DE60300004D1 - Knetprodukt aus Al-Cu-Mg-Legierung für das Strukturbauteil eines Flugzeugs - Google Patents

Knetprodukt aus Al-Cu-Mg-Legierung für das Strukturbauteil eines Flugzeugs

Info

Publication number
DE60300004D1
DE60300004D1 DE60300004T DE60300004T DE60300004D1 DE 60300004 D1 DE60300004 D1 DE 60300004D1 DE 60300004 T DE60300004 T DE 60300004T DE 60300004 T DE60300004 T DE 60300004T DE 60300004 D1 DE60300004 D1 DE 60300004D1
Authority
DE
Germany
Prior art keywords
alloy
less
aircraft
structural component
product made
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
DE60300004T
Other languages
English (en)
Other versions
DE60300004T2 (de
DE60300004T3 (de
Inventor
Timothy Warner
Ronan Dif
Bernard Bes
Herve Ribes
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
Pechiney 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=29763743&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE60300004(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Pechiney Rhenalu SAS filed Critical Pechiney Rhenalu SAS
Publication of DE60300004D1 publication Critical patent/DE60300004D1/de
Publication of DE60300004T2 publication Critical patent/DE60300004T2/de
Application granted granted Critical
Publication of DE60300004T3 publication Critical patent/DE60300004T3/de
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
    • 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
    • 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)
  • Organic Chemistry (AREA)
  • Metallurgy (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Heat Treatment Of Steel (AREA)
  • Metal Rolling (AREA)
  • Conductive Materials (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Shaping Metal By Deep-Drawing, Or The Like (AREA)
  • Laminated Bodies (AREA)
  • Powder Metallurgy (AREA)
DE60300004T 2002-07-11 2003-07-09 Knetprodukt aus Al-Cu-Mg-Legierung für das Strukturbauteil eines Flugzeugs Expired - Lifetime DE60300004T3 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0208737A FR2842212B1 (fr) 2002-07-11 2002-07-11 Element de structure d'avion en alliage a1-cu-mg
FR0208737 2002-07-11
EP03356108A EP1382698B2 (de) 2002-07-11 2003-07-09 Knetprodukt aus Al-Cu-Mg-Legierung für das Strukturbauteil eines Flugzeugs

Publications (3)

Publication Number Publication Date
DE60300004D1 true DE60300004D1 (de) 2004-07-01
DE60300004T2 DE60300004T2 (de) 2005-01-20
DE60300004T3 DE60300004T3 (de) 2013-06-20

Family

ID=29763743

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60300004T Expired - Lifetime DE60300004T3 (de) 2002-07-11 2003-07-09 Knetprodukt aus Al-Cu-Mg-Legierung für das Strukturbauteil eines Flugzeugs

Country Status (6)

Country Link
US (2) US7294213B2 (de)
EP (1) EP1382698B2 (de)
AT (1) ATE267885T1 (de)
DE (1) DE60300004T3 (de)
ES (1) ES2220902T5 (de)
FR (1) FR2842212B1 (de)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050034794A1 (en) * 2003-04-10 2005-02-17 Rinze Benedictus High strength Al-Zn alloy and method for producing such an alloy product
WO2004090185A1 (en) 2003-04-10 2004-10-21 Corus Aluminium Walzprodukte Gmbh An al-zn-mg-cu 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
RU2455529C2 (ru) * 2006-04-29 2012-07-10 Ёрликон Лайбольд Вакуум Гмбх Ротор или статор турбомолекулярного насоса
US8608876B2 (en) 2006-07-07 2013-12-17 Aleris Aluminum Koblenz Gmbh AA7000-series aluminum alloy products and a method of manufacturing thereof
US8002913B2 (en) * 2006-07-07 2011-08-23 Aleris Aluminum Koblenz Gmbh AA7000-series aluminum alloy products and a method of manufacturing thereof
DE602008002822D1 (de) * 2007-03-14 2010-11-11 Aleris Aluminum Koblenz Gmbh Al-cu-legierungsprodukt, das für die luft- und raumfahrtanwendung geeignet ist
WO2010042498A1 (en) * 2008-10-10 2010-04-15 Gkn Sinter Metals, Llc Aluminum alloy powder metal bulk chemistry formulation
CA2750394C (en) 2009-01-22 2015-12-08 Alcoa Inc. Improved aluminum-copper alloys containing vanadium
SI3141624T1 (sl) 2011-09-16 2021-11-30 Ball Corporation Udarno iztiskani vsebniki iz recikliranega odpadnega aluminija
CN102732849A (zh) * 2012-06-29 2012-10-17 武汉理工大学 镁合金与铝合金表面改性处理及高强连接的方法
CN107985713A (zh) 2013-04-09 2018-05-04 鲍尔公司 由再循环的铝和增强的合金制造的具有带螺纹的颈部的冲挤的铝瓶
CN104711498B (zh) * 2013-12-13 2016-09-07 天津大学 高强度铝合金二次拉伸成型中表面橘皮效应的控制方法
CN104451298A (zh) * 2014-11-19 2015-03-25 无锡鸿声铝业有限公司 一种改进的2024铝合金
DE102016205221A1 (de) * 2016-03-30 2017-10-05 Sms Group Gmbh Vorrichtung und Verfahren zum Plattieren einer warmen Bramme
US20180044155A1 (en) 2016-08-12 2018-02-15 Ball Corporation Apparatus and Methods of Capping Metallic Bottles
CA3032261A1 (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
EP3529394A4 (de) 2016-10-24 2020-06-24 Shape Corp. Mehrstufiges formen von aluminiumlegierungen und thermisches behandlungsverfahren zur herstellung von fahrzeugkomponenten
BR122020012460B1 (pt) 2016-12-30 2022-09-06 Ball Corporation Liga de alumínio, método para produzir um recipiente e recipiente
MX2019009745A (es) 2017-02-16 2020-02-07 Ball Corp Aparato y metodo para formar y aplicar tapas a prueba de robo giratorias en cuellos roscados de contenedores de metal.
US11185909B2 (en) 2017-09-15 2021-11-30 Ball Corporation System and method of forming a metallic closure for a threaded container
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

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1133113A (en) * 1965-02-05 1968-11-06 Aluminum Co Of America Improvements in forged aluminium base alloy members
US3333990A (en) * 1965-02-05 1967-08-01 Aluminum Co Of America Aluminum base alloy forgings
US3826688A (en) * 1971-01-08 1974-07-30 Reynolds Metals Co Aluminum alloy system
US4336075A (en) * 1979-12-28 1982-06-22 The Boeing Company Aluminum alloy products and method of making same
US5137686A (en) * 1988-01-28 1992-08-11 Aluminum Company Of America Aluminum-lithium alloys
JPH03236441A (ja) 1990-02-14 1991-10-22 Nkk Corp 高強度アルミニウム合金および高強度アルミニウム合金材の製造方法
US5213639A (en) 1990-08-27 1993-05-25 Aluminum Company Of America Damage tolerant aluminum alloy products useful for aircraft applications such as skin
BR9103666A (pt) * 1990-08-27 1992-05-19 Aluminum Co Of America Metodo de producao de um produto de folha de liga a base de aluminio e produto feito pelo dito metodo
GB9021565D0 (en) * 1990-10-04 1990-11-21 Allied Colloids Ltd Dewatering compositions and processes
US5376192A (en) * 1992-08-28 1994-12-27 Reynolds Metals Company High strength, high toughness aluminum-copper-magnesium-type aluminum alloy
FR2704557B1 (fr) 1993-04-28 1995-06-02 Pechiney Rhenalu Alliage de revêtement à base d'Al et produit composite plaqué sur alliages 2000 ou 6000.
FR2731440B1 (fr) * 1995-03-10 1997-04-18 Pechiney Rhenalu Toles en alliage al-cu-mg a faible niveau de contraintes residuelles
US5879475A (en) * 1995-03-22 1999-03-09 Aluminum Company Of America Vanadium-free, lithium-free aluminum alloy suitable for forged aerospace products
US5652063A (en) * 1995-03-22 1997-07-29 Aluminum Company Of America Sheet or plate product made from a substantially vanadium-free aluminum alloy
US5630889A (en) * 1995-03-22 1997-05-20 Aluminum Company Of America Vanadium-free aluminum alloy suitable for extruded aerospace products
US6077363A (en) * 1996-06-17 2000-06-20 Pechiney Rhenalu Al-Cu-Mg sheet metals with low levels of residual stress
FR2792001B1 (fr) * 1999-04-12 2001-05-18 Pechiney Rhenalu Procede de fabrication de pieces de forme en alliage d'aluminium type 2024
JP2001330757A (ja) * 2000-05-23 2001-11-30 Yazaki Corp 光コネクタ
US6562154B1 (en) * 2000-06-12 2003-05-13 Aloca Inc. Aluminum sheet products having improved fatigue crack growth resistance and methods of making same

Also Published As

Publication number Publication date
FR2842212A1 (fr) 2004-01-16
DE60300004T2 (de) 2005-01-20
ES2220902T3 (es) 2004-12-16
US7294213B2 (en) 2007-11-13
US7993474B2 (en) 2011-08-09
EP1382698A1 (de) 2004-01-21
EP1382698B2 (de) 2013-01-09
EP1382698B1 (de) 2004-05-26
US20080210350A1 (en) 2008-09-04
ES2220902T5 (es) 2013-05-09
US20040086418A1 (en) 2004-05-06
DE60300004T3 (de) 2013-06-20
ATE267885T1 (de) 2004-06-15
FR2842212B1 (fr) 2004-08-13

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