AU703162B2 - Aircraft structural element, particularly for a supersonic aircraft, made of aluminium alloy with long life, good tolerance to damage and good resistance to stress corrosion - Google Patents

Aircraft structural element, particularly for a supersonic aircraft, made of aluminium alloy with long life, good tolerance to damage and good resistance to stress corrosion

Info

Publication number
AU703162B2
AU703162B2 AU60754/96A AU6075496A AU703162B2 AU 703162 B2 AU703162 B2 AU 703162B2 AU 60754/96 A AU60754/96 A AU 60754/96A AU 6075496 A AU6075496 A AU 6075496A AU 703162 B2 AU703162 B2 AU 703162B2
Authority
AU
Australia
Prior art keywords
aircraft
good
damage
aluminium alloy
structural element
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.)
Ceased
Application number
AU60754/96A
Other versions
AU6075496A (en
Inventor
Yann Philippe Barbaux
Gilles Pons
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of AU6075496A publication Critical patent/AU6075496A/en
Application granted granted Critical
Publication of AU703162B2 publication Critical patent/AU703162B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C22C21/12—Alloys based on aluminium with copper as the next major constituent
    • C22C21/16—Alloys based on aluminium with copper as the next major constituent with magnesium

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Heat Treatment Of Steel (AREA)
  • Conductive Materials (AREA)
AU60754/96A 1995-07-28 1996-07-26 Aircraft structural element, particularly for a supersonic aircraft, made of aluminium alloy with long life, good tolerance to damage and good resistance to stress corrosion Ceased AU703162B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9509246A FR2737224B1 (en) 1995-07-28 1995-07-28 ELEMENT OF STRUCTURE OF AIRCRAFT, AND PARTICULARLY OF SUPERSONIC AIRCRAFT, IN ALUMINUM ALLOY HAVING A LONG SERVICE LIFE, A GOOD TOLERANCE TO DAMAGES AND A GOOD RESISTANCE TO CORROSION UNDER STRESS
FR9509246 1995-07-28

Publications (2)

Publication Number Publication Date
AU6075496A AU6075496A (en) 1997-02-06
AU703162B2 true AU703162B2 (en) 1999-03-18

Family

ID=9481516

Family Applications (1)

Application Number Title Priority Date Filing Date
AU60754/96A Ceased AU703162B2 (en) 1995-07-28 1996-07-26 Aircraft structural element, particularly for a supersonic aircraft, made of aluminium alloy with long life, good tolerance to damage and good resistance to stress corrosion

Country Status (7)

Country Link
EP (1) EP0756016B1 (en)
JP (1) JP3791972B2 (en)
AU (1) AU703162B2 (en)
CA (1) CA2182058C (en)
DE (1) DE69608506T2 (en)
ES (1) ES2148699T3 (en)
FR (1) FR2737224B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5879181B2 (en) * 2011-06-10 2016-03-08 株式会社神戸製鋼所 Aluminum alloy with excellent high temperature characteristics

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5512112A (en) * 1992-08-28 1996-04-30 Reynolds Metals Company Method of making high strength, high toughness aluminum-copper-magnesium-type aluminum alloy

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE735314C (en) * 1937-06-29 1943-05-12 Ernst Heinkel Flugzeugwerke G Use of aluminum alloys as a material for rivets
FR2087439A5 (en) * 1970-05-20 1971-12-31 British Aluminium Co Ltd Aluminium alloys suitable for eloxation - for decorative applications
US4000007A (en) * 1973-02-13 1976-12-28 Cegedur Societe De Transformation De L'aluminium Pechiney Method of making drawn and hemmed aluminum sheet metal and articles made thereby
FR2279852B1 (en) * 1974-07-23 1977-01-07 Cegedur Transf Aumin Pechiney ALUMINUM ALLOY WITH GOOD CREEP RESISTANCE AND IMPROVED CRICK PROPAGATION RESISTANCE
US4062704A (en) * 1976-07-09 1977-12-13 Swiss Aluminium Ltd. Aluminum alloys possessing improved resistance weldability
CH668269A5 (en) 1985-10-31 1988-12-15 Bbc Brown Boveri & Cie AL/CU/MG TYPE ALUMINUM ALLOY WITH HIGH STRENGTH IN THE TEMPERATURE RANGE BETWEEN 0 AND 250 C.

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5512112A (en) * 1992-08-28 1996-04-30 Reynolds Metals Company Method of making high strength, high toughness aluminum-copper-magnesium-type aluminum alloy

Also Published As

Publication number Publication date
FR2737224A1 (en) 1997-01-31
AU6075496A (en) 1997-02-06
JPH09104941A (en) 1997-04-22
CA2182058A1 (en) 1997-01-29
EP0756016B1 (en) 2000-05-24
EP0756016A1 (en) 1997-01-29
CA2182058C (en) 2008-12-09
ES2148699T3 (en) 2000-10-16
DE69608506D1 (en) 2000-06-29
FR2737224B1 (en) 1997-10-17
JP3791972B2 (en) 2006-06-28
DE69608506T2 (en) 2001-01-18

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