DE60017868D1 - Strukturelement eines Flugzeugs aus Al-Cu-Mg Legierung - Google Patents
Strukturelement eines Flugzeugs aus Al-Cu-Mg LegierungInfo
- Publication number
- DE60017868D1 DE60017868D1 DE60017868T DE60017868T DE60017868D1 DE 60017868 D1 DE60017868 D1 DE 60017868D1 DE 60017868 T DE60017868 T DE 60017868T DE 60017868 T DE60017868 T DE 60017868T DE 60017868 D1 DE60017868 D1 DE 60017868D1
- Authority
- DE
- Germany
- Prior art keywords
- alloy
- structural element
- aircraft made
- aircraft
- structural
- 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.)
- Revoked
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
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/922—Static electricity metal bleed-off metallic stock
- Y10S428/923—Physical dimension
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12229—Intermediate article [e.g., blank, etc.]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
- Y10T428/12764—Next to Al-base component
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)
- Heat Treatment Of Steel (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9916610A FR2802946B1 (fr) | 1999-12-28 | 1999-12-28 | Element de structure d'avion en alliage al-cu-mg |
FR9916610 | 1999-12-28 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60017868D1 true DE60017868D1 (de) | 2005-03-10 |
DE60017868T2 DE60017868T2 (de) | 2005-12-29 |
Family
ID=9553940
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60017868T Revoked DE60017868T2 (de) | 1999-12-28 | 2000-12-20 | Strukturelement eines Flugzeugs aus Al-Cu-Mg Legierung |
Country Status (4)
Country | Link |
---|---|
US (2) | US6569542B2 (de) |
EP (1) | EP1114877B1 (de) |
DE (1) | DE60017868T2 (de) |
FR (1) | FR2802946B1 (de) |
Families Citing this family (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7323068B2 (en) | 2002-08-20 | 2008-01-29 | Aleris Aluminum Koblenz Gmbh | High damage tolerant Al-Cu alloy |
US7604704B2 (en) * | 2002-08-20 | 2009-10-20 | Aleris Aluminum Koblenz Gmbh | Balanced Al-Cu-Mg-Si alloy product |
US7494552B2 (en) | 2002-08-20 | 2009-02-24 | Aleris Aluminum Koblenz Gmbh | Al-Cu alloy with high toughness |
FR2848480B1 (fr) | 2002-12-17 | 2005-01-21 | Pechiney Rhenalu | Procede de fabrication d'elements structuraux par usinage de toles epaisses |
AU2003300632A1 (en) * | 2002-12-17 | 2004-07-14 | Pechiney Rhenalu | Method for making structural elements by machining thick plates |
GB2414242B (en) * | 2003-03-17 | 2006-10-25 | Corus Aluminium Walzprod Gmbh | Method for producing an integrated monolithic aluminium structure |
US7666267B2 (en) * | 2003-04-10 | 2010-02-23 | Aleris Aluminum Koblenz Gmbh | Al-Zn-Mg-Cu alloy with improved damage tolerance-strength combination properties |
US20050034794A1 (en) * | 2003-04-10 | 2005-02-17 | Rinze Benedictus | High strength Al-Zn alloy and method for producing such an alloy product |
CA2519390C (en) * | 2003-04-10 | 2015-06-02 | Corus Aluminium Walzprodukte Gmbh | An al-zn-mg-cu alloy |
US8043445B2 (en) | 2003-06-06 | 2011-10-25 | Aleris Aluminum Koblenz Gmbh | High-damage tolerant alloy product in particular for aerospace applications |
DE10332003B3 (de) * | 2003-07-14 | 2004-12-16 | Eads Deutschland Gmbh | Geschweißtes Aluminium-Strukturbauteil mit Aluminium-Guss-Werkstoffelementen |
FR2858984B1 (fr) * | 2003-08-19 | 2007-01-19 | Corus Aluminium Walzprod Gmbh | Produit en alliage ai-cu a haute tenacite et son procede de production |
US20060032560A1 (en) * | 2003-10-29 | 2006-02-16 | Corus Aluminium Walzprodukte Gmbh | Method for producing a high damage tolerant aluminium alloy |
US20050098245A1 (en) * | 2003-11-12 | 2005-05-12 | Venema Gregory B. | Method of manufacturing near-net shape alloy product |
US7883591B2 (en) * | 2004-10-05 | 2011-02-08 | Aleris Aluminum Koblenz Gmbh | High-strength, high toughness Al-Zn alloy product and method for producing such product |
US20070151636A1 (en) * | 2005-07-21 | 2007-07-05 | Corus Aluminium Walzprodukte Gmbh | Wrought aluminium AA7000-series alloy product and method of producing said product |
US20070204937A1 (en) * | 2005-07-21 | 2007-09-06 | Aleris Koblenz Aluminum Gmbh | Wrought aluminium aa7000-series alloy product and method of producing said product |
BRPI0617699A2 (pt) * | 2005-10-25 | 2011-08-02 | Aleris Aluminium Koblenz Gmbh | liga de al-cu-mg adequada para aplicação aeroespacial |
US20070151637A1 (en) * | 2005-10-28 | 2007-07-05 | Aleris Aluminum Koblenz Gmbh | Al-Cu-Mg ALLOY SUITABLE FOR AEROSPACE APPLICATION |
US8002913B2 (en) | 2006-07-07 | 2011-08-23 | Aleris Aluminum Koblenz Gmbh | AA7000-series aluminum alloy products and a method of manufacturing thereof |
WO2008003506A2 (en) * | 2006-07-07 | 2008-01-10 | Aleris Aluminum Koblenz Gmbh | Aa7000-series aluminium alloy products and a method of manufacturing thereof |
RU2524291C2 (ru) | 2009-01-16 | 2014-07-27 | Алерис Алюминум Кобленц Гмбх | Способ изготовления продукта-плиты из алюминиевого сплава с низкими уровнями остаточного напряжения |
US9314826B2 (en) | 2009-01-16 | 2016-04-19 | Aleris Rolled Products Germany Gmbh | Method for the manufacture of an aluminium alloy plate product having low levels of residual stress |
CN102108476B (zh) * | 2010-12-28 | 2012-02-22 | 重庆市宇一机械有限公司 | 一种高强高韧铝合金航空安全件改性制备方法 |
US9123930B1 (en) | 2011-04-29 | 2015-09-01 | Greatbatch Ltd. | Dual glass to metal seal cell |
CN103805924B (zh) * | 2012-11-14 | 2016-01-20 | 北京有色金属研究总院 | 一种适用于镁合金铸锭的均匀化处理及后续加工的方法 |
CN103103370A (zh) * | 2012-12-11 | 2013-05-15 | 龙口市丛林铝材有限公司 | 用于刹车片铝合金型材生产工艺 |
FR3011252B1 (fr) * | 2013-09-30 | 2015-10-09 | Constellium France | Tole d'intrados a proprietes de tolerance aux dommages ameliorees |
FR3040711B1 (fr) * | 2015-09-03 | 2017-08-11 | Constellium Issoire | Produit extrude en alliage al-cu-mg a compromis ameliore entre resistance mecanique et tenacite |
FR3047253B1 (fr) * | 2016-02-03 | 2018-01-12 | Constellium Issoire | Toles epaisses en alliage al - cu - li a proprietes en fatigue ameliorees |
WO2018037390A2 (en) | 2016-08-26 | 2018-03-01 | Shape Corp. | Warm forming process and apparatus for transverse bending of an extruded aluminum beam to warm form a vehicle structural component |
US11072844B2 (en) | 2016-10-24 | 2021-07-27 | Shape Corp. | Multi-stage aluminum alloy forming and thermal processing method for the production of vehicle components |
CN106513638B (zh) * | 2016-11-18 | 2019-07-12 | 喀左金牛铸造有限公司 | 2a12铝合金铸造工艺 |
CN107309658B (zh) * | 2017-06-19 | 2019-05-14 | 江西洪都航空工业集团有限责任公司 | 一种窄长蒙皮零件加工工装及工艺 |
CN107090569A (zh) * | 2017-07-07 | 2017-08-25 | 哈尔滨中飞新技术股份有限公司 | 制备高强度硬铝合金的热处理工艺 |
US20190233921A1 (en) * | 2018-02-01 | 2019-08-01 | Kaiser Aluminum Fabricated Products, Llc | Low Cost, Low Density, Substantially Ag-Free and Zn-Free Aluminum-Lithium Plate Alloy for Aerospace Application |
CN110205446B (zh) * | 2019-06-17 | 2021-02-12 | 西安理工大学 | 一种g520马氏体沉淀硬化不锈钢热处理方法 |
CN110724866A (zh) * | 2019-11-28 | 2020-01-24 | 西南铝业(集团)有限责任公司 | 一种2014铝合金航空精密轮毂模锻件的无锆毛坯 |
CN114293077B (zh) * | 2021-12-29 | 2022-09-30 | 北京理工大学 | 一种用于航空航天结构件的高强铝铜合金及制备方法 |
CN115786787B (zh) * | 2022-07-18 | 2024-02-23 | 山东浩信机械有限公司 | 一种高强韧Al-Cu系铸造铝合金及其制备方法 |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1379764A (fr) * | 1963-10-17 | 1964-11-27 | Pechiney Prod Chimiques Sa | Application nouvelle d'un alliage léger |
US3874213A (en) * | 1974-05-23 | 1975-04-01 | Alusuisse | Extrusion method for high strength heat treatable aluminum alloys |
JPS5669346A (en) | 1979-11-07 | 1981-06-10 | Showa Alum Ind Kk | Aluminum alloy for working and its manufacture |
GB2065516B (en) * | 1979-11-07 | 1983-08-24 | Showa Aluminium Ind | Cast bar of an alumium alloy for wrought products having mechanical properties and workability |
US4610733A (en) * | 1984-12-18 | 1986-09-09 | Aluminum Company Of America | High strength weldable aluminum base alloy product and method of making same |
US5376192A (en) * | 1992-08-28 | 1994-12-27 | Reynolds Metals Company | High strength, high toughness aluminum-copper-magnesium-type aluminum alloy |
FR2731440B1 (fr) * | 1995-03-10 | 1997-04-18 | Pechiney Rhenalu | Toles en alliage al-cu-mg a faible niveau de contraintes residuelles |
-
1999
- 1999-12-28 FR FR9916610A patent/FR2802946B1/fr not_active Expired - Fee Related
-
2000
- 2000-12-13 US US09/734,661 patent/US6569542B2/en not_active Expired - Lifetime
- 2000-12-20 EP EP00420263A patent/EP1114877B1/de not_active Revoked
- 2000-12-20 DE DE60017868T patent/DE60017868T2/de not_active Revoked
-
2003
- 2003-04-24 US US10/421,774 patent/US6692589B2/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE60017868T2 (de) | 2005-12-29 |
US6692589B2 (en) | 2004-02-17 |
EP1114877B1 (de) | 2005-02-02 |
US20030207141A1 (en) | 2003-11-06 |
US20010006082A1 (en) | 2001-07-05 |
EP1114877A1 (de) | 2001-07-11 |
US6569542B2 (en) | 2003-05-27 |
FR2802946A1 (fr) | 2001-06-29 |
FR2802946B1 (fr) | 2002-02-15 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE60017868D1 (de) | Strukturelement eines Flugzeugs aus Al-Cu-Mg Legierung | |
DE69911507D1 (de) | Flügelstruktur aus Faserverbundstoff | |
DE60104342D1 (de) | Flugzeugtriebwerksaufhängung | |
DE60200897D1 (de) | Gekoppeltes Flugzeugrotorsystem | |
DE19981425D2 (de) | Zwischenschicht, insbesondere Bindungsschicht, aus einer Legierung auf Aluminiumbasis | |
FR2859510B1 (fr) | Structure d'assemblage | |
DE60023413D1 (de) | Flugzeugsitz | |
DE60218456D1 (de) | Shampoos enthaltend behenylalkohol | |
DE60108338D1 (de) | Erweiterbare Toiletteneinheit eines Flugzeuges | |
DE60108920D1 (de) | Gedämpfte Schubbefestigung eines Triebwerkes | |
NO20004845L (no) | Marin konstruksjon | |
DE60135725D1 (de) | Federbeinlagerbefestigung | |
FR2819028B1 (fr) | Assemblage tubulaire | |
DE60228514D1 (de) | Integriertes Flugmanagementsystem | |
DE50001069D1 (de) | Partikelfilter aus metallfolie | |
DE59805788D1 (de) | Turbofan-flugtriebwerk | |
DE60220625D1 (de) | Verbesserungen an Turbomaschineninjektoren | |
DE60015963D1 (de) | Ermüdungserleichterung an der struktur eines luftfahrzeuges | |
DK1168920T3 (da) | (S)-enantiomerberiget fipronilpræparat | |
FR2806446B1 (fr) | Turbocompresseur | |
DE69911818D1 (de) | Luft-und raumfahrtsystem | |
DE29718613U1 (de) | Zusammenbaubares, flugfähiges Modell eines Fluggeräts | |
ATA801399A (de) | Landungsnetz | |
DE29904171U1 (de) | Tragflügel für Fluggeräte | |
UA5823S (uk) | Літак сільськогосподарський |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8331 | Complete revocation |