be located in and/or between different polymer coating layers and/or on and/or the structure of the medical device. As can also be appreciated, many other and/or additional coating combinations and/or configurations can be used. The concentration of one or more agents, the type of polymer, the type and/or shape of internal structures in the medical device and/or the coating thickness of one or more agents can be used to control the release time, the release rate and/or the dosage amount of one or more agents; however, other or additional combinations can be used. As such, the agent and polymer system combination and location on the medical device can be numerous. As can also be appreciated, one or more agents can be deposited on the top surface of the medical device to provide an initial uncontrolled burst effect of the one or more agents prior to 1) the controlled release of the one or more agents through one or more layers of a polymer system that include one or more non-porous polymers and/or 2) the uncontrolled release of the one or more agents through one or more layers of a polymer system. The one or more agents and/or polymers can be coated on the medical device by a variety of mechanisms such as, but not limited to, spraying (e.g., atomizing spray techniques, etc.), dip coating, roll coating, sonication, brushing, plasma deposition, and/or depositing by vapor deposition.

[0052] The thickness of each polymer layer and/or layer of agent is generally at least about 0.01 pm and is generally less than about 150 pm (e.g., 0.01-149.9999 pm and all values and ranges therebetween). In one non-limiting embodiment, the thickness of a polymer layer and/or layer of agent is about 0.02-75pm, more particularly about 0.05-50 pm, and even more particularly about 1-30 pm.

[0053] When the medical device includes and/or is coated with one or more agents such that at least one of the agents is at least partially controllably released from the medical device, the need or use of body -wide therapy for extended periods of time can be reduced or eliminated. In the past, the use of body -wide therapy was used by the patient long after the patient left the hospital or other type of medical facility. This body-wide therapy could last days, weeks, months or sometimes over a year after surgery. The medical device of the present invention can be applied or inserted into a treatment area and 1) merely requires reduced use and/or extended use of body wide therapy after application or insertion of the medical device, or 2) does not require use and/or extended use of body -wide therapy after application or insertion of the medical device. As can be appreciated, use and/or extended use of body -wide therapy can be used after application or insertion of the medical device at the treatment area. In one non-limiting example, no body-wide therapy is needed after the insertion of the medical device into a patient. In another and/or alternative non-limiting example, short-term use of body -wide therapy is needed or used after the insertion of the medical device into a patient. Such short- term use can be terminated after the release of the patient from the hospital or other type of medical facility, or one to two days or weeks after the release of the patient from the hospital or other type of medical facility; however, it will be appreciated that other time periods of body-wide therapy can be used. As a result of the use of the medical device of the present invention, the use of body-wide therapy after a medical procedure involving the insertion of a medical device into a treatment area can be significantly reduced or eliminated.

[0054] In another and/or alternative non-limiting aspect of the present invention, controlled release of one or more agents from the medical device, when controlled release is desired, can be accomplished by using one or more non-porous polymer layers; however, other and/or additional mechanisms can be used to controllably release the one or more agents. The one or more agents are at least partially controllably released by molecular diffusion through the one or more non- porous polymer layers. When one or more non-porous polymer layers are used, the one or more polymer layers are typically biocompatible polymers; however, this is not required. The one or more non-porous polymers can be applied to the medical device without the use of chemicals, solvents, and/or catalysts; however, this is not required. In one non-limiting example, the non- porous polymer can be at least partially applied by, but not limited to, vapor deposition and/or plasma deposition. The non-porous polymer can be selected so as to polymerize and cure merely upon condensation from the vapor phase; however, this is not required. The application of the one or more non-porous polymer layers can be accomplished without increasing the temperature above room temperature; however, this is not required. The non-porous polymer system can be mixed with one or more agents prior to being coated on the medical device and/or be coated on a medical device that previously included one or more agents; however, this is not required. The use of one or more non-porous polymer layers allow for accurate controlled release of the agent from the medical device. The controlled release of one or more agents through the non-porous polymer is at least partially controlled on a molecular level utilizing the motility of diffusion of the agent through the non-porous polymer. In one non-limiting example, the one or more non- porous polymer layers can include, but are not limited to, polyamide, parylene (e.g., parylene C, parylene N) and/or a parylene derivative.

[0055] In still another and/or alternative non-limiting aspect of the present invention, controlled release of one or more agents from the medical device, when controlled release is desired, can be accomplished by using one or more polymers that form a chemical bond with one or more agents. In one non-limiting example, at least one agent includes trapidil, trapidil derivative or a salt thereof that is covalently bonded to at least one polymer such as, but not limited to, an ethylene-acrylic acid copolymer. The ethylene is the hydrophobic group and acrylic acid is the hydrophilic group. The mole ratio of the ethylene to the acrylic acid in the copolymer can be used to control the hydrophobicity of the copolymer. The degree of hydrophobicity of one or more polymers can also be used to control the release rate of one or more agents from the one or more polymers. The amount of agent that can be loaded with one or more polymers may be a function of the concentration of anionic groups and/or cationic groups in the one or more polymer. For agents that are anionic, the concentration of agent that can be loaded on the one or more polymers is generally a function of the concentration of cationic groups (e.g. amine groups and the like) in the one or more polymer and the fraction of these cationic groups that can ionically bind to the anionic form of the one or more agents. For agents that are cationic (e.g., trapidil, etc.), the concentration of agent that can be loaded on the one or more polymers is generally a function of the concentration of anionic groups (i.e., carboxylate groups, phosphate groups, sulfate groups, and/or other organic anionic groups) in the one or more polymers, and the fraction of these anionic groups that can ionically bind to the cationic form of the one or more agents. As such, the concentration of one or more agents that can be bound to the one or more polymers can be varied by controlling the amount of hydrophobic and hydrophilic monomer in the one or more polymers, by controlling the efficiency of salt formation between the agent, and/or the anionic/cationic groups in the one or more polymers.

[0056] In still another and/or alternative non-limiting aspect of the present invention, controlled release of one or more agents from the medical device, when controlled release is desired, can be accomplished by using one or more polymers that include one or more induced cross-links. These one or more cross-links can be used to at least partially control the rate of release of the one or more agents from the one or more polymers. The cross-linking in the one or more polymers can be instituted by a number to techniques such as, but not limited to, using catalysts, radiation, heat, and/or the like. The one or more cross-links formed in the one or more polymers can result in the one or more agents becoming partially or fully entrapped within the cross-linking, and/or form a bond with the cross-linking. As such, the partially or fully entrapped agent takes longer to release itself from the cross-linking, thereby delaying the release rate of the one or more agents from the one or more polymers. Consequently, the amount of agent, and/or the rate at which the agent is released from the medical device over time can be at least partially controlled by the amount or degree of cross-linking in the one or more polymers.

[0057] In still a further and / or alternative aspect of the present invention, a variety of polymers can be coated on the medical device and/or be used to form at least a portion of the medical device. The one or more polymers can be used on the medical for a variety of reasons such as, but not limited to, 1) forming a portion of the medical device, 2) improving a physical property of the medical device (e.g., improve strength, improve durability, improve biocompatibility, reduce friction, etc.), 3) forming a protective coating on one or more surface structures on the medical device, 4) at least partially forming one or more surface structures on the medical device, and/or 5) at least partially controlling a release rate of one or more agents from the medical device. As can be appreciated, the one or more polymers can have other or additional uses on the medical device. The one or more polymers can be porous, non-porous, biostable, biodegradable (i.e., dissolves, degrades, is absorbed, or any combination thereof in the body), and/or biocompatible. When the medical device is coated with one or more polymers, the polymer can include 1) one or more coatings of non-porous polymers; 2) one or more coatings of a combination of one or more porous polymers and one or more non-porous polymers; 3) one or more coatings of one or more porous polymers and one or more coatings of one or more non-porous polymers; 4) one or more coating of porous polymer, or 5) one or more combinations of options 1, 2, 3 and 4. The thickness of one or more of the polymer layers can be the same or different. When one or more layers of polymer are coated onto at least a portion of the medical device, the one or more coatings can be applied by a variety of techniques such as, but not limited to, vapor deposition and/or plasma deposition, spraying, dip-coating, roll coating, sonication, atomization, brushing and/or the like; however, other or additional coating techniques can be used. The one or more polymers that can be coated on the medical device and/or used to at least partially form the medical device can be polymers that are considered to be biodegradable, bioresorbable, or bioerodable; polymers that are considered to be biostable; and/or polymers that can be made to be biodegradable and/or bioresorbable with modification. Non-limiting examples of polymers that are considered to be biodegradable, bioresorbable, or bioerodable include, but are not limited to, aliphatic polyesters; poly(glycolic acid) and/or copolymers thereof (e.g., poly(glycolide trimethylene carbonate); poly(caprolactone glycolide)); poly(lactic acid) and/or isomers thereof (e.g., poly-L(lactic acid) and/or poly-D Lactic acid) and/or copolymers thereof (e.g. DL-PLA), with and without additives (e.g. calcium phosphate glass), and/or other copolymers (e.g. poly(caprolactone lactide), poly(lactide glycolide), poly(lactic acid ethylene glycol)); poly(ethylene glycol); poly(ethylene glycol) diacrylate; poly(lactide); polyalkylene succinate; polybutylene diglycolate; polyhydroxybutyrate (PHB); polyhydroxyvalerate (PHV); polyhydroxybutyrate/polyhydroxyvalerate copolymer (PHB/PHV); poly(hydroxybutyrate-co- valerate); polyhydroxyalkaoates (PHA); polycaprolactone; poly(caprolactone-polyethylene glycol) copolymer; poly(valerolactone); polyanhydrides; poly(orthoesters) and/or blends with polyanhydrides; poly(anhydride-co-imide); polycarbonates (aliphatic); poly(hydroxyl-esters); polydioxanone; polyanhydrides; polyanhydride esters; poly cyanoacrylates; poly(alkyl 2- cyanoacrylates); poly(amino acids); poly(phosphazenes); polypropylene fumarate); polypropylene fumarate-co-ethylene glycol); poly(fumarate anhydrides); fibrinogen; fibrin; gelatin; cellulose and/or cellulose derivatives and/or cellulosic polymers (e.g., cellulose acetate, cellulose acetate butyrate, cellulose butyrate, cellulose ethers, cellulose nitrate, cellulose propionate, cellophane); chitosan and/or chitosan derivatives (e.g., chitosan NOCC, chitosan NOOC-G); alginate; polysaccharides; starch; amylase; collagen; poly carboxylic acids; poly(ethyl ester-co-carboxylate carbonate) (and/or other tyrosine derived polycarbonates); poly(iminocarbonate); poly(BPA-iminocarbonate); poly(trimethylene carbonate); poly(iminocarbonate-amide) copolymers and/or other pseudo-poly (amino acids); poly (ethylene glycol); poly(ethylene oxide); poly(ethylene oxide)/poly(butylene terephthalate) copolymer; poly(epsilon-caprolactone-dimethyltrimethylene carbonate); poly(ester amide); poly(amino acids) and conventional synthetic polymers thereof; poly(alkylene oxalates); poly(alkylcarbonate); poly(adipic anhydride); nylon copolyamides; NO-carboxymethyl chitosan NOCC); carboxymethyl cellulose; copoly(ether-esters) (e.g., PEO/PLA dextrans); polyketals; biodegradable polyethers; biodegradable polyesters; polydihydropyrans; polydepsipeptides; polyarylates (L-tyrosine-derived) and/or free acid polyarylates; polyamides (e.g., nylon 6-6, polycaprolactam); polypropylene fumarate-co-ethylene glycol) (e.g., fumarate anhydrides); hyaluronates; poly-p-dioxanone; polypeptides and proteins; polyphosphoester; polyphosphoester urethane; polysaccharides; pseudo-poly(amino acids); starch; terpolymer; (copolymers of glycolide, lactide, or dimethyltrimethylene carbonate); rayon; rayon triacetate; latex; and/pr copolymers, blends, and/or composites of above. Non-limiting examples of polymers that considered to be biostable include, but are not limited to, parylene; parylene c; parylene f; parylene n; parylene derivatives; maleic anyhydride polymers; phosphorylchobne; poly n-butyl methacrylate (PBMA); polyethylene-co-vinyl acetate (PEVA); PBMA/PEVA blend or copolymer; polytetrafluoroethene (Teflon®) and derivatives; poly-paraphenylene terephthalamide (Kevlar®); poly(ether ketone) (PEEK); poly(styrene-b-isobutylene-b-styrene) (Translute™); tetramethyldisiloxane (side chain or copolymer); polyimides polysulfides; poly(ethylene terephthalate); poly(methyl methacrylate); poly(ethylene-co-methyl methacrylate); styrene-ethylene/butylene-styrene block copolymers; ABS; SAN; acrylic polymers and/or copolymers (e.g., n-butyl-acrylate, n-butyl methacrylate, 2-ethylhexyl acrylate, lauryl-acrylate, 2- hydroxy-propyl acrylate, polyhydroxy ethyl, methacrylate/methylmethacrylate copolymers); glycosaminoglycans; alkyd resins; elastin; polyether sulfones; epoxy resin; poly(oxymethylene); polyolefins; polymers of silicone; polymers of methane; polyisobutylene; ethylene-alphaolefm copolymers; polyethylene; polyacrylonitrile; fluorosilicones; polypropylene oxide); polyvinyl aromatics (e.g. polystyrene); poly(vinyl ethers) (e.g. polyvinyl methyl ether); poly(vinyl ketones); poly(vinylidene halides) (e.g. polyvinylidene fluoride, polyvinylidene chloride); poly(vinylpyrolidone); poly(vinylpyrolidone)/vinyl acetate copolymer; polyvinylpridine prolastin or silk-elastin polymers (SELP); silicone; silicone rubber; polyurethanes (polycarbonate polyurethanes, silicone urethane polymer) (e.g., chronoflex varieties, bionate varieties); vinyl halide polymers and/or copolymers (e.g. polyvinyl chloride); polyacrylic acid; ethylene acrylic acid copolymer; ethylene vinyl acetate copolymer; polyvinyl alcohol; poly(hydroxyl alkylmethacrylate); polyvinyl esters (e.g. polyvinyl acetate); and/or copolymers, blends, and/or composites of above. Non-limiting examples of polymers that can be made to be biodegradable and/or bioresorbable with modification include, but are not limited to, hyaluronic acid (hyanluron); polycarbonates; polyorthocarbonates; copolymers of vinyl monomers; polyacetals; biodegradable polyurethanes; polyacrylamide; polyisocyanates; polyamide; and/or copolymers, blends, and/or composites of above. As can be appreciated, other and/or additional polymers and/or derivatives of one or more of the above listed polymers can be used. The one or more polymers can be coated on the medical device by a variety of mechanisms such as, but not limited to, spraying (e.g., atomizing spray techniques, etc.), dip coating, roll coating, sonication, brushing, plasma deposition, and/or depositing by vapor deposition. The thickness of each polymer layer is generally at least about 0.01 pm and is generally less than about 150 pm (e.g., 0.01 pm to 150 pm and all values and ranges therebetween); however, other thicknesses can be used. In one non- limiting embodiment, the thickness of a polymer layer and/or layer of agent is about 0.02-75pm, more particularly about 0.05-50 pm, and even more particularly about 1-30 pm. As can be appreciated, other thicknesses can be used. In one non-limiting embodiment, the medical device includes and/or is coated with parylene, PLGA, POE, PGA, PLLA, PAA, PEG, chitosan and/or derivatives of one or more of these polymers. In another and/or alternative non-limiting embodiment, the medical device includes and/or is coated with a non-porous polymer that includes, but is not limited to, polyamide, Parylene C, Parylene N and/or a parylene derivative. In still another and/or alternative non-limiting embodiment, the medical device includes and/or is coated with poly (ethylene oxide), poly(ethylene glycol), and polypropylene oxide), polymers of silicone, methane, tetrafluoroethylene (including TEFLON™ brand polymers), tetramethyldisiloxane, and the like.

[0058] In another and/or alternative non-limiting aspect of the present invention, the medical device, when including and/or is coated with one or more agents, can include and/or can be coated with one or more agents that are the same or different in different regions of the medical device and/or have differing amounts and/or concentrations in differing regions of the medical device. For instance, the medical device can 1) be coated with and/or include one or more biologicals on at least one portion of the medical device and at least another portion of the medical device is not coated with and/or includes agent; 2) be coated with and/or include one or more biologicals on at least one portion of the medical device that is different from one or more biologicals on at least another portion of the medical device; and/or 3) be coated with and/or include one or more biologicals at a concentration on at least one portion of the medical device that is different from the concentration of one or more biologicals on at least another portion of the medical device; etc. [0059] In still yet another and/or alternative non-limiting aspect of the present invention, one or more portions of the medical device can 1) include the same or different agents, 2) include the same or different amount of one or more agents, 3) include the same or different polymer coatings, 4) include the same or different coating thicknesses of one or more polymer coatings, 5) have one or more portions of the medical device controllably release and/or uncontrollably release one or more agents, and/or 6) have one or more portions of the medical device controllably release one or more agents and one or more portions of the medical device uncontrollably release one or more agents.

[0060] In still another and/or alternative non-limiting aspect of the present invention, one or more surfaces of the medical device can be treated to achieve the desired coating properties of the one or more agents and one or more polymers coated on the medical device. Such surface treatment techniques include, but are not limited to, cleaning, buffing, smoothing, nitriding, annealing, swaging, cold working, etching (chemical etching, plasma etching, etc.), etc. When an etching process is used, various gasses can be used for such a surface treatment process such as, but not limited to, carbon dioxide, nitrogen, oxygen, Freon®, helium, hydrogen, etc. The plasma etching process can be used to clean the surface of the medical device, change the surface properties of the medical device so as to affect the adhesion properties, lubricity properties, etc. of the surface of the medical device. As can be appreciated, other or additional surface treatment processes can be used prior to the coating of one or more agents and/or polymers on the surface of the medical device. In one non-limiting manufacturing process, one or more portions of the medical device are cleaned and/or plasma etched; however, this is not required. Plasma etching can be used to clean the surface of the medical device, and/or to form one or more non-smooth surfaces on the medical device to facilitate in the adhesion of one or more coatings of agents and/or one or more coatings of polymer on the medical device. The gas for the plasma etching can include carbon dioxide and/or other gasses. Once one or more surface regions of the medical device have been treated, one or more coatings of polymer and/or agent can be applied to one or more regions of the medical device. For instance, 1) one or more layers of porous or non-porous polymer can be coated on an outer and/or inner surface of the medical device, 2) one or more layers of agent can be coated on an outer and/or inner surface of the medical device, or 3) one or more layers of porous or non-porous polymer that includes one or more agents can be coated on an outer and/or inner surface of the medical device. The one or more layers of agent can be applied to the medical device by a variety of techniques (e.g., dipping, rolling, brushing, spraying, particle atomization, etc.). One non-limiting coating technique is by an ultrasonic mist coating process wherein ultrasonic waves are used to break up the droplet of agent and form a mist of very fine droplets. These fine droplets have an average droplet diameter of about 0.1-3 microns. The fine droplet mist facilitates in the formation of a uniform coating thickness and can increase the coverage area on the medical device.

[0061] In yet another and/or alternative non-limiting aspect of the invention, the medical device can include a marker material that facilitates enabling the medical device to be properly positioned in a body passageway. The marker material is typically designed to be visible to electromagnetic waves (e.g., x-rays, microwaves, visible light, infrared waves, ultraviolet waves, etc.); sound waves (e.g., ultrasound waves, etc.); magnetic waves (e.g., MRI, etc.); and/or other types of electromagnetic waves (e.g., microwaves, visible light, infrared waves, ultraviolet waves, etc.). In one non-limiting embodiment, the marker material is visible to x-rays (i.e., radiopaque). The marker material can form all or a portion of the medical device and/or be coated on one or more portions (flaring portion and/or body portion, at ends of medical device, at or near transition of body portion and flaring section, etc.) of the medical device. The location of the marker material can be on one or multiple locations on the medical device. The size of the one or more regions that include the marker material can be the same or different. The marker material can be spaced at defined distances from one another so as to form ruler-like markings on the medical device to facilitate in the positioning of the medical device in a body passageway. The marker material can be a rigid or flexible material. The marker material can be a biostable or biodegradable material. When the marker material is a rigid material, the marker material is typically formed of a metal material (e.g., metal band, metal plating, etc.); however, other or additional materials can be used. The metal, which at least partially forms the medical device, can function as a marker material; however, this is not required. When the marker material is a flexible material, the marker material typically is formed of one or more polymers that are marker materials in-of-themselves and/or include one or more metal powders and/or metal compounds. In one non-limiting embodiment, the flexible marker material includes one or more metal powders in combinations with parylene, PLGA, POE, PGA, PLLA, PAA, PEG, chitosan and/or derivatives of one or more of these polymers. In another and/or alternative non-limiting embodiment, the flexible marker material includes one or more metals and/or metal powders of aluminum, barium, bismuth, cobalt, copper, chromium, gold, iron, stainless steel, titanium, vanadium, nickel, zirconium, niobium, lead, molybdenum, platinum, yttrium, calcium, rare earth metals, rhenium, zinc, silver, depleted radioactive elements, tantalum and/or tungsten; and/or compounds thereof. The marker material can be coated with a polymer protective material; however, this is not required. When the marker material is coated with a polymer protective material, the polymer coating can be used to 1) at least partially insulate the marker material from body fluids, 2) facilitate in retaining the marker material on the medical device, 3) at least partially shield the marker material from damage during a medical procedure and/or 4) provide a desired surface profile on the medical device. As can be appreciated, the polymer coating can have other or additional uses. The polymer protective coating can be a biostable polymer or a biodegradable polymer (e.g., degrades and/or is absorbed). The coating thickness of the protective coating polymer material, when used, is typically less than about 300 microns (e.g., 0.001-299.999 microns and all values and ranges therebetween); however, other thickness can be used. In one non-limiting embodiment, the protective coating materials include parylene, PLGA, POE, PGA, PLLA, PAA, PEG, chitosan and/or derivatives of one or more of these polymers.

[0062] In a further and/or alternative non-limiting aspect of the present invention, the medical device or one or more regions of the medical device can be constructed by use of one or more microelectromechanical manufacturing (MEMS) techniques (e.g., micro-machining, laser micro machining, laser micro-machining, micro-molding, etc.); however, other or additional manufacturing techniques can be used.

[0063] The medical device can include one or more surface structures (e.g., pore, channel, pit, rib, slot, notch, bump, teeth, needle, well, hole, groove, etc.). These structures can be at least partially formed by MEMS (e.g., micro-machining, etc.) technology and/or other types of technology.

[0064] The medical device can include one or more micro-structures (e.g., micro-needle, micro-pore, micro-cylinder, micro-cone, micro-pyramid, micro-tube, micro-parallelopiped, micro-prism, micro-hemisphere, teeth, rib, ridge, ratchet, hinge, zipper, zip-tie like structure, etc.) on the surface of the medical device. As defined herein, a “micro-structure” is a structure that has at least one dimension (e.g., average width, average diameter, average height, average length, average depth, etc.) that is no more than about 2mm, and typically no more than about 1 mm. As can be appreciated, when the medical device includes one or more surface structures, 1) all the surface structures can be micro-structures, 2) all the surface structures can be non-micro structures, or 3) a portion of the surface structures can be micro-structures and a portion can be non-micro-structures. Non-limiting examples of structures that can be formed on the medical devices are illustrated in United States Patent Publication Nos. 2004/0093076 and 2004/0093077, which are incorporated herein by reference. Typically, the micro-structures, when formed, extend from or into the outer surface no more than about 400 microns (0.01-400 microns and all values and ranges therebetween), and more typically less than about 300 microns, and more typically about 15-250 microns; however, other sizes can be used. The micro-structures can be clustered together or disbursed throughout the surface of the medical device. Similar shaped and/or sized micro-structures and/or surface structures can be used, or different shaped and/or sized micro structures can be used. When one or more surface structures and/or micro-structures are designed to extend from the surface of the medical device, the one or more surface structures and/or micro structures can be formed in the extended position and/or be designed so as to extend from the medical device during and/or after deployment of the medical device in a treatment area. The micro-structures and/or surface structures can be designed to contain and/or be fluidly connected to a passageway, cavity, etc.; however, this is not required. The one or more surface structures and/or micro-structures can be used to engage and/or penetrate surrounding tissue or organs once the medical device has be position on and/or in a patient; however, this is not required. The one or more surface structures and/or micro-structures can be used to facilitate in forming maintaining a shape of a medical device (i.e., see devices in United States Patent Publication Nos. 2004/0093076 and 2004/0093077). The one or more surface structures and/or micro-structures can be at least partially formed by MEMS (e.g., micro-machining, laser micro-machining, micro molding, etc.) technology; however, this is not required. In one non-limiting embodiment, the one or more surface structures and/or micro-structures can be at least partially formed of an agent and/or be formed of a polymer. One or more of the surface structures and/or micro-structures can include one or more internal passageways that can include one or more materials (e.g., agent, polymer, etc.); however, this is not required. The one or more surface structures and/or micro structures can be formed by a variety of processes (e.g., machining, chemical modifications, chemical reactions, MEMS (e.g., micro-machining, etc.), etching, laser cutting, etc.). The one or more coatings and/or one or more surface structures and/or micro-structures of the medical device can be used for a variety of purposes such as, but not limited to, 1) increasing the bonding and/or adhesion of one or more agents, adhesives, marker materials and/or polymers to the medical device, 2) changing the appearance or surface characteristics of the medical device, and/or 3) controlling the release rate of one or more agents. The one or more micro-structures and/or surface structures can be biostable, biodegradable, etc. One or more regions of the medical device that are at least partially formed by MEMS techniques can be biostable, biodegradable, etc. The medical device or one or more regions of the medical device can be at least partially covered and/or filled with a protective material so to at least partially protect one or more regions of the medical device, and/or one or more micro-structures and/or surface structures on the medical device from damage.

[0065] One or more regions of the medical device, and/or one or more micro-structures and/or surface structures on the medical device can be damaged when the medical device is 1) packaged and/or stored, 2) unpackaged, 3) connected to and/or other secured and/or placed on another medical device, 4) inserted into a treatment area, and/or 5) handled by a user. As can be appreciated, the medical device can be damaged in other or additional ways. The protective material can be used to protect the medical device and one or more micro-structures and/or surface structures from such damage. The protective material can include one or more polymers previously identified above. The protective material can be 1) biostable and/or biodegradable and/or 2) porous and/or non-porous.

[0066] In one non-limiting design, the polymer is at least partially biodegradable so as to at least partially expose one or more micro-structures and/or surface structures to the environment after the medical device has been at least partially inserted into a treatment area. In another and/or additional non-limiting design, the protective material includes, but is not limited to, sugar (e.g., glucose, fructose, sucrose, etc.), carbohydrate compound, salt (e.g., NaCl, etc.), parylene, PLGA, POE, PGA, PLLA, PAA, PEG, chitosan and/or derivatives of one or more of these materials; however, other and/or additional materials can be used. In still another and/or additional non- limiting design, the thickness of the protective material is generally less than about 300 microns (e.g., 0.01 microns to 299.9999 microns and all values and ranges therebetween), and typically less than about 150 microns; however, other thicknesses can be used. The protective material can be coated by one or more mechanisms previously described herein.

[0067] In still yet another and/or alternative non-limiting aspect of the present invention, the medical device can include and/or be used with a physical hindrance. The physical hindrance can include, but is not limited to, an adhesive, sheath, magnet, tape, wire, string, etc. The physical hindrance can be used to 1) physically retain one or more regions of the medical device in a particular form or profile, 2) physically retain the medical device on a particular deployment device, 3) protect one or more surface structures and/or micro-structures on the medical device, and/or 4) form a barrier between one or more surface regions, surface structures and/or micro structures on the medical device and the fluids in a body passageway. As can be appreciated, the physical hindrance can have other and/or additional functions. The physical hindrance is typically a biodegradable material; however, a biostable material can be used. The physical hindrance can be designed to withstand sterilization of the medical device; however, this is not required. The physical hindrance can be applied to, included in and/or be used in conjunction with one or more medical devices. Additionally or alternatively, the physical hindrance can be designed to be used with and/or conjunction with a medical device for a limited period of time and then 1) disengage from the medical device after the medical device has been partially or fully deployed and/or 2) dissolve and/or degrade during and/or after the medical device has been partially or fully deployed; however, this is not required. Additionally or alternatively, the physical hindrance can be designed and be formulated to be temporarily used with a medical device to facilitate in the deployment of the medical device; however, this is not required. In one non-limiting use of the physical hindrance, the physical hindrance is designed or formulated to at least partially secure a medical device to another device that is used to at least partially transport the medical device to a location for treatment. In another and/or alternative non-limiting use of the physical hindrance, the physical hindrance is designed or formulated to at least partially maintain the medical device in a particular shape or form until the medical device is at least partially positioned in a treatment location. In still another and/or alternative non-limiting use of the physical hindrance, the physical hindrance is designed or formulated to at least partially maintain and/or secure one type of medical device to another type of medical instrument or device until the medical device is at least partially positioned in a treatment location. The physical hindrance can also or alternatively be designed and formulated to be used with a medical device to facilitate in the use of the medical device. In one non-limiting use of the physical hindrance, when in the form of an adhesive, can be formulated to at least partially secure a medical device to a treatment area so as to facilitate in maintaining the medical device at the treatment area. For instance, the physical hindrance can be used in such use to facilitate in maintaining a medical device on or at a treatment area until the medical device is properly secured to the treatment area by sutures, stitches, screws, nails, rod, etc.; however, this is not required. Additionally or alternatively, the physical hindrance can be used to facilitate in maintaining a medical device on or at a treatment area until the medical device has partially or fully accomplished its objective. The physical hindrance is typically a biocompatible material so as to not cause unanticipated adverse effects when properly used. The physical hindrance can be biostable or biodegradable (e.g., degrades and/or is absorbed, etc.). When the physical hindrance includes or has one or more adhesives, the one or more adhesives can be applied to the medical device by, but is not limited to, spraying (e.g., atomizing spray techniques, etc.), dip coating, roll coating, sonication, brushing, plasma deposition, and/or depositing by vapor deposition, brushing, painting, etc.) on the medical device. The physical hindrance can also or alternatively form at least a part of the medical device. One or more regions and/or surfaces of a medical device can also or alternatively include the physical hindrance. The physical hindrance can include one or more biological agents and/or other materials (e.g., marker material, polymer, etc.); however, this is not required. When the physical hindrance is or includes an adhesive, the adhesive can be formulated to controllably release one or more biological agents in the adhesive and/or coated on and/or contained within the medical device; however, this is not required. The adhesive can also or alternatively control the release of one or more biological agents located on and/or contained in the medical device by forming a penetrable or non-penetrable barrier to such biological agents; however, this is not required. The adhesive can include and/or be mixed with one or more polymers; however, this is not required. The one or more polymers can be used to 1) control the time of adhesion provided by the adhesive, 2) control the rate of degradation of the adhesive, and/or 3) control the rate of release of one or more biological agents from the adhesive and/or diffusing or penetrating through the adhesive layer; however, this is not required. When the physical hindrance includes a sheath, the sheath can be designed to partially or fully encircle the medical device. The sheath can be designed to be physically removed from the medical device after the medical device is deployed to a treatment area; however, this is not required. The sheath can be formed of a biodegradable material that at least partially degrades over time to at least partially expose one or more surface regions, micro-structures and/or surface structures of the medical device; however, this is not required. The sheath can include and/or be at least partially coated with one or more biological agents. The sheath includes one or more polymers; however, this is not required. The one or more polymers can be used for a variety of reasons such as, but not limited to, 1) forming a portion of the sheath, 2) improving a physical property of the sheath (e.g., improve strength, improve durability, improve biocompatibility, reduce friction, etc.), and/or 3) at least partially controlling a release rate of one or more biological agents from the sheath. As can be appreciated, the one or more polymers can have other or additional uses on the sheath. [0068] In another and/or alternative non-limiting aspect of the invention, the medical device can include a bistable construction. In such a design, the medical device has two or more stable configurations, including a first stable configuration with a first cross-sectional shape and a second stable configuration with a second cross-sectional shape. All or a portion of the medical device can include the bistable construction. The bistable construction can result in a generally uniform change in shape of the medical device, or one portion of the medical device can change into one or more configurations and one or more other portions of the medical device can change into one or more other configurations.

[0069] In still another and/or alternative aspect of the invention, the medical device can be an expandable device that can be expanded by use of some other device (e.g., balloon, etc.) and/or is self-expanding. The expandable medical device can be fabricated from a material that has no or substantially no shape-memory characteristics or can be partially fabricated from a material having shape-memory characteristics. Typically, when one or more shape-memory materials are used, the shape-memory material composition is selected such that the shape-memory material remains in an unexpanded configuration at a cold temperature (e.g., below body temperature); however, this is not required. When the shape-memory material is heated (e.g., to body temperature) the expandable body section can be designed to expand to at least partially seal and secure the medical device in a body passageway or other region; however, this is not required. [0070] In still another and/or alternative non-limiting aspect of the invention, the medical device can be used in conjunction with one or more other biological agents that are not on the medical device. For instance, the success of the medical device can be improved by infusing, injecting or consuming orally one or more biological agents. Such biological agents can be the same and/or different from the one or more biological agents on and/or in the medical device. Use of one or more biological agents is commonly used in the systemic treatment (such as body-wide therapy) of a patient after a medical procedure; such systemic treatment can be reduced or eliminated after the medical device made with the novel allow has been inserted in the treatment area. Although the medical device of the present invention can be designed to reduce or eliminate the need for long periods of body -wide therapy after the medical device has been inserted in the treatment area, the use of one or more biological agents can be used in conjunction with the medical device to enhance the success of the medical device and/or reduce or prevent the occurrence of one or more biological problems (e.g., infection, rejection of the medical device, etc.). For instance, solid dosage forms of biological agents for oral administration, and/or for other types of administration (e.g., suppositories, etc.) can be used. Such solid forms can include, but are not limited to, capsules, tablets, effervescent tablets, chewable tablets, pills, powders, sachets, granules and gels. The solid form of the capsules, tablets, effervescent tablets, chewable tablets, pills, etc. can have a variety of shapes such as, but not limited to, spherical, cubical, cylindrical, pyramidal, and the like. In such solid dosage form, one or more biological agents can be admixed with at least one filler material such as, but not limited to, sucrose, lactose or starch; however, this is not required. Such dosage forms can include additional substances such as, but not limited to, inert diluents (e.g., lubricating agents, etc.). When capsules, tablets, effervescent tablets or pills are used, the dosage form can also include buffering agents; however, this is not required. Soft gelatin capsules can be prepared to contain a mixture of the one or more biological agents in combination with vegetable oil or other types of oil; however, this is not required. Hard gelatin capsules can contain granules of the one or more biological agents in combination with a solid carrier such as, but not limited to, lactose, potato starch, com starch, cellulose derivatives of gelatin, etc.; however, this is not required. Tablets and pills can be prepared with enteric coatings for additional time release characteristics; however, this is not required. Liquid dosage forms of the one or more biological agents for oral administration can include pharmaceutically acceptable emulsions, solutions, suspensions, syrups, elixirs, etc.; however, this is not required. In one non limiting embodiment, when at least a portion of one or more biological agents is inserted into a treatment area (e.g., gel form, paste form, etc.) and/or provided orally (e.g., pill, capsule, etc.) and/or anally (suppository, etc.), one or more of the biological agents can be controllably released; however, this is not required. In one non-limiting example, one or more biological agents can be given to a patient in solid dosage form and one or more of such biological agents can be controllably released from such solid dosage forms. In another and/or alternative non-limiting example, trapidil, trapidil derivatives, taxol, taxol derivatives, cytochalasin, cytochalasin derivatives, pacbtaxel, pacbtaxel derivatives, rapamycin, rapamycin derivatives, 5- phenylmethimazole, 5-phenylmethimazole derivatives, GM-CSF, GM-CSF derivatives, or combinations thereof are given to a patient prior to, during and/or after the insertion of the medical device in a treatment area. As can be appreciated, other or additional biological agents can be used.

[0071] Certain types of biological agents may be desirable to be present in a treated area for an extended period of time in order to utilize the full or nearly full clinical potential of the biological agent. For instance, trapidil and/or trapidil derivatives is a compound that has many clinical attributes including, but not limited to, anti-platelet effects, inhibition of smooth muscle cells and monocytes, fibroblast proliferation and increased MAPK-1 which in turn deactivates kinase, a vasodilator, etc. These attributes can be effective in improving the success of a medical device that has been inserted at a treatment area. In some situations, these positive effects of trapidil and/or trapidil derivatives need to be prolonged in a treatment area in order to achieve complete clinical competency. Trapidil and/or trapidil derivatives have a half-life in vivo of about 2-4 hours with hepatic clearance of 48 hours. In order to utilize the full clinical potential of trapidil and/or trapidil derivatives, trapidil and/or trapidil derivatives should be metabolized over an extended period of time without interruption; however, this is not required. By inserting trapidil and/or trapidil derivatives in a solid dosage form, the trapidil and/or trapidil derivatives could be released in a patient over extended periods of time in a controlled manner to achieve complete or nearly complete clinical competency of the trapidil and/or trapidil derivatives.

[0072] In another and/or alternative non-limiting example, one or more biological agents are at least partially encapsulated in one or more polymers. The one or more polymers can be biodegradable, non-biodegradable, porous, and/or non-porous. When the one or more polymers are biodegradable, the rate of degradation of the one or more biodegradable polymers can be used to at least partially control the rate at which one or more biological agents are released into a body passageway and/or other parts of the body over time. The one or more biological agents can be at least partially encapsulated with different polymer coating thickness, different numbers of coating layers, and/or with different polymers to alter the rate at which one or more biological agents are released in a body passageway and/or other parts of the body over time. The rate of degradation of the polymer is principally a function of the 1) water permeability and solubility of the polymer, 2) chemical composition of the polymer and/or biological agent, 3) mechanism of hydrolysis of the polymer, 4) biological agent encapsulated in the polymer, 5) size, shape and surface volume of the polymer, 6) porosity of the polymer, 7) molecular weight of the polymer, 8) degree of cross-linking in the polymer, 9) degree of chemical bonding between the polymer and biological agent, and/or 10) structure of the polymer and/or biological agent. As can be appreciated, other factors may also affect the rate of degradation of the polymer. When the one or more polymers are biostable, the rate at when the one or more biological agents are released from the biostable polymer is a function of the 1) porosity of the polymer, 2) molecular diffusion rate of the biological agent through the polymer, 3) degree of cross-linking in the polymer, 4) degree of chemical bonding between the polymer and biological agent, 5) chemical composition of the polymer and/or biological agent, 6) biological agent encapsulated in the polymer, 7) size, shape and surface volume of the polymer, and/or 8) structure of the polymer and/or biological agent. As can be appreciated, other factors may also affect the rate of release of the one or more biological agents from the biostable polymer. Many different polymers can be used such as, but not limited to, aliphatic polyester compounds (e.g., PLA (i.e., poly (D, L-lactic acid), poly (L- lactic acid)), PLGA (i.e. poly (lactide-co-glycoside), etc.), POE, PEG, PLLA, parylene, chitosan and/or derivatives thereof. As can be appreciated, the at least partially encapsulated biological agent can be introduced into a patient by means other than by oral introduction, such as, but not limited to, injection, topical applications, intravenously, eye drops, nasal spray, surgical insertion, suppositories, intrarticularly, intraocularly, intranasally, intradermally, sublingually, intravesically, intrathecally, intraperitoneally, intracranially, intramuscularly, subcutaneously, directly at a particular site, and the like.

[0073] In still yet another and / or alternative non-limiting aspect of the present invention, there is provided a near net process for a metal alloy or medical device. One non-limiting issue with pressed powder used to form a metal alloy or medical device is the lack of cold work in the material. In general, one can press a metal powder into a green part, and then sinter the green part to increase the mechanical integrity of the resulting part. However, there has been no way to impart cold work into the sintered material to increase the mechanical strength of a powder pressed part. In one non-limiting embodiment of the invention, there is provided a method of powder pressing materials and increasing the strength post sintering by imparting additional cold work. In one non-limiting embodiment, the green part is pressed and then sintered. Thereafter, the sintered part is again pressed to increase its mechanical strength by imparting cold work into the pressed and sintered part. Generally, the temperature during the pressing process after the sintering process is 20-100°C (and all values and ranges therebetween), typically 20-80°C, and more typically 20-40°C. As defined herein, cold working is occurs at a temperature of no more than 150°C (e.g., 10-150°C and all values and ranges therebetween). The change in the shape of the repressed post-sintered part needs to be determined so the final part (pressed, sintered and re pressed) meets the dimensional requirements of the final formed part. For a Mo47.5Re alloy, MoRe alloy, ReW alloy, molybdenum alloy, tungsten alloy, rhenium alloy, other type of refractory alloy, or TWIP alloy formed of a high titanium content, a prepress pressure of 1-300 tsi (1 ton per square inch) (and all values and ranges therebetween) can be used followed by a sintering process of at least 1600°C (e.g., 1600-2600°C and all values and ranges therebetween) and a post sintering press at a pressure of 1-300 tsi (and all values and ranges therebetween) at a temperature of at least 20°C (e.g., 20-100°C and all values and ranges therebetween; 20-40°C, etc.). There is also provided a process of increasing the mechanical strength of a pressed metal part by repressing the post-sintered part to add additional cold work into the material, thereby increasing its mechanical strength. There is also provided a process of powder pressing to a near net or final part using metal powder. In one non-limiting embodiment, the metal powder used to form the near net or final part includes a minimum of 40% rhenium by weight and at least 30% molybdenum, and remainder can optionally include one or more elements of tungsten, tantalum, zirconium, iridium, titanium, bismuth, and yttrium. In another non-limiting embodiment, the metal powder used to form the near net or final part includes 20-80 wt.% Re (and all values and ranges therebetween), 20-80 wt.% Mo (and all values and ranges therebetween), and optionally one or more elements of tungsten, tantalum, zirconium, iridium, titanium, bismuth, and yttrium. In another non-limiting embodiment, the metal powder used to form the near net or final part includes W (20-60 wt.% and all values and ranges therebetween), Re (20-80 wt.% and all values and ranges therebetween) and one or more other elements 0-5 wt.% (and all values and ranges therebetween). In another non-limiting embodiment, the metal powder used to form the near net or final part includes W (20-80 wt.% and all values and ranges therebetween), Re (20-80 wt.% and all values and ranges therebetween), Mo (0-15 wt.% and all values and ranges therebetween), and one or more other elements 0-5 wt.% (and all values and ranges therebetween). In another non-limiting embodiment, the metal powder used to form the near net or final part includes W (20-80 wt.% and all values and ranges therebetween), Cu (1-30 wt.% and all values and ranges therebetween), and one or more other elements 0-5 wt.% (and all values and ranges therebetween). In another non-limiting embodiment, the metal powder used to form the near net or final part includes a Ti alloy or a Co alloy. The ductility of the metal alloy measured as % reduction in area can increase and yield and ultimate tensile strength can increase.

[0074] In still yet another and / or alternative non-limiting aspect of the present invention, there is provided a press of near net or finished part composite. The process of pressing metals into near net of finished parts is well established; however, pressing a composite structure formed of metal powder and polymer for purposes of making complex part geometries and foam like structures is new. Similarly using a pressing process to impart particular biologic substances into the metal matrix is also new. In one non-limiting embodiment, there is provided a process of creating a metal part with pre-defined voids to create a trabecular or foam structure composed of mixing a metal and polymer powder, and then pressing the powder into a finished part or semi finished green part, and then sintering the part under which conditions the polymer leaves the metal behind through a process of thermal degradation of the polymer. The resulting part has a porosity associated with the size of the polymer particles as well as the homogeneity of the mixture upon pressing prior to sintering. In another non-limiting embodiment, there is provided a process by which a residual of the polymer is left behind after thermal degradation, on the metal substrate, and the polymer residual has some desired biological affect (e.g., masking the metal from the body by encapsulation, promotion of cellular attachment and growth). The polymer and metal powders can be of varying sizes to create a multiplied of voids some large creating a pathway for cellular growth and other small creating a ruff surface to promote cellular attachment.

[0075] As can be appreciated, the polymer can be uniformly or non-uniformly dispersed with the metal powder. For example, if the final formed part is to have a uniform density and pore structure, the polymer material is uniformly dispersed with the metal powder prior to consolidating and pressing the polymer and metal powders together and then subsequently sintering together the metal powder to form the metal part or medical device. Alternatively, if the formed metal part or medical device is to have one or more channels, passageways and/or voids on the outer surface and/or within the formed part or medical device, at least a portion of the polymer is not uniformly distributed with the metal powder, but instead is concentrated or forms all of the region that is to be the one or more channels, passageways and/or voids on the outer surface and/or within the formed part or medical device such that when the polymer and metal powder is sintered, some or all of the polymer is degraded and removed from the part or medical device thereby forming such one or more channels, passageways and/or voids on the outer surface and/or within the formed part or medical device. As such, the use of polymer in combination with metal powder and subsequent pressing and sintering can be used to form novel and customized shapes for medical device or the near net form of the medical device. Generally, the polymer constitutes about 0.1- 70 vol.% (and all values and ranges therebetween) of the consolidated and pressed material prior to the sintering step, typically the polymer constitutes about 1-60 vol.% of the consolidated and pressed material prior to the sintering step, more typically the polymer constitutes about 2-50 vol.% of the consolidated and pressed material prior to the sintering step, and even more typically the polymer constitutes about 2-45 vol.% of the consolidated and pressed material prior to the sintering step. As such, if the polymer constitutes about 5 vol.% of the consolidated and pressed material prior to the sintering step, if after the sintering step at least 99% of the polymer is degraded and removed from the part or medical device, then the part could include up to about 5 vol.% cavities and/or passageways in the part or medical device.

[0076] The type of polymer and the type of metal powder is non-limiting. The polymer and metal powders can be of varying sizes to create multiple voids/passageways/channels which can be used to create a pathway for cellular growth, create a ruff surface to promote cellular attachment, have a biological agent inserted into one or more of the voids/passageways/channels, have biological material inserted into one or more of the voids/passageways/channels, etc. In one non-limiting embodiment, the average particle size of the polymer is greater than the average particle size of the metal powder.

[0077] In another non-limiting aspect of the present invention, after the sintering process, at least 98 vol.% of the polymer is thermally degraded and/or removed from the sintered material, typically at least 99 vol.% of the polymer is thermally degraded and/or removed from the sintered material, more typically at least 99.5 vol.% of the polymer is thermally degraded and/or removed from the sintered material, still even more typically at least 99.9 vol.% of the polymer is thermally degraded and/or removed from the sintered material, and even still more typically at least 99.95 vol.% of the polymer is thermally degraded and/or removed from the sintered material. The resulting part or medical device has a porosity associated with the size of the polymer particles as well as the homogeneity of the mixture upon pressing prior to sintering.

[0078] In another non-limiting aspect of the present invention, after the sintering process, some of the polymer remains in the sintered part or the medical device. The remaining polymer in the sintered part or the medical device can optionally have some desired biological affect (e.g., masking the metal from the body by encapsulation, promotion of cellular attachment and growth). The remaining polymer can optionally include one or more biological agents that remain active after the sintering process. In one non-limiting embodiment, after the sintering process, about 5- 97.5 vol.% (and all values and ranges therebetween) of the polymer is thermally degraded and/or removed from the sintered material, typically about 10-95 vol.% of the polymer is thermally degraded and removed from the sintered material, and more typically about 10-80 vol.% of the polymer is thermally degraded and removed from the sintered material.

[0079] In still yet another and/or alternative non-limiting aspect of the present invention, there is provided medical devices made from TWIP alloys. Certain alloys exhibit a property know as Twinning Induced Plasticity (TWIP) which creates high strength and high ductility after severe plastic deformation. This property is advantageous for medical devices wherein it is desired to increased strength and greater ductility — properties which are usually at odds with each other. While reducing traditional alloys to obtain smaller profile devices, the strength is increased somewhat, but the ductility is severely reducing thereby leading to a reduced fatigue life. The use of TWIP alloys for medical devices having reduced profile and increased ductility provides a medical device with both enhanced strength and increased fatigue resistant while providing smaller profile implants.

[0080] In a further and/or alternative non-limiting aspect of the present invention, the novel alloy used to at least partially form the medical device is initially formed into a blank, a rod, a tube, etc. and then finished into final form by one or more finishing processes. The novel metal alloy blank, rod, tube, etc. can be formed by various techniques such as, but not limited to, 1) melting the novel metal alloy and/or metals that form the novel metal alloy (e.g., vacuum arc melting, etc.) and then extruding and/or casting the novel metal alloy into a blank, rod, tube, etc., 2) melting the novel metal alloy and/or metals that form the novel metal alloy, forming a metal strip and then rolling and welding the strip into a blank, rod, tube, etc., or 3) consolidating metal power of the novel metal alloy and/or metal powder of metals that form the novel metal alloy into a blank, rod, tube, etc. When the novel metal alloy is formed into a blank, the shape and size of the blank is non-limiting. When the novel metal alloy is formed into a rod or tube, the rod or tube generally has a length of about 48 inches or less (e.g., 0.1-48 inches and all values and ranges therebetween); however, longer lengths can be formed. In one non-limiting arrangement, the length of the rod or tube is about 8-20 inches. The average outer diameter of the rod or tube is generally less than about 2 inches (i.e., less than about 3.14 sq. in. cross-sectional area), more typically less than about 1 inch outer diameter, and even more typically no more than about 0.5 inch outer diameter; however, larger rod or tube diameter sizes can be formed. In one non-limiting configuration for a tube, the tube has an inner diameter of about 0.31 inch plus or minus about 0.002 inch and an outer diameter of about 0.5 inch plus or minus about 0.002 inch. The wall thickness of the tube is about 0.095 inch plus or minus about 0.002 inch. As can be appreciated, this is just one example of many different sized tubes that can be formed. In one non-limiting process, the near net medical device, blank, rod, tube, etc. can be formed from one or more ingots of metal or novel metal alloy. In one non-limiting process, an arc melting process (e.g., vacuum arc melting process, etc.) can be used to form the near net medical device, blank, rod, tube, etc. In another non-limiting process, rhenium powder and tungsten powder and optionally molybdenum powder can be placed in a crucible (e.g., silica crucible, etc.) and heated under a controlled atmosphere (e.g., vacuum environment, carbon monoxide environment, hydrogen and argon environment, helium, argon, etc.) by an induction melting furnace to form the near net medical device, blank, rod, tube, etc. As can be appreciated, other metal particles can be used to form other novel metal alloys (e.g., Mo alloys, Re alloys, MoReCr alloys, FeCrMoCB alloys, WCu alloys, WRe alloys, Ti alloys, Cr alloys, etc.) by various process such as melting, sintering, particle compression plus heat, etc. It can be appreciated that other or additional processes can be used to form the metal alloy. When a tube of novel metal alloy is to be formed, a close-fitting rod can be used during the extrusion process to form the tube; however, this is not required. In another and/or additional non-limiting process, the tube of the novel metal alloy can be formed from a strip or sheet of novel metal alloy. The strip or sheet of novel metal alloy can be formed into a tube by rolling the edges of the sheet or strip and then welding together the edges of the sheet or strip. The welding of the edges of the sheet or strip can be accomplished in several ways such as, but not limited to, a) holding the edges together and then e-beam welding the edges together in a vacuum, b) positioning a thin strip of novel metal alloy above and/or below the edges of the rolled strip or sheet to be welded, then welding the one or more strips along the rolled strip or sheet edges, and then grinding off the outer strip, or c) laser welding the edges of the rolled sheet or strip in a vacuum, oxygen reducing atmosphere, or inert atmosphere. In still another and/or additional non-limiting process, the near net medical device, blank, rod, tube, etc. of the novel metal alloy is formed by consolidating metal powder. In this process, fine particles of metal (e.g., Re, W, Mo, Ti, Cu, Ni, Cr, etc.) along with any additives are mixed to form a homogenous blend of particles. Typically, the average particle size of the metal powders is less than about 200 mesh (e.g., less than 74 microns). A larger average particle size can interfere with the proper mixing of the metal powders and/or adversely affect one or more physical properties of the near net medical device, blank, rod, tube, etc. formed from the metal powders. In one non-limiting embodiment, the average particle size of the metal powders is less than about 230 mesh (e.g., less than 63 microns). In another and/or alternative non-limiting embodiment, the average particle size of the metal powders is about 2-63 microns, and more particularly about 5-40 microns. As can be appreciated, smaller average particle sizes can be used. The purity of the metal powders should be selected so that the metal powders contain very low levels of carbon, oxygen and nitrogen. Typically, the carbon content of the metal powder used to form the novel metal alloy is less than about 100 ppm, the oxygen content is less than about 50 ppm, and the nitrogen content is less than about 20 ppm. Typically, metal powder used to form the novel metal alloy has a purity grade of at least 99.9 and more typically at least about 99.95. The blend of metal powder is then pressed together to form a solid solution of the novel metal alloy into a near net medical device, blank, rod, tube, etc. Typically the pressing process is by an isostatic process (i.e., uniform pressure applied from all sides on the metal powder); however other processes can be used. When the metal powders are pressed together isostatically, cold isostatic pressing (CIP) is typically used to consolidate the metal powders; however, this is not required. The pressing process can be performed in an inert atmosphere, an oxygen reducing atmosphere (e.g., hydrogen, argon and hydrogen mixture, etc.) and/or under a vacuum; however, this is not required. The average density of the near net medical device, blank, rod, tube, etc. that is achieved by pressing together the metal powders is about 80-95% (and all values and ranges therebetween) of the final average density of the near net medical device, blank, rod, tube, etc. or about 70-96% (and all values and ranges therebetween) the minimum theoretical density of the novel metal alloy. Pressing pressures of at least about 300 MPa are generally used. Generally, the pressing pressure is about 400-700MPa; however, other pressures can be used. After the metal powders are pressed together, the pressed metal powders are sintered at a temperature of at least 1600°C (e.g., 1600-3500°C and all values and ranges therebetween) to partially or fully fuse the metal powders together to form the near net medical device, blank, rod, tube, etc. The sintering of the consolidated metal powder can be performed in an oxygen reducing atmosphere (e.g., helium, argon, hydrogen, argon and hydrogen mixture, etc.) and/or under a vacuum; however, this is not required. At the high sintering temperatures, a high hydrogen atmosphere will reduce both the amount of carbon and oxygen in the formed near net medical device, blank, rod, tube, etc. The sintered metal powder generally has an as-sintered average density of about 90-99% the minimum theoretical density of the novel metal alloy. Typically, the sintered metal alloy has a final average density of at least about 5 gm/cc, and typically at least about 8.3 gm/cc, and can be up to or greater than about 16 gm/cc; however, this is not required. The density of the formed near net medical device, blank, rod, tube, etc. will generally depend on the type of novel metal alloy used.

[0081] In a still further and/or alternative non-limiting aspect of the present invention, when a solid rod of the novel metal alloy is formed, the rod is then formed into a tube prior to reducing the outer cross-sectional area or diameter of the rod. The rod can be formed into a tube by a variety of processes such as, but not limited to, cutting or drilling (e.g., gun drilling, etc.) or by cutting (e.g., EDM, EDM sinker, wire EDM, etc.). The cavity or passageway formed in the rod typically is formed fully through the rod; however, this is not required.

[0082] In yet a further and / or alternative non-limiting aspect of the present invention, the near net medical device, blank, rod, tube, etc. can be cleaned and/or polished after the near net medical device, blank, rod, tube, etc. has been form; however, this is not required. Typically, the near net medical device, blank, rod, tube, etc. is cleaned and/or polished prior to being further processed; however, this is not required. When a rod of the novel metal alloy is formed into a tube, the formed tube is typically cleaned and/or polished prior to being further processed; however, this is not required. When the near net medical device, blank, rod, tube, etc. is resized and/or annealed, the resized and/or annealed, the near net medical device, blank, rod, tube, etc. is typically cleaned and/or polished prior to and/or after each or after a series of resizing and/or annealing processes; however, this is not required. The cleaning and/or polishing of the near net medical device, blank, rod, tube, etc. is used to remove impurities and/or contaminants from the surfaces of the near net medical device, blank, rod, tube, etc. Impurities and contaminants can become incorporated into the novel metal alloy during the processing of the near net medical device, blank, rod, tube, etc. The inadvertent incorporation of impurities and contaminants in the near net medical device, blank, rod, tube, etc. can result in an undesired amount of carbon, nitrogen and/or oxygen, and/or other impurities in the novel metal alloy. The inclusion of impurities and contaminants in the novel metal alloy can result in premature micro-cracking of the novel metal alloy and/or an adverse effect on one or more physical properties of the novel metal alloy (e.g., decrease in tensile elongation, increased ductility, increased brittleness, etc.). The cleaning of the novel metal alloy can be accomplished by a variety of techniques such as, but not limited to, 1) using a solvent (e.g., acetone, methyl alcohol, etc.) and wiping the novel metal alloy with a Kimwipe or other appropriate towel, 2) by at least partially dipping or immersing the novel metal alloy in a solvent and then ultrasonically cleaning the novel metal alloy, and/or 3) by at least partially dipping or immersing the novel metal alloy in a pickling solution. As can be appreciated, the novel metal alloy can be cleaned in other or additional ways. If the novel metal alloy is to be polished, the novel metal alloy is generally polished by use of a polishing solution that typically includes an acid solution; however, this is not required. In one non-limiting example, the polishing solution includes sulfuric acid; however, other or additional acids can be used. In one non-limiting polishing solution, the polishing solution can include by volume 60-95% sulfuric acid and 5-40% de-ionized water (DI water). Typically, the polishing solution that includes an acid will increase in temperature during the making of the solution and/or during the polishing procedure. As such, the polishing solution is typically stirred and/or cooled during making of the solution and/or during the polishing procedure. The temperature of the polishing solution is typically about 20-100°C (and all values and ranges therebetween), and typically greater than about 25°C. One non-limiting polishing technique that can be used is an electropolishing technique. When an electropolishing technique is used, a voltage of about 2-30 V (and all values and ranges therebetween), and typically about 5-12 V is applied to the near net medical device, blank, rod, tube, etc. during the polishing process; however, it will be appreciated that other voltages can be used. The time used to polish the novel metal alloy is dependent on both the size of the near net medical device, blank, rod, tube, etc. and the amount of material that needs to be removed from the near net medical device, blank, rod, tube, etc. The near net medical device, blank, rod, tube, etc. can be processed by use of a two-step polishing process wherein the novel metal alloy piece is at least partially immersed in the polishing solution for a given period (e.g., 0.1-15 minutes, etc.), rinsed (e.g., DI water, etc.) for a short period of time (e.g., 0.02-1 minute, etc.), and then flipped over and at least partially immersed in the solution again for the same or similar duration as the first time; however, this is not required. The novel metal alloy can be rinsed (e.g., DI water, etc.) for a period of time (e.g., 0.01-5 minutes, etc.) before rinsing with a solvent (e.g., acetone, methyl alcohol, etc.); however, this is not required. The novel metal alloy can be dried (e.g., exposure to the atmosphere, maintained in an inert gas environment, etc.) on a clean surface. These polishing procedures can be repeated until the desired amount of polishing of the near net medical device, blank, rod, tube, etc. is achieved. The near net medical device, blank, rod, tube, etc. can be uniformly electropolished or selectively electropolished. When the near net medical device, blank, rod, tube, etc. is selectively electropolished, the selective electropolishing can be used to obtain different surface characteristics of the near net medical device, blank, rod, tube, etc. and/or selectively expose one or more regions of the near net medical device, blank, rod, tube, etc.; however, this is not required.

[0083] In still yet a further and/or alternative non-limiting aspect of the present invention, the near net medical device, blank, rod, tube, etc. can be resized to the desired dimension of the medical device. In one non-limiting embodiment, the cross-sectional area or diameter of the near net medical device, blank, rod, tube, etc. is reduced to a final near net medical device, blank, rod, tube, etc. dimension in a single step or by a series of steps. The reduction of the outer cross- sectional area or diameter of the near net medical device, blank, rod, tube, etc. may be obtained by centerless grinding, turning, electropolishing, drawing process, grinding, laser cutting, shaving, polishing, EDM cutting, etc. The outer cross-sectional area or diameter size of the near net medical device, blank, rod, tube, etc. can be reduced by the use of one or more drawing processes; however, this is not required. During the drawing process, care should be taken to not form micro cracks in the near net medical device, blank, rod, tube, etc. during the reduction of the near net medical device, blank, rod, tube, etc. outer cross-sectional area or diameter. Generally, the near net medical device, blank, rod, tube, etc. should not be reduced in cross-sectional area by more about 25% each time the near net medical device, blank, rod, tube, etc. is drawn through a reducing mechanism (e.g., a die, etc.). In one non-limiting process step, the near net medical device, blank, rod, tube, etc. is reduced in cross-sectional area by about 0.1-20% each time the near net medical device, blank, rod, tube, etc. is drawn through a reducing mechanism. In another and/or alternative non-limiting process step, the near net medical device, blank, rod, tube, etc. is reduced in cross-sectional area by about 1-15% each time the near net medical device, blank, rod, tube, etc. is drawn through a reducing mechanism. In still another and/or alternative non-limiting process step, the near net medical device, blank, rod, tube, etc. is reduced in cross-sectional area by about 2-15% each time the near net medical device, blank, rod, tube, etc. is drawn through reducing mechanism. In yet another one non-limiting process step, the near net medical device, blank, rod, tube, etc. is reduced in cross-sectional area by about 5-10% each time the near net medical device, blank, rod, tube, etc. is drawn through reducing mechanism. In another and/or alternative non-limiting embodiment of the invention, the near net medical device, blank, rod, tube, etc. of novel metal alloy is drawn through a die to reduce the cross-sectional area of the near net medical device, blank, rod, tube, etc. Generally, before drawing the near net medical device, blank, rod, tube, etc. through a die, one end of the near net medical device, blank, rod, tube, etc. is narrowed down (nosed) so as to allow it to be fed through the die; however, this is not required. The tube drawing process is typically a cold drawing process or a plug drawing process through a die. When a cold drawing or mandrel drawing process is used, a lubricant (e.g., molybdenum paste, grease, etc.) is typically coated on the outer surface of the near net medical device, blank, rod, tube, etc. and the near net medical device, blank, rod, tube, etc. is then drawn though the die. Typically, little or no heat is used during the cold drawing process. After the near net medical device, blank, rod, tube, etc. has been drawn through the die, the outer surface of the near net medical device, blank, rod, tube, etc. is typically cleaned with a solvent to remove the lubricant so as to limit the amount of impurities that are incorporated in the novel metal alloy; however, this is not required. This cold drawing process can be repeated several times until the desired outer cross-sectional area or diameter, inner cross-sectional area or diameter and/or wall thickness of the near net medical device, blank, rod, tube, etc. is achieved. A plug drawing process can also or alternatively be used to size the near net medical device, blank, rod, tube, etc. The plug drawing process typically does not use a lubricant during the drawing process. The plug drawing process typically includes a heating step to heat the near net medical device, blank, rod, tube, etc. prior and/or during the drawing of the near net medical device, blank, rod, tube, etc. through the die. The elimination of the use of a lubricant can reduce the incidence of impurities being introduced into the novel metal alloy during the drawing process. During the plug drawing process, the near net medical device, blank, rod, tube, etc. can be protected from oxygen by use of a vacuum environment, a non-oxygen environment (e.g., hydrogen, argon and hydrogen mixture, nitrogen, nitrogen and hydrogen, etc.) or an inert environment. One non-limiting protective environment includes argon, hydrogen or argon and hydrogen; however, other or additional inert gasses can be used. As indicated above, the near net medical device, blank, rod, tube, etc. is typically cleaned after each drawing process to remove impurities and/or other undesired materials from the surface of the near net medical device, blank, rod, tube, etc.; however, this is not required. Typically, the near net medical device, blank, rod, tube, etc. should be shielded from oxygen and nitrogen when the temperature of the near net medical device, blank, rod, tube, etc. is increased to above 500°C, and typically above 450°C, and more typically above 400°C; however, this is not required. When the near net medical device, blank, rod, tube, etc. is heated to temperatures above about 400- 500°C, the near net medical device, blank, rod, tube, etc. tends to begin forming nitrides and/or oxides in the presence of nitrogen and oxygen. In these higher temperature environments, a hydrogen environment, an argon and hydrogen environment, etc. is generally used. When the near net medical device, blank, rod, tube, etc. is drawn at temperatures below 400-500°C, the near net medical device, blank, rod, tube, etc. can be exposed to air with little or no adverse effects; however, an inert or slightly reducing environment is generally more desirable.

[0084] In another and/or alternative non-limiting aspect of the present invention, a rod of metal alloy is partially or fully reduced to the desired outer diameter prior to forming a tube from the rod. The rod can be formed by 1) melting the novel metal alloy and/or metals that form the novel metal alloy (e.g., vacuum arc melting, etc.) and then extruding and/or casting the novel metal alloy into a solid metal rod, or 2) consolidating metal power of the novel metal alloy and/or metal powder of metals that form the novel metal alloy into a solid metal rod. Once the solid metal rod is formed, the outer diameter of the metal rod is reduced by cold working the rod using or more techniques such as, but not limited to, use of a mandrel, use of one or more rollers, use of an extrusion process, use of a die, squeezing processes, cold rolling process, a rotary swaging process, cold forging process, sizing processes, drawing processes, etc. The rod can be processed one or more times using one or more cold working techniques prior to achieving the desired outer diameter of the rod. Generally, the rod is not reduced in cross-sectional area by more about 25% each time the rod is subjected to a reducing mechanism. During the reducing process, the solid rod can be annealed one or more times to facilitate in the reduction of the outer diameter of the rod. The rod may or may not be annealed each time the rod is subjected to a reducing mechanism. Once the solid rod has obtained it desired outer diameter, the solid rod is typically not further annealed so as to maintain the hardness properties and yield strength properties that were obtained by the cold working of the rod. The above discussed parameters for reducing the outer diameter of the solid rod to the desired outer diameter can be used. Once the solid rod has the desired outer diameter, the solid rod is formed into a tube by gun drilling the rod or EDM cutting of the rod. Further processing of the tube can occur to finalize the wall thickness of the tube and uniformity of the wall thickness of the tube. One non-limiting process that can be used is a wire EDM machining process. Once the tube is formed, the tube can be subject to one or more treatment processes such as cleaning, polishing, sterilizing, nitrided, etc. for final processing of the metal tube. The metal tube can be further processed by cutting the metal tube into a portion of or the complete final form (e.g., final medical device - stent, TAVR, screw, etc.). It has been found that refractory metal tubes that are first formed by reducing the outer diameter of the rod and then hollowing out the rod to form a tube have a final yield strength of at least 30% greater than tubes that are first formed and then the outer diameter of the tube is reduced. For example, MoRe alloy tubes that have yield strengths of 130 ksi when formed from a tube that has been reduced in outer diameter (and not annealed after achieving its final outer diameter) can have yield strengths of at least 200 ksi when formed by first reducing a solid rod by a cold working process and then hollowing out the solid rod to form a tube after the rod has been reduced to the desired outer diameter.

[0085] In still a further and/or alternative non-limiting aspect of the present invention, the near net medical device, blank, rod, tube, etc. during the drawing process can be nitrided; however, this is not required. The nitride layer on the near net medical device, blank, rod, tube, etc. can function as a lubricating surface during the drawing process to facilitate in the drawing of the near net medical device, blank, rod, tube, etc. The near net medical device, blank, rod, tube, etc. is generally nitrided in the presence of nitrogen or a nitrogen mixture. In one non-limiting embodiment of the invention, the surface of the near net medical device, blank, rod, tube, etc. is nitrided prior to at least one drawing step for the near net medical device, blank, rod, tube, etc. In one non-limiting aspect of this embodiment, the surface of the near net medical device, blank, rod, tube, etc. is nitrided prior to a plurality of drawing steps. In another non-limiting aspect of this invention, after the near net medical device, blank, rod, tube, etc. has been annealed, the near net medical device, blank, rod, tube, etc. is nitrided prior to being drawn. In another and/or alternative non-limiting embodiment, the near net medical device, blank, rod, tube, etc. is cleaned to remove nitride compounds on the surface of the near net medical device, blank, rod, tube, etc. prior to annealing the rod to tube. The nitride compounds can be removed by a variety of steps such as, but not limited to, grit blasting, polishing, etc. After the near net medical device, blank, rod, tube, etc. has been annealed, the near net medical device, blank, rod, tube, etc. can be again nitrided prior to one or more drawing steps; however, this is not required. As can be appreciated, the complete outer surface of the near net medical device, blank, rod, tube, etc. can be nitrided or a portion of the outer surface of the near net medical device, blank, rod, tube, etc. can be nitrided. Nitriding only selected portions of the outer surface of the near net medical device, blank, rod, tube, etc. can be used to obtain different surface characteristics of the near net medical device, blank, rod, tube, etc.; however, this is not required.

[0086] In yet a further and / or alternative non-limiting aspect of the present invention, the near net medical device, blank, rod, tube, etc. is cooled after being annealed; however, this is not required. Generally, the near net medical device, blank, rod, tube, etc. is cooled at a fairly quick rate after being annealed so as to inhibit or prevent the formation of a sigma phase in the novel metal alloy; however, this is not required. Generally, the near net medical device, blank, rod, tube, etc. is cooled at a rate of at least about 50°C per minute (e.g., 50-500°C per minute and all values and ranges therebetween) after being annealed, typically at least about 75°C per minute after being annealed, more typically at least about 100°C per minute after being annealed, even more typically about 100-400°C per minute after being annealed, still even more typically about 150-350°C per minute after being annealed, and yet still more typically about 200-300°C per minute after being annealed, and still yet even more typically about 250-280°C per minute after being annealed; however, this is not required.

[0087] In still yet a further and/or alternative non-limiting aspect of the present invention, the near net medical device, blank, rod, tube, etc. is annealed after one or more drawing processes. The novel metal alloy blank, rod, tube, etc. can be annealed after each drawing process or after a plurality of drawing processes. The novel metal alloy blank, rod, tube, etc. is typically annealed prior to about a 60% cross-sectional area size reduction of the novel metal alloy blank, rod, tube, etc. In other words, the near net medical device, blank, rod, tube, etc. should not be reduced in cross-sectional area by more than 60% before being annealed (e.g., 0.1-60% reduction and all values and ranges therebetween). A too-large reduction in the cross-sectional area of the novel metal alloy blank, rod, tube, etc. during the drawing process prior to the near net medical device, blank, rod, tube, etc. being annealed can result in micro-cracking of the near net medical device, blank, rod, tube, etc. In one non-limiting processing step, the novel metal alloy blank, rod, tube, etc. is annealed prior to about a 50% cross-sectional area size reduction of the novel metal alloy blank, rod, tube, etc. In another and/or alternative non-limiting processing step, the novel metal alloy blank, rod, tube, etc. is annealed prior to about a 45% cross-sectional area size reduction of the novel metal alloy blank, rod, tube, etc. In still another and/or alternative non-limiting processing step, the novel metal alloy blank, rod, tube, etc. is annealed prior to about a 1-45% cross-sectional area size reduction of the novel metal alloy blank, rod, tube, etc. In yet another and/or alternative non-limiting processing step, the novel metal alloy blank, rod, tube, etc. is annealed prior to about a 5-30% cross-sectional area size reduction of the novel metal alloy blank, rod, tube, etc. In still yet another and/or alternative non-limiting processing step, the novel metal alloy blank, rod, tube, etc. is annealed prior to about a 5-15% cross-sectional area size reduction of the novel metal alloy blank, rod, tube, etc.

[0088] In another and/or alternative non-limiting aspect of the invention, when the near net medical device, blank, rod, tube, etc. is annealed, the near net medical device, blank, rod, tube, etc. is typically heated to a temperature of about 500-1700°C (and all values and ranges therebetween) for a period of about 1-200 minutes (and all values and ranges therebetween); however, other temperatures and/or times can be used. In one non-limiting processing step, the near net medical device, blank, rod, tube, etc. is annealed at a temperature of about 1000-1600°C for about 2-100 minutes. In another non-limiting processing step, the near net medical device, blank, rod, tube, etc. is annealed at a temperature of about 1100-1500°C for about 5-30 minutes. The annealing process typically occurs in an inert environment or an oxygen-reducing environment so as to limit the amount of impurities that may embed themselves in the novel metal alloy during the annealing process. One non-limiting oxygen-reducing environment that can be used during the annealing process is a hydrogen environment; however, it can be appreciated that a vacuum environment can be used or one or more other or additional gasses can be used to create the oxygen-reducing environment. At the annealing temperatures, a hydrogen-containing atmosphere can further reduce the amount of oxygen in the near net medical device, blank, rod, tube, etc. The chamber in which the near net medical device, blank, rod, tube, etc. is annealed should be substantially free of impurities (e.g., carbon, oxygen, and/or nitrogen) so as to limit the amount of impurities that can embed themselves in the near net medical device, blank, rod, tube, etc. during the annealing process. The annealing chamber typically is formed of a material that will not impart impurities to the near net medical device, blank, rod, tube, etc. as the near net medical device, blank, rod, tube, etc. is being annealed. A non-limiting material that can be used to form the annealing chamber includes, but is not limited to, molybdenum, rhenium, tungsten, molybdenum TZM alloy, cobalt, chromium, ceramic, etc. When the near net medical device, blank, rod, tube, etc. is restrained in the annealing chamber, the restraining apparatuses that are used to contact the near net medical device, blank, rod, tube, etc. are typically formed of materials that will not introduce impurities to the novel metal alloy during the processing of the near net medical device, blank, rod, tube, etc. Non-limiting examples of materials that can be used to at least partially form the restraining apparatuses include, but are not limited to, molybdenum, titanium, yttrium, zirconium, rhenium, cobalt, chromium, tantalum, and/or tungsten. In still another and/or alternative non-limiting processing step, the parameters for annealing can be changed as the near net medical device, blank, rod, tube, etc. as the cross-sectional area or diameter; and/or wall thickness of the near net medical device, blank, rod, tube, etc. are changed. It has been found that good grain size characteristics of the near net medical device, blank, rod, tube, etc. can be achieved when the annealing parameters are varied as the parameters of the near net medical device, blank, rod, tube, etc. change. For example, as the wall thickness is reduced, the annealing temperature is correspondingly reduced; however, the times for annealing can be increased. As can be appreciated, the annealing temperatures of the near net medical device, blank, rod, tube, etc. can be decreased as the wall thickness decreases, but the annealing times can remain the same or also be reduced as the wall thickness reduces. After each annealing process, the grain size of the metal in the near net medical device, blank, rod, tube, etc. should be no greater than 4 ASTM. Generally, the grain size range is about 4-20 ASTM (and all values and ranges therebetween). It is believed that as the annealing temperature is reduced as the wall thickness reduces, small grain sizes can be obtained. The grain size of the metal in the near net medical device, blank, rod, tube, etc. should be as uniform as possible. In addition, the sigma phase of the metal in the near net medical device, blank, rod, tube, etc. should be as reduced as much as possible. The sigma phase is a spherical, elliptical or tetragonal crystalline shape in the novel metal alloy. After the final drawing of the near net medical device, blank, rod, tube, etc., a final annealing of the near net medical device, blank, rod, tube, etc. can be done for final strengthening of the near net medical device, blank, rod, tube, etc.; however, this is not required. This final annealing process, when used, generally occurs at a temperature of about 500-1600°C (and all values and ranges therebetween) for at least about 1 minutes; however, other temperatures and/or time periods can be used.

[0089] In another and/or alternative non-limiting aspect of the present invention, the near net medical device, blank, rod, tube, etc. can be cleaned prior to and/or after being annealed. The cleaning process is designed to remove impurities, lubricants (e.g., nitride compounds, molybdenum paste, grease, etc.) and/or other materials from the surfaces of the near net medical device, blank, rod, tube, etc. Impurities that are on one or more surfaces of the near net medical device, blank, rod, tube, etc. can become permanently embedded into the near net medical device, blank, rod, tube, etc. during the annealing processes. These imbedded impurities can adversely affect the physical properties of the novel metal alloy as the near net medical device, blank, rod, tube, etc. is formed into a medical device, and/or can adversely affect the operation and/or life of the medical device. In one non-limiting embodiment of the invention, the cleaning process includes a delubrication or degreasing process which is typically followed by pickling process; however, this is not required. The delubrication or degreasing process followed by pickling process is typically used when a lubricant has been used on the near net medical device, blank, rod, tube, etc. during a drawing process. Lubricants commonly include carbon compounds, nitride compounds, molybdenum paste, and other types of compounds that can adversely affect the novel metal alloy if such compounds and/or elements in such compounds become associated and/or embedded with the novel metal alloy during an annealing process. The delubrication or degreasing process can be accomplished by a variety of techniques such as, but not limited to, 1) using a solvent (e.g., acetone, methyl alcohol, etc.) and wiping the novel metal alloy with a Kimwipe or other appropriate towel, 2) by at least partially dipping or immersing the novel metal alloy in a solvent and then ultrasonically cleaning the novel metal alloy, 3) sand blasting the novel metal alloy, and/or 4) chemical etching the novel metal alloy. As can be appreciated, the novel metal alloy can be delubricated or degreased in other or additional ways. After the near net medical device, blank, rod, tube, etc. has been delubricated or degreased, the near net medical device, blank, rod, tube, etc. can be further cleaned by use of a pickling process; however, this is not required. The pickling process (when used) includes the use of one or more acids to remove impurities from the surface of the near net medical device, blank, rod, tube, etc. Non-limiting examples of acids that can be used as the pickling solution include, but are not limited to, nitric acid, acetic acid, sulfuric acid, hydrochloric acid, and/or hydrofluoric acid. These acids are typically analytical reagent (ACS) grade acids. The acid solution and acid concentration are selected to remove oxides and other impurities on the near net medical device, blank, rod, tube, etc. surface without damaging or over-etching the surface of the near net medical device, blank, rod, tube, etc. A near net medical device, blank, rod, tube, etc. surface that includes a large amount of oxides and/or nitrides typically requires a stronger pickling solution and/or long pickling process times. Non-limiting examples of pickling solutions include 1) 25-60% DI water (and all values and ranges therebetween), 30-60% nitric acid (and all values and ranges therebetween), and 2-20% sulfuric acid (and all values and ranges therebetween); 2) 40-75% acetic acid (and all values and ranges therebetween), 10-35% nitric acid (and all values and ranges therebetween), and 1-12% hydrofluoric acid (and all values and ranges therebetween); and 3) 50-100% hydrochloric acid (and all values and ranges therebetween). As can be appreciated, one or more different pickling solutions can be used during the pickling process. During the pickling process, the near net medical device, blank, rod, tube, etc. is fully or partially immersed in the pickling solution for a sufficient amount of time to remove the impurities from the surface of the near net medical device, blank, rod, tube, etc. Typically, the time period for pickling is about 2-120 seconds (and all values and ranges therebetween); however, other time periods can be used. After the near net medical device, blank, rod, tube, etc. has been pickled, the near net medical device, blank, rod, tube, etc. is typically rinsed with a water (e.g., DI water, etc.) and/or a solvent (e.g., acetone, methyl alcohol, etc.) to remove any pickling solution from the near net medical device, blank, rod, tube, etc. and then the near net medical device, blank, rod, tube, etc. is allowed to dry. The near net medical device, blank, rod, tube, etc. may be keep in a protective environment during the rinse and/or drying process to inhibit or prevent oxides from reforming on the surface of the near net medical device, blank, rod, tube, etc. prior to the near net medical device, blank, rod, tube, etc. being drawn and/or annealed; however, this is not required.

[0090] In yet another and/or alternative non-limiting aspect of the present invention, the restraining apparatuses that are used to contact the novel metal alloy during an annealing process and/or drawing process are typically formed of materials that will not introduce impurities to the novel metal alloy during the processing of the metal alloy. In one non-limiting embodiment, when the novel metal alloy is exposed to temperatures above 150°C, the materials that contact the novel metal alloy during the processing of the metal alloy are typically made from chromium, cobalt, molybdenum, rhenium, tantalum and/or tungsten. When the novel metal alloy is processed at lower temperatures (i.e., 150°C or less), materials made from Teflon™ parts can also or alternatively be used.

[0091 ] In still another and / or alternative non-limiting aspect of the present invention, the novel metal alloy near net medical device, blank, rod, tube, etc., after being formed to the desired shape, the outer cross-sectional area or diameter, inner cross-sectional area or diameter and/or wall thickness, can be cut and/or etched to at least partially form the desired configuration of the medical device (e.g., stent, TAVR valve, pedicle screw, PFO device, valve, spinal implant, vascular implant, graft, guide wire, sheath, stent catheter, electrophysiology catheter, hypotube, catheter, staple, cutting device, dental implant, bone implant, prosthetic implant or device to repair, replace and/or support a bone and/or cartilage, nail, rod, screw, post, cage, plate, cap, hinge, joint system, wire, needle, anchor, spacer, shaft, anchor, disk, ball, tension band, locking connector, or other structural assembly that is used in a body to support a structure, mount a structure and/or repair a structure in a body, etc.). The near net medical device, blank, rod, tube, etc. can be cut or otherwise formed by one or more processes (e.g., centerless grinding, turning, electropolishing, drawing process, grinding, laser cutting, shaving, polishing, EDM cutting, etching, micro-machining, laser micro-machining, micro-molding, machining, etc.). In one non limiting embodiment of the invention, the novel metal alloy near net medical device, blank, rod, tube, etc. is at least partially cut by a laser. The laser is typically desired to have a beam strength which can heat the novel metal alloy near net medical device, blank, rod, tube, etc. to a temperature up to at least about 2200-2300°C. In one non-limiting aspect of this embodiment, a pulsed Nd:YAG neodymium-doped yttrium aluminum garnet (Nd:Y ₃ AlsOi ₂ ) or CO2 laser is used to at least partially cut a pattern of a medical device out of the novel metal alloy blank, rod, tube, etc. In another and/or alternative non-limiting aspect of this embodiment, the cutting of the novel metal alloy near net medical device, blank, rod, tube, etc. by the laser can occur in a vacuum environment, an oxygen-reducing environment, or an inert environment; however, this is not required. It has been found that laser cutting of the near net medical device, blank, rod, tube, etc. in a non-protected environment can result in impurities being introduced into the cut near net medical device, blank, rod, tube, etc., which introduced impurities can induce micro-cracking of the near net medical device, blank, rod, tube, etc. during the cutting of the near net medical device, blank, rod, tube, etc. One non-limiting oxygen-reducing environment includes a combination of argon and hydrogen; however, a vacuum environment, an inert environment, or other or additional gasses can be used to form the oxygen reducing environment. In still another and/or alternative non-limiting aspect of this embodiment, the novel metal alloy near net medical device, blank, rod, tube, etc. is stabilized so as to limit or prevent vibration of the near net medical device, blank, rod, tube, etc. during the cutting process. The apparatus used to stabilize the near net medical device, blank, rod, tube, etc. can be formed of molybdenum, rhenium, tungsten, tantalum, cobalt, chromium, molybdenum TZM alloy, ceramic, etc. so as to not introduce contaminants to the near net medical device, blank, rod, tube, etc. during the cutting process; however, this is not required. Vibrations in the near net medical device, blank, rod, tube, etc. during the cutting of the near net medical device, blank, rod, tube, etc. can result in the formation of micro-cracks in the near net medical device, blank, rod, tube, etc. as the near net medical device, blank, rod, tube, etc. is cut. The average amplitude of vibration during the cutting of the near net medical device, blank, rod, tube, etc. is generally no more than about 150% of the wall thickness of the near net medical device, blank, rod, tube, etc.; however, this is not required. In one non-limiting aspect of this embodiment, the average amplitude of vibration is no more than about 100% of the wall thickness of the near net medical device, blank, rod, tube, etc. In another non-limiting aspect of this embodiment, the average amplitude of vibration is no more than about 75% of the wall thickness of the near net medical device, blank, rod, tube, etc. In still another non-limiting aspect of this embodiment, the average amplitude of vibration is no more than about 50% of the wall thickness of the near net medical device, blank, rod, tube, etc. In yet another non-limiting aspect of this embodiment, the average amplitude of vibration is no more than about 25% of the wall thickness of the near net medical device, blank, rod, tube, etc. In still yet another non-limiting aspect of this embodiment, the average amplitude of vibration is no more than about 15% of the wall thickness of the near net medical device, blank, rod, tube, etc.

[0092] In still yet another and/or alternative non-limiting aspect of the present invention, the novel metal alloy near net medical device, blank, rod, tube, etc., after being formed to the desired medical device, can be cleaned, polished, sterilized, nitrided, etc. for final processing of the medical device. In one non-limiting embodiment of the invention, the medical device is electropolished. In one non-limiting aspect of this embodiment, the medical device is cleaned prior to being exposed to the polishing solution; however, this is not required. The cleaning process (when used) can be accomplished by a variety of techniques such as, but not limited to, 1) using a solvent and wiping the medical device with a Kimwipe or other appropriate towel, and/or 2) by at least partially dipping or immersing the medical device in a solvent and then ultrasonically cleaning the medical device. As can be appreciated, the medical device can be cleaned in other or additional ways. In another and/or alternative non-limiting aspect of this embodiment, the polishing solution can include one or more acids. In yet another and/or alternative non-limiting aspect of this embodiment, the medical device is rinsed with water and/or a solvent and allowed to dry to remove polishing solution on the medical device. In another and/or alternative non-limiting embodiment of the invention, the formed medical device is optionally nitrided. After the medical device is nitrided, the medical device is typically cleaned; however, this is not required. During the nitride process, the surface of the medical device is modified by the present of nitrogen. The nitriding process for the medical device can be used to increase surface hardness and/or wear resistance of the medical device. For example, the nitriding process can be used to increase the wear resistance of articulation surfaces or surface wear on the medical device to extend the life of the medical device, and/or to increase the wear life of mating surfaces on the medical device (e.g., polyethylene liners of joint implants like knees, hips, shoulders, etc.), and/or to reduce particulate generation from use of the medical device.

[0093] The use of the novel alloy (when used) to form all or a portion of the medical device can result in several advantages over medical devices formed from other materials. These advantages include, but are not limited to:

[0094] · The novel alloy has increased strength and/or hardness as compared with stainless steel or chromium-cobalt alloys, thus less quantity of novel alloy can be used in the medical device to achieve similar strengths as compared to medical devices formed of different metals. As such, the resulting medical device can be made smaller and less bulky by use of the novel alloy without sacrificing the strength and durability of the medical device. The medical device can also have a smaller profile, thus can be inserted into smaller areas, openings and/or passageways. The increased strength of the novel alloy also results in the increased radial strength of the medical device. For instance, the thickness of the walls of the medical device and/or the wires used to form the medical device can be made thinner and achieve a similar or improved radial strength as compared with thicker walled medical devices formed of stainless steel or cobalt and chromium alloy.

[0095] · The novel alloy has improved stress-strain properties, bendability properties, elongation properties and/or flexibility properties of the medical device as compared with stainless steel or chromium-cobalt alloys, thus resulting in an increase life for the medical device. For instance, the medical device can be used in regions that subject the medical device to repeated bending. Due to the improved physical properties of the medical device from the novel alloy, the medical device has improved resistance to fracturing in such frequent bending environments. These improved physical properties at least in part result from the composition of the novel alloy, the grain size of the novel alloy, the carbon, oxygen and nitrogen content of the novel alloy; and/or the carbon/oxygen ratio of the novel alloy.

[0096] · The novel alloy has a reduced degree of recoil during the crimping and/or expansion of the medical device as compared with stainless steel or chromium-cobalt alloys. The medical device formed of the novel alloy better maintains its crimped form and/or better maintains its expanded form after expansion due to the use of the novel alloy. As such, when the medical device is to be mounted onto a delivery device when the medical device is crimped, the medical device better maintains its smaller profile during the insertion of the medical device in a body passageway. Also, the medical device better maintains its expanded profile after expansion so as to facilitate in the success of the medical device in the treatment area.

[0097] · The novel alloy has improved radiopaque properties as compared to standard materials such as stainless steel or cobalt-chromium alloy, thus reducing or eliminating the need for using marker materials on the medical device. For instance, the novel alloy is at least about 10-20% more radiopaque than stainless steel or cobalt-chromium alloy.

[0098] · The novel alloy is less of an irritant to the body than stainless steel or cobalt- chromium alloy, thus can result in reduced inflammation, faster healing, increased success rates of the medical device. When the medical device is expanded in a body passageway, some minor damage to the interior of the passageway can occur. When the body begins to heal such minor damage, the body has less adverse reaction to the presence of the novel alloy than compared to other metals such as stainless steel or cobalt-chromium alloy.

[0099] In still yet another and/or alternative non-limiting aspect of the present invention, there is provided a foam VGF/Growth factor. There is also provided method for using the foam wherein foam VGF, growth factor, steam cell, or additional cellular, biological or pharmaceutical agents is injected within a cavity of a bone or between bone segments for purposes of inducing, facilitating, supporting and/or promoting bone growth to fill the void. The injected foam can be used to enhance tissue growth to fill a void. There can be provided the mixing of a substance within a carrier for purposes of filling a temporary void within or between tissue masses wherein the substance is used to facilitate in tissue growth and/or the fusing of one or more tissue masses, and wherein the carrier creates a stable foam upon injection to fill the void without going beyond a prescribed boundary or the void.

[00100] One non-limiting object of the present invention is the provision of novel alloy in accordance with the present invention that can be used to partially or fully form a medical device, automotive parts, springs, aerospace parts, industrial machinery and parts, tools (e.g., medical tools, industrial tools, household tools, etc.), etc.

[00101 ] Another and/or alternative non-limiting object of the present invention is the provision of a novel alloy in accordance with the present invention that can be coated partially or fully on an outer surface of a metal body (e.g., Ti or Ti alloys, Co or Co alloys, Cr alloys, CoCr alloys, stainless steel, Fe and Fe alloys, Ni alloys, W alloys, Mo or Mo alloys, Re or Re alloys, Mo-Re alloys, Mo-Re-Cr alloys, Fe-Cr-Mo-CB alloys, dual phase austenitic steel, Hi-entropy alloy systems, WCu alloys, WRe alloys, etc.), polymer body, ceramic body, or composite body by a plasma coating process, a chemical vapor deposition process, or 3D printing process.

[00102] Another and/or alternative non-limiting object of the present invention is the provision of a cutting tool (e.g., metal cutting tool., etc.) that includes a metal body and an outer coating of novel alloy in accordance with the present invention that was coated by a plasma coating process, a chemical vapor deposition process, or 3D printing process.

[00103] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or medical tool that includes a metal body, polymer body, ceramic body, or composite body and an outer coating of the novel alloy in accordance with the present invention that was coated by a plasma coating process, a chemical vapor deposition process, or 3D printing process.

[00104] Another and/or alternative non-limiting object of the present invention is the provision of a medical device that is partially or fully form of the novel alloy of the present invention and which medical device has improved procedural success rates. [00105] Another and/or alternative non-limiting object of the present invention is the provision of a method and process for forming the novel alloy in accordance with the present invention that inhibits or prevents the formation of micro-cracks during the processing of the novel alloy.

[00106] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that is partially or fully formed of the novel alloy in accordance with the present invention and wherein the medical device or tool has improved physical properties. [00107] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that is at least partially formed of the novel alloy in accordance with the present invention that has increased strength and/or hardness and can optionally also be used as a marker material.

[00108] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that at least partially includes the novel alloy in accordance with the present invention and which novel alloy enables the medical device or tool to be formed with less material without sacrificing the strength of the medical device or tool as compared to prior medical devices.

[00109] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that at least partially includes the novel alloy in accordance with the present invention that is simple and cost effective to manufacture.

[00110] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that at least partially includes the novel alloy in accordance with the present invention that is at least partially coated with one or more polymer coatings.

[00111] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that at least partially includes the novel alloy in accordance with the present invention that is coated with one or more biological agents.

[00112] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that at least partially includes the novel alloy in accordance with the present invention that has one or more polymer coatings to at least partially control the release rate of one or more biological agents.

[00113] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that at least partially includes the novel alloy in accordance with the present invention that includes one or more surface structures and/or micro-structures. [00114] Another and/or alternative non-limiting object of the present invention is the provision of a method and process for forming the novel alloy in accordance with the present invention so as to partially or fully form a medical device or tool.

[00115] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that at least partially includes the novel alloy in accordance with the present invention that includes one or more markers.

[00116] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that at least partially includes the novel alloy in accordance with the present invention that includes and/or is used with one or more physical hindrances.

[00117] Another and/or alternative non-limiting object of the present invention is the provision of a medical device or tool that at least partially includes the novel alloy in accordance with the present invention that can be used in conjunction with one or more biological agents not on or in the medical device.

[00118] Another and/or alternative non-limiting object of the present invention is the provision of a method and process for forming the novel alloy in accordance with the present invention so as to inhibit or prevent the formation of micro-cracks during the processing of the novel alloy into a medical device or tool.

[00119] Another and/or alternative non-limiting object of the present invention is the provision of a method and process for forming the novel alloy in accordance with the present invention that inhibits or prevents the introduction of impurities into the novel alloy during the processing of the novel alloy into a medical device or tool.

[00120] Another and/or alternative non-limiting object of the present invention is the provision of a method and process for forming the novel alloy in accordance with the present invention that inhibits or prevents crack propagation and/or fatigue failure of the novel alloy.

[00121 ] Another and/or alternative non-limiting object of the present invention is the provision of a medical device that is used in orthopedics (e.g., orthopedic device, nail, rod, screw, post, cage, plate, pedicle screw, cap, hinge, joint system, wire, anchor, spacer, shaft, spinal implant, anchor, disk, ball, tension band, locking connector, bone implant, prosthetic implant or device to repair, replace and/or support a bone, etc.), which medical device may or may not be expandable, and which medical device is partially or fully formed of the novel alloy in accordance with the present invention. [00122] Another and/or alternative non-limiting object of the present invention is the provision of a medical device that is in the form of implant for insertion into a body passageway (e.g., PFO device, stent, TAVR valve, valve, spinal implant, vascular implant; graft, guide wire, sheath, stent catheter, electrophysiology catheter, hypotube, catheter, etc.), which medical device may or may not be expandable, and which medical device is partially or fully formed of the novel alloy in accordance with the present invention.

[00123] Another and/or alternative non-limiting object of the present invention is the provision of a medical device that is used in dentistry and orthodontics (e.g., dental restorations, dental implants, crowns, bridges, braces, dentures, wire, anchors, spacers, retainers, tubes, pins, screws, posts, rods, plates, palatal expander, orthodontic headgear, orthodontic archwire, teeth aligners, quadhelix, etc.), which medical device may or may not be expandable, and which medical device is partially or fully formed of the novel alloy in accordance with the present invention.

[00124] Another and/or alternative non-limiting object of the present invention is the provision of a medical device in the form of a stent that can be used in spinal fusion applications, and which medical device is partially or fully formed of the novel alloy in accordance with the present invention.

[00125] Another and/or alternative non-limiting object of the present invention is the provision of a medical device that includes a novel metal alloy that has had a nitriding process to form a nitride layer on the outer surface of the novel metal alloy.

[00126] Another and/or alternative non-limiting object of the present invention is the provision of a medical device that includes a novel metal alloy that has had a swaging process.

[00127] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device comprising the steps of a) forming a metal rod; the metal rod having a surface and an outer cross-sectional area; the metal rod is formed of a metal alloy; b) reducing the outer cross-sectional area of the metal rod to a first drawn down cross-sectional area by a reducing mechanism; the metal rod being drawn down at least once second drawn down cross-sectional area to obtain the first drawn down cross-sectional area; c) optionally annealing the metal rod prior to the metal rod having the outer cross-sectional area drawn down by more than about 50%; the optional annealing at a first annealing temperature in a low oxygen environment; the optional annealing occurring after the metal rod has been drawn down to the first drawn down cross-sectional area; d) optionally reducing the cross-sectional area of the metal rod to a second drawn down cross-sectional area by the reducing mechanism; the metal rod being drawn down at least once second drawn down cross-sectional area to obtain the second drawn down cross-sectional area; the second drawn down cross-sectional area smaller than the first drawn down cross-sectional area; the outer cross-sectional area of the metal rod reduced by no more than about 25% during each drawing down process second drawn down cross-sectional area; and, e) not annealing the metal rod after a final step of reducing the cross-sectional area of the metal rod.

[00128] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device further including the step of hollowing out the metal rod to form a metal tube.

[00129] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the step of optionally hollowing the metal rod to form the metal tube includes one or more of gun drilling, EDM cutting, and wire EDM cutting. [00130] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device further including the step of controlling an atmosphere about the metal rod during one or more of the steps of reducing and/or annealing so that the metal alloy of the metal rod after final step of reducing includes less than about 30 ppm nitrogen, less than about 150 ppm carbon, and less than about 100 ppm oxygen and a carbon to oxygen atomic ratio of at least about 0.2:1.

[00131 ] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the step of forming the metal rod includes a process of isostatically pressing metal powder together and subsequently sintering the metal power to form the metal rod; the process of isostatically pressing together the metal powder and / the process of sintering occurs in a controlled atmosphere; the metal rod has an average density of about 0.7-0.95 a minimum theoretical density of the metal alloy; the metal rod has an average density of at least 5 gm/cc; the controlled atmosphere including an inert atmosphere, an oxygen reducing atmosphere, or a partial or full vacuum.

[00132] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the step of forming the metal rod includes a) partially or fully melting one or more metals or a master alloy, and b) extruding or casting the partially or fully melted one or more metals or a master alloy to form the metal rod. [00133] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the metal alloy includes one or more alloy selected from the group consisting of Ti alloys, Co alloys, Cr alloys, CoCr alloys, Ni alloys, Fe- Cr-Mo-CB alloys, dual phase austenitic steel, Hi-entropy alloy systems, and refractory metal alloy.

[00134] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the metal rod is partially or fully formed of the refractory metal alloy; the refractory metal alloy is selected from the group consisting of MoRe alloy, ReW alloy, MoReCr alloy, MoReTa alloy, MoReTi alloy, WCu alloy, ReCr alloy, Mo alloy, Re alloy, W alloy, Ta alloy, and Nb alloy, the refractory metal alloy includes at least 20 wt.% of one or more of Mo, Re, Nb, Ta or W.

[00135] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the refractory metal alloy includes 30-60 wt.% Re and 40-70 wt.% one or more metal additives selected from the group consisting of Mo, Bi, Nb, Ni, Ta, Ti, V, W, Mn, Zr, Ir, Tc, Ru, Rh, Hf, Os, Cu, and Y.

[00136] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the refractory metal alloy includes 30-60 wt.% Re and 40-70 wt.% Mo.

[00137] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device further including the step of nitriding the metal rod to form a nitride layer on the metal rod.

[00138] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the step of annealing the metal rod includes the steps of a) annealing the metal rod at an annealing temperature of at least about 1480°C for a time period of at least about 5 minutes when the metal rod has wall thickness of greater than about 0.015 inch, b) annealing the metal rod at an annealing temperature of about 1450-1480°C for a time period of at least about 5 minutes when the metal rod has wall thickness of about 0.008-0.015 inch, and/or c) annealing the metal rod at an annealing temperature of less than about 1450°C for a time period of at least about 5 minutes when the metal rod has wall thickness of less than about 0.008 inch. [00139] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the medical device is a stent, TAVR valve, orthopedic device, or spinal device.

[00140] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the medical device is orthopedic rod, an expandable stent, and expandable valve, expandable graph, or expandable sheath.

[00141 ] Another and/or alternative non-limiting object of the present invention is the provision of a method for forming a medical device wherein the metal rod is cut to partially or fully form the medical device.

[00142] Other or additional features of the invention are disclosed in US 7,488,444; US 7,452,502; US 7,540,994; US 7,452,501; US 8,398,916; US Ser. No. 12/373,380; US Ser. No. 61/816,357; US Ser. No. 61/959,260; US Ser. No. 61/871,902; US Ser. No. 61/881,499; PCT/US2013/045543; and PCT/US2013/062804, which are all incorporated by reference herein. [00143] A more complete understanding of the articles/devices, processes and components disclosed herein can be obtained by reference to the accompanying drawings. These figures are merely schematic representations based on convenience and the ease of demonstrating the present disclosure, and are, therefore, not intended to indicate relative size and dimensions of the devices or components thereof and/or to define or limit the scope of the exemplary embodiments.

[00144] Although specific terms are used in the following description for the sake of clarity, these terms are intended to refer only to the particular structure of the embodiments selected for illustration in the drawings and are not intended to define or limit the scope of the disclosure. In the drawings and the following description below, it is to be understood that like numeric designations refer to components of like function.

[00145] The singular forms “a,” “an,” and “the” include plural referents unless the context clearly dictates otherwise.

[00146] As used in the specification and in the claims, the term “comprising” may include the embodiments “consisting of’ and “consisting essentially of.” The terms “comprise(s),” “include(s),” “having,” “has,” “can,” “contain(s),” and variants thereof, as used herein, are intended to be open-ended transitional phrases, terms, or words that require the presence of the named ingredients/steps and permit the presence of other ingredients/steps. However, such description should be construed as also describing compositions or processes as “consisting of’ and “consisting essentially of’ the enumerated ingredients/steps, which allows the presence of only the named ingredients/steps, along with any unavoidable impurities that might result therefrom, and excludes other ingredients/steps.

[00147] Numerical values in the specification and claims of this application should be understood to include numerical values which are the same when reduced to the same number of significant figures and numerical values which differ from the stated value by less than the experimental error of conventional measurement technique of the type described in the present application to determine the value.

[00148] All ranges disclosed herein are inclusive of the recited endpoint and independently combinable (for example, the range of “from 2 grams to 10 grams” is inclusive of the endpoints, 2 grams and 10 grams, and all the intermediate values).

[00149] The terms “about” and “approximately” can be used to include any numerical value that can vary without changing the basic function of that value. When used with a range, “about” and “approximately” also disclose the range defined by the absolute values of the two endpoints, e.g., “about 2 to about 4” also discloses the range “from 2 to 4.” Generally, the terms “about” and “approximately” may refer to plus or minus 10% of the indicated number.

[00150] Percentages of elements should be assumed to be percent by weight of the stated element, unless expressly stated otherwise.

[00151 ] Although the operations of exemplary embodiments of the disclosed method may be described in a particular, sequential order for convenient presentation, it should be understood that disclosed embodiments can encompass an order of operations other than the particular, sequential order disclosed. For example, operations described sequentially may in some cases be rearranged or performed concurrently. Further, descriptions and disclosures provided in association with one particular embodiment are not limited to that embodiment, and may be applied to any embodiment disclosed.

[00152] For the sake of simplicity, the attached figures may not show the various ways (readily discemable, based on this disclosure, by one of ordinary skill in the art) in which the disclosed system, method and apparatus can be used in combination with other systems, methods and apparatuses. Additionally, the description sometimes uses terms such as “produce” and “provide” to describe the disclosed method. These terms are abstractions of the actual operations that can be performed. The actual operations that correspond to these terms can vary depending on the particular implementation and are, based on this disclosure, readily discernible by one of ordinary skill in the art.

[00153] Although example embodiments have been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of the claims. For that reason, the following claims should be studied to determine their true scope and content.

[00154] It will thus be seen that the objects set forth above, among those made apparent from the preceding description, are efficiently attained, and since certain changes may be made in the constructions set forth without departing from the spirit and scope of the disclosure, it is intended that all matter contained in the above description and shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense. The disclosure has been described with reference to preferred and alternate embodiments. Modifications and alterations will become apparent to those skilled in the art upon reading and understanding the detailed discussion of the disclosure provided herein. This disclosure is intended to include all such modifications and alterations insofar as they come within the scope of the present disclosure. It is also to be understood that the following claims are intended to cover all of the generic and specific features of the disclosure herein described and all statements of the scope of the disclosure which, as a matter of language, might be said to fall therebetween. The disclosure has been described with reference to the preferred embodiments. These and other modifications of the preferred embodiments, as well as other embodiments of the disclosure, will be obvious from the disclosure herein, whereby the foregoing descriptive matter is to be interpreted merely as illustrative of the disclosure and not as a limitation. It is intended to include all such modifications and alterations insofar as they come within the scope of the appended claims.

[00155] To aid the Patent Office and any readers of this application and any resulting patent in interpreting the claims appended hereto, applicants do not intend any of the appended claims or claim elements to invoke 35 U.S.C. 112(f) unless the words “means for” or “step for” are explicitly used in the particular claim.