PRIORITY CLAIM

[0001] This disclosure claims priority to United States Provisional Application Serial Nos. 62/690,071 filed on June 26, 2018, United States Provisional Application Nos. 62/702,411, 62/702,401 and 62/702,429 all filed on July 24, 2018, all of which are incorporated by reference in their entirety.

TECHNICAL FIELD

[0002] This disclosure relates to a sonotrode or“horn” for use in ultrasonic welding applications, for example.

BACKGROUND

[0003] In a typical ultrasonic welding application, a fixture supports a workpiece to be welded, which may comprise multiple plastic components. An ultrasonic welder typically includes a converter having a piezoelectric stack that selectively vibrates in response to power from a generator. A booster may be used at a working end of the converter to modify the amplitude of the vibrational frequency supplied by the converter. A hom is mounted to the booster opposite the converter and is used to impart vibration to the workpiece.

[0004] During a welding operation, the horn is advanced by a pneumatic cylinder to engage the workpiece. The pneumatic cylinder maintains a desired force on the workpiece via the hom. A controller energizes the generator for a time sufficient to weld the components to one another. The hom is retracted once the weld is complete.

[0005] Typical hom materials include steel, aluminum and titanium. The horns are constructed from extmded bar stock that is cut to length to provide blanks, which are then CNC lathe machined, for example, to a desired profile that corresponds to a desired design frequency. A computer software suite is often used to design a hom profile that will meet the desired design frequency, which may be between l5kHz and 40kHz, but the initial iteration of the machined hom is often not at the desired frequency.

[0006] One common plastic welding horn profile includes a narrow cylindrical shaft connected to a cylindrical base by an annular fillet. The base includes a threaded hole that is used to secure the horn to the booster, if one is used, or to the converter. A terminal end of the shaft is polished and includes a shape chosen for the type of welding operation. All external surfaces of the horn are machined by a cutting operation.

[0007] The converter, booster and horn are tuned for the overall effectiveness and efficiency in ultrasonic welding. The sonotrode has multiple modes that each have a resonant frequency. For ultrasonic welding, the sonotrode is designed to resonate at a longitudinal mode, which induces a particular displacement at the sonotrode tip used to generate heat and weld the workpiece. Typical machined horns are not repeatable part-to-part such that each hom must be checked to determine if it is at the desired resonant frequency at the longitudinal mode, otherwise a“near neighbor”, such as a twisting or a bending mode, may reach resonance. This results in the hom failing to achieve a sufficient displacement in the longitudinal direction, which can compromise the weld or damage the sonotrode over time. Accordingly, it is common to tune each individual horn after machining to ensure resonance at the desired longitudinal mode. Each horn is excited post-machining to determine its vibrational characteristics. The horn’s profile is then further machined to increase or decrease its vibrational frequency to match the desired design frequency for the given welding application.

SUMMARY

[0008] In one exemplary embodiment, a sonotrode includes multiple layers of a material melted to one another to form a structure. The structure provides a base that has an attachment feature that is configured to operatively secure to an ultrasonic converter. The structure includes a shaft that extends from the base to a terminal end that provides a working surface that is configured to selectively engage a workpiece.

[0009] In a further embodiment of the above, the structure includes an outer surface that is provided by a substantially unmachined surface.

[0010] In a further embodiment of any of the above, the unmachined surface is at least 50% of an area of the outer surface.

[0011] In a further embodiment of any of the above, the shaft and base are interconnected by an integral fillet. The fillet is provided by the unmachined surface.

[0012] In a further embodiment of any of the above, the structure has multiple shafts that include a first shaft that extends from the base to a first terminal end that provides a first working surface that is configured to selectively engage a workpiece. The multiple shafts include a second shaft that extends from the base to a second terminal end that provides a second working surface that is configured to selectively engage the workpiece.

[0013] In a further embodiment of any of the above, the first and second shafts are integrally formed with the base to provide an unbroken, monolithic construction.

[0014] In a further embodiment of any of the above, the base and the first and second shafts are constructed of the same material.

[0015] In a further embodiment of any of the above, the first shaft has a first length and the second shaft has a second length that is different than the first length.

[0016] In a further embodiment of any of the above, an internal cavity is substantially enclosed by the multiple layers and arranged interiorly of an exterior surface of the structure.

[0017] In a further embodiment of any of the above, a cooling passage is provided within the structure and formed in situ within the multiple layers.

[0018] In a further embodiment of any of the above, the cooling passage includes multiple passageways intersecting one another at non-perpendicular junctions.

[0019] In a further embodiment of any of the above, the cooling passage is curved and provides an extrados and an intrados at the junction.

[0020] In a further embodiment of any of the above, the structure has a density that varies across at least portions of the multiple layers by greater than 0.1%.

[0021] In a further embodiment of any of the above, the attachment feature is one of a stud and a threaded hole. The attachment feature has an unmachined external surface formed by the multiple layers.

[0022] In a further embodiment of any of the above, the structure extends in a longitudinal direction from the base to the working surface. The attachment feature is provided at a mounting face of the base. The mounting face has a first central point. The working surface has a second central point. The first and second central points are offset relative to one another with respect to the longitudinal direction.

[0023] In another exemplary embodiment, a method of manufacturing a sonotrode includes the steps of laser sintering layers of material to provide a structure having an outer surface, providing an attachment feature and a working surface at opposing ends of the outer surface, and leaving a majority of the outer surface unmachined to provide a sonotrode with desired tuning characteristics.

[0024] In a further embodiment of any of the above, the laser sintering step includes forming an internal cavity that is substantially enclosed by the multiple layers and arranged interiorly of the outer surface.

[0025] In a further embodiment of any of the above, the laser sintering step includes forming more than one of the sonotrodes on a common plate.

[0026] In a further embodiment of any of the above, the method includes the step of removing the sonotrodes from the plate. A frequency of each of the sonotrodes are within 0.75% of one another and of the desired design frequency subsequent to the removing step.

[0027] In another exemplary embodiment, an ultrasonic welding system includes an ultrasonic converter that is configured to vibrate at a desired frequency in response to a signal. A sonotrode includes multiple layers of a material melted to one another. The sonotrode provides a base that has an attachment feature operatively mounted to the ultrasonic converter. The structure includes a shaft that extends from the base to a terminal end that provides a working surface that is configured to selectively engage a workpiece.

BRIEF DESCRIPTION OF THE DRAWINGS

[0028] The disclosure can be further understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:

[0029] Figure 1 schematically illustrates a common ultrasonic welder.

[0030] Figure 2 depicts an example machine used to manufacture the disclosed sonotrode.

[0031] Figure 3A is an isometric view of one example sonotrode.

[0032] Figure 3B is an isometric view of an end of the sonotrode shown in Figure

3A.

[0033] Figure 4 is a schematic view of multiple sonotrodes printed on a plate.

[0034] Figure 5A schematically illustrates raw, laser sintered layers of the sonotrode.

[0035] Figure 5B depicts the sintered layers shown in Figure 5A after media blasting. [0036] Figure 6 is a flow chart illustrating an example method of manufacturing the disclosed sonotrode.

[0037] Figure 7 is a schematic view of an ultrasonic welding machine using at least one disclosed sonotrode to weld a workpiece.

[0038] Figure 8 depicts one example mother-daughter sonotrode.

[0039] Figure 9 illustrates a terminal end with a waffle pattern suitable for staking operations.

[0040] Figure 10 is a cross-sectional view through a sonotrode, illustrating multiple types of cavities and different length shafts.

[0041] Figure 11 is a cross-section through one example sonotrode illustrating a fluid flow feature.

[0042] Figure 11A is a partial cross-sectional view of an end of a prior art sonotrode.

[0043] Figure 12A is a partial perspective view of a base of the sonotrode shown in Figure 11.

[0044] Figure 12B is a partial perspective view of an end of the sonotrode shown in Figure 11.

[0045] Figure 12C is an enlarged cross-sectional view of another example sonotrode end.

[0046] Figure 13 is an isometric view of another example sonotrode illustrating a corkscrew cooling passage.

[0047] Figure 14A is a partial cross-sectional view of one example cooling passage restriction.

[0048] Figure 14B is a partial cross-sectional view of another example cooling passage restriction.

[0049] Figure 15 is a perspective view illustrating a sonotrode end with porosity extending to the external surface to provide a cooling passage outlet.

[0050] Figure 16 is a partial perspective view illustrating an annular cooling passage.

[0051] Figure 17A and 17B depict example attachment features for a sonotrode. [0052] Figure 18 illustrates a denser region containing a nodal point to provide strengthening.

[0053] Figure 19 shows an integrated fluid attachment·

[0054] Figure 20 illustrates circumferentially spaced holes formed during the laser sintering process and configured to receive a tool for installation of the sonotrode.

[0055] Figure 21 depicts a unitary booster and sonotrode that are produced together in the same laser sintering process.

[0056] Figure 22 illustrates a sonotrode with a terminal end offset from the base.

[0057] Figure 23 shows an internal cavity that has a larger diameter than the mounting face to provide a“drum effect” when excited by the generator.

[0058] The embodiments, examples and alternatives of the preceding paragraphs, the claims, or the following description and drawings, including any of their various aspects or respective individual features, may be taken independently or in any combination. Features described in connection with one embodiment are applicable to all embodiments, unless such features are incompatible. In many instances, like numerals (e.g., 34, 134, 234, etc.) are used to indicate like features.

DETAILED DESCRIPTION

[0059] An example ultrasonic welder 10 is shown in Figure 1. The welder 10 is typically used to join multiple components of a workpiece 14 that is supported in a fixture 12. In one example, the workpiece 14 includes plastic automotive components. It should be understood that the ultrasonic welder 10 can be used in other applications, such as packaging and food processing, for example. The disclosed sonotrode can be used with other materials.

[0060] A sonotrode 20 selectively engages the workpiece 14 to impart a vibration on the workpiece 14 sufficient to generate heat and melt the components to one another. To this end, the sonotrode 20 is operatively secured to an ultrasonic converter 16, which includes piezoelectric or other elements that vibrate (e.g., at up to 50 kHz) in response to a signal from a generator 22 commanded by a controller 24. The sonotrode 20 may be designed to be used at other frequencies, if desired. A booster 18 may be mounted between the converter 16 and the sonotrode 20 to tune the frequency provided by the converter 16 to the sonotrode 20. The sonotrode 20 has a shaft 34 that extends from a base 32 to a terminal end 38. A fillet 36 provides a transition between the base 32 and the shaft 34.

[0061] During operation, a cylinder 26, which may be pneumatic, advances the sonotrode 20 to engage the surface 40 of the workpiece 14 with the terminal end 38 and maintain a contact pressure. Cylinder movement may be regulated by a valve 30 that selectively controls the flow of compress air from an air source 28 to the cylinder 26 in response to a command from the controller 24. The welder 10 can be configured in a different manner than described.

[0062] The sonotrode 20 is manufactured using a three dimensional printing process, such as direct metal laser sintering (DMLS). One example DMLS machine is an EOS 290. An example DMLS machine 50 is schematically shown in Figure 2. Multiple layers 54 of a material 66 are deposited onto a plate 52 in an enclosed environment 56 filled with a shielding gas 58. As each layer 54 is laid down by a depositing element 62 onto the prior layer, a scraper or roller 68 levels the deposited layer to a desired layer thickness, for example, 20-60 pm. The scraper 68 does not provide any significant compacting, that is, the material 66 does not“stick” to itself, and is primarily used to level the layer.

[0063] A hopper 64 supplies the material 66 to the depositing element 62. The material 66 is at least one of titanium (e.g., Ti 6-4), aluminum and steel, including stainless steel. In one example, the material consists of only one of titanium, aluminum and steel. The material 66 comprises spherically shaped particles of varying sizes, which enables close packing of the particles resulting in maximum density.

[0064] The DMLS machine 50 is provided three dimensional CAD data 72 relating to a structure 70 to be manufactured, i.e., the sonotrode 20. The CAD data is parsed into cross- sections that correspond to the layers 54. A computer guided laser 60 sinters the layers 54 together to provide the structure 70 layer-by-layer. In one example, the laser 60 may move at speeds up to 7 m/s. Control parameters 74, such as laser speed and/or intensity, may be varied to achieve desired characteristics of the structure 70, such as density. In one example, the density of the structure 70 is 99.95% of a similarly sized component of the same chemical makeup. In the example, substantially uniform density is maintained in the sonotrode 20 from the base 32 to the terminal end 38. [0065] Multiple parts, i.e., sonotrodes 20, are manufactured on a common plate 52, as shown in Figure 4. Since the parts are laser welded to the plate 52 during one example printing process, the parts must be removed from the plate, such as by wire electrodischarge machining (EDM).

[0066] An example sonotrode 20 produced by a DMLS machine 50 is shown in Figures 3A-3B. The sonotrode 20 is constructed on the plate 52 from the base 32 to the terminal end 38 along a longitudinal direction 80, although other build orientations may be used. The base 32, the fillet 36 and the shaft 34 respectively extend in the longitudinal direction 80 first, second and third lengths 82, 84, 86. The base 32 includes a generally planar mounting face 88 that has an attachment feature 90, such as a threaded hole. The attachment feature 90 is used to secure the sonotrode 20 to the converter 16 or the booster 18, for example.

[0067] The terminal end 38 provides a working surface 92 that is configured to engage the workpiece 14 during ultrasonic welding. In the example, the working surface 92 is provided by a machined surface 98, which includes geometry adapted for the particular application. One example is a dimple 94, or raised area, that extends from a concavity 96, or recessed area. Such a geometry is suitable for upsetting a plastic component during welding under the pressure of the cylinder 26. The disclosed sonotrode can be used with other materials.

[0068] The sonotrode 20 has an outer surface 100 that is significantly rougher than the machined surface 98. In one example, the machined surface 98 has an average surface roughness of less than 30 Ra, for example, less than 10 Ra. As shown in Figures 5A-5B, the outer surface 100 has an unmachined surface 104. The laser sintering process may result in scale 102 or undesired remnants at the periphery of the outer surface 100; the outer periphery circumscribes the longitudinal direction of the shaft 34. Media blasting, such as by using glass beads or other material, can remove this scale 102 providing a smoother media-blasted surface 106. In this disclosure,“machining” does not include media blasting; rather,“machining” is interpreted as cutting with a cutting tool carried by a cutting fixture, such as by a CNC mill or lathe or a grinding machine. Even so, the average surface roughness of the unmachined surface is greater than 150 Ra, for example, 150-450 Ra. In one example, the unmachined surface has an average surface roughness of 325 Ra +/- 10% and the machined surface has an average surface roughness of 3.2 Ra +/- 50%. [0069] A sonotrode manufacturing method 110 is shown in Figure 6. The method 110 includes the step of laser sintering layers 54 to form the sonotrode 20 according to CAD data 72, as indicated in block 112. The sonotrodes 20 are removed from the plate 52, for example, by wire EDM. The sonotrode 20 may then media blasted to remove undesired remnants, as indicated at block 114, or this step may be omitted. The working surface 92 is machined (block 116) while the majority of the outer surface 100 is left unmachined (block 118) to produce a finished sonotrode having desired tuning characteristics for the welder 10 (block 120).

[0070] It is possible that the working surface 92 need not be machined and step 116 omitted if, for example, the layers at the tip are deposited and sintered at a finer resolution, i.e., using thinner layers. That is, some layers may be, for example, 60 pm, and the layers at the tip may be 20-30 pm or less. The finer resolution will result in a smoother surface finish at the working surface 92 providing a suitable Ra for plastic welding.

[0071] Unlike prior methods of manufacturing sonotrodes, a substantial area of the outer surface 100 of the sonotrode 20 is provided by an unmachined surface 104. In one example, at least 50% is unmachined, and in another example, at least 75% is unmachined. In still another example sonotrode, at least 90% of the outer surface 100 is unmachined, for example, 95% or more, but less than 100%, for example. The outer surface of the base 32, shaft 34 and fillet 36 is left unmachined, in one embodiment. Machining of the mounting face 88 may also be omitted (i.e., left as an unmachined surface) with precise laser sintering of the layers 54, although a machining process may be used if desired to smooth the surface after cutting the sonotrodes from the plate 52.

[0072] According to the disclosed manufacturing method, the sonotrode is laser sintered with the desired tuning characteristics such that the typical machining is not needed. The desired tuning characteristics correspond to transmitting a desired frequency to the workpiece 14 via the working surface 92. The homogeneous properties of the powdered material within a batch and batch-to-batch is quite uniform and the DMLS process is very precise such that harmonics of the end sonotrode are highly repeatable. Sonotrodes of the same part number produced on a common plate and/or plate-to-plate are within 0.75% (e.g., for approximately a 20 kHz converter) of the longitudinal mode resonant frequency of one another and of the desired design frequency for the longitudinal mode so that the individual sonotrodes need not be tuned after manufacturing. In another example, the sonotrodes are repeatable within 0.50% (e.g., for approximately a 35 kHz converter) of one another and the desired frequency, and in another example the sonotrodes are repeatable within 0.25% (e.g., for approximately a 40 kHz converter) of one another and the desired frequency. That is, the sonotrode frequency need not be checked and then machined for being out of frequency, as is commonplace with current sonotrode manufacturing practices in order to avoid resonating at undesired near neighbor modes. Said another way, no more that one machining operation is used at the terminal end to provide the initial surface finish to the working surface, nor is machining needed on unmachined surfaces at other locations on the sonotrode; additional machining of the sonotrode is not required to bring the sonotrode within the desired frequency.

[0073] As shown in Figure 7, a typical workpiece 14’ may include multiple weld points that are welded simultaneously during the manufacturing operation. The workpiece 14’ is held in a fixture, and the sonotrodes 20, 20’ are respectively operatively mounted to converters 16, 16’. The sonotrodes are advanced and excited to weld the components to one another, as described in connection with Figure 1. The performance and/or efficiency of the sonotrodes 20, 20’ may be improved by incorporating one or more internal cavities 122, 122’, which may be used for cooling, lightening or other performance enhancing effects. In one example, the sonotrodes may be lightened such that smaller converters may be used, which may significantly lower the overall cost of the welding system.

[0074] As shown in Figure 7, some sonotrodes 20’ have multiple points, referred to as“mother-daughter”, such that a single sonotrode may be used to weld multiple weld points. That is, the base 232 includes multiple shafts 234 that each provide a terminal end 238 for welding. More than one attachment feature 290 may be provided on the base 232 depending upon its size. Thus, a first shaft extends from the base to a first terminal end providing a first working surface configured to selectively engage a workpiece, and a second shaft extends from the base to a second terminal end providing a second working surface configured to selectively engage the workpiece. The first and second working surfaces are spaced apart and discrete from one another.

[0075] As shown in Figure 9, the working surface has multiple raised features providing an increased surface area as compared to a planar working surface bounded by a correspondingly sized and shaped periphery. For example, the working surface of the terminal end 238 may include a waffle or PIP pattern 60, which may be entirely or substantially (e.g., greater than 50%) 3D-printed rather than machined, if desired.

[0076] A typical multi-point sonotrode is constructed from shafts that are discrete and separate from the base. The shafts and base are separately manufactured, and then the shafts are secured to the base, for example, by a stud. One common type of multi-point sonotrode manufactures the base from a light weight material, such as aluminum, and the shafts of a more durable material, such as steel or titanium. By way of contrast, the disclosed multi point sonotrode forms the first and second shafts integrally with the base to provide an unbroken, monolithic construction.

[0077] In one example, the base 232 and the shafts 234 are constructed of the same material, such as titanium or steel, which are relatively heavy compared to aluminum. The heavy base 232 may be lightened by incorporating one or more substantially enclosed internal cavities 262 or substantially open cavities 264, for example, as shown in Figure 10, that are provided within the structure and formed in situ within the multiple layers 54 (Fig. 2). The cavity 264 is surrounded substantially entirely by the multiple layers 54 and arranged interiorly of an exterior surface of the structure (e.g., outer surface 100; Figs. 5A-5B). The substantially enclosed internal cavity (e.g., at least 75%, and in another example, at least 90%) may include at least a small hole sufficient to permit the unsintered powder to escape the cavity subsequent to printing. A fully, 100% enclosed cavity would otherwise retain all of the loose powder. In one example, the base 232 includes at least one opening that extends laterally from one side through to another side (e.g., substantially open cavity 264) in a direction that is at an angle to the longitudinal direction of the shafts 234.

[0078] Various portions of the sonotrode may be manufactured to vary the characteristics of the portions. With continuing reference to Figure 10, at least two of the shafts extend in a longitudinal direction and have lengths that are different than one another. In another example, the base 232 has a first density and at least one of the shafts 234 has a second density that is different than the first density. The density of the shafts may also be varied among one another such that the density of one shaft is greater than the density of another shaft. The greater density may be achieved through porosity differences and/or by varying the thickness of the sintered layers, for example. [0079] The disclosed mother-daughter are provided by a single piece, without separate discrete shafts as is typical in prior art arrangements. There is no complicated set up procedure as the multiple shafts are provided as an integrated inseparable structure with the base. Moreover, a potential failure mode at the prior threaded connection between the mother- daughters is eliminated.

[0080] The base can be made lighter than the shafts by incorporating one or more cavities or forming the base in a less dense manner than the shafts during the laser sintering process. The cavities may be internal, external or a combination thereof. This ensures that the base is not too heavy to excite to achieve the desired frequency and amplitude, which enables a smaller, less costly generator.

[0081] Internal cavities may also be used to provide cooling passages that are not possible based upon known sonotrode manufacturing techniques. Referring to Figure 11, a cooling passage 350 is fluidly connected to the air source 28 (Fig. 1) at one or more inlets 352. A portion of the cooling passage 350 is curved from the inlet 352 to a junction 354 where the cooling passage 350 extends longitudinally within the shaft 334 to one or more outlets 370 at an end of the shaft 334.

[0082] The cooling passage 350 includes an intrados 356 and an extrados 358, which extend to the junction 354 in the example. Where multiple portions of the cooling passage 350 extend from multiple inlets 352, a peak 360 may be formed. This smooth transition of intersecting passageways reduces restrictions and associated losses within the cooling passage 350, providing more efficient use and delivery of the cooling fluid.

[0083] The cooling passage 350 may include a venturi 362 provided by first and second tapered portions 364, 366 joined at a throat 368. The venturi 362 increases velocity and reduces pressure downstream from the throat 368, which may be beneficial for cooling the terminal end 338. A diffuser provided by a single taper may also be used, if desired.

[0084] The portion of the cooling passage 350 extending to the outlet 370 may be at a non-perpendicular angle with respect to the longitudinally extending portion within the shaft 334. A protrusion 372 may be provided where multiple outlet portions are joined to one another. Thus, fluid exiting the venturi 362 may impinge upon the protrusion 372, which provides increased cooling surface and, thus, increased cooling of the terminal end 338. The cooling may further be enhanced by providing one or more roughened or dimpled surfaces 376 to enable heat to dissipate more quickly near the terminal end, as shown in Figure 12C. These configurations provide smoother fluid flow and reduced losses as compared with intersecting, straight passages as is found in drilled cooling passages of prior art horns (Fig. 11 A). Such configurations may, at best, may have a dimple 374 provided as an artifact of drilling the cooling passage 350, which is not repeatable and has minimal effect. Moreover, conventional drilled features may lead to stress risers that result in failure of the sonotrode from repeated cycling.

[0085] Other fluid flow- and cooling-enhancing features may be incorporated into the sonotrode, as shown in Figures 13-16. These features, which are much more elaborate than possible with conventional drilling operations, are formed in situ during the laser sintering process of the multiple layers of material. Figure 13 illustrates a spiral or corkscrew cooling passage 378 which provides increased length and surface area in addition to providing a swirling motion of fluid exiting the outlet 370.

[0086] Figures 14A and 14B illustrate restrictions that may create a Joule- Thompson effect. In the example shown in Figure 14A, a porous plug or blockage 380 is provided in the cooling passage 350, separating the passage into first and second passageways 350A, 350B. In the example shown in Figure 14B, the restriction is provided by a valve or orifice 382 that throttles the fluid flow. As a result of the restriction, the temperature downstream of the restriction is reduced.

[0087] Figure 15 illustrates an arrangement in which an end of the shaft 334 near the terminal end 338 incorporates external porosity 384 intentionally created during the 3D laser sintering that extends radially inward to fluidly connect to the cooling passage 350. The porosity is like a“fish filter” and provides diffuse, distributed flow at the outlet of the cooling passage 350. The porosity 384 may extend about the entire circumference of the shaft 334 or just portions of its circumference.

[0088] Another cooling configuration is shown in Figure 16. An annular passage 386 is arranged in the base 332, the annular passage 386 received fluid from the inlet 352 and is fluidly connected to multiple secondary passages 388 that deliver cooling fluid to fillet 336, which expels the fluid through the outlet 372 and down the exterior of the shaft 334. The secondary passages may be angled or otherwise shaped to generate a vortex of cooling fluid down the shaft 334. [0089] The above-described cooling features can provide improved cooling of the sonotrode, which increases duty cycle, improves weld quality thereby eliminating the need for external vortex coolers that are sometimes used on high duty cycle applications.

[0090] Referring to Figures 17A and 17B, the attachment feature 490 arranged at the mounting face 432 is provided by an unmachined external surface formed by the multiple layers. That is, the attachment features 490 are not machined by a cutting tool, but rather formed during the DMLS process. In the examples, the attachment feature 490 is one of a stud (Fig. 17 A) and a threaded hole (Fig. 17B).

[0091] As described, the density within the sonotrode may be varied. In one example, it may be desirable to vary the density across at least portions of the multiple layers by greater than 0.1%, for example. The ultrasonic converter 16 (Fig. 1) is configured to induce a vibratory frequency in the structure that produces a wave form having at least one nodal point, as schematically illustrated in Figure 18. The nodal points in the shaft 434 experience greater stresses. In one example, the wave form is configured to flow in a direction that runs primarily through the multiple layers, although other layer orientations may be employed. The structure has a greater density in a region 494 of the structure with the nodal point than in adjacent regions 492, which provides increased strength at the nodal point.

[0092] Increased strength may also be provided at the tip of the sonotrode. In one example, it is desirable to have a greater density and/or less porosity or voids at the terminal end and the working surface as compared to adjacent structure in the shaft. For example, a first portion of the structure extending from the working surface to 10% of the length has a first density, and the adjacent structure has a second density that is less than the first density.

[0093] Referring to Figure 19, the sonotrode, for example, the base 432, has a fluid attachment 496 provided at the outer surface by the multiple layers, i.e., integral with the sonotrode and without machining. The fluid attachment 496, which may be near the fillet 436, is in fluid communication with an internal fluid passage 450. In the example, the fluid attachment 496 is a barb configured to connect to a fluid line to the air source 28 (Fig. 1).

[0094] The base 432 may include circumferentially spaced holes 498 each provided by an unmachined external surface formed by the multiple layers, i.e., integral with the sonotrode and without machining, as shown in Figure 20. An installation tool cooperates with the holes 498 to torque the sonotrode relative to the converter 16 (Fig. 1). [0095] Referring to Figure 21, the attachment feature is not provided by a stud or threaded hole, but is instead an integral transition to a booster 418 configured to attenuate a frequency from the ultrasonic converter 16 (Fig. 1). In the example, the booster 418, the base 432 and the shaft 434 provide a monolithic, unitary structure.

[0096] As shown in Figure 22, the sonotrode extends in a longitudinal direction from the base 432 to the working surface of the terminal end 438. The longitudinal direction is perpendicular to at least one of the mounting face and the working surface. The mounting face has a first central point 499, and the working surface has a second central point 400, such that the first and second central points 499, 400 are offset relative to one another with respect to the longitudinal direction. In this manner, the working surface may be positioned in difficult to reach work areas that would not be feasible using traditional sonotrode manufacturing methods.

[0097] Figure 23 depicts an internal cavity 402 that has a larger diameter D than the diameter d of the mounting face to provide a“drum effect” when excited by the generator.

[0098] It should also be understood that although a particular component arrangement is disclosed in the illustrated embodiment, other arrangements will benefit herefrom. Although particular step sequences are shown, described, and claimed, it should be understood that steps may be performed in any order, separated or combined unless otherwise indicated and will still benefit from the present invention.

[0099] Although the different examples have specific components shown in the illustrations, embodiments of this invention are not limited to those particular combinations. It is possible to use some of the components or features from one of the examples in combination with features or components from another one of the examples.

[00100] Although an example embodiment has 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.