IP Library › Granted Patent US 6,883,220
Granted Patent B2
US 6,883,220 · App. 10/197,039 · Granted Apr 26, 2005

Method for forming a tube-walled article

Assignee: The Boeing Company
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Quick Facts
Patent No.
US 6,883,220
App. No.
10/197,039
Granted
Apr 26, 2005
Kind
B2
Abstract

A method for forming an article having a wall that is at least partially fabricated from tubing. The methodology employs a pressurized fluid to deform the tubing such that an outer surface of the tubing substantially conforms to a predetermined first wall configuration, an inner surface of the tubing substantially conforms to a predetermined second wall configuration and each of segment or loop of the tubing is substantially contiguous with at least one other segment or loop between the first and second surfaces.

Claims (65)

1. A method for forming an article having a wall that is at least partially formed from a tube, the method comprising the steps of:

providing at least one tube;

stacking the at least one tube in a predetermined manner such that the at least one tube forms a plurality of tube seqments that are approximately abutted against one another; and

employing a pressurized fluid to compress the plurality of tube seqments such that a first surface of the at least one tube substantially conforms to a predetermined first wall configuration, a second surface of the at least one tube that is disposed opposite the first surface substantially conforms to a predetermined second wall configuration and each of the tube seqments is substantially contiguous with at least one other tube segment;

wherein the at least one tube is evacuated prior to the step of exposing the at least one tube to a pressurized fluid.

2. The method of claim 1 , further comprising the step of heating the at least one tube to a predetermined temperature.

3. The method of claim 2 , wherein the step of heating the at least one tube and the step of exposing the at least one tube to the pressurized fluid are performed substantially simultaneously.

4. The method of claim 2 , further comprising the step of brazing the tube segments together.

5. The method of claim 1 , wherein the first and second surfaces are generally parallel to one another.

6. The method of claim 1 , wherein the pressurized fluid is a gas that is selected from a group of gasses consisting of argon, nitrogen and helium.

7. The method of claim 1 , wherein prior to the step of exposing the at least one tube to the pressurized fluid the method further comprises the steps of:

providing a first closeout skin structure, the first closeout skin structure having a first skin surface that defines the predetermined first wall configuration; and

abutting the first skin surface to the first surface of the at least one tube.

8. The method of claim 7 , wherein prior to the step of exposing the at least one tube to the pressurized fluid the method further comprises the steps of:

providing a second closeout skin structure, the second closeout skin structure having a second skin surface that defines the predetermined second wall configuration; and

abutting the second skin surface to the second surface of the at least one tube.

9. The method of claim 8 , further comprising the step of removing at least one of the first and second closeout skin structures from the at least one tube after the step of exposing the at least one tube to the pressurized fluid.

10. A method for forming an article having a wall that is at least partially formed from a tube, the method comprising the steps of:

providing at least one tube:

stacking the at least one tube in a predetermined manner such that the at least one tube forms a plurality of tube segments that are approximately abutted against one another; and

employing a pressurized fluid to compress the plurality of tube segments such that a first surface of the at least one tube substantially conforms to a predetermined first wall configuration, a second surface of the at least one tube that is disposed opposite the first surface substantially conforms to a predetermined second wall configuration and each of the tube segments is substantially contiguous with at least one other tube segment;

wherein prior to the step of exposing the at least one tube to the pressurized fluid the method further comprises the step of at least partially filling the at least one tube with a fluid.

11. The method of claim 10 , wherein the fluid in the at least one tube is a compressible fluid.

12. The method of claim 11 , wherein the compressible fluid is an inert gas.

13. The method of claim 10 , further comprising the step of heating the at least one tube to a predetermined temperature.

14. The method of claim 13 , wherein the step of heating the at least one tube and the step of exposing the at least one tube to the pressurized fluid are performed substantially simultaneously.

15. The method of claim 13 , further comprising the step of brazing the tube segments together.

16. The method of claim 10 , wherein the first and second surfaces are generally parallel to one another.

17. The method of claim 10 , wherein the pressurized fluid is a gas that is selected from a group of gasses consisting of argon, nitrogen and helium.

18. The method of claim 10 , wherein prior to the step of exposing the at least one tube to the pressurized fluid the method further comprises the steps of:

providing a first closeout skin structure, the first closeout skin structure having a first skin surface that defines the predetermined first wall configuration; and

abutting the first skin surface to the first surface of the at least one tube.

19. The method of claim 18 , wherein prior to the step of exposing the at least one tube to the pressurized fluid the method further comprises the steps of:

providing a second closeout skin structure, the second closeout skin structure having a second skin surface that defines the predetermined second wall configuration; and

abutting the second skin surface to the second surface of the at least one tube.

20. The method of claim 19 , further comprising the step of removing at least one of the first and second closeout skin structures from the at least one tube after the step of exposing the at least one tube to the pressurized fluid.

21. A method for forming an article having a wall that is at least partially formed from a tube, the method comprising the steps of;

providing at least one tube;

arranging the at least one tube in a predetermined manner such that the at least one tube forms a plurality of tube segments that are abutted against one another in a stacked arrangement, each of the tube segments having an annular cross-section with an outer circumference, the annular cross-section being taken generally perpendicularly to a longitudinal axis of the tube segment;

employing a pressurized gas to compress the plurality of tube seqments such that a surface of the at least one tube substantially conforms to a predetermined wall configuration and each of the tube seqments contacts at least one adjacent tube seqment over an area that exceeds about 5% of the circumference of the tube segment; and

heating the at least one tube to a predetermined temperature;

wherein the at least one tube is evacuated prior to the step of exposing the at least one tube to a pressurized fluid.

22. The method of claim 21 , wherein the step of exposing the at least one tube to the pressurized gas and the step of heating the at least one tube are performed substantially simultaneously.

23. The method of claim 21 , further comprising the step of brazing the tube segments together.

24. The method of claim 21 , wherein the pressurized fluid is a gas that is selected from a group of gasses consisting of argon, nitrogen and helium.

25. The method of claim 21 , wherein prior to the step of exposing the at least one tube to the pressurized gas the method further comprises the steps of:

providing a closeout skin structure, the closeout skin structure having a skin surface that defines the predetermined wall configuration; and

abutting the skin surface to the surface of the at least one tube.

26. The method of claim 25 , further comprising the step of removing the closeout skin structure from the at least one tube after the step of heating the at least one tube.

27. A method for forming an article having a wall that is at least partially formed from a tube, the method comprising the steps of:

providing at least one tube;

arranging the at least one tube in a predetermined manner such that the at least one tube forms a plurality of tube seqments that are abutted against one another in a stacked arrangement, each of the tube segments having an annular cross-section with an outer circumference, the annular cross-section being taken generally perpendicularly to a longitudinal axis of the tube seqment;

employing a pressurized gas to compress the plurality of tube segments such that a surface of the at least one tube substantially conforms to a predetermined wall configuration and each of the tube seqments contacts at least one adjacent tube seqment over an area that exceeds about 5% of the circumference of the tube segment; and

heating the at least one tube to a predetermined temperature;

wherein prior to the step of heating the at least one tube the method further comprises the step of at least partially filling the at least one tube with a fluid.

28. The method of claim 27 , wherein the fluid in the at least one tube is a compressible fluid.

29. The method of claim 28 , wherein the compressible fluid is an inert gas.

30. The method of claim 27 , further comprising the step of pressurizing the fluid.

31. The method of claim 27 , wherein the step of exposing the least one tube to the pressurized gas and the step of heating the least one tube are performed substantially simultaneously.

32. The method of claim 27 , further comprising the step of brazing the tube segments together.

33. The method of claim 27 , wherein the pressurized fluid is a gas that is selected from a group of gasses consisting of argon, nitrogen and helium.

34. The method of claim 27 , wherein prior to the step of exposing the at least one tube to the pressurized gas the method further comprises the steps of:

providing a closeout skin structure, the closeout skin structure having a skin surface that defines the predetermined wall configuration; and

abutting the skin surface to the surface of the at least one tube.

35. The method of claim 34 , further comprising the step of removing the closeout skin structure from the at least one tube after the step of heating the at least one tube.

Assignments (19)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 064424/0050 →
RELEASE OF SECURITY INTEREST Recorded Aug 29, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: CAMCAR INTELLECTUAL PROPERTIES, LLC ET AL
Reel/Frame 039562/0501 →
RELEASE OF SECURITY INTEREST Recorded Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
NOTICE OF SUCCESSION OF AGENCY (INTELLECTUAL PROPERTY) Recorded Jun 20, 2016
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS THE RESIGNING AGENT
To: BANK OF AMERICA, N.A., AS THE SUCCESSOR AGENT
Reel/Frame 039079/0857 →
CHANGE OF NAME Recorded May 14, 2016
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 038707/0175 →
SECURITY AGREEMENT Recorded Jun 21, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: U.S. BANK NATIONAL ASSOCIATION
Reel/Frame 030656/0615 →
SECURITY AGREEMENT Recorded Jun 17, 2013
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: WELLS FARGO BANK, NATIONAL ASSOCIATION
Reel/Frame 030628/0408 →
CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNEE'S NAME ON ORIGINAL COVER SHEET PREVIOUSLY RECORDED ON REEL 017882 FRAME 0126. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNEE WAS INCORRECTLY RECORDED AS "UNITED TECHNOLOGIES CORPORATION". ASSIGNEE SHOULD BE "RUBY ACQUISITION ENTERPRISES CO.". Recorded Jun 12, 2013
From: THE BOEING COMPANY AND BOEING MANAGEMENT COMPANY
To: RUBY ACQUISITION ENTERPRISES CO.
Reel/Frame 030592/0954 →
CHANGE OF NAME Recorded Jun 12, 2013
From: RUBY ACQUISITION ENTERPRISES CO.
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 030593/0055 →
RELEASE OF PATENT SECURITY INTEREST Recorded Aug 3, 2010
From: WILMINGTON TRUST FSB, AS THE AGENT
To: KING HOLDING CORPORATION; ACUMENT GLOBAL TECHNOLOGIES, INC.; ACUMENT INTELLECTUAL PROPERTIES, LLC; KING HOLDING US CORPORATION; CAMCAR LLC; RING SCREW LLC; ELCO FASTENING SYSTEMS LLC; FLEXALLOY, INC.; SATURN FASTENERS, INC.; AVDEL USA LLC; ACUMENT FASTENING SYSTEMS LLC; WOLVERINE METAL SPECIALTIES, INC.
Reel/Frame 024776/0651 →
RELEASE OF SECURITY INTEREST Recorded Sep 24, 2009
From: WELLS FARGO FOOTHILL, INC., AS COLLATERAL AGENT
To: CAMCAR INTELLECTUAL PROPERTIES, LLC; KING HOLDING CORPORATION; KING HOLDING US CORPORATION; AVDEL CHERRY LLC; CHERRY AEROSPACE LLC; FLEXALLOY INC.; BURKLAND TEXTRON INC.; WOLVERINE METAL SPECIALTIES, INC.; ELCO FASTENING SYSTEMS LLC; CAMCAR LLC; TFS FASTENING SYSTEMS LLC; RING SCREW LLC
Reel/Frame 023273/0891 →
RELEASE OF SECURITY AGREEMENT Recorded Sep 23, 2009
From: CREDIT SUISSE, CAYMAN ISLANDS BRANCH, AS COLLATERAL AGENT; WILMINGTON TRUST FSB, AS COLLATERAL AGENT
To: CAMCAR INTELLECTUAL PROPERTIES, LLC; KING HOLDING CORPORATION; KING HOLDING US CORPORATION; AVDEL CHERRY LLC; CHERRY AEROSPACE LLC; FLEXALLOY INC.; BURKLAND TEXTRON INC.; WOLVERINE METAL SPECIALTIES, INC.; ELCO FASTENING SYSTEMS LLC; CAMCAR LLC; TFS FASTENING SYSTEMS LLC; RING SCREW LLC
Reel/Frame 023273/0086 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 19, 2007
From: UNITED TECHNOLOGIES CORPORATION
To: PRATT & WHITNEY ROCKETDYNE, INC.
Reel/Frame 019458/0247 →
SECURITY AGREEMENT Recorded Jan 26, 2007
From: CAMCAR INTELLECTUAL PROPERTIES, LLC; KING HOLDING CORPORATION; KING HOLDING US CORPORATION; AVDEL CHERRY LLC; CHERRY AEROSPACE LLC; FLEXALLOY INC.; BURKLAND TEXTRON INC.; WOLVERINE METAL SPECIALTIES, INC.; ELCO FASTENING SYSYTEMS LLC; CAMCAR LLC; TFS FASTENING SYSTEMS LLC; RING SCREW LLC
To: U.S. BANK NATIONAL ASSOCIATION, AS COLLATERAL AGENT
Reel/Frame 018806/0296 →
SECURITY AGREEMENT Recorded Jan 26, 2007
From: CAMCAR INTELLECTUAL PROPERTIES, LLC; KING HOLDING CORPORATION; KING HOLDING US CORPORATION; AVDEL CHERRY LLC; CHERRY AEROSPACE LLC; FLEXALLOY INC.; BURKLAND TEXTRON INC.; WOLVERINE METAL SPECIALTIES, INC.; ELCO FASTENING SYSYTEMS LLC; CAMCAR LLC; TFS FASTENING SYSTEMS LLC; RING SCREW LLC
To: WELLS FARGO FOOTHILL, INC., AS COLLATERAL AGENT
Reel/Frame 018806/0538 →
SECURITY AGREEMENT Recorded Jan 26, 2007
From: CAMCAR INTELLECTUAL PROPERTIES, LLC; KING HOLDING CORPORATION; KING HOLDING US CORPORATION; AVDEL CHERRY LLC; CHERRY AEROSPACE LLC; FLEXALLOY INC.; BURKLAND TEXTRON INC.; WOLVERINE METAL SPECIALTIES, INC.; ELCO FASTENING SYSYTEMS LLC; CAMCAR LLC; TFS FASTENING SYSTEMS LLC; RING SCREW LLC
To: CREDIT SUISSE, CAYMAN ISLANDS BRANCH, AS COLLATERAL AGENT
Reel/Frame 018806/0167 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 16, 2006
From: BOEING C OMPANY AND BOEING MANAGEMENT COMPANY, THE
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 017882/0126 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 27, 2006
From: BOEING COMPANY AND BOEING MANAGEMENT COMPANY, THE
To: UNITED TECHNOLOGIES CORPORATION
Reel/Frame 017681/0537 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 17, 2002
From: HORN, MARK DAVID
To: THE BOEING COMPANY
Reel/Frame 013113/0940 →
Continuity (1)
Related Publication 20040010900A1 · Jan 22, 2004