IP Library Granted Patent US 11,179,763
Granted Patent B2
US 11,179,763 · App. 15/896,759 · Granted Nov 23, 2021

Compressive forming processes for enhancing collapse resistance in metallic tubular products

Inventors: Peter W. Moore (Houston, TX); Bisen Lin (Katy, TX)
Assignee: United States Steel Corporation
B21D35/005B21B17/14B21B19/06B21B45/004B21D3/02B21D3/10B21D22/28B21H1/20C21D7/10C21D9/08
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Quick Facts
Patent No.
US 11,179,763
App. No.
15/896,759
Granted
Nov 23, 2021
Kind
B2
Abstract

A method to improve the collapse resistance of metallic tubular products is disclosed. Stress is applied to the metallic tubular products in order to change the residual stress profile of the metallic tubular products, such as those that have completed a straightening process, resulting in a residual stress profile that improves collapse resistance. The metallic tubular product is subjected to radial compression processing to control the residual stress profile and to enhance collapse resistance. The radial compression process may be applied after the tubular product has been subjected to a straightening process.

Claims (49)

1. A method of enhancing collapse resistance of a metallic hollow tubular product, the method comprising:

straightening a metallic hollow tubular product to produce a straightened metallic hollow tubular product having an outer diameter OD and an inner diameter ID;

radially compressing the straightened metallic hollow tubular product to produce a radially compressed metallic hollow tubular product having an outer diameter OD′ and an inner diameter ID′,

wherein the straightened metallic hollow tubular product has a compressive residual hoop stress adjacent to an inner surface thereof, and a tensile residual hoop stress adjacent to an outer surface thereof,

and wherein the radially compressed metallic hollow tubular product has a collapse resistance that is at least 2 percent greater than a collapse resistance of the straightened metallic hollow tubular product, and has:

(a) a substantially reduced compressive residual hoop stress adjacent to an inner surface thereof; or

(b) a tensile residual hoop stress adjacent to the inner surface thereof; and

the radially compressed metallic hollow tubular product has:

(a) a substantially reduced tensile residual hoop stress adjacent to an outer surface thereof; or

(b) a compressive residual hoop stress adjacent to the outer surface thereof.

2. The method of claim 1 , wherein the straightening is performed by rotary straightening or gag straightening.

3. The method of claim 1 , wherein the outer diameter OD′ of the radially compressed metallic hollow tubular product is at least 0.002 percent smaller than the outer diameter OD of the straightened metallic hollow tubular product, and the inner diameter ID′ of the radially compressed metallic hollow tubular product is at least 0.002 percent smaller than the inner diameter ID of the straightened metallic hollow tubular product.

4. The method of claim 3 , wherein the outer diameter OD′ of the radially compressed metallic hollow tubular product is from 0.002 percent to 0.2 percent smaller than the outer diameter OD of the straightened metallic hollow tubular product, and the inner diameter ID′ of the radially compressed metallic hollow tubular product is from 0.002 percent to 0.2 percent smaller than the inner diameter ID of the straightened metallic hollow tubular product.

5. The method of claim 1 , wherein the straightened metallic hollow tubular product has a wall thickness T W and the radially compressed metallic hollow tubular product has a wall thickness T′ W , and the wall thickness T′ W of the radially compressed metallic hollow tubular product is thicker than the wall thickness T W of the straightened metallic hollow tubular product.

6. The method of claim 4 , wherein the straightened metallic hollow tubular product has a D/t ratio of greater than or equal to 10:1 and less than or equal to 40:1.

7. The method of claim 1 , wherein the radially compressed metallic hollow tubular product has a residual hoop stress adjacent to the inner surface of from −10 to +30 percent of a yield strength of the radially compressed metallic hollow tubular product.

8. The method of claim 1 , wherein the radially compressed metallic hollow tubular product has a substantially reduced compressive residual hoop stress adjacent to the inner surface thereof.

9. The method of claim 1 , wherein the radially compressed metallic hollow tubular product has a tensile residual hoop stress adjacent to the inner surface thereof.

10. The method of claim 1 , wherein the radial compression is performed at an axial location along the straightened metallic hollow tubular product, with a radial compressive force acting on one side of a circumference of the straightened metallic hollow tubular product and is opposed by a radial compressive force acting on an opposite side of the circumference of the straightened metallic hollow tubular product.

11. The method of claim 10 , wherein, at the axial location along the straightened metallic hollow tubular product, the radial compressive force is applied circumferentially around contact areas totaling at least 180 degrees of the outer surface of the radially straightened metallic hollow tubular product.

12. The method of claim 1 , wherein the straightened metallic hollow tubular product is radially compressed by at least one set of opposing compression rollers to produce the radially compressed metallic hollow tubular product.

13. The method of claim 12 , further comprising a plurality of opposing compression rollers in an axial direction of the straightened metallic hollow tubular product.

14. The method of claim 1 , wherein the straightened metallic hollow tubular product is radially compressed by at least one set of three compression rollers to produce the radially compressed metallic hollow tubular product.

15. The method of claim 1 , wherein the straightened metallic hollow tubular product is radially compressed in a compression chamber to produce the radially compressed metallic hollow tubular product.

16. The method of claim 15 , wherein a stabilizing mandrel is placed inside the straightened metallic hollow tubular product before the straightened metallic hollow tubular product is radially compressed.

17. The method of claim 1 , wherein the straightened metallic hollow tubular product is radially compressed in a drawing die to produce the radially compressed metallic hollow tubular product.

18. The method of claim 1 , wherein the straightened metallic hollow tubular product is radially compressed in a forming die to produce the radially compressed metallic hollow tubular product.

19. The method of claim 1 , wherein the straightened metallic hollow tubular product is radially compressed at a temperature above ambient temperature.

20. The method of claim 1 , wherein the straightened metallic hollow tubular product is radially compressed at an ambient temperature.

21. A method of enhancing collapse resistance of a metallic hollow tubular product, the method comprising:

straightening a metallic hollow tubular product to produce a straightened metallic hollow tubular product having an outer diameter OD and an inner diameter ID;

radially compressing the straightened metallic hollow tubular product to produce a radially compressed metallic hollow tubular product having an outer diameter OD′ and an inner diameter ID′,

wherein the straightened metallic hollow tubular product has a compressive residual hoop stress adjacent to an inner surface thereof, and a tensile residual hoop stress adjacent to an outer surface thereof,

and wherein the radially compressed metallic hollow tubular product has a residual hoop stress adjacent to the inner surface of from −10 to +30 percent of a yield strength of the radially compressed metallic hollow tubular product, and has:

(a) a substantially reduced compressive residual hoop stress adjacent to an inner surface thereof; or

(b) a tensile residual hoop stress adjacent to the inner surface thereof; and

the radially compressed metallic hollow tubular product has:

(a) a substantially reduced tensile residual hoop stress adjacent to an outer surface thereof; or

(b) a compressive residual hoop stress adjacent to the outer surface thereof.

22. A method of enhancing collapse resistance of a metallic hollow tubular product, the method comprising:

straightening a metallic hollow tubular product to produce a straightened metallic hollow tubular product having an outer diameter OD and an inner diameter ID;

radially compressing the straightened metallic hollow tubular product by at least one set of opposing compression rollers to produce a radially compressed metallic hollow tubular product having an outer diameter OD′ and an inner diameter ID′,

wherein the straightened metallic hollow tubular product has a compressive residual hoop stress adjacent to an inner surface thereof, and a tensile residual hoop stress adjacent to an outer surface thereof,

and wherein the radially compressed metallic hollow tubular product has:

(a) a substantially reduced compressive residual hoop stress adjacent to an inner surface thereof; or

(b) a tensile residual hoop stress adjacent to the inner surface thereof; and

the radially compressed metallic hollow tubular product has:

(a) a substantially reduced tensile residual hoop stress adjacent to an outer surface thereof; or

(b) a compressive residual hoop stress adjacent to the outer surface thereof.

Assignments (3)
RELEASE OF SECURITY INTEREST Recorded Mar 31, 2021
From: U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGENT
To: UNITED STATES STEEL CORPORATION; U. S. STEEL TUBULAR PRODUCTS, INC.
Reel/Frame 055782/0355 →
SECURITY INTEREST Recorded May 29, 2020
From: UNITED STATES STEEL CORPORATION; U. S. STEEL TUBULAR PRODUCTS, INC.
To: U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGENT
Reel/Frame 052790/0364 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 5, 2018
From: MOORE, PETER W.; LIN, BISEN
To: UNITED STATES STEEL CORPORATION
Reel/Frame 045447/0927 →
Continuity (3)
Provisional Application 62458838 · Feb 14, 2017
Provisional Application 62487016 · Apr 19, 2017
Related Publication 20180229289A1 · Aug 16, 2018