DE202008018370U1 - Al-Cu-Li Legierungsprodukt, welches für eine Luftfahrzeuganwendung geeignet ist - Google Patents

Al-Cu-Li Legierungsprodukt, welches für eine Luftfahrzeuganwendung geeignet ist Download PDF

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Publication number
DE202008018370U1
DE202008018370U1 DE202008018370U DE202008018370U DE202008018370U1 DE 202008018370 U1 DE202008018370 U1 DE 202008018370U1 DE 202008018370 U DE202008018370 U DE 202008018370U DE 202008018370 U DE202008018370 U DE 202008018370U DE 202008018370 U1 DE202008018370 U1 DE 202008018370U1
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DE
Germany
Prior art keywords
product
aluminum alloy
alloy product
range
aluminum
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
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DE202008018370U
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German (de)
English (en)
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.)
Novelis Koblenz GmbH
Original Assignee
Aleris Rolled Products Germany GmbH
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Filing date
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Application filed by Aleris Rolled Products Germany GmbH filed Critical Aleris Rolled Products Germany GmbH
Publication of DE202008018370U1 publication Critical patent/DE202008018370U1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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
    • 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
DE202008018370U 2007-09-21 2008-09-16 Al-Cu-Li Legierungsprodukt, welches für eine Luftfahrzeuganwendung geeignet ist Expired - Lifetime DE202008018370U1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
EP07018595 2007-09-21
EP07018595.4 2007-09-21

Publications (1)

Publication Number Publication Date
DE202008018370U1 true DE202008018370U1 (de) 2013-04-30

Family

ID=38754771

Family Applications (2)

Application Number Title Priority Date Filing Date
DE112008002522T Withdrawn DE112008002522T5 (de) 2007-09-21 2008-09-16 Al-Cu-Li Legierungsprodukt, welches für eine Luftfahrzeuganwendung geeignet ist
DE202008018370U Expired - Lifetime DE202008018370U1 (de) 2007-09-21 2008-09-16 Al-Cu-Li Legierungsprodukt, welches für eine Luftfahrzeuganwendung geeignet ist

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE112008002522T Withdrawn DE112008002522T5 (de) 2007-09-21 2008-09-16 Al-Cu-Li Legierungsprodukt, welches für eine Luftfahrzeuganwendung geeignet ist

Country Status (5)

Country Link
CN (2) CN103266246B (zh)
CA (1) CA2700250C (zh)
DE (2) DE112008002522T5 (zh)
RU (2) RU2481412C2 (zh)
WO (1) WO2009036953A1 (zh)

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EP2829623B1 (en) 2007-12-04 2018-02-07 Arconic Inc. Improved aluminum-copper-lithium alloys
FR2947282B1 (fr) * 2009-06-25 2011-08-05 Alcan Rhenalu Alliage aluminium cuivre lithium a resistance mecanique et tenacite ameliorees
EP3404123A1 (en) * 2010-04-12 2018-11-21 Arconic Inc. 2xxx series aluminum lithium alloys having low strength differential
CA2810250A1 (en) * 2010-09-08 2012-03-15 Alcoa Inc. Improved aluminum-lithium alloys, and methods for producing the same
CN102021457B (zh) * 2010-10-27 2012-06-27 中国航空工业集团公司北京航空材料研究院 一种高强韧铝锂合金及其制备方法
CN101967588B (zh) * 2010-10-27 2012-08-29 中国航空工业集团公司北京航空材料研究院 一种耐损伤铝锂合金及其制备方法
CN101967589B (zh) * 2010-10-27 2013-02-20 中国航空工业集团公司北京航空材料研究院 一种中强高韧铝锂合金及其制备方法
FR2969177B1 (fr) * 2010-12-20 2012-12-21 Alcan Rhenalu Alliage aluminium cuivre lithium a resistance en compression et tenacite ameliorees
US20120225271A1 (en) * 2011-02-17 2012-09-06 Alcoa Inc. 2xxx series aluminum lithium alloys
FR2975403B1 (fr) * 2011-05-20 2018-11-02 Constellium Issoire Alliage aluminium magnesium lithium a tenacite amelioree
WO2013172910A2 (en) 2012-03-07 2013-11-21 Alcoa Inc. Improved 2xxx aluminum alloys, and methods for producing the same
FR2989387B1 (fr) 2012-04-11 2014-11-07 Constellium France Alliage aluminium cuivre lithium a resistance au choc amelioree
CN102634706A (zh) * 2012-04-28 2012-08-15 中南大学 一种高强、高韧、耐蚀Al-Cu-Mg铝合金
US9458528B2 (en) 2012-05-09 2016-10-04 Alcoa Inc. 2xxx series aluminum lithium alloys
US20140050936A1 (en) * 2012-08-17 2014-02-20 Alcoa Inc. 2xxx series aluminum lithium alloys
EP2937435A4 (en) * 2012-12-21 2016-09-07 Kawasaki Heavy Ind Ltd METHOD FOR MANUFACTURING AN ALUMINUM ALLOY SHAPED COMPONENT FOR AN AIRCRAFT AND SHAPED COMPONENT FOR AN AIRCRAFT
US9587298B2 (en) 2013-02-19 2017-03-07 Arconic Inc. Heat treatable aluminum alloys having magnesium and zinc and methods for producing the same
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.
FR3007423B1 (fr) * 2013-06-21 2015-06-05 Constellium France Element de structure extrados en alliage aluminium cuivre lithium
CN103397229B (zh) * 2013-08-02 2015-04-08 贵州合润铝业高新科技发展有限公司 一种铝合金的制备方法
CN103352146B (zh) * 2013-08-02 2015-04-08 贵州合润铝业高新科技发展有限公司 铝合金
CN104018043B (zh) * 2014-06-19 2016-08-24 芜湖市泰美机械设备有限公司 一种高强度航空用铸造铝合金及其热处理方法
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
US10253404B2 (en) * 2014-10-26 2019-04-09 Kaiser Aluminum Fabricated Products, Llc High strength, high formability, and low cost aluminum-lithium alloys
EP3072984B2 (de) 2015-03-27 2020-05-06 Otto Fuchs KG Al-cu-mg-li-legierung sowie daraus hergestelltes legierungsprodukt
EP3380640B1 (de) * 2015-11-25 2019-02-27 Otto Fuchs - Kommanditgesellschaft - Rohr zur verwendung im zusammenhang mit einer tiefbohrung
EP3390678B1 (en) 2015-12-18 2020-11-25 Novelis, Inc. High strength 6xxx aluminum alloys and methods of making the same
KR20170125984A (ko) * 2015-12-18 2017-11-15 노벨리스 인크. 고-강도 6xxx 알루미늄 합금 및 이것의 제조 방법
FR3047253B1 (fr) 2016-02-03 2018-01-12 Constellium Issoire Toles epaisses en alliage al - cu - li a proprietes en fatigue ameliorees
CN109072358A (zh) * 2016-02-09 2018-12-21 爱励轧制产品德国有限责任公司 Al-Cu-Li-Mg-Mn-Zn合金锻制产品
CN106131719B (zh) * 2016-08-30 2019-02-05 宁波泊人艾电子有限公司 一种便携音箱
CN106131720B (zh) * 2016-08-30 2019-02-05 宁波泊人艾电子有限公司 一种多功能便携音箱
CN106358115A (zh) * 2016-08-30 2017-01-25 宁波大诚和电子有限公司 一种多功能便携音箱的扬声控制单元
CN106591649A (zh) * 2016-12-14 2017-04-26 沈阳工业大学 一种高强Al‑Cu‑Mg‑Mn‑Er变形铝合金及其制备方法
DE202017100517U1 (de) 2017-01-31 2018-05-03 Aleris Rolled Products Germany Gmbh Al-Cu-Li-Mg-Mn-Zn Knetlegierungsprodukt
CN106893911B (zh) * 2017-02-27 2018-05-15 广东省材料与加工研究所 一种高强耐热Al-Cu系铝合金及其制备方法
CN106884129A (zh) * 2017-03-14 2017-06-23 广州金邦液态模锻技术有限公司 一种用于挤压铸造铝合金转向节的热处理工艺
CN108118271B (zh) * 2017-12-08 2019-08-06 北京星航机电装备有限公司 一种异形铝合金舱段热处理变形控制方法
FR3080861B1 (fr) 2018-05-02 2021-03-19 Constellium Issoire Procede de fabrication d'un alliage aluminium cuivre lithium a resistance en compression et tenacite ameliorees
FR3080860B1 (fr) 2018-05-02 2020-04-17 Constellium Issoire Alliage aluminium cuivre lithium a resistance en compression et tenacite ameliorees
WO2020097169A1 (en) * 2018-11-07 2020-05-14 Arconic Inc. 2xxx aluminum lithium alloys
EP3880857A4 (en) * 2018-11-14 2022-08-03 Arconic Technologies LLC ENHANCED 7XXX ALUMINUM ALLOYS
CN110423927A (zh) * 2019-07-17 2019-11-08 中南大学 一种超高强铝锂合金及其制备方法
CN111020425B (zh) * 2019-12-25 2021-04-16 辽宁忠旺集团有限公司 一种2系铝合金热处理工艺
CN111575561B (zh) * 2020-05-25 2022-02-08 江苏豪然喷射成形合金有限公司 一种大深度承压壳体用铝锂合金及其制备方法
CN113981280B (zh) * 2021-11-01 2022-05-17 北京理工大学 一种低密度高强高弹性模量的铝锂合金及制备方法
CN114214548A (zh) * 2021-12-17 2022-03-22 中南大学 一种高强高淬透性铝锂合金及其制备方法
CN115386818A (zh) * 2022-08-25 2022-11-25 中南大学 一种Al-Cu-Li系合金热轧板坯的形变热处理方法
CN115505807B (zh) * 2022-09-21 2023-06-27 郑州轻研合金科技有限公司 一种高比强铝锂合金及其制备方法和应用
CN115710662B (zh) * 2022-11-21 2024-02-06 郑州轻研合金科技有限公司 一种高强高韧铝锂合金板材及其生产工艺

Citations (3)

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Publication number Priority date Publication date Assignee Title
US20040071586A1 (en) 1998-06-24 2004-04-15 Rioja Roberto J. Aluminum-copper-magnesium alloys having ancillary additions of lithium
WO2004106570A1 (en) 2003-05-28 2004-12-09 Pechiney Rolled Products New al-cu-li-mg-ag-mn-zr alloy for use as stractural members requiring high strength and high fracture toughness
US20070181229A1 (en) 2005-12-20 2007-08-09 Bernard Bes High fracture toughness aluminum-copper-lithium sheet or light-gauge plates suitable for fuselage panels

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BR8807653A (pt) * 1987-08-10 1990-06-12 Martin Marietta Corp Ligas de aluminio-litio soldaveis de resistencia ultra elevada
JPH03107440A (ja) * 1989-09-20 1991-05-07 Showa Alum Corp ロードセル用アルミニウム合金
US5211910A (en) * 1990-01-26 1993-05-18 Martin Marietta Corporation Ultra high strength aluminum-base alloys
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
US5393357A (en) * 1992-10-06 1995-02-28 Reynolds Metals Company Method of minimizing strength anisotropy in aluminum-lithium alloy wrought product by cold rolling, stretching and aging
US6869490B2 (en) * 2000-10-20 2005-03-22 Pechiney Rolled Products, L.L.C. High strength aluminum alloy
ES2393366B2 (es) * 2003-04-10 2013-07-01 Aleris Aluminum Koblenz Gmbh UNA ALEACIÓN DE Al-Zn-Mg-Cu.
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

Patent Citations (3)

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Publication number Priority date Publication date Assignee Title
US20040071586A1 (en) 1998-06-24 2004-04-15 Rioja Roberto J. Aluminum-copper-magnesium alloys having ancillary additions of lithium
WO2004106570A1 (en) 2003-05-28 2004-12-09 Pechiney Rolled Products New al-cu-li-mg-ag-mn-zr alloy for use as stractural members requiring high strength and high fracture toughness
US20070181229A1 (en) 2005-12-20 2007-08-09 Bernard Bes High fracture toughness aluminum-copper-lithium sheet or light-gauge plates suitable for fuselage panels

Non-Patent Citations (2)

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ASTM B871-96
EN10.002

Also Published As

Publication number Publication date
RU2481412C2 (ru) 2013-05-10
CA2700250C (en) 2016-06-28
CN103266246B (zh) 2016-09-21
RU2013102512A (ru) 2014-07-27
WO2009036953A1 (en) 2009-03-26
CN101855376B (zh) 2013-06-05
RU2627085C2 (ru) 2017-08-03
CN101855376A (zh) 2010-10-06
CA2700250A1 (en) 2009-03-26
CN103266246A (zh) 2013-08-28
RU2010110350A (ru) 2011-09-27
DE112008002522T5 (de) 2010-08-26

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Representative=s name: MUELLER SCHUPFNER & PARTNER PATENT- UND RECHTS, DE

R150 Term of protection extended to 6 years
R207 Utility model specification

Effective date: 20130627

R151 Term of protection extended to 8 years
R151 Term of protection extended to 8 years

Effective date: 20140826

R152 Term of protection extended to 10 years
R071 Expiry of right