ES2316779T3 - Productos forjados de aleaciones al-zn-mg-cu de caracteristicas mecanicas muy elevadas y elementos de estructura de aeronave. - Google Patents

Productos forjados de aleaciones al-zn-mg-cu de caracteristicas mecanicas muy elevadas y elementos de estructura de aeronave. Download PDF

Info

Publication number
ES2316779T3
ES2316779T3 ES03740569T ES03740569T ES2316779T3 ES 2316779 T3 ES2316779 T3 ES 2316779T3 ES 03740569 T ES03740569 T ES 03740569T ES 03740569 T ES03740569 T ES 03740569T ES 2316779 T3 ES2316779 T3 ES 2316779T3
Authority
ES
Spain
Prior art keywords
stiffeners
product according
elements
mpa
fuselage
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 - Lifetime
Application number
ES03740569T
Other languages
English (en)
Spanish (es)
Inventor
Frank Eberl
Christophe Sigli
Timothy Warner
Sjoerd Van Der Veen
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.)
Constellium Issoire SAS
Original Assignee
Alcan Rhenalu 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=28052134&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ES2316779(T3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Alcan Rhenalu SAS filed Critical Alcan Rhenalu SAS
Application granted granted Critical
Publication of ES2316779T3 publication Critical patent/ES2316779T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • C22F1/053—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 zinc 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
    • C22C21/10—Alloys based on aluminium with zinc as the next major constituent

Landscapes

  • Chemical & Material Sciences (AREA)
  • Organic Chemistry (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Heat Treatment Of Steel (AREA)
  • Extrusion Of Metal (AREA)
  • Conductive Materials (AREA)
  • Crushing And Pulverization Processes (AREA)
  • Preparation Of Clay, And Manufacture Of Mixtures Containing Clay Or Cement (AREA)
  • Metal Rolling (AREA)
  • Physical Vapour Deposition (AREA)
ES03740569T 2002-04-05 2003-04-04 Productos forjados de aleaciones al-zn-mg-cu de caracteristicas mecanicas muy elevadas y elementos de estructura de aeronave. Expired - Lifetime ES2316779T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0204250 2002-04-05
FR0204250A FR2838135B1 (fr) 2002-04-05 2002-04-05 PRODUITS CORROYES EN ALLIAGES A1-Zn-Mg-Cu A TRES HAUTES CARACTERISTIQUES MECANIQUES, ET ELEMENTS DE STRUCTURE D'AERONEF

Publications (1)

Publication Number Publication Date
ES2316779T3 true ES2316779T3 (es) 2009-04-16

Family

ID=28052134

Family Applications (1)

Application Number Title Priority Date Filing Date
ES03740569T Expired - Lifetime ES2316779T3 (es) 2002-04-05 2003-04-04 Productos forjados de aleaciones al-zn-mg-cu de caracteristicas mecanicas muy elevadas y elementos de estructura de aeronave.

Country Status (9)

Country Link
US (2) US20050072497A1 (fr)
EP (1) EP1492896B1 (fr)
JP (1) JP2005530032A (fr)
AT (1) ATE415498T1 (fr)
AU (1) AU2003260003A1 (fr)
DE (2) DE60324903D1 (fr)
ES (1) ES2316779T3 (fr)
FR (1) FR2838135B1 (fr)
WO (1) WO2003085146A1 (fr)

Families Citing this family (63)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2292331B2 (es) * 2003-03-17 2009-09-16 Corus Aluminium Walzprodukte Gmbh Metodo para producir una estructura monolitica de aluminio integrada y un producto de aluminio mecanizado a partir de esa estructura.
DE112004003147B4 (de) * 2003-04-10 2022-11-17 Novelis Koblenz Gmbh Al-Zn-Mg-Cu-Legierung
US20050034794A1 (en) * 2003-04-10 2005-02-17 Rinze Benedictus High strength Al-Zn alloy and method for producing such an alloy product
US20060032560A1 (en) * 2003-10-29 2006-02-16 Corus Aluminium Walzprodukte Gmbh Method for producing a high damage tolerant aluminium alloy
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
ES2292075T5 (es) 2005-01-19 2010-12-17 Otto Fuchs Kg Aleacion de aluminio no sensible al enfriamiento brusco, asi como procedimiento para fabricar un producto semiacabado a partir de esta aleacion.
EP1848835A2 (fr) * 2005-02-01 2007-10-31 Timothy Langan Alliages d'alumnium-zinc-magnesium-scandium et leurs procedes de fabrication
US20060289093A1 (en) * 2005-05-25 2006-12-28 Howmet Corporation Al-Zn-Mg-Ag high-strength alloy for aerospace and automotive castings
US8157932B2 (en) * 2005-05-25 2012-04-17 Alcoa Inc. Al-Zn-Mg-Cu-Sc high strength alloy for aerospace and automotive castings
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
US8083871B2 (en) 2005-10-28 2011-12-27 Automotive Casting Technology, Inc. High crashworthiness Al-Si-Mg alloy and methods for producing automotive casting
MX2008016076A (es) * 2006-06-30 2009-01-15 Alcan Rolled Products Ravenswood Llc Aleacion de aluminio al-zn-mg termo-tratable de alta resistencia.
FR2907796B1 (fr) * 2006-07-07 2011-06-10 Aleris Aluminum Koblenz Gmbh Produits en alliage d'aluminium de la serie aa7000 et leur procede de fabrication
US8088234B2 (en) * 2006-07-07 2012-01-03 Aleris Aluminum Koblenz Gmbh AA2000-series aluminum alloy products and a method of manufacturing thereof
FR2910874B1 (fr) * 2007-01-02 2009-02-13 Airbus France Sas Lisses assemblees au niveau d'une jonction circonferentielle d'un fuselage d'avion.
KR20090127185A (ko) 2007-03-30 2009-12-09 디렉터 제너럴, 디펜스 리써치 앤드 디벨롭먼트 오거니제이션 합금 조성물 및 그 제조방법
US8673209B2 (en) * 2007-05-14 2014-03-18 Alcoa Inc. Aluminum alloy products having improved property combinations and method for artificially aging same
US8840737B2 (en) * 2007-05-14 2014-09-23 Alcoa Inc. Aluminum alloy products having improved property combinations and method for artificially aging same
US8017072B2 (en) 2008-04-18 2011-09-13 United Technologies Corporation Dispersion strengthened L12 aluminum alloys
US7875131B2 (en) 2008-04-18 2011-01-25 United Technologies Corporation L12 strengthened amorphous aluminum alloys
US20090263273A1 (en) 2008-04-18 2009-10-22 United Technologies Corporation High strength L12 aluminum alloys
US7811395B2 (en) 2008-04-18 2010-10-12 United Technologies Corporation High strength L12 aluminum alloys
US7879162B2 (en) * 2008-04-18 2011-02-01 United Technologies Corporation High strength aluminum alloys with L12 precipitates
US8002912B2 (en) 2008-04-18 2011-08-23 United Technologies Corporation High strength L12 aluminum alloys
US7875133B2 (en) 2008-04-18 2011-01-25 United Technologies Corporation Heat treatable L12 aluminum alloys
US7871477B2 (en) 2008-04-18 2011-01-18 United Technologies Corporation High strength L12 aluminum alloys
US8409373B2 (en) 2008-04-18 2013-04-02 United Technologies Corporation L12 aluminum alloys with bimodal and trimodal distribution
US8778098B2 (en) 2008-12-09 2014-07-15 United Technologies Corporation Method for producing high strength aluminum alloy powder containing L12 intermetallic dispersoids
US8778099B2 (en) 2008-12-09 2014-07-15 United Technologies Corporation Conversion process for heat treatable L12 aluminum alloys
US8206517B1 (en) 2009-01-20 2012-06-26 Alcoa Inc. Aluminum alloys having improved ballistics and armor protection performance
US9611522B2 (en) 2009-05-06 2017-04-04 United Technologies Corporation Spray deposition of L12 aluminum alloys
US9127334B2 (en) 2009-05-07 2015-09-08 United Technologies Corporation Direct forging and rolling of L12 aluminum alloys for armor applications
US8728389B2 (en) 2009-09-01 2014-05-20 United Technologies Corporation Fabrication of L12 aluminum alloy tanks and other vessels by roll forming, spin forming, and friction stir welding
US8409496B2 (en) 2009-09-14 2013-04-02 United Technologies Corporation Superplastic forming high strength L12 aluminum alloys
US9194027B2 (en) 2009-10-14 2015-11-24 United Technologies Corporation Method of forming high strength aluminum alloy parts containing L12 intermetallic dispersoids by ring rolling
US8409497B2 (en) 2009-10-16 2013-04-02 United Technologies Corporation Hot and cold rolling high strength L12 aluminum alloys
CN102108463B (zh) 2010-01-29 2012-09-05 北京有色金属研究总院 一种适合于结构件制造的铝合金制品及制备方法
US9163304B2 (en) 2010-04-20 2015-10-20 Alcoa Inc. High strength forged aluminum alloy products
JP5535957B2 (ja) * 2011-02-21 2014-07-02 三菱航空機株式会社 翼パネルの形成方法
US9551050B2 (en) * 2012-02-29 2017-01-24 The Boeing Company Aluminum alloy with additions of scandium, zirconium and erbium
KR101526660B1 (ko) 2013-05-07 2015-06-05 현대자동차주식회사 복합 미세조직을 갖는 내마모성 합금
KR101526656B1 (ko) 2013-05-07 2015-06-05 현대자동차주식회사 복합 미세조직을 갖는 내마모성 합금
KR101526661B1 (ko) 2013-05-07 2015-06-05 현대자동차주식회사 복합 미세조직을 갖는 내마모성 합금
DE112014003239T5 (de) * 2013-07-12 2016-04-07 Magna International Inc. Verfahren zur Formung von Aluminiumlegierungsteilen mit angepassten mechanischen Eigenschaften
DE102013012259B3 (de) * 2013-07-24 2014-10-09 Airbus Defence and Space GmbH Aluminium-Werkstoff mit verbesserter Ausscheidungshärtung, Verfahren zu dessen Herstellung und Verwendung des Aluminium-Werkstoffes
CN103572106B (zh) * 2013-11-22 2016-08-17 湖南稀土金属材料研究院 铝合金材料
WO2015132932A1 (fr) * 2014-03-06 2015-09-11 株式会社Uacj Alliage d'aluminium structural et son procédé de production
CN104109784B (zh) * 2014-04-30 2016-09-14 广西南南铝加工有限公司 一种超高强度Al-Zn-Mg-Cu系铝合金大规格扁铸锭及其制造方法
JP6638193B2 (ja) * 2015-02-20 2020-01-29 日本軽金属株式会社 アルミニウム合金加工材及びその製造方法
JP6638192B2 (ja) * 2015-02-20 2020-01-29 日本軽金属株式会社 アルミニウム合金加工材及びその製造方法
CN106367644B (zh) * 2016-09-23 2018-03-13 北京工业大学 一种超高强、高硬度TiB2颗粒增强Al‑Zn‑Mg‑Cu复合材料及其制备方法
CN106399776B (zh) * 2016-11-11 2018-05-01 佛山科学技术学院 一种800MPa级超高强铝合金及其制备方法
WO2020099174A1 (fr) * 2018-11-12 2020-05-22 Aleris Rolled Products Germany Gmbh Produit en alliage d'aluminium série 7xxx
CN109977457B (zh) * 2019-02-02 2020-11-24 浙江大学 一种考虑温卷影响的加钒钢制筒节极限载荷预测方法
US11958140B2 (en) 2019-05-10 2024-04-16 General Cable Technologies Corporation Aluminum welding alloys with improved performance
CN110331319B (zh) * 2019-05-27 2020-06-30 中国航发北京航空材料研究院 一种含钪和铒的高强、高塑性耐蚀铝合金及其制备方法
MX2021010324A (es) * 2019-06-03 2021-09-28 Novelis Inc Productos de aleacion de aluminio de ultra alta resistencia y metodos para producir los mismos.
CN112226636A (zh) * 2020-09-08 2021-01-15 烟台南山学院 一种高强耐蚀Al-Zn-Mg-Cu-Zr-Ce合金板材的制备方法
CN112981196B (zh) * 2021-02-10 2022-04-22 北京科技大学 一种超高强度、高韧性Al-Zn-Mg-Cu铝合金及其制备方法
CN115216674B (zh) * 2022-07-11 2023-02-24 上海交通大学 一种汽车用7000系铝合金薄板及其制备方法
CN115287511A (zh) * 2022-09-06 2022-11-04 安徽辉隆集团辉铝新材料科技有限公司 一种7020超硬铝合金型材及制备方法
CN115537615A (zh) * 2022-10-26 2022-12-30 山东南山铝业股份有限公司 一种用于汽车门窗饰条高光亮铝合金及制备方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4863528A (en) * 1973-10-26 1989-09-05 Aluminum Company Of America Aluminum alloy product having improved combinations of strength and corrosion resistance properties and method for producing the same
US4063936A (en) * 1974-01-14 1977-12-20 Alloy Trading Co., Ltd. Aluminum alloy having high mechanical strength and elongation and resistant to stress corrosion crack
FR2457908A1 (fr) * 1979-06-01 1980-12-26 Gerzat Metallurg Procede de fabrication de corps creux en alliage d'aluminium et produits ainsi obtenus
FR2517702B1 (fr) * 1981-12-03 1985-11-15 Gerzat Metallurg
JPH0635624B2 (ja) * 1985-05-10 1994-05-11 昭和アルミニウム株式会社 高強度アルミニウム合金押出材の製造法
FR2601967B1 (fr) * 1986-07-24 1992-04-03 Cerzat Ste Metallurg Alliage a base d'al pour corps creux sous pression.
US5221377A (en) * 1987-09-21 1993-06-22 Aluminum Company Of America Aluminum alloy product having improved combinations of properties
FR2640644B1 (fr) * 1988-12-19 1991-02-01 Pechiney Recherche Procede d'obtention par " pulverisation-depot " d'alliages d'al de la serie 7000 et de materiaux composites a renforts discontinus ayant pour matrice ces alliages a haute resistance mecanique et bonne ductilite
FR2716896B1 (fr) * 1994-03-02 1996-04-26 Pechiney Recherche Alliage 7000 à haute résistance mécanique et procédé d'obtention.
US6562154B1 (en) * 2000-06-12 2003-05-13 Aloca Inc. Aluminum sheet products having improved fatigue crack growth resistance and methods of making same
FR2838136B1 (fr) * 2002-04-05 2005-01-28 Pechiney Rhenalu PRODUITS EN ALLIAGE A1-Zn-Mg-Cu A COMPROMIS CARACTERISTIQUES STATISTIQUES/TOLERANCE AUX DOMMAGES AMELIORE
US7060139B2 (en) * 2002-11-08 2006-06-13 Ues, Inc. High strength aluminum alloy composition

Also Published As

Publication number Publication date
WO2003085146A1 (fr) 2003-10-16
EP1492896A1 (fr) 2005-01-05
AU2003260003A1 (en) 2003-10-20
FR2838135A1 (fr) 2003-10-10
ATE415498T1 (de) 2008-12-15
FR2838135B1 (fr) 2005-01-28
JP2005530032A (ja) 2005-10-06
DE03740569T1 (de) 2005-06-23
US20060182650A1 (en) 2006-08-17
EP1492896B1 (fr) 2008-11-26
US20050072497A1 (en) 2005-04-07
DE60324903D1 (de) 2009-01-08

Similar Documents

Publication Publication Date Title
ES2316779T3 (es) Productos forjados de aleaciones al-zn-mg-cu de caracteristicas mecanicas muy elevadas y elementos de estructura de aeronave.
ES2338314T3 (es) Productos de aleaciones al-zn-mg-cu.
EP3026136B1 (fr) Produits en alliage d'aluminium présentant des combinaisons de propriétés améliorées et procédés pour leur vieillissement artificiel
ES2393366B2 (es) UNA ALEACIÓN DE Al-Zn-Mg-Cu.
US20190136356A1 (en) Aluminium-copper-lithium products
US8961715B2 (en) Aluminum alloy products having improved property combinations and method for artificially aging same
ES2314929T3 (es) Chapa de aluminio-cobre-litio con alta tenacidad para fuselaje de avion.
US7744704B2 (en) High fracture toughness aluminum-copper-lithium sheet or light-gauge plate suitable for use in a fuselage panel
RU2345172C2 (ru) Способ изготовления цельной монолитной алюминиевой конструкции и алюминиевое изделие, изготовленное путем механической обработки резанием из такой конструкции
US20080145266A1 (en) High damage tolerant aa6xxx-series alloy for aerospace application
US20120291925A1 (en) Aluminum magnesium lithium alloy with improved fracture toughness
US10196722B2 (en) Method for manufacturing a structural element having a variable thickness for aircraft production
US20110209801A2 (en) Aluminum-Copper-Lithium Alloy With Improved Mechanical Strength and Toughness
US20170218493A1 (en) Method for manufacturing products made of magnesium-lithium-aluminum alloy
BRPI0411873B1 (pt) elementos de estrutura para construção aeronáutica, fabricado a partir de pelo menos um produto trefilado, laminado ou forjado em liga de alumínio e processo de fabricação
KR20210126107A (ko) 클래드 2xxx-계열 항공우주 제품
KR20220046673A (ko) 클래드 2xxx 시리즈 항공우주 제품