CROSS REFERENCE TO RELATED APPLICATIONS

[0001] This application claims the benefit of an earlier filing date from U.S. Provisional Application Serial No. 60/602,573 filed August 18, 2004, the entire disclosure of which is incorporated herein by reference.

BACKGROUND

[0002] Coring is an integral part of hydrocarbon exploration and recovery activities because it provides material from specific subterranean regions for analysis. This in turn helps the ultimate goal of hydrocarbon (or other target fluid) recovery. [0003] Coring devices are known to the art and include a core bit, a core barrel and in many cases a barrel liner. Barrel liners help keep the core in a more pristine condition, which assists in the overall information gainable therefrom. On the negative side however once the core barrel is removed from the well to retrieve the core sample, the liners are cut either into segments of predetermined length or open (often by circular saws) along their lengths to expose the core. The act of cutting the liner open is often detrimental to core integrity and additional tends to contaminate the core with metal cuttings and cause thermal damage as well. [0004] Since contamination reduces analytical accuracy, rendering suspect the reliability of information obtained by the analysis, present methods of coring are less than ideal.

SUMMARY [0005] Disclosed herein is a coring tubular. The tubular has a body, at least one opening hole radially oriented in the tubular body and a parting line in the tubular body. [0006] Further disclosed herein is a method for reducing contamination of a core sample. The method includes installing a coring tubular having features set forth in the foregoing paragraph in a coring tubular, running the core tubular to obtain a

INT-0008 1 564-39391 -US sample and exposing the core by prying the tubular open at an opening hole along the parting line.

BRIEF DESCRIPTION OF THE DRAWINGS [0007] Referring now to the drawings wherein like elements are numbered alike in the several figures: [0008] Figure 1 is a plan view of a liner as disclosed herein illustrating parting line and axial shear arrangement; [0009] Figure 2 is an enlarged view of circumscribed portion 2 of Figure 1; [0010] Figure 3 is a plan view of Vi of the liner of Figure 1 and taken along line 3-3; [0011] Figure 4 is a schematic view of an uphole end of the liner with assembled support structures; [0012] Figure 5 is a schematic view of a downhole end of the liner with assembled support structures; and [0013] Figure 6 is a schematic view of a cross section of the liner with perforations of varying depth.

DETAILED DESCRIPTION [0014] Referring to Figure 1, a plan view of a coring tubular, depicted as an inner barrel liner 10, is illustrated. Liner 10 includes a parting line 12 where the material of liner 10, usually metal such as aluminum or steel (or could be other materials having properties consistent with the purpose of the liner 10), is rendered easily defeatable. This can be accomplished by perforating the liner at intervals, which may be regular. The perforations 8 (see Figure 6) may pass completely through the material thickness of the liner or may extend merely partly through the material thickness of the liner. The parting line is not intended to be cut all the way through the material thickness at all points. In order to be considered a "parting line" for purposes of this invention, there must be connection across the parting line at least in some places such that there is some structural connection across the parting line. This definition does not include adhesively backed material wrapped around a liner that is formed of two or more pieces and then "taped" together with such adhesive backed material. The perforation may be of any geometric shape such as circular, rectangular, etc. and may be such as to account for more space than the material of the

INT-0008 2 564-39391 -US liner left in place (i.e. merely tabs of the liner are left after perforation). The easily defeatable nature of parting line 12 can also be created by causing the material of liner 10 to be thinner at the location of the parting line. Yet another means by which the desired property of the parting line can be accomplished is through the use of alternate materials at the line or alternate composition or structure of the same material at the parting line. The overriding requirement is that the parting line 12 be easily defeatable thereby rendering the liner 10 easily openable without resort to machines, which might otherwise contaminate the sample core contained within the liner 10 (at the time the liner is to be opened by introduction of contaminants or heat from the rapidly moving blade). [0015] In addition to the parting line, one embodiment hereof provides one or more opening holes 14. Opening holes 14 are in one embodiment sized for easily available hand tools such as a screwdriver, small pry bar etc. In the illustrated embodiment, (for a screw driver) the length and width of the opening holes 14 are sufficient to easily allow insertion of the screw driver therein but small enough to allow the screw driver to lever the liner apart along the parting line 12 with a twisting motion of the screwdriver. Proportional dimensions would be employed if it is intended that a crow bar be used to pry the liner open. Opening holes 14 are provided during the manufacturing process and therefore the sizes thereof are fixed. In one embodiment, (not specifically shown) several different sizes of holes 14 are provided for ease of opening along the parting line with whatever tool is handy to the final user. In the illustrated embodiment several opening holes 14 are provided along parting line 14 to allow sequential "popping" open of the parting line or to allow several people to pry the liner open at the same time. The opened liner 10 is visible in Figure 3. [0016] Referring now to Figure 2, one element of parting line 12 in one embodiment is illustrated in enlarged form. This element is a shear arrangement 16. It is to be understood that the liner could be constructed without the shear arrangement 16 even though the liner of Figure 1 does include the arrangement 16. The purpose of arrangement 16 is to prevent one half (or other percentage portion of the liner) of the liner 10 from moving axially relative to the other half (or other percentage portion of the liner) of liner 10 during the core capturing operation or core withdrawal operation. In the embodiment of Figure 2, a zig zag pattern of parting line 12 is provided for just this result. While many different angles of the zig zag pattern (including simple repeating angular patterns, alternating or otherwise changing angular patterns where INT-0008 3 564-39391 -US changes occur in either frequency or amplitude or both or even square toothed patterns for example) are employable with greater axial retention being provided by larger angles measured from the straight portion of the parting line, it has been found that about 45° is easily created and functions as intended. Shear arrangement 16 is in normal operation of liner 10 not used as the liner 10 is not easily susceptible to shear when the parting line is intact. In the event that parting line 12 is parted prematurely, shear movement of the liner can become detrimental to core integrity. It is in this situation that the shear arrangement 16 is put into service and is instrumental in avoiding problems with the core sample. [0017] In the assembled condition of a coring assembly wherein the liner as disclosed herein is utilized, the assembly is much like that of the prior art except that the shoe on bottom and plug on top end of the liner are slightly modified relative to the prior art. With reference to Figures 4 and 5, the distinction between the shoes of the prior art and those employed herein is discussed. The uphole end of the liner is illustrated in Figure 4 while the downhole end is illustrated in Figure 5. Referring to Figure 4, the liner 10 is illustrated being supported at an inside dimension thereof by a pressure relief plug 20. One of ordinary skill in the art will recognize the relief plug because it is almost identical to such plug as was used in the prior art. The only difference in this plug is that the outside dimension thereof is larger than the prior art. It is larger by about a 5/8 inch over the diameter thereof so that a clearance of about 3/32 inch is available between the liner 10 and the plug 20. The clearance is identified at 22. As the balance of the plug is known, no further discussion thereof is necessary. [0018] Referring to Figure 5, the downhole end of liner 10 is illustrated in assembled form with a coring assembly so that the unique support therefore may be appreciated. One of ordinary skill in the art will recognize the top end of inner barrel shoe 24 as it is similar to the prior art. The distinction between this component and its cousin in the prior art is that top end inner barrel shoe 24 has been bored out to create a liner receiver 26. One of skill in the art will note that top end inner barrel shoes of the art do not receive the liner. Rather, the liner stops at the thread 28 of the inner barrel 30. In this embodiment, and in order to provide additional support for the liner 10 and also an easy way to remove the liner from the coring assembly, the liner 10 is extended in overall length and the receiver 26 provided to receive that extended length. Clearance 32 is about 1/16 inch around the outside dimension of the liner for

INT-0008 4 564-39391 -US support and to take into consideration thermal expansion of the components at depth. The extended length of the liner 10 assists in disassembly of the liner from the balance of components of the coring assembly because it allows for the structure of the liner to be grasped by unscrewing the top end inner barrel shoe 24 from the inner barrel 30. Although not specifically shown, one can easily appreciate that unscrewing the identified sections and removing the top end inner barrel shoe will expose the portion of the liner 10 that extends downhole of the inner barrel 30. The liner 10 may then be grasped manually or by a tool to be withdrawn from the remainder of the inner barrel 30. [0019] While preferred embodiments have been shown and described, modifications and substitutions may be made thereto without departing from the spirit and scope of the invention. Accordingly, it is to be understood that the present invention has been described by way of illustrations and not limitation.

INT-0008 564-39391 -US