IP Library Granted Patent US 7,100,259
Granted Patent B2
US 7,100,259 · App. 10/738,345 · Granted Sep 5, 2006

Method of metallic sandwiched foam composite forming

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Quick Facts
Patent No.
US 7,100,259
App. No.
10/738,345
Granted
Sep 5, 2006
Kind
B2
Abstract

Disclosed is a method of forming metallic composite structures The method utilizes superplastic and quickplastic formation methodologies in conjunction with the use of appended engineered metallic foams to provide energy absorbing materials.

Claims (26)

1. A method for forming a metallic composite structure, comprising:

placing undeformed sheet metal between a die and a platen, said die and said platen configured to sealingly engage a periphery of said sheet metal for forming a die enclosed area of the sheet metal, said die having a forming surface defining a cavity between said forming surface and said metal sheet;

moving said die and platen to their closed position such that said die engages the periphery of said sheet metal;

adjusting the temperature of said sheet metal to a material blow forming temperature to reduce the density of said metallic composite structure;

applying positive gas pressure to a surface of the sheet metal so as to superplastically form the sheet metal to at least partially conform with said die forming surface; and

coupling metallic foam substrate to the sheet metal.

2. The method according to claim 1 , wherein coupling metallic foam substrate to the sheet metal occurs prior to applying gas pressure to form the sheet metal.

3. The method according to claim 1 , wherein coupling metallic foam substrate to the sheet metal occurs after to applying gas pressure to form the sheet metal.

4. The method according to claim 3 , further comprising applying an adhesive between the metallic foam and the sheet metal.

5. The method according to claim 1 , wherein coupling metallic foam substrate to the sheet metal comprises deforming the sheet metal to form a pair of interfacial surfaces which couple to a pair of surfaces on the metallic foam.

6. The method according to claim 1 , wherein placing sheet metal between a die and a platen comprises placing a metal sheet having a depending metallic foam substrate disposed thereon.

7. The method according to claim 1 , wherein placing sheet metal between a die and a platen comprises placing a metal sandwich structure having a first and second sheet metal layers, and coupling a metallic foam substrate comprises positioning a metallic foam layer therebetween.

8. The method according to claim 1 , wherein the sheet metal is a superplastically formable alloy.

9. The method according to claim 1 , wherein the metallic foam is a superplastically formable alloy.

10. The method according to claim 1 , further comprising brazing material between the metallic foam substrate and the sheet metal.

11. The method according to claim 1 , wherein the metallic foam is a high purity aluminum alloy reinforced with a low volume fraction of (˜1 micron) ceramic particles.

12. A method for superplastically forming a composite metallic foam sandwich structure, comprising:

arranging a metallic foam substrate between two opposing undeformed metal alloy sheet layers to form a sandwich structure;

placing said sandwich structure between upper and lower die members configured to sealingly engage at least a periphery of said sandwich structure;

heating said sandwich structure to a suitable superplastic blow forming temperature to reduce the density of said metallic foam;

moving said die members to a closed position configured to form a cavity with an enclosed area of at least one of said metal alloy sheet layers; and

applying positive gas pressure to said at least one metal sheet layer and superplastically blow forming said sandwich structure within said die members.

13. The method according to claim 12 , further comprising applying at least one of an adhesive and brazing material between said metallic foam and said metal alloy sheet layers.

14. The method according to claim 12 , wherein said metallic foam comprises a high purity aluminum alloy reinforced with a low volume fraction of (˜1 micron) ceramic particles.

15. The method according to claim 12 , further comprising coupling said metallic foam substrate to said metal alloy sheets prior to applying positive gas pressure and superplastically blow forming said sandwich structure.

16. The method according to claim 15 , wherein coupling said metallic foam substrate to said metal alloy sheets comprises deforming at least one of said metal alloy sheets to form a pair of interfacial surfaces configured to couple with a pair of surfaces on said metallic foam substrate.

Assignments (13)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034371/0676 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025780/0902 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025327/0262 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025245/0347 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025311/0725 →
SECURITY AGREEMENT Recorded Aug 28, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023161/0911 →
SECURITY AGREEMENT Recorded Aug 27, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023156/0001 →
RELEASE OF SECURITY INTEREST Recorded Aug 21, 2009
From: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023127/0468 →
RELEASE OF SECURITY INTEREST Recorded Aug 20, 2009
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023124/0429 →
SECURITY AGREEMENT Recorded Apr 16, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
Reel/Frame 022553/0446 →
SECURITY AGREEMENT Recorded Feb 4, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 022201/0547 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 14, 2009
From: GENERAL MOTORS CORPORATION
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 022102/0533 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 17, 2003
From: MORALES, ARIANNA T.; KRAJEWSKI, PAUL E.
To: GENERAL MOTORS CORPORATION
Reel/Frame 014818/0483 →