EP1118685A1 - Alliage d'Aluminium coulé - Google Patents

Alliage d'Aluminium coulé Download PDF

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Publication number
EP1118685A1
EP1118685A1 EP00810040A EP00810040A EP1118685A1 EP 1118685 A1 EP1118685 A1 EP 1118685A1 EP 00810040 A EP00810040 A EP 00810040A EP 00810040 A EP00810040 A EP 00810040A EP 1118685 A1 EP1118685 A1 EP 1118685A1
Authority
EP
European Patent Office
Prior art keywords
weight
max
alloy
cast aluminum
aluminum 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.)
Withdrawn
Application number
EP00810040A
Other languages
German (de)
English (en)
Inventor
Hubert Koch
Horst Schramm
Peter Krug
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.)
Aluminium Rheinfelden GmbH
Original Assignee
Aluminium Rheinfelden 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 Aluminium Rheinfelden GmbH filed Critical Aluminium Rheinfelden GmbH
Priority to EP00810040A priority Critical patent/EP1118685A1/fr
Priority to JP2000398674A priority patent/JP2001220639A/ja
Priority to AT01810014T priority patent/ATE250149T1/de
Priority to DE50100622T priority patent/DE50100622D1/de
Priority to MXPA01000063A priority patent/MXPA01000063A/es
Priority to EP01810014A priority patent/EP1118686B1/fr
Priority to CA002330992A priority patent/CA2330992A1/fr
Priority to NO20010288A priority patent/NO20010288L/no
Priority to US09/764,758 priority patent/US6306342B2/en
Priority to BR0100105-1A priority patent/BR0100105A/pt
Publication of EP1118685A1 publication Critical patent/EP1118685A1/fr
Withdrawn legal-status Critical Current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
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/12Making non-ferrous alloys by processing in a semi-solid state, e.g. holding the alloy in the solid-liquid phase
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium

Definitions

  • the invention relates to an aluminum casting alloy, in particular an aluminum die casting alloy.
  • Die casting technology has developed so far today that it is possible To produce castings with high quality standards.
  • the quality of one Die-cast piece depends not only on the machine setting and the selected method, but also to a large extent from the chemical Composition and structure of the cast alloy used. These last two parameters are known to influence the Pourability, the feeding behavior (G. Schindelbauer, J. Czikel “Mold filling capacity and volume deficit of common aluminum die casting alloys " Giessereiforschung 42, 1990, pp. 88/89), the mechanical properties and - particularly important in die casting - the lifespan of the Casting tools (L.A. Norström, B. Klarenfjord, M. Svenson "General Aspects on Wash-out Mechanism in Aluminum Diecasting Dies ", 17th International NADCA Diecasting Congress 1993, Cleveland OH).
  • AIMg alloys are also known, which are characterized by high ductility award. Such an alloy is for example in US-A-5 573 606. However, these alloys have the disadvantage of high mold wear and bring problems with shaping what productivity significantly reduced.
  • the present invention is therefore based on the object of creating a die-casting alloy with a high elongation at break with an acceptable yield strength, which has good castability and sticks as little as possible in the mold.
  • the following minimum values must be achieved in the as-cast state: Elongation (A5): 14% proof stress (Rp 0.2): 100 MPa
  • the alloy should also be easy to weld, a high corrosion resistance exhibit and in particular no susceptibility to stress corrosion cracking demonstrate.
  • the solution according to the invention is that the alloy 0.5 to 2.0 % By weight magnesium Max. 0.15 % By weight silicon 0.50 to 2.0 Wt% manganese Max. 0.70 Wt% iron Max. 0.10 % Copper Max. 0.05 Wt% chromium Max. 0.10 % By weight zinc Max. 0.20 % By weight titanium 0.10 to 0.60 Wt% cobalt Max. 0.80 % By weight of cerium 0.05 to 0.50 % Zircon 0.005 to 0.15 % By weight vanadium Max. 0.50 % By weight hafnium and aluminum as the rest with further impurities individually max. 0.05% by weight, total max. 0.2% by weight.
  • the degree of purity of the aluminum used to produce the alloy corresponds to a hut aluminum of quality Al 99.8 H.
  • the alloy content is set as a general condition to keep close to the wrought alloy groups so that when later recycling of alloys used in vehicle construction, for example a reusable alloy system is retained or with mixing associated with an increase in entropy is limited.
  • the alloy according to the invention has a well molded ⁇ -phase in the cast state.
  • the eutectic predominantly made of Al 6 (Mn, Fe) phases, is very fine and therefore leads to a highly ductile fracture behavior.
  • the manganese content prevents sticking in the mold and ensures good mold release.
  • the magnesium content in connection with manganese gives the casting a high level of design stability, so that very little or no distortion can be expected even when demolding.
  • this alloy can also be used for use thixocasting or thixo forging.
  • the ⁇ phase forms in the Remelt immediately, giving excellent thixotropic properties available. At the usual heating speeds, a grain size becomes of ⁇ 100 ⁇ m.
  • Zircon increases the proof stress and produces a finer grain, so that the required mechanical properties, in particular the yield strength in the as-cast state, can be achieved.
  • the tendency of the casting to stick in the mold can be drastically reduced and the molding behavior can be significantly improved if additional is added to manganese cobalt and / or cerium.
  • the alloy preferably contains therefore 0.30 to 0.60% by weight of cobalt and / or 0.05 to 0.80% by weight, in particular 0.10 to 0.50% by weight of cerium. An optimal effect is then achieved if the sum of the contents of cobalt, cerium and manganese in the alloy is at least 1.5% by weight and the alloy is at least 1.4% by weight Contains manganese.
  • the alloy contains 0.005 to 0.15% by weight, in particular 0.01 to 0.03 % By weight of vanadium in order to improve the pourability or the flowability. Tests have shown that the mold filling capacity can be determined by a Vanadium addition is significantly improved. It also prevents vanadium the tendency to scratch known with AlMg alloys, in particular because no beryllium is added to the alloy.
  • the cast aluminum alloy according to the invention is particularly suitable for thixocasting or thixo forging.
  • the alloy is easy to weld, shows excellent casting behavior, a practically negligible tendency to stick and can be shaped well.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Moulds For Moulding Plastics Or The Like (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Mold Materials And Core Materials (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Continuous Casting (AREA)
  • Sealing Battery Cases Or Jackets (AREA)
  • Conductive Materials (AREA)
  • Forging (AREA)
EP00810040A 2000-01-19 2000-01-19 Alliage d'Aluminium coulé Withdrawn EP1118685A1 (fr)

Priority Applications (10)

Application Number Priority Date Filing Date Title
EP00810040A EP1118685A1 (fr) 2000-01-19 2000-01-19 Alliage d'Aluminium coulé
JP2000398674A JP2001220639A (ja) 2000-01-19 2000-12-27 アルミニウム鋳造用合金
AT01810014T ATE250149T1 (de) 2000-01-19 2001-01-08 Aluminium-gusslegierung
DE50100622T DE50100622D1 (de) 2000-01-19 2001-01-08 Aluminium-Gusslegierung
MXPA01000063A MXPA01000063A (es) 2000-01-19 2001-01-08 Aleacion de fundicion de aluminio.
EP01810014A EP1118686B1 (fr) 2000-01-19 2001-01-08 Alliage de coulée à base d'aluminium
CA002330992A CA2330992A1 (fr) 2000-01-19 2001-01-15 Alliage de moulage d'aluminium
NO20010288A NO20010288L (no) 2000-01-19 2001-01-17 Aluminium-stöpelegering
US09/764,758 US6306342B2 (en) 2000-01-19 2001-01-18 Aluminum casting alloy
BR0100105-1A BR0100105A (pt) 2000-01-19 2001-01-18 Liga de fundição de alumìnio

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP00810040A EP1118685A1 (fr) 2000-01-19 2000-01-19 Alliage d'Aluminium coulé

Publications (1)

Publication Number Publication Date
EP1118685A1 true EP1118685A1 (fr) 2001-07-25

Family

ID=8174525

Family Applications (1)

Application Number Title Priority Date Filing Date
EP00810040A Withdrawn EP1118685A1 (fr) 2000-01-19 2000-01-19 Alliage d'Aluminium coulé

Country Status (8)

Country Link
US (1) US6306342B2 (fr)
EP (1) EP1118685A1 (fr)
JP (1) JP2001220639A (fr)
AT (1) ATE250149T1 (fr)
BR (1) BR0100105A (fr)
CA (1) CA2330992A1 (fr)
DE (1) DE50100622D1 (fr)
MX (1) MXPA01000063A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111961931A (zh) * 2020-08-14 2020-11-20 福建祥鑫股份有限公司 一种高强耐腐蚀5系铝合金及其制备方法

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US6783730B2 (en) * 2001-12-21 2004-08-31 Alcoa Inc. Al-Ni-Mn casting alloy for automotive and aerospace structural components
US20040261916A1 (en) * 2001-12-21 2004-12-30 Lin Jen C. Dispersion hardenable Al-Ni-Mn casting alloys for automotive and aerospace structural components
US20050161128A1 (en) * 2002-03-19 2005-07-28 Dasgupta Rathindra Aluminum alloy
US6908590B2 (en) * 2002-03-19 2005-06-21 Spx Corporation Aluminum alloy
JP2004099972A (ja) * 2002-09-10 2004-04-02 Kyushu Mitsui Alum Kogyo Kk 陽極酸化処理用アルミニウム合金及びそれを用いたプラズマ処理装置
US20050173032A1 (en) * 2004-02-11 2005-08-11 Hubert Koch Casting of an aluminium alloy
US20070102071A1 (en) * 2005-11-09 2007-05-10 Bac Of Virginia, Llc High strength, high toughness, weldable, ballistic quality, castable aluminum alloy, heat treatment for same and articles produced from same
US20070297936A1 (en) * 2006-06-23 2007-12-27 Zaki Ahmad Aluminum alloy
SE530437C2 (sv) 2006-10-13 2008-06-03 Sapa Heat Transfer Ab Rankmaterial med hög hållfasthet och högt saggingmotstånd
US8349462B2 (en) 2009-01-16 2013-01-08 Alcoa Inc. Aluminum alloys, aluminum alloy products and methods for making the same
US20100215926A1 (en) * 2009-02-25 2010-08-26 Askin Albert L Aluminum alloy substrates having a multi-color effect and methods for producing the same
BR112015001784B1 (pt) 2012-07-27 2019-12-03 Graenges Sweden Ab material de tira com excelente resistência à corrosão após brasagem
DE112015003865T5 (de) * 2014-08-27 2017-08-03 Arconic Inc. Verbesserte Aluminiumgusslegierungen mit Mangan, Zink und Zirconium
KR20170124963A (ko) * 2016-05-03 2017-11-13 손희식 고내식 주물용 알루미늄 합금
CN107460379A (zh) * 2016-06-02 2017-12-12 文登市恒佳熔铸材料制品厂 可阳极氧化的压铸铝锭
CN107587006A (zh) * 2017-10-31 2018-01-16 桂林加宏汽车修理有限公司 一种高弹性模量铝合金
CN109136679B (zh) * 2018-11-01 2021-05-28 中南大学 一种用于连续深冲加工小型五金冲压件的铝合金带材及其制备方法
CN112453359B (zh) * 2020-12-12 2022-08-05 安徽瑞荣汽车零部件有限公司 一种高强度铝合金汽车电机壳体
CN112626391B (zh) * 2021-01-07 2022-05-03 重庆慧鼎华创信息科技有限公司 一种低硅高导热压铸铝合金及其制备方法
CN116377289A (zh) * 2023-04-10 2023-07-04 帅翼驰新材料集团有限公司 适于钎焊的高压铸造铝合金
CN116377288A (zh) * 2023-04-10 2023-07-04 帅翼驰新材料集团有限公司 可用于钎焊的高压铸造铝合金
CN116377262A (zh) * 2023-04-10 2023-07-04 帅翼驰新材料集团有限公司 可用于钎焊的高压铸造铝合金的制作方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4673551A (en) * 1984-05-25 1987-06-16 Sumitomo Light Metal Industries, Ltd. Fin stock material for use in plate fin heat exchanger adapted for superhigh pressure service
EP0908527A1 (fr) * 1997-10-08 1999-04-14 ALUMINIUM RHEINFELDEN GmbH Alliage de coulée à base d'aluminium
EP0911420A1 (fr) * 1997-10-08 1999-04-28 ALUMINIUM RHEINFELDEN GmbH Alliage de coulée à base d'aluminium

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JPS5921385B2 (ja) * 1977-05-09 1984-05-19 住友アルミニウム製錬株式会社 レンズ回り部品の製造法
JPS6063345A (ja) * 1983-09-16 1985-04-11 Sumitomo Light Metal Ind Ltd 電気抵抗が高く成形性に優れたアルミニウム合金
US5573606A (en) * 1995-02-16 1996-11-12 Gibbs Die Casting Aluminum Corporation Aluminum alloy and method for making die cast products
ATE188259T1 (de) * 1996-04-10 2000-01-15 Alusuisse Lonza Services Ag Bauteil

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4673551A (en) * 1984-05-25 1987-06-16 Sumitomo Light Metal Industries, Ltd. Fin stock material for use in plate fin heat exchanger adapted for superhigh pressure service
EP0908527A1 (fr) * 1997-10-08 1999-04-14 ALUMINIUM RHEINFELDEN GmbH Alliage de coulée à base d'aluminium
EP0911420A1 (fr) * 1997-10-08 1999-04-28 ALUMINIUM RHEINFELDEN GmbH Alliage de coulée à base d'aluminium

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111961931A (zh) * 2020-08-14 2020-11-20 福建祥鑫股份有限公司 一种高强耐腐蚀5系铝合金及其制备方法
CN111961931B (zh) * 2020-08-14 2021-05-07 福建祥鑫股份有限公司 一种高强耐腐蚀5系铝合金及其制备方法

Also Published As

Publication number Publication date
JP2001220639A (ja) 2001-08-14
CA2330992A1 (fr) 2001-07-19
BR0100105A (pt) 2001-08-28
US20010016175A1 (en) 2001-08-23
US6306342B2 (en) 2001-10-23
ATE250149T1 (de) 2003-10-15
MXPA01000063A (es) 2002-10-23
DE50100622D1 (de) 2003-10-23

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