EP1029097B1 - Schweissbare, korrosionsbeständige hochmagnesiumhaltige aluminium-magnesium-legierung, insbesondere für luftfahrtanwendung - Google Patents

Schweissbare, korrosionsbeständige hochmagnesiumhaltige aluminium-magnesium-legierung, insbesondere für luftfahrtanwendung Download PDF

Info

Publication number
EP1029097B1
EP1029097B1 EP99952347A EP99952347A EP1029097B1 EP 1029097 B1 EP1029097 B1 EP 1029097B1 EP 99952347 A EP99952347 A EP 99952347A EP 99952347 A EP99952347 A EP 99952347A EP 1029097 B1 EP1029097 B1 EP 1029097B1
Authority
EP
European Patent Office
Prior art keywords
weight
magnesium
scandium
almg
alloy
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
EP99952347A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP1029097A1 (de
Inventor
Blanka Lenczowski
Viktor Yelagin
Rainer Rauh
Valeri Zakharov
Yuri Filatov
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.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
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
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of EP1029097A1 publication Critical patent/EP1029097A1/de
Application granted granted Critical
Publication of EP1029097B1 publication Critical patent/EP1029097B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/06Alloys based on aluminium with magnesium as the next major constituent

Definitions

  • the invention relates to a weldable, corrosion-resistant high magnesium-containing aluminum-magnesium alloy, which as an essential component of a ternary aluminum scandium zirconium phase contains.
  • a weldable, corrosion-resistant high magnesium-containing aluminum-magnesium alloy which as an essential component of a ternary aluminum scandium zirconium phase contains.
  • Such an alloy is for example from the US 5,624,632 and is known for its low density, high strength and corrosion resistance especially for applications in the aviation of interest.
  • elements of rare earth or rare earth elements are similar in the aluminum-magnesium alloy Dispersoids produced according to the o. G. US patent a higher strength and produce corrosion resistance. With regard to the weldability of such Alloy can the o. G. US patent no indication can be taken.
  • JP-A-52-11143 is an aluminum-magnesium alloy with low manganese content and at least one of lanthanides disclosed.
  • this new alloy has a significantly lower compared to the known alloy Manganese content, which surprisingly improved corrosion resistance, especially in the sensitized state the parts made of this alloy showed that is, for example, when cold-formed parts are exposed to an elevated temperature for a long time become. It is believed that these positive qualities are mainly due to the ratio from manganese to scandium. This shows an improved corrosion resistance at a ratio Mn: Sc ⁇ 2. Also, in contrast to the known alloy contained titanium contributes, in addition to the effect as a grain refining agent to increase strength because titanium can replace the zirconium in the ternary Al-Sc-Zr phase, with the However, solubility of titanium is lower than that of zirconium
  • a particularly favorable alloy for aircraft applications contains at least 0.15% by weight Scandium.
  • the addition of lanthanides advantageously moves in a weight percent range between 0.05 and 0.35, which range when using a lanthanide mixture refers to the total mixture.
  • the alloy tolerates impurities in silicon up to 0.1% by weight; above all, the dynamic properties deteriorate.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Preventing Corrosion Or Incrustation Of Metals (AREA)
  • Powder Metallurgy (AREA)
  • Arc Welding In General (AREA)
  • Conductive Materials (AREA)
  • Prevention Of Electric Corrosion (AREA)
  • Laminated Bodies (AREA)
EP99952347A 1998-08-21 1999-08-10 Schweissbare, korrosionsbeständige hochmagnesiumhaltige aluminium-magnesium-legierung, insbesondere für luftfahrtanwendung Expired - Lifetime EP1029097B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19838018 1998-08-21
DE19838018A DE19838018C2 (de) 1998-08-21 1998-08-21 Geschweißtes Bauteil aus einer schweißbaren, korrosionsbeständigen hochmagnesiumhaltigen Aluminium-Magnesium-Legierung
PCT/DE1999/002492 WO2000011232A1 (de) 1998-08-21 1999-08-10 Schweissbare, korrosionsbeständige hochmagnesiumhaltige aluminium - magnesium - legierung, insbesondere für luftfahrtanwendung

Publications (2)

Publication Number Publication Date
EP1029097A1 EP1029097A1 (de) 2000-08-23
EP1029097B1 true EP1029097B1 (de) 2005-07-06

Family

ID=7878286

Family Applications (1)

Application Number Title Priority Date Filing Date
EP99952347A Expired - Lifetime EP1029097B1 (de) 1998-08-21 1999-08-10 Schweissbare, korrosionsbeständige hochmagnesiumhaltige aluminium-magnesium-legierung, insbesondere für luftfahrtanwendung

Country Status (9)

Country Link
US (1) US6531004B1 (enExample)
EP (1) EP1029097B1 (enExample)
JP (1) JP2002523622A (enExample)
CN (1) CN1103827C (enExample)
CA (1) CA2306912C (enExample)
DE (2) DE19838018C2 (enExample)
ES (1) ES2242427T3 (enExample)
RU (1) RU2226565C2 (enExample)
WO (1) WO2000011232A1 (enExample)

Families Citing this family (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6139653A (en) * 1999-08-12 2000-10-31 Kaiser Aluminum & Chemical Corporation Aluminum-magnesium-scandium alloys with zinc and copper
US6676899B2 (en) * 2000-12-21 2004-01-13 Eads Deutschland Gmbh Non-hardenable aluminum alloy as a semi-finished product for structures
EP1217085B1 (de) * 2000-12-21 2003-10-01 EADS Deutschland GmbH Nichtaushärtbare Aluminiumlegierung als Halbzeug für Strukturen
DE10248594B4 (de) * 2001-12-14 2006-04-27 Eads Deutschland Gmbh Verfahren zum Herstellen eines Scandium (Sc)- legierten Aluminiumblechmaterials mit hoher Risszähigkeit
DE10332003B3 (de) * 2003-07-14 2004-12-16 Eads Deutschland Gmbh Geschweißtes Aluminium-Strukturbauteil mit Aluminium-Guss-Werkstoffelementen
DE10331990A1 (de) * 2003-07-14 2005-02-24 Eads Deutschland Gmbh Geschweißtes Aluminium-Strukturbauteil mit metallisch induzierter Rissabeichung
US7875132B2 (en) * 2005-05-31 2011-01-25 United Technologies Corporation High temperature aluminum alloys
BRPI0614527B1 (pt) * 2005-08-16 2015-08-18 Aleris Aluminum Koblenz Gmbh Produto de liga de alumínio
US20080311421A1 (en) * 2007-06-15 2008-12-18 United Technologies Corporation Friction stir welded structures derived from AL-RE-TM alloys
US20090263273A1 (en) * 2008-04-18 2009-10-22 United Technologies Corporation High strength L12 aluminum alloys
US7871477B2 (en) * 2008-04-18 2011-01-18 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
US20090260724A1 (en) * 2008-04-18 2009-10-22 United Technologies Corporation Heat treatable L12 aluminum alloys
US8017072B2 (en) * 2008-04-18 2011-09-13 United Technologies Corporation Dispersion strengthened L12 aluminum alloys
US8002912B2 (en) * 2008-04-18 2011-08-23 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
US7875131B2 (en) 2008-04-18 2011-01-25 United Technologies Corporation L12 strengthened amorphous aluminum alloys
US7875133B2 (en) * 2008-04-18 2011-01-25 United Technologies Corporation Heat treatable L12 aluminum alloys
US8778099B2 (en) * 2008-12-09 2014-07-15 United Technologies Corporation Conversion process for heat treatable L12 aluminum alloys
US20100143177A1 (en) * 2008-12-09 2010-06-10 United Technologies Corporation Method for forming high strength aluminum alloys containing L12 intermetallic dispersoids
US8778098B2 (en) * 2008-12-09 2014-07-15 United Technologies Corporation Method for producing high strength aluminum alloy powder containing L12 intermetallic dispersoids
NL1037667C2 (nl) 2009-02-12 2010-08-16 Aleris Aluminum Koblenz Gmbh Werkwijze voor het vervaardigen van een almg-legering vliegtuigconstructiedeel.
US20100226817A1 (en) * 2009-03-05 2010-09-09 United Technologies Corporation High strength l12 aluminum alloys produced by cryomilling
US20100254850A1 (en) * 2009-04-07 2010-10-07 United Technologies Corporation Ceracon forging of l12 aluminum alloys
US20100252148A1 (en) * 2009-04-07 2010-10-07 United Technologies Corporation Heat treatable l12 aluminum alloys
CN102395693B (zh) * 2009-04-16 2014-04-09 阿勒里斯铝业科布伦茨有限公司 可焊接的金属制品
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
US20110044844A1 (en) * 2009-08-19 2011-02-24 United Technologies Corporation Hot compaction and extrusion of l12 aluminum alloys
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
US20110064599A1 (en) * 2009-09-15 2011-03-17 United Technologies Corporation Direct extrusion of shapes with 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
US20110091345A1 (en) * 2009-10-16 2011-04-21 United Technologies Corporation Method for fabrication of tubes using rolling and extrusion
US8409497B2 (en) * 2009-10-16 2013-04-02 United Technologies Corporation Hot and cold rolling high strength L12 aluminum alloys
US20110091346A1 (en) * 2009-10-16 2011-04-21 United Technologies Corporation Forging deformation of L12 aluminum alloys
EP2546373A1 (en) 2011-07-13 2013-01-16 Aleris Aluminum Koblenz GmbH Method of manufacturing an Al-Mg alloy sheet product
CN104195387B (zh) * 2014-09-05 2016-03-16 天津立中合金集团有限公司 一种轮胎模具用高纯净铝镁合金材料及其制备方法
CN104498785B (zh) * 2014-11-23 2016-07-06 北京工业大学 一种Al-Mg-Er-Zr耐热铝合金及其制备工艺
EP3181711B1 (de) 2015-12-14 2020-02-26 Apworks GmbH Scandiumhaltige aluminiumlegierung für pulvermetallurgische technologien
JP7229181B2 (ja) 2017-06-21 2023-02-27 オプシチェストボ エス オグラニチェンノイ オトヴェストヴェンノストユ “オベディネンナヤ カンパニア ルサール インゼネルノ-テクノロギケスキー チェントル” アルミニウム系合金
CN107460380B (zh) * 2017-09-04 2019-07-09 佛山科学技术学院 一种高强耐蚀铝合金及其制备方法
CN109457148B (zh) * 2018-12-25 2019-10-22 惠州市田宇中南铝合金新材料科技有限公司 一种Al-Mg-Mn-Cu合金及其制备方法
JP7273174B2 (ja) 2019-12-27 2023-05-12 オブシュチェストボ・エス・オグラニチェノイ・オトベツトベノスティウ“オベディネナヤ・コンパニヤ・ルサール・インツェネルノ-テフノロギチェスキー・ツェントル” アルミニウム系合金
EP4628610A1 (en) 2022-12-02 2025-10-08 Obshchestvo S Ogranichennoj Otvetstvennost'Yu "Institut Legkikh Materialov I Tekhnologij" Aluminium-based alloy

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU561349A1 (ru) * 1975-07-07 1978-08-25 Всесоюзный научно-исследовательский, проектно-конструкторский и технологический институт электросварочного оборудования Сплав дл алитировани оболочки порошковой проволоки
JPS5211143A (en) 1975-07-18 1977-01-27 Nippon Keikinzoku Sougou Kenki Aluminium alloy filler matertal
JPS59159961A (ja) 1983-02-28 1984-09-10 Mitsubishi Alum Co Ltd 超塑性Al合金
JPS63179040A (ja) 1987-01-20 1988-07-23 Showa Alum Corp 表面平滑性に優れたシリンダ用アルミニウム合金
JPS63248593A (ja) * 1987-03-31 1988-10-14 Showa Alum Corp アルミニウム合金溶加材
JP3286982B2 (ja) * 1990-04-25 2002-05-27 菱化マックス株式会社 金型素材
US5597529A (en) * 1994-05-25 1997-01-28 Ashurst Technology Corporation (Ireland Limited) Aluminum-scandium alloys
US5624632A (en) * 1995-01-31 1997-04-29 Aluminum Company Of America Aluminum magnesium alloy product containing dispersoids
RU2081934C1 (ru) * 1995-07-13 1997-06-20 Акционерное общество открытого типа "Всероссийский институт легких сплавов" Деформируемый термически неупрочняемый сплав на основе алюминия
CA2280191C (en) * 1997-02-10 2007-07-31 Aluminum Company Of America Aluminum alloy product
EP0918095B1 (de) * 1997-11-20 2003-03-26 Alcan Technology & Management AG Verfahren zur Herstellung eines Strukturbauteiles aus einer Aluminium-Druckgusslegierung

Also Published As

Publication number Publication date
CN1103827C (zh) 2003-03-26
CN1274392A (zh) 2000-11-22
DE59912240D1 (de) 2005-08-11
CA2306912A1 (en) 2000-03-02
CA2306912C (en) 2008-12-23
WO2000011232A1 (de) 2000-03-02
DE19838018A1 (de) 2000-03-02
ES2242427T3 (es) 2005-11-01
US6531004B1 (en) 2003-03-11
RU2226565C2 (ru) 2004-04-10
DE19838018C2 (de) 2002-07-25
EP1029097A1 (de) 2000-08-23
JP2002523622A (ja) 2002-07-30

Similar Documents

Publication Publication Date Title
EP1029097B1 (de) Schweissbare, korrosionsbeständige hochmagnesiumhaltige aluminium-magnesium-legierung, insbesondere für luftfahrtanwendung
DE19838017C2 (de) Schweißbare, korrosionsbeständige AIMg-Legierungen, insbesondere für die Verkehrstechnik
DE19838015C2 (de) Gewalztes, stranggepreßtes, geschweißtes oder geschmiedetes Bauteil aus einer schweißbaren, korrosionsbeständigen hochmagnesiumhaltigen Aluminium-Magnesium-Legierung
DE60007882T2 (de) Aluminium-magnesium-scandium-legierungen mit zink und kupfer
RU2000112642A (ru) Обладающий свариваемостью, коррозионностойкий алюминиево-магниевый сплав с высоким содержанием магния, прежде всего для применения в авиастроении
DE3210700A1 (de) Magnesiumlegierungen
DE4446898A1 (de) Magnesiumlegierung
AT511397B1 (de) Verfahren zur raffination und gefügemodifikation von aimgsi-legierungen
DE202006006518U1 (de) Aluminiumgusslegierung
DE3503110C2 (enExample)
DE2023446A1 (de) Aluminiumgußlegierung von hoher Festigkeit
DE2558915A1 (de) Magnesiumlegierungen
WO2007025528A2 (de) Al-gusslegierungen
DE102017103148A1 (de) Al-Gusslegierung
DE102008024531A1 (de) Hochwarmfeste Aluminium-Gusslegierung sowie Verwendung einer hochwarmfesten Aluminium-Gusslegierung
DE1433542A1 (de) Herstellung von magnesiumfreiem Gusseisen mit Kugelgraphit
EP4605569A1 (de) Verfahren zum herstellen einer aluminiumlegierung und bauteil
DE102018117418A1 (de) Aluminiumdruckgusslegierung
DE1257438B (de) Kupferlegierung, besonders fuer Konstruktionsgussstuecke
DE102015205895A1 (de) Aluminium-Gusslegierung, Verfahren zur Herstellung eines Motorbauteils, Motorbauteil und Verwendung einer Aluminium-Gusslegierung zur Herstellung eines Motorbauteils

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): DE ES FR GB IT

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: EADS DEUTSCHLAND GMBH

17P Request for examination filed

Effective date: 20000211

17Q First examination report despatched

Effective date: 20040804

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: AIRBUS DEUTSCHLAND GMBH

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): DE ES FR GB IT

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

REF Corresponds to:

Ref document number: 59912240

Country of ref document: DE

Date of ref document: 20050811

Kind code of ref document: P

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20050824

REG Reference to a national code

Ref country code: ES

Ref legal event code: FG2A

Ref document number: 2242427

Country of ref document: ES

Kind code of ref document: T3

ET Fr: translation filed
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20060407

REG Reference to a national code

Ref country code: ES

Ref legal event code: PC2A

Owner name: AIRBUS OPERATIONS GMBH

Effective date: 20110930

REG Reference to a national code

Ref country code: FR

Ref legal event code: CD

Owner name: AIRBUS OPERATIONS GMBH

Effective date: 20111118

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 18

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 19

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: IT

Payment date: 20180830

Year of fee payment: 20

Ref country code: FR

Payment date: 20180827

Year of fee payment: 20

Ref country code: ES

Payment date: 20180921

Year of fee payment: 20

Ref country code: DE

Payment date: 20180823

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20180822

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 59912240

Country of ref document: DE

REG Reference to a national code

Ref country code: GB

Ref legal event code: PE20

Expiry date: 20190809

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20190809

REG Reference to a national code

Ref country code: ES

Ref legal event code: FD2A

Effective date: 20220103

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: ES

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20190811