AU3723997A - Method for forming a bi-metallic structural assembly - Google Patents

Method for forming a bi-metallic structural assembly

Info

Publication number
AU3723997A
AU3723997A AU37239/97A AU3723997A AU3723997A AU 3723997 A AU3723997 A AU 3723997A AU 37239/97 A AU37239/97 A AU 37239/97A AU 3723997 A AU3723997 A AU 3723997A AU 3723997 A AU3723997 A AU 3723997A
Authority
AU
Australia
Prior art keywords
forming
structural assembly
metallic structural
metallic
assembly
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
AU37239/97A
Inventor
James M. Hannah
Kevin D. Walters
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
McDonnell Douglas Corp
Original Assignee
JAMES M HANNAH
KEVIN D WALTERS
McDonnell Douglas Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by JAMES M HANNAH, KEVIN D WALTERS, McDonnell Douglas Corp filed Critical JAMES M HANNAH
Publication of AU3723997A publication Critical patent/AU3723997A/en
Abandoned legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00—Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/08—Non-ferrous metals or alloys
    • B23K2103/10—Aluminium or alloys thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2103/00—Materials to be soldered, welded or cut
    • B23K2103/08—Non-ferrous metals or alloys
    • B23K2103/14—Titanium or alloys thereof
AU37239/97A 1996-07-12 1997-07-11 Method for forming a bi-metallic structural assembly Abandoned AU3723997A (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US69507296A 1996-07-12 1996-07-12
US08695072 1996-07-12
PCT/US1997/012038 WO1998002277A1 (en) 1996-07-12 1997-07-11 Method for forming a bi-metallic structural assembly

Publications (1)

Publication Number Publication Date
AU3723997A true AU3723997A (en) 1998-02-09

Family

ID=24791444

Family Applications (1)

Application Number Title Priority Date Filing Date
AU37239/97A Abandoned AU3723997A (en) 1996-07-12 1997-07-11 Method for forming a bi-metallic structural assembly

Country Status (2)

Country Link
AU (1) AU3723997A (en)
WO (1) WO1998002277A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10360809A1 (en) * 2003-12-19 2005-07-28 Airbus Deutschland Gmbh seat rail
DE102007048283A1 (en) * 2007-10-08 2009-04-16 Eads Deutschland Gmbh Stiffening profile for aircraft structures
US10611498B2 (en) 2017-08-24 2020-04-07 Aurora Flight Sciences Corporation Rail recovery system for aircraft

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3645803A (en) * 1970-04-16 1972-02-29 Us Navy Method for improving the fracture toughness of metals and alloys
US4151012A (en) * 1977-04-11 1979-04-24 Latrobe Steel Company High strength, corrosion resistant tubular products and methods of making the same
US4890784A (en) * 1983-03-28 1990-01-02 Rockwell International Corporation Method for diffusion bonding aluminum
US4896815A (en) * 1987-05-29 1990-01-30 Avco Lycoming Method for forming titanium aluminide-ductile titanium aluminum alloy matrix composites
ES2038300T3 (en) * 1987-09-18 1993-07-16 Imperial Chemical Industries Plc JOINT UNION OF METAL COMPONENTS.
US4811766A (en) * 1987-10-08 1989-03-14 Mcdonnell Douglas Corporation Explosively bonded expanded structure
US4851071A (en) * 1988-07-22 1989-07-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method for maintaining precise suction strip porosities
GB9008273D0 (en) * 1990-04-11 1990-06-13 Ici Plc Manufacture of bi-metallic tube by explosive bonding,hot extrusion and co-extrusion
GB9027802D0 (en) * 1990-12-21 1991-02-13 Ici Plc Method of explosively bonding composite metal structures
GB2257384B (en) * 1991-07-12 1995-03-01 Ici Plc Method of manufacturing laminer-metallic tubing
US5226579A (en) * 1992-02-14 1993-07-13 E. I. Du Pont De Nemours And Company Process for explosively bonding metals
US5226982A (en) * 1992-05-15 1993-07-13 The United States Of America As Represented By The Secretary Of The Air Force Method to produce hollow titanium alloy articles
US5415336A (en) * 1992-11-19 1995-05-16 Alliedsignal Inc. Method for preparing a composite surface for diffusion bonding
US5531369A (en) * 1993-08-02 1996-07-02 Electric Power Research Institute Process for making machines resistant to cavitation and liquid droplet erosion
US5433835B1 (en) * 1993-11-24 1997-05-20 Applied Materials Inc Sputtering device and target with cover to hold cooling fluid
US5630890A (en) * 1995-01-30 1997-05-20 General Electric Company Manufacture of fatigue-resistant hollow articles

Also Published As

Publication number Publication date
WO1998002277A1 (en) 1998-01-22

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