WO2003085145A3 - Produits en alliages al-zn-mg- cu - Google Patents

Produits en alliages al-zn-mg- cu Download PDF

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Publication number
WO2003085145A3
WO2003085145A3 PCT/FR2003/001062 FR0301062W WO03085145A3 WO 2003085145 A3 WO2003085145 A3 WO 2003085145A3 FR 0301062 W FR0301062 W FR 0301062W WO 03085145 A3 WO03085145 A3 WO 03085145A3
Authority
WO
WIPO (PCT)
Prior art keywords
tolerance
damage
mechanical properties
alloy products
static mechanical
Prior art date
Application number
PCT/FR2003/001062
Other languages
English (en)
Other versions
WO2003085145A2 (fr
Inventor
Timothy Warner
Christophe Sigli
Bernard Bes
Original Assignee
Pechiney Rhenalu
Timothy Warner
Christophe Sigli
Bernard Bes
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=28052141&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=WO2003085145(A3) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Pechiney Rhenalu, Timothy Warner, Christophe Sigli, Bernard Bes filed Critical Pechiney Rhenalu
Priority to AU2003260001A priority Critical patent/AU2003260001A1/en
Priority to AT03740568T priority patent/ATE452216T1/de
Priority to EP03740568A priority patent/EP1492895B1/fr
Priority to DE60330547T priority patent/DE60330547D1/de
Priority to JP2003582320A priority patent/JP4535731B2/ja
Priority to DE03740568T priority patent/DE03740568T1/de
Publication of WO2003085145A2 publication Critical patent/WO2003085145A2/fr
Publication of WO2003085145A3 publication Critical patent/WO2003085145A3/fr

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/10Alloys based on aluminium with zinc as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/053Changing 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

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Heat Treatment Of Steel (AREA)
  • Extrusion Of Metal (AREA)
  • Metal Rolling (AREA)
  • Laminated Bodies (AREA)
  • Conductive Materials (AREA)
  • Forging (AREA)
  • Contacts (AREA)

Abstract

L'invention concerne un produit laminé, filé ou forgé en alliage Al-Zn-Mg-Cu, caractérisé en ce qu'il contient (en pourcents massiques) : a) Zn 8,3 - 14,0 Cu 0,3 - 4,0 Mg 0,5 - 4,5 Zr 0,03 - 0,15 Fe + Si < 0,25 b) au moins un élément sélectionné dans le groupe composé de Sc, Hf, La, Ti, Ce, Nd, Eu, Gd, Tb, Dy, Ho, Er, Y, Yb, la teneur de chacun desdit éléments, s'il est sélectionné, étant comprise entre 0,02 et 0,7 %, c) le reste aluminium et impuretés inévitables, et en qu'il satisfait aux conditions d) Mg / Cu < 2,4 et e) (7,7 - 0,4 Zn) > (Cu + Mg) > (6,4 - 0,4 Zn). Ces produits peuvent être utilisés comme éléments de structure (par exemple caisson de voilure, extrados de voilure) en construction aéronautique.
PCT/FR2003/001062 2002-04-05 2003-04-04 Produits en alliages al-zn-mg- cu WO2003085145A2 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
AU2003260001A AU2003260001A1 (en) 2002-04-05 2003-04-04 Al-zn-mg-cu alloy products displaying an improved compromise between static mechanical properties and tolerance to damage
AT03740568T ATE452216T1 (de) 2002-04-05 2003-04-04 Produkte aus al-zn-mg-cu-legierung
EP03740568A EP1492895B1 (fr) 2002-04-05 2003-04-04 Produits en alliages al-zn-mg-cu
DE60330547T DE60330547D1 (de) 2002-04-05 2003-04-04 Produkte aus al-zn-mg-cu-legierung
JP2003582320A JP4535731B2 (ja) 2002-04-05 2003-04-04 静的機械的特性/耐損傷性の調和が向上したal−zn−mg−cu合金製品
DE03740568T DE03740568T1 (de) 2002-04-05 2003-04-04 Produkte aus al-zn-mg-cu-legierungen

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0204257A FR2838136B1 (fr) 2002-04-05 2002-04-05 PRODUITS EN ALLIAGE A1-Zn-Mg-Cu A COMPROMIS CARACTERISTIQUES STATISTIQUES/TOLERANCE AUX DOMMAGES AMELIORE
FR02/04257 2002-04-05

Publications (2)

Publication Number Publication Date
WO2003085145A2 WO2003085145A2 (fr) 2003-10-16
WO2003085145A3 true WO2003085145A3 (fr) 2004-04-01

Family

ID=28052141

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2003/001062 WO2003085145A2 (fr) 2002-04-05 2003-04-04 Produits en alliages al-zn-mg- cu

Country Status (9)

Country Link
US (1) US7550110B2 (fr)
EP (1) EP1492895B1 (fr)
JP (1) JP4535731B2 (fr)
AT (1) ATE452216T1 (fr)
AU (1) AU2003260001A1 (fr)
DE (2) DE03740568T1 (fr)
ES (1) ES2338314T3 (fr)
FR (1) FR2838136B1 (fr)
WO (1) WO2003085145A2 (fr)

Families Citing this family (62)

* Cited by examiner, † Cited by third party
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US20050217770A1 (en) * 2004-03-23 2005-10-06 Philippe Lequeu Structural member for aeronautical construction with a variation of usage properties
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
DE102005045341A1 (de) * 2004-10-05 2006-07-20 Corus Aluminium Walzprodukte Gmbh Hochfestes, hochzähes Al-Zn-Legierungsprodukt und Verfahren zum Herstellen eines solches Produkts
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US20070151636A1 (en) * 2005-07-21 2007-07-05 Corus Aluminium Walzprodukte Gmbh Wrought aluminium AA7000-series alloy product and method of producing said product
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US8017072B2 (en) 2008-04-18 2011-09-13 United Technologies Corporation Dispersion strengthened L12 aluminum alloys
US8409373B2 (en) 2008-04-18 2013-04-02 United Technologies Corporation L12 aluminum alloys with bimodal and trimodal distribution
US7871477B2 (en) 2008-04-18 2011-01-18 United Technologies Corporation High strength L12 aluminum alloys
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US7879162B2 (en) * 2008-04-18 2011-02-01 United Technologies Corporation High strength aluminum alloys with L12 precipitates
US7811395B2 (en) 2008-04-18 2010-10-12 United Technologies Corporation High strength L12 aluminum alloys
RU2503735C2 (ru) * 2008-06-24 2014-01-10 Алерис Алюминум Кобленц Гмбх ИЗДЕЛИЕ ИЗ Al-Zn-Mg СПЛАВА С ПОНИЖЕННОЙ ЧУВСТВИТЕЛЬНОСТЬЮ К ЗАКАЛКЕ
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US8778099B2 (en) 2008-12-09 2014-07-15 United Technologies Corporation Conversion process for heat treatable L12 aluminum alloys
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
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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
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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
WO2015132932A1 (fr) * 2014-03-06 2015-09-11 株式会社Uacj Alliage d'aluminium structural et son procédé de production
CN105349852A (zh) * 2015-10-28 2016-02-24 无棣向上机械设计服务有限公司 高强度铝合金
CN105401026B (zh) * 2015-12-08 2017-12-26 艾瑞福斯特(北京)技术开发有限公司 一种超高强铝合金粉
CN105609751A (zh) * 2016-03-15 2016-05-25 江苏中科亚美新材料有限公司 一种用于电池负极的镁合金
CN105838947B (zh) * 2016-06-02 2017-05-10 薛元良 一种超高强度抗耐磨铝合金材料及其生产工艺
CA3032261A1 (fr) 2016-08-26 2018-03-01 Shape Corp. Procede de formage a chaud et appareil de pliage transversal d'une poutre d'aluminium profilee pour former a chaud un composant structural de vehicule
EP3305926B1 (fr) * 2016-10-05 2019-07-24 Aleris Rolled Products Germany GmbH Élément structurel soudé et procédé de fabrication et d'utilisation de celui-ci
EP3529394A4 (fr) 2016-10-24 2020-06-24 Shape Corp. Procédé de formage et de traitement thermique d'un alliage d'aluminium en plusieurs étapes pour la production de composants pour véhicules
CN107475572A (zh) * 2017-08-16 2017-12-15 吴振江 超细铝合金线材及其制造方法以及相应的衍生品
CN109161743A (zh) * 2018-09-28 2019-01-08 武汉理工大学 一种耐腐蚀稀土微合金化铝合金及其制备方法
KR102203716B1 (ko) * 2019-03-08 2021-01-15 한국생산기술연구원 압출성 및 강도가 향상된 고열전도도 알루미늄 합금, 상기 알루미늄 합금 제조 방법 및 상기 알루미늄 합금 압출성형제품 제작 방법
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
WO2021029925A1 (fr) * 2019-06-03 2021-02-18 Novelis Inc. Produits en alliage d'aluminium à ultra-haute résistance et leurs procédés de fabrication
CN110669968A (zh) * 2019-09-23 2020-01-10 山东南山铝业股份有限公司 一种耐热稀土铝合金及其制备方法
CN110846525B (zh) * 2019-11-29 2020-10-23 内蒙古工业大学 一种铝-硅-镁铸造合金力学性能的改善方法
CN111101033A (zh) * 2019-12-20 2020-05-05 山东南山铝业股份有限公司 一种低合金化铝合金及其多级热处理强化工艺
CN111020315A (zh) * 2019-12-20 2020-04-17 山东南山铝业股份有限公司 一种稀土耐热铝合金及其制备方法
CN111057920B (zh) * 2020-01-07 2022-05-06 西南交通大学 一种超高强铝合金及其制备方法
CN111959608B (zh) * 2020-08-14 2021-06-29 福建祥鑫股份有限公司 一种铝合金轻卡大梁及其制备方法
CN113215458B (zh) * 2021-07-02 2023-02-24 中国航发北京航空材料研究院 一种铝合金及铝合金的制作方法
CN114134375B (zh) * 2021-11-01 2022-09-27 湖南中创空天新材料股份有限公司 一种耐应力腐蚀Al-Zn-Mg-Cu合金及其制备方法
CN114990395B (zh) * 2022-04-13 2024-01-16 山东南山铝业股份有限公司 一种含稀土元素的高强度变形铝合金及其制备方法
CN115961191B (zh) * 2022-04-25 2024-06-21 江苏大学 一种锶锆钛钇四元复合微合金化的800MPa强度级高性能铝合金及制备方法
CN115710661B (zh) * 2022-10-31 2024-04-09 中国航发北京航空材料研究院 一种Al-Zn-Mg-Cu系铝合金及提高其应力腐蚀性能的方法

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EP0081441A1 (fr) * 1981-12-03 1983-06-15 Societe Metallurgique De Gerzat Méthode pour l'obtention de produits filés en alliages type Al-Zn-Mg-Cu à haute résistance et à tenacité sens travers améliorée
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EP0670377A1 (fr) * 1994-03-02 1995-09-06 Pechiney Recherche (Gie) Alliage d'aluminium 7000 à haute résistance mécanique et procédé d'obtention
EP1231290A1 (fr) * 2001-02-07 2002-08-14 Pechiney Rhenalu Procédé de fabrication d'un produit corroyé à haute résistance en alliage AIZnMgCu

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Also Published As

Publication number Publication date
ATE452216T1 (de) 2010-01-15
DE03740568T1 (de) 2005-07-14
EP1492895A2 (fr) 2005-01-05
WO2003085145A2 (fr) 2003-10-16
US7550110B2 (en) 2009-06-23
JP2005528521A (ja) 2005-09-22
AU2003260001A1 (en) 2003-10-20
ES2338314T3 (es) 2010-05-06
JP4535731B2 (ja) 2010-09-01
FR2838136B1 (fr) 2005-01-28
EP1492895B1 (fr) 2009-12-16
FR2838136A1 (fr) 2003-10-10
DE60330547D1 (de) 2010-01-28
US20030219353A1 (en) 2003-11-27

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