Enhanced welded pipe, threaded connections, and methods for achieving the same

Patent metadata

Field	Value
Publication number	US-10961787-B2
Application number	US-201815883722-A
Country	US
Kind code	B2
Filing date	Jan 30, 2018
Priority date	Jan 30, 2017
Publication date	Mar 30, 2021
Grant date	Mar 30, 2021

Abstract

A tubular member includes a tube body, a tube end, an exterior surface, an interior surface, a nominal wall thickness, a longitudinal axis, a welded seam, and a patch of material. The welded seam forms an arcuate portion of the interior surface, and the patch covers a portion of the interior surface that includes a portion of the welded seam, extending from the tube end to an axially spaced first location. The resulting interior surface from the tube end to the axially spaced first location has a uniform inside diameter.

First claim

What is claimed is:

1. A method for modifying a tubular member having a tube end, an exterior surface, an interior surface, a nominal wall thickness, a central axis, and a welded seam, wherein the welded seam forms a portion of the interior surface, the method comprising:
applying an arcuate patch of weld material to the interior surface, wherein the patch covers an arcuate segment of less than an entire circumference of the tubular member along the interior surface at the location of the arcuate patch, wherein the arcuate segment includes the welded seam and extends axially from the tube end to an axially spaced first location; and
machining the patch such that the interior surface of the tubular member from the tube end to the axially spaced first location has a uniform inside diameter.

2. The method of claim 1 wherein the patch is machined such that, in an axial cross section of the tubular member taken between the tube end and the axially spaced first location, the wall thickness is uniform around the circumference of the tubular member.

3. The method of claim 2 further comprising: blanking-in the exterior surface by machining the tubular member to taper from a minimum wall thickness adjacent the tube end to a greater thickness at a second location that is axially spaced from the tube end.

4. The method of claim 3 further comprising: machining threads on the exterior surface after blanking-in the exterior surface;
wherein the threads include a root surface; and
wherein the uniform wall thickness extends radially at least from interior surface to the root surface.

5. The method of claim 4 further comprising: securing the tubular member in a machine and, before removing the tubular member from the machine, machining the patch, blanking-in the exterior surface, and machining the threads on the exterior surface.

6. The method of claim 4 wherein the method further comprises: engaging threadingly a pin end of a first tubular member and a box end of a second tubular member;
wherein engaging threadingly includes forming a circumferentially extending interference fit between a non-threaded portion of the pin end and a non-threaded portion of the box end, the non-threaded portion of the pin end including a portion of the patch.

7. The method of claim 6 wherein the outside diameter of the box end is the same as the outside diameter of the first tubular member.

8. The method of claim 6 wherein the outside diameter of the box end of the second tubular member is greater than the outside diameter of the first tubular member.

9. The method of claim 8 wherein the box end comprises a forging that is welded to a non-threaded end of the second tubular member.

10. The method of claim 1 wherein applying the patch comprises welding a first layer of weld material to the interior surface, and welding a second layer of weld material to the first layer.

11. The method of claim 10 wherein, measured radially, the first layer has a thickness T 1 before machining the patch, and the second layer has a thickness T 2 before machining the patch; and
wherein machining the patch removes all of T 2 and a portion of T 1 .

12. The method of claim 10 wherein welding the first layer is performed at a first heat input; and
wherein welding the second layer is performed at a second heat input that differs from the first heat input.

13. The method of claim 10 wherein applying a first layer of weld material comprises applying a plurality of weld passes, each of the weld passes contacting another of the weld passes that is adjacent.

14. The method of claim 13 wherein each of the weld passes extends circumferentially and contacts another of the weld passes that is axially adjacent.

15. The method of claim 10 wherein the patch comprises a pair of circumferentially spaced ends, and a radial thickness; and
wherein machining the patch comprises tapering the radial thickness of the patch at the circumferentially spaced ends.

16. The method of claim 15 wherein tapering the radial thickness of the patch comprises tapering the radial thickness of the patch so that an inner surface of the patch is flush with the interior surface of the tubular member at the circumferentially spaced ends.

17. The method of claim 16 wherein the machining comprises machining the inner surface of the patch to be disposed at the uniform inside diameter with a remaining portion of the interior surface of the tubular member that is not covered by the patch.

18. The method of claim 17 wherein the tubular member comprises a uniform wall thickness around the circumference.

19. The method of claim 1 wherein applying the patch comprises welding the patch using a heat input not greater than 50 kilo-Joules per inch of weld length.

20. The method of claim 1 further comprising: blanking-in the interior surface by machining the tubular member to taper from a minimum wall thickness adjacent the tube end to a greater thickness at a second location that is axially spaced from the tube end; and
machining threads on the interior surface after blanking-in the interior surface.

21. The method of claim 1 further comprising: swaging the tubular member adjacent the tube end, resulting in the tube end being expanded in diameter.

22. The method of claim 1 further comprising: swaging the tubular member adjacent the tube end, resulting in the tube end being contracted in diameter.

23. The method of claim 1 wherein the patch comprises a pair of circumferentially spaced ends, and a radial thickness, and wherein machining the patch comprises machining the patch to taper the radial thickness at the circumferentially spaced ends.

24. The method of claim 23 wherein applying the patch comprises welding a first layer of weld material to the interior surface, and welding a second layer of weld material to the first layer.

25. The method of claim 24 wherein welding the first layer of weld material comprises applying a plurality of weld passes, each of the weld passes contacting another of the weld passes that is axially adjacent.

26. The method of claim 25 wherein machining the patch comprises tapering the radial thickness of the patch so that an inner surface of the patch is flush with the interior surface of the tubular member at the circumferentially spaced ends.

27. The method of claim 23 further comprising:
blanking-in the interior surface by machining the tubular member to taper from a minimum wall thickness adjacent the tube end to a greater thickness at a second location that is axially spaced from the tube end; and
machining threads on the interior surface after blanking-in the interior surface.

28. The method of claim 1 wherein the patch comprises a pair of circumferentially spaced ends, and a radial thickness, and wherein machining the patch comprises machining the patch to taper the radial thickness at circumferentially spaced ends so that an inner surface of the patch is flush with the interior surface of the tubular member at the circumferentially spaced ends.

29. The method of claim 28 wherein the machining comprises machining the patch such that, in an axial cross section of the tubular member taken between the tube end and the axially spaced first location, the wall thickness is uniform around the circumference of the tubular member.

30. The method of claim 29 further c

Assignees

• Nat Oilwell Vareo L P
• Nat Oilwell Varco Lp

Inventors

• Ethridge Roger Edward
• Desadier Christopher E

Classifications

• F16L9/02

  of metal (F16L9/16 - F16L9/22 take precedence) · CPC title

• B29C66/52

  Joining tubular articles, bars or profiled elements · CPC title

• B21C37/0811

  removing or treating the weld bead · CPC title

• B23K15/0053

  Seam welding · CPC title

• E21B17/00

  Drilling rods or pipes; Flexible drill strings; Kellies; Drill collars; Sucker rods; {Cables;} Casings; Tubings · CPC title