EP0804626A1 - Werkstoff für geschweisste konstruktionen aus eine aluminium-magnesium-mangan legierung mit verbesserten mechanischen eigenschaften - Google Patents

Werkstoff für geschweisste konstruktionen aus eine aluminium-magnesium-mangan legierung mit verbesserten mechanischen eigenschaften

Info

Publication number
EP0804626A1
EP0804626A1 EP96904891A EP96904891A EP0804626A1 EP 0804626 A1 EP0804626 A1 EP 0804626A1 EP 96904891 A EP96904891 A EP 96904891A EP 96904891 A EP96904891 A EP 96904891A EP 0804626 A1 EP0804626 A1 EP 0804626A1
Authority
EP
European Patent Office
Prior art keywords
welded
product
product according
resistance
mpa
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.)
Granted
Application number
EP96904891A
Other languages
English (en)
French (fr)
Other versions
EP0804626B1 (de
Inventor
Guy-Michel Raynaud
Jean-Luc Hoffmann
Laurent Cottignies
Georges Pillet
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=26231789&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=EP0804626(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority claimed from FR9502387A external-priority patent/FR2731018B1/fr
Application filed by Pechiney Rhenalu SAS filed Critical Pechiney Rhenalu SAS
Priority to EP98123582A priority Critical patent/EP0909828A3/de
Publication of EP0804626A1 publication Critical patent/EP0804626A1/de
Application granted granted Critical
Publication of EP0804626B1 publication Critical patent/EP0804626B1/de
Anticipated expiration legal-status Critical
Revoked 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 the field of laminated or extruded products, such as sheets, profiles, wires or tubes, of aluminum alloy of the AlMgMn type at Mg> 3% by weight, intended for welded constructions having a high elastic limit, a good resistance to fatigue and good toughness for structural applications, such as, for example, boats, industrial vehicles or welded bicycle frames.
  • Japanese patent application JP 06-212373 proposes, in order to minimize the reduction in mechanical resistance due to welding, to use an alloy containing from 1.0 to 2.0% of M from 3.0 to 6.0% of Mg and less than 0.15% iron.
  • an alloy with such a high manganese content leads to a reduction in the fatigue strength and toughness.
  • the object of the invention is, under determined welding conditions, to significantly improve the mechanical strength and the fatigue life of the structures welded in AlMgMn alloy, without adverse consequences on other parameters such as toughness, resistance to corrosion and cutting deformation due to internal stress.
  • the subject of the invention is products intended for welded constructions of AlMgMn alloy of composition (e weight%):
  • Zn ⁇ 0.40 optionally at least one of the elements Cr, Cu, Ti, Zr such that:
  • the Mn content must be> 0.5%, and preferably> 0.8%, to have sufficient mechanical characteristics, but must not exceed 1%, if we want to avoid degradation of the toughness and the resistance to fatigue.
  • the addition of zinc in combination with manganese has been shown to have a beneficial effect on the mechanical characteristics of the sheets and welded joints. However, it is better not to exceed 0.4%, as this can cause problems with welding.
  • Magnesium is preferably maintained> 4.3%, because it has a favorable effect on the elastic limit and the resistance to fatigue, but above 5% the corrosion resistance is less good.
  • the addition of Cu and Cr are also favorable to the elastic limit, but Cr is preferably maintained ⁇ 0.15% to maintain good resistance to fatigue.
  • the mechanical resistance of the sheets depends on both the content of magnesium in solid solution and the manganese dispersoids. It has been found that the volume fraction of these dispersoids, which is linked to the iron and manganese contents, should preferably be maintained above 1.2%. This volume fraction is calculated from the average of the surface fractions measured on polished sections made in the 3 directions (length, width and thickness) by scanning electron microscopy and image analysis.
  • the products according to the invention can be rolled or extruded products such as hot or cold rolled sheets, wires, profiles or optionally re-drawn extruded tubes.
  • the sheets according to the invention assembled by butt welding using a MIG or TIG process and with a chamfer of the order of 45 e over approximately 2/3 of the thickness, present in the welded zone an elastic limit R 2 which can be at least 25 MPa higher than that of a conventional alloy having the same magnesium content, ie a gai of around 20%.
  • the width of the heat affected zone is reduced by around a third compared to a usual 5083 alloy, and the hardness of the welded joint increases from around 75 Hv to more than 80 Hv.
  • Welded joints also have a breaking strength which exceeds the minimum imposed by the inspection bodies for raw sheets of unwelded rolls.
  • the sheets according to the invention have a resistance to fatigue, measured in planar bending with a stress ratio R * 0.1 on test pieces taken in the transverse section, greater than:
  • the sheets according to the invention are most often thicker than 1.5 mm. For thicknesses greater than 2.5 mm, they can be obtained directly by hot rolling, without the need for subsequent cold rolling, and, moreover, these hot rolled sheets exhibit less distortion on cutting than the cold rolled sheets.
  • the products according to the invention have a corrosion resistance as good as the usual alloys with the same magnesium content, for example 5083 of common composition. widely used in shipbuilding.
  • the reference 0 corresponds to a conventional composition of 5083 and the reference 1 has a composition slightly outside the invention.
  • the other 11 (ref. 2 to 12) have a composition according to the invention.
  • the compositions were as follows (% by weight):
  • the samples all have, after rolling, an elastic limit Ro, 2 > 220 MPa in the direction L.
  • the mechanical resistance of the welded joints was measured from these sheets under the following conditions: automatic continuous butt MIG welding, with a symmetrical chamfer of slope 45 * relative to the vertical over a thickness of 4 mm and wire 5183 alloy intake.
  • the mechanical characteristics (tensile strength R m , elastic limit Q, 2) orvt been obtained by traction on test pieces standardized by the Norwegian inspection body DNV for shipbuilding, length 140 mm, width 35 mm, the weld bead width 15 mm being the center and the length of the narrow part of the test piece being 27 mm, the sum of the width of the bead and times the thickness (15 + 12 mm).
  • the elastic limit of the welded samples according to the invention has, compared to the reference sample, an increase of between 15 and 35 MPa.
  • the sheets according to the invention have a resistance to fatigue at least as good as that of conventional 5083 sheets.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Heat Treatment Of Steel (AREA)
  • Conductive Materials (AREA)
  • Laminated Bodies (AREA)
  • Arc Welding In General (AREA)
  • Butt Welding And Welding Of Specific Article (AREA)
  • Heat Treatment Of Articles (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
EP96904891A 1995-02-24 1996-02-21 Geschweisste konstruktionen aus einer aluminium-magnesium-mangan legierung mit verbesserten mechanischen eigenschaften Revoked EP0804626B1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP98123582A EP0909828A3 (de) 1995-02-24 1996-02-21 Erzeugnis für geschweisste Bauteile aus AlMgMn Legierung mit verbesserte mechanische Eigenschaften

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
FR9502387A FR2731018B1 (fr) 1995-02-24 1995-02-24 Tole pour construction soudee en alliage almgmn a resistance mecanique amelioree
FR9502387 1995-02-24
FR9512065 1995-10-09
FR9512065A FR2731019B1 (fr) 1995-02-24 1995-10-09 Produit pour construction soudee en alliage almgmn a resistance mecanique amelioree
PCT/FR1996/000279 WO1996026299A1 (fr) 1995-02-24 1996-02-21 PRODUIT POUR CONSTRUCTION SOUDEE EN ALLIAGE AlMgMn A RESISTANCE MECANIQUE AMELIOREE

Related Child Applications (1)

Application Number Title Priority Date Filing Date
EP98123582A Division EP0909828A3 (de) 1995-02-24 1996-02-21 Erzeugnis für geschweisste Bauteile aus AlMgMn Legierung mit verbesserte mechanische Eigenschaften

Publications (2)

Publication Number Publication Date
EP0804626A1 true EP0804626A1 (de) 1997-11-05
EP0804626B1 EP0804626B1 (de) 2001-07-11

Family

ID=26231789

Family Applications (2)

Application Number Title Priority Date Filing Date
EP96904891A Revoked EP0804626B1 (de) 1995-02-24 1996-02-21 Geschweisste konstruktionen aus einer aluminium-magnesium-mangan legierung mit verbesserten mechanischen eigenschaften
EP98123582A Ceased EP0909828A3 (de) 1995-02-24 1996-02-21 Erzeugnis für geschweisste Bauteile aus AlMgMn Legierung mit verbesserte mechanische Eigenschaften

Family Applications After (1)

Application Number Title Priority Date Filing Date
EP98123582A Ceased EP0909828A3 (de) 1995-02-24 1996-02-21 Erzeugnis für geschweisste Bauteile aus AlMgMn Legierung mit verbesserte mechanische Eigenschaften

Country Status (20)

Country Link
US (1) US6444059B2 (de)
EP (2) EP0804626B1 (de)
JP (1) JPH11500783A (de)
CN (1) CN1078622C (de)
AR (1) AR001000A1 (de)
AU (1) AU690433C (de)
CA (1) CA2211433C (de)
DE (2) DE804626T1 (de)
DK (1) DK0804626T3 (de)
ES (1) ES2161347T3 (de)
FI (1) FI121471B (de)
FR (1) FR2731019B1 (de)
NO (1) NO973681D0 (de)
NZ (1) NZ302706A (de)
PL (1) PL321887A1 (de)
RU (1) RU2156319C2 (de)
TR (1) TR199700843T1 (de)
UA (1) UA49823C2 (de)
UY (1) UY24172A1 (de)
WO (1) WO1996026299A1 (de)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2752244B1 (fr) 1996-08-06 1998-09-18 Pechiney Rhenalu Produit pour construction soudee en alliage almgmn a tenue a la corrosion amelioree
EP0892077A1 (de) * 1997-07-18 1999-01-20 Aluminum Company Of America Aluminiumgiesslegierung und daraus hergestellte Komponenten
PT1078109E (pt) * 1998-02-20 2003-06-30 Corus Aluminium Walzprod Gmbh Material de liga de aluminio e magnesio forjavel de alta resistencia para aplicacao em estruturas soldadas
ATE353983T1 (de) 2000-03-31 2007-03-15 Corus Aluminium Voerde Gmbh Druckgusserzeugnis aus aluminiumlegierung
DE10231437B4 (de) * 2001-08-10 2019-08-22 Corus Aluminium N.V. Verfahren zur Herstellung eines Aluminiumknetlegierungsprodukts
DE10231422A1 (de) * 2001-08-13 2003-02-27 Corus Aluminium Nv Aluminium-Magnesium-Legierungserzeugnis
JP2003301230A (ja) * 2002-02-05 2003-10-24 Furukawa Electric Co Ltd:The 多段成形性に優れるアルミニウム合金管
US6659331B2 (en) * 2002-02-26 2003-12-09 Applied Materials, Inc Plasma-resistant, welded aluminum structures for use in semiconductor apparatus
FR2837499B1 (fr) * 2002-03-22 2004-05-21 Pechiney Rhenalu PRODUITS EN ALLIAGES Al-Mg POUR CONSTRUCTION SOUDEE
AU2003235302A1 (en) * 2002-05-30 2003-12-19 Honda Giken Kogyo Kabushiki Kaisha Die casting having high toughness
RU2230131C1 (ru) * 2002-09-20 2004-06-10 Региональный общественный фонд содействия защите интеллектуальной собственности Сплав системы алюминий-магний-марганец и изделие из этого сплава
CA2617528C (en) 2005-08-16 2013-12-24 Aleris Aluminum Koblenz Gmbh High strength weldable al-mg alloy
JP2008024964A (ja) * 2006-07-18 2008-02-07 Nippon Light Metal Co Ltd 高強度アルミニウム合金板およびその製造方法
CN101585387B (zh) * 2008-05-22 2013-05-01 唐山亨利车料有限公司 折叠盒销及其加工方法
EP2456899A4 (de) 2009-07-24 2015-01-14 Alcoa Inc Verbesserte 5xxx-aluminiumlegierungen und daraus hergestellte aluminiumlegierungs-schmiedeprodukte
KR101399301B1 (ko) * 2010-10-08 2014-05-27 스미토모 게이 긴조쿠 고교 가부시키가이샤 알루미늄 합금 접합 부재
CN103173667A (zh) * 2011-12-22 2013-06-26 加铝(天津)铝合金产品有限公司 一种用于电缆铠装的铝合金材料
CN103540814A (zh) * 2013-10-17 2014-01-29 常熟市良益金属材料有限公司 一种铝镁合金
CN103572116A (zh) * 2013-10-21 2014-02-12 姚富云 一种高强度并具有高韧性的铝合金
CN103993207A (zh) * 2014-04-24 2014-08-20 广东兴发铝业有限公司 高速船舶用5xxx系列铝合金挤压型材配方及制造工艺
CN104805322B (zh) * 2015-04-10 2017-03-22 凤阳爱尔思轻合金精密成型有限公司 非热处理自强化铝镁合金及其制备工艺
CN106244872A (zh) * 2016-08-30 2016-12-21 吉林化工学院 一种高耐蚀性的船用Al‑Mg铝合金中厚板材的制备方法
CN106756310A (zh) * 2017-01-09 2017-05-31 镇江华中电器有限公司 海洋电缆敷设装置板材专用新型高抗腐蚀高强度铝锰合金及其制备方法
CN106756311A (zh) * 2017-01-09 2017-05-31 镇江华中电器有限公司 海洋电缆敷设装置挤压型材专用新型高抗腐蚀高强度铝锰合金及制备方法和成型工艺
CN106834829B (zh) * 2017-02-27 2018-10-16 东莞市铝美铝型材有限公司 一种船舶用高强耐蚀铝合金及其制备方法
FR3085968B1 (fr) 2018-09-13 2022-08-12 Constellium Issoire PRODUIT EN ALLIAGE AlMgMn A TENUE A LA CORROSION AMELIOREE
CN109576616B (zh) * 2018-12-11 2020-07-14 广东省材料与加工研究所 一种铝合金管材尺寸回弹控制方法
CN109593996A (zh) * 2018-12-28 2019-04-09 宁波合力模具科技股份有限公司 一种高强韧挤压铸造铝镁硅合金及其制备方法
CN110387492A (zh) * 2019-09-05 2019-10-29 合肥工业大学 一种提高5系铝合金焊接接头抗应力腐蚀性能的方法

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Publication number Priority date Publication date Assignee Title
US5181969A (en) 1990-06-11 1993-01-26 Sky Aluminum Co., Ltd. Rolled aluminum alloy adapted for superplastic forming and method for making

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SU531883A1 (ru) * 1974-07-08 1976-10-15 Предприятие П/Я Р-6585 Сплав на основе алюмини
DE2443332C3 (de) * 1974-09-06 1980-04-10 Siemens Ag, 1000 Berlin Und 8000 Muenchen Kapselung für eine druckgasisolierte Hochspannungsanlage
FR2333053A1 (fr) * 1975-11-25 1977-06-24 Cegedur Procede de preparation de toles d'aluminium destinees a etre soudees, a resistance a la corrosion amelioree
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FR2448684A1 (fr) * 1979-02-12 1980-09-05 Bretagne Atel Chantiers Dispositif pour revaporiser des gaz liquefies
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US5181969A (en) 1990-06-11 1993-01-26 Sky Aluminum Co., Ltd. Rolled aluminum alloy adapted for superplastic forming and method for making

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"Effect of Alloying Elements", ALUMINUM STANDARDS AND DATA 1986 METRIC SI, 1986, pages 15 - 16, XP002932867
B.A.CASSIE ET AL: "Composition Affects Tensile Strenght of Welded Aluminium-Magnesium Alloy", METAL CONSTRUCTION AND BRITISH WELDING JOURNAL, January 1973 (1973-01-01), pages 11 - 19, XP000847525
NAGATA M. ET AL: "NRIM FATIGUE DATA SHEET", vol. 64, 25 December 1990, NATIONAL RESEARCH INSTITUTE FOR METALS, TOKYO, JAPAN, article "Data Sheets on Fatigue Properties for Butt Welded Joints of A5083P-O (A1-4.5Mg-0.6Mn) Aluminium Alloy Plates", pages: 1 - 10, XP002932868
See also references of WO9626299A1

Also Published As

Publication number Publication date
UY24172A1 (es) 1996-04-15
NO973681L (no) 1997-08-11
CA2211433C (fr) 2009-04-28
UA49823C2 (uk) 2002-10-15
AU690433C (en) 2002-06-06
DE69613812T2 (de) 2002-04-04
TR199700843T1 (tr) 1998-02-21
DE804626T1 (de) 1998-01-29
RU2156319C2 (ru) 2000-09-20
EP0909828A2 (de) 1999-04-21
DK0804626T3 (da) 2001-11-12
EP0804626B1 (de) 2001-07-11
CA2211433A1 (fr) 1996-08-29
FR2731019B1 (fr) 1997-08-22
FI121471B (fi) 2010-11-30
FR2731019A1 (fr) 1996-08-30
CN1078622C (zh) 2002-01-30
NO973681D0 (no) 1997-08-11
PL321887A1 (en) 1997-12-22
AU690433B2 (en) 1998-04-23
WO1996026299A1 (fr) 1996-08-29
JPH11500783A (ja) 1999-01-19
AU4930596A (en) 1996-09-11
DE69613812D1 (de) 2001-08-16
FI963290L (fi) 1996-08-25
FI963290A0 (fi) 1996-08-23
ES2161347T3 (es) 2001-12-01
HK1002201A1 (en) 1998-08-07
AR001000A1 (es) 1997-08-27
EP0909828A3 (de) 1999-06-16
US6444059B2 (en) 2002-09-03
US20010050118A1 (en) 2001-12-13
CN1175983A (zh) 1998-03-11
NZ302706A (en) 1999-04-29

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