CA2182058A1 - Element de structure d'aeronef, particulierement pour un aeronef supersonique, fait en alliage d'aluminium presentant une longue duree, une bonne tolerance aux dommages et une bonne resistance a la corrosion sous contrainte - Google Patents
Element de structure d'aeronef, particulierement pour un aeronef supersonique, fait en alliage d'aluminium presentant une longue duree, une bonne tolerance aux dommages et une bonne resistance a la corrosion sous contrainteInfo
- Publication number
- CA2182058A1 CA2182058A1 CA 2182058 CA2182058A CA2182058A1 CA 2182058 A1 CA2182058 A1 CA 2182058A1 CA 2182058 CA2182058 CA 2182058 CA 2182058 A CA2182058 A CA 2182058A CA 2182058 A1 CA2182058 A1 CA 2182058A1
- Authority
- CA
- Canada
- Prior art keywords
- aircraft
- aluminium alloy
- structural element
- good
- damage
- 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.)
- Granted
Links
- 229910000838 Al alloy Inorganic materials 0.000 title abstract 2
- 230000007797 corrosion Effects 0.000 title 1
- 238000005260 corrosion Methods 0.000 title 1
- 239000011777 magnesium Substances 0.000 abstract 4
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 abstract 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 abstract 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 abstract 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 abstract 2
- BQCADISMDOOEFD-UHFFFAOYSA-N Silver Chemical compound [Ag] BQCADISMDOOEFD-UHFFFAOYSA-N 0.000 abstract 2
- 229910052749 magnesium Inorganic materials 0.000 abstract 2
- 229910052710 silicon Inorganic materials 0.000 abstract 2
- 239000010703 silicon Substances 0.000 abstract 2
- 229910052709 silver Inorganic materials 0.000 abstract 2
- 239000004332 silver Substances 0.000 abstract 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 abstract 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 abstract 1
- 229910045601 alloy Inorganic materials 0.000 abstract 1
- 239000000956 alloy Substances 0.000 abstract 1
- 229910052802 copper Inorganic materials 0.000 abstract 1
- 239000010949 copper Substances 0.000 abstract 1
- 229910052742 iron Inorganic materials 0.000 abstract 1
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 abstract 1
- 229910052759 nickel Inorganic materials 0.000 abstract 1
- 230000002787 reinforcement Effects 0.000 abstract 1
- 239000010936 titanium Substances 0.000 abstract 1
- 229910052719 titanium Inorganic materials 0.000 abstract 1
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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9509246A FR2737224B1 (fr) | 1995-07-28 | 1995-07-28 | Element de structure d'aeronef, et notamment d'avion supersonique, en alliage d'aluminium presentant une longue duree de vie, une bonne tolerance aux dommages et une bonne resistance a la corrosion sous contrainte |
FR9509246 | 1995-07-28 |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2182058A1 true CA2182058A1 (fr) | 1997-01-29 |
CA2182058C CA2182058C (fr) | 2008-12-09 |
Family
ID=9481516
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA 2182058 Expired - Fee Related CA2182058C (fr) | 1995-07-28 | 1996-07-25 | Element de structure d'aeronef, particulierement pour un aeronef supersonique, fait en alliage d'aluminium presentant une longue duree, une bonne tolerance aux dommages et une bonne resistance a la corrosion sous contrainte |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP0756016B1 (fr) |
JP (1) | JP3791972B2 (fr) |
AU (1) | AU703162B2 (fr) |
CA (1) | CA2182058C (fr) |
DE (1) | DE69608506T2 (fr) |
ES (1) | ES2148699T3 (fr) |
FR (1) | FR2737224B1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5879181B2 (ja) * | 2011-06-10 | 2016-03-08 | 株式会社神戸製鋼所 | 高温特性に優れたアルミニウム合金 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE735314C (de) * | 1937-06-29 | 1943-05-12 | Ernst Heinkel Flugzeugwerke G | Verwendung von Aluminiumlegierungen als Werkstoff fuer Nieten |
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 (fr) * | 1974-07-23 | 1977-01-07 | Cegedur Transf Aumin Pechiney | Alliage d'aluminium de bonne tenue au fluage et de resistance a la propagation des criques amelioree |
US4062704A (en) * | 1976-07-09 | 1977-12-13 | Swiss Aluminium Ltd. | Aluminum alloys possessing improved resistance weldability |
CH668269A5 (de) | 1985-10-31 | 1988-12-15 | Bbc Brown Boveri & Cie | Aluminium-knetlegierung des typs al/cu/mg mit hoher festigkeit im temperaturbereich zwischen 0 und 250 c. |
US5376192A (en) * | 1992-08-28 | 1994-12-27 | Reynolds Metals Company | High strength, high toughness aluminum-copper-magnesium-type aluminum alloy |
-
1995
- 1995-07-28 FR FR9509246A patent/FR2737224B1/fr not_active Expired - Fee Related
-
1996
- 1996-07-25 CA CA 2182058 patent/CA2182058C/fr not_active Expired - Fee Related
- 1996-07-26 JP JP19814996A patent/JP3791972B2/ja not_active Expired - Fee Related
- 1996-07-26 AU AU60754/96A patent/AU703162B2/en not_active Ceased
- 1996-07-26 DE DE1996608506 patent/DE69608506T2/de not_active Expired - Fee Related
- 1996-07-26 EP EP19960401680 patent/EP0756016B1/fr not_active Expired - Lifetime
- 1996-07-26 ES ES96401680T patent/ES2148699T3/es not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2737224A1 (fr) | 1997-01-31 |
EP0756016A1 (fr) | 1997-01-29 |
ES2148699T3 (es) | 2000-10-16 |
JP3791972B2 (ja) | 2006-06-28 |
CA2182058C (fr) | 2008-12-09 |
DE69608506T2 (de) | 2001-01-18 |
AU703162B2 (en) | 1999-03-18 |
FR2737224B1 (fr) | 1997-10-17 |
DE69608506D1 (de) | 2000-06-29 |
EP0756016B1 (fr) | 2000-05-24 |
AU6075496A (en) | 1997-02-06 |
JPH09104941A (ja) | 1997-04-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |