FR2889542B1 - Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion - Google Patents
Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avionInfo
- Publication number
- FR2889542B1 FR2889542B1 FR0508374A FR0508374A FR2889542B1 FR 2889542 B1 FR2889542 B1 FR 2889542B1 FR 0508374 A FR0508374 A FR 0508374A FR 0508374 A FR0508374 A FR 0508374A FR 2889542 B1 FR2889542 B1 FR 2889542B1
- Authority
- FR
- France
- Prior art keywords
- sheet
- copper
- lithium
- plaster
- plate
- 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
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
- C22C21/14—Alloys based on aluminium with copper as the next major constituent with silicon
-
- 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
-
- 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
-
- 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
- C22C21/18—Alloys based on aluminium with copper as the next major constituent with zinc
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/057—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with copper as the next major constituent
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Metal Rolling (AREA)
- Heat Treatment Of Steel (AREA)
- Forging (AREA)
- Extrusion Of Metal (AREA)
Priority Applications (11)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0508374A FR2889542B1 (fr) | 2005-08-05 | 2005-08-05 | Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion |
EP06764718A EP1891247B1 (fr) | 2005-06-06 | 2006-06-02 | Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion |
CA2608971A CA2608971C (fr) | 2005-06-06 | 2006-06-02 | Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion |
ES06764718T ES2314929T3 (es) | 2005-06-06 | 2006-06-02 | Chapa de aluminio-cobre-litio con alta tenacidad para fuselaje de avion. |
RU2007145191/02A RU2415960C2 (ru) | 2005-06-06 | 2006-06-02 | Алюминиево-медно-литиевый лист с высокой вязкостью разрушения для фюзеляжа самолета |
DE602006003656T DE602006003656D1 (de) | 2005-06-06 | 2006-06-02 | Hochfestes aluminium-kupfer-lithium-blech für flugzeugrümpfe |
PCT/FR2006/001250 WO2006131627A1 (fr) | 2005-06-06 | 2006-06-02 | Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion |
CN201110377207.7A CN102400020B (zh) | 2005-06-06 | 2006-06-02 | 用于飞机机身的高韧度的铝-铜-锂合金板材 |
EP08018130A EP2017361A1 (fr) | 2005-06-06 | 2006-06-02 | Tôle en aluminium-cuivre-lithium à haute ténacité pour fuselage d'avion |
AT06764718T ATE414183T1 (de) | 2005-06-06 | 2006-06-02 | Hochfestes aluminium-kupfer-lithium-blech für flugzeugrümpfe |
BRPI0610937A BRPI0610937B1 (pt) | 2005-06-06 | 2006-06-02 | processo de fabricação de uma chapa em liga de alumínio e chapa em liga de alumínio produzida pelo processo |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0508374A FR2889542B1 (fr) | 2005-08-05 | 2005-08-05 | Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2889542A1 FR2889542A1 (fr) | 2007-02-09 |
FR2889542B1 true FR2889542B1 (fr) | 2007-10-12 |
Family
ID=36581721
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0508374A Expired - Fee Related FR2889542B1 (fr) | 2005-06-06 | 2005-08-05 | Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion |
Country Status (2)
Country | Link |
---|---|
CN (1) | CN102400020B (fr) |
FR (1) | FR2889542B1 (fr) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9458528B2 (en) * | 2012-05-09 | 2016-10-04 | Alcoa Inc. | 2xxx series aluminum lithium alloys |
FR3004197B1 (fr) | 2013-04-03 | 2015-03-27 | Constellium France | Toles minces en alliage d'aluminium-cuivre-lithium pour la fabrication de fuselages d'avion. |
FR3026747B1 (fr) * | 2014-10-03 | 2016-11-04 | Constellium France | Toles isotropes en alliage d'aluminium-cuivre-lithium pour la fabrication de fuselages d'avion |
RU2747180C1 (ru) * | 2020-09-17 | 2021-04-28 | Федеральное государственное бюджетное учреждение науки Самарский федеральный исследовательский центр Российской академии наук (СамНЦ РАН) | ВЫСОКОПРОЧНЫЙ ТЕРМОСТОЙКИЙ МЕЛКОЗЕРНИСТЫЙ СПЛАВ НА ОСНОВЕ СИСТЕМЫ Al-Cu-Mn-Mg-Sc-Nb-Hf И ИЗДЕЛИЕ ИЗ НЕГО |
FR3132306B1 (fr) * | 2022-01-28 | 2024-05-03 | Constellium Issoire | Tôle mince améliorée en alliage d’aluminium-cuivre-lithium |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BR8807653A (pt) * | 1987-08-10 | 1990-06-12 | Martin Marietta Corp | Ligas de aluminio-litio soldaveis de resistencia ultra elevada |
US5455003A (en) * | 1988-08-18 | 1995-10-03 | Martin Marietta Corporation | Al-Cu-Li alloys with improved cryogenic fracture toughness |
US5198045A (en) * | 1991-05-14 | 1993-03-30 | Reynolds Metals Company | Low density high strength al-li alloy |
US5389165A (en) * | 1991-05-14 | 1995-02-14 | Reynolds Metals Company | Low density, high strength Al-Li alloy having high toughness at elevated temperatures |
US7438772B2 (en) * | 1998-06-24 | 2008-10-21 | Alcoa Inc. | Aluminum-copper-magnesium alloys having ancillary additions of lithium |
WO2004106570A1 (fr) * | 2003-05-28 | 2004-12-09 | Pechiney Rolled Products | Nouvel alliage de al-cu-li-mg-ag-mn-zr utilise comme elements structurels exigeant une haute resistance ainsi qu'une grande tenacite a la rupture |
RU2237098C1 (ru) * | 2003-07-24 | 2004-09-27 | Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" | Сплав на основе алюминия и изделие, выполненное из него |
-
2005
- 2005-08-05 FR FR0508374A patent/FR2889542B1/fr not_active Expired - Fee Related
-
2006
- 2006-06-02 CN CN201110377207.7A patent/CN102400020B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
CN102400020B (zh) | 2015-10-28 |
CN102400020A (zh) | 2012-04-04 |
FR2889542A1 (fr) | 2007-02-09 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ATE414183T1 (de) | Hochfestes aluminium-kupfer-lithium-blech für flugzeugrümpfe | |
CN102839297B (zh) | 一种高温钛合金的制备方法 | |
CN103451583B (zh) | 生产飞机机翼长桁用型材的方法 | |
DK1902149T4 (da) | Fremgansmåde til fremstilling af en aluminiumslegeringsfolie som er af typen al-fe-si og folie deraf | |
US20110221151A1 (en) | Automobile suspension part and manufacturing of the same | |
CN104388777A (zh) | 一种高强度铝合金厚板及其制造方法 | |
RU2008152793A (ru) | Продукты из алюминиевых сплавов серии аа2000 и способ их производства | |
JP5870791B2 (ja) | プレス成形性と形状凍結性に優れたアルミニウム合金板およびその製造方法 | |
FR2889542B1 (fr) | Tole en aluminium-cuivre-lithium a haute tenacite pour fuselage d'avion | |
CN102433476A (zh) | Led背板用铝合金板带材及其制造方法 | |
JP6176393B2 (ja) | 曲げ加工性と形状凍結性に優れた高強度アルミニウム合金板 | |
CN104342590A (zh) | 切削用铝合金挤压材 | |
JP2007021533A (ja) | 成形用アルミニウム合金板の製造方法および成形用アルミニウム合金の連続鋳造装置 | |
CA2597248C (fr) | Procede de moulage d'un alliage de titane | |
CN102626770A (zh) | 一种裂解型连杆的制造方法 | |
US10927436B2 (en) | Aluminum alloys | |
CN105838928A (zh) | 高强度铝合金板 | |
CN107338379B (zh) | 一种镁-锡-锌-铝-锰变形镁合金及其制备方法 | |
EP2011591A3 (fr) | Appareil de distribution de métal fondu et procédé de fabrication d'un tel appareil | |
CN203791594U (zh) | 用于金属的连铸成型加工设备 | |
CN109022964A (zh) | 一种高硬度89-104mm淬透性7000系铸态铝合金 | |
CN109097644A (zh) | 一种用于汽车转向节的高强度铝合金及其制备汽车转向节的方法 | |
Antonyuk et al. | Titanium alloys for aircraft industry of Ukraine. | |
WO2007015131A3 (fr) | Electrode et son procede de formation | |
ZA200609947B (en) | Casting method and casting installation for aluminium or aluminium alloys |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
ST | Notification of lapse |
Effective date: 20110502 |