FR2737224B1 - 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 - Google Patents

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

Info

Publication number
FR2737224B1
FR2737224B1 FR9509246A FR9509246A FR2737224B1 FR 2737224 B1 FR2737224 B1 FR 2737224B1 FR 9509246 A FR9509246 A FR 9509246A FR 9509246 A FR9509246 A FR 9509246A FR 2737224 B1 FR2737224 B1 FR 2737224B1
Authority
FR
France
Prior art keywords
aircraft
good
damages
service life
aluminum alloy
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.)
Expired - Fee Related
Application number
FR9509246A
Other languages
French (fr)
Other versions
FR2737224A1 (en
Inventor
Gilles Pons
Yann Philippe Barbaux
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
Priority to FR9509246A priority Critical patent/FR2737224B1/en
Priority to CA 2182058 priority patent/CA2182058C/en
Priority to JP19814996A priority patent/JP3791972B2/en
Priority to ES96401680T priority patent/ES2148699T3/en
Priority to DE1996608506 priority patent/DE69608506T2/en
Priority to AU60754/96A priority patent/AU703162B2/en
Priority to EP19960401680 priority patent/EP0756016B1/en
Publication of FR2737224A1 publication Critical patent/FR2737224A1/en
Application granted granted Critical
Publication of FR2737224B1 publication Critical patent/FR2737224B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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)
  • Conductive Materials (AREA)
  • Heat Treatment Of Steel (AREA)
FR9509246A 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 Expired - Fee Related FR2737224B1 (en)

Priority Applications (7)

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
CA 2182058 CA2182058C (en) 1995-07-28 1996-07-25 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
ES96401680T ES2148699T3 (en) 1995-07-28 1996-07-26 AIRCRAFT STRUCTURE ELEMENT, IN PARTICULAR OF A SUPERSONIC AIRCRAFT, MADE WITH AN ALUMINUM ALLOY THAT PRESENTS A LONG LIFE DURATION, A GOOD TOLERANCE TO DAMAGE AND A GOOD TOLERANCE TO CORROSION UNDER TENSION.
DE1996608506 DE69608506T2 (en) 1995-07-28 1996-07-26 Cell component, especially for supersonic aircraft, made of an aluminum alloy with a long service life, good damage tolerance and high stress corrosion resistance
JP19814996A JP3791972B2 (en) 1995-07-28 1996-07-26 Structural material for aircraft, in particular supersonic aircraft, consisting of an aluminum alloy with long life and good tolerance to damage and good resistance to stress corrosion
AU60754/96A 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
EP19960401680 EP0756016B1 (en) 1995-07-28 1996-07-26 Aircraft body member, more particularly for supersonic aircraft, made from a long-living, damage tolerant aluminium alloy with good stress corrosion resistance

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
FR2737224A1 FR2737224A1 (en) 1997-01-31
FR2737224B1 true FR2737224B1 (en) 1997-10-17

Family

ID=9481516

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9509246A Expired - Fee Related 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

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

Family Cites Families (7)

* 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.
US5376192A (en) * 1992-08-28 1994-12-27 Reynolds Metals Company High strength, high toughness aluminum-copper-magnesium-type aluminum alloy

Also Published As

Publication number Publication date
DE69608506D1 (en) 2000-06-29
JPH09104941A (en) 1997-04-22
EP0756016B1 (en) 2000-05-24
EP0756016A1 (en) 1997-01-29
JP3791972B2 (en) 2006-06-28
AU703162B2 (en) 1999-03-18
AU6075496A (en) 1997-02-06
CA2182058A1 (en) 1997-01-29
ES2148699T3 (en) 2000-10-16
DE69608506T2 (en) 2001-01-18
CA2182058C (en) 2008-12-09
FR2737224A1 (en) 1997-01-31

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CD Change of name or company name
TP Transmission of property
ST Notification of lapse

Effective date: 20110331