CN103889746A - Cast part - Google Patents

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Publication number
CN103889746A
CN103889746A CN201280049889.1A CN201280049889A CN103889746A CN 103889746 A CN103889746 A CN 103889746A CN 201280049889 A CN201280049889 A CN 201280049889A CN 103889746 A CN103889746 A CN 103889746A
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CN
China
Prior art keywords
minutes
foundry goods
particularly preferably
weight
preferred
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
CN201280049889.1A
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Chinese (zh)
Other versions
CN103889746B (en
Inventor
卢茨·沃尔肯施泰因
克劳斯·格雷文
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KSM Castings Group GmbH
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KSM Castings GmbH
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Publication date
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Publication of CN103889746A publication Critical patent/CN103889746A/en
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Publication of CN103889746B publication Critical patent/CN103889746B/en
Expired - Fee Related legal-status Critical Current
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    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • C22C21/04Modified aluminium-silicon alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C21/00Alloys based on aluminium
    • C22C21/02Alloys based on aluminium with silicon as the next major constituent
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • C22F1/043Changing 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 silicon as the next major constituent

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Heat Treatment Of Articles (AREA)
  • Conductive Materials (AREA)
  • Body Structure For Vehicles (AREA)
  • Dental Preparations (AREA)
  • Materials For Medical Uses (AREA)
  • Prostheses (AREA)

Abstract

The invention relates to a cast part.

Description

Foundry goods
Technical field
The present invention relates to a kind of foundry goods of particularly applying as chassis.
Background technology
Conventionally adopt hypoeutectic, to there is 7-12 % by weight Si content Al alloy for chassis application.In gravity cast-in chills, conventionally adopt alloy A lSi11Mg, in low-pressure chill casting, conventionally adopt alloy A lSi7Mg.Known to the few AlSiMg alloy of Si by WO2007/025528A2 and WO/2009/059593, the mechanical characteristics that this alloy phase has clear improvement for above-mentioned general AlSi casting alloy tool.
Summary of the invention
Based on prior art, the object of the invention is to, further improve by the foundry goods forming containing the few Al alloy of Si for the mechanical characteristics of foundry goods.
According to the present invention, realize this object by the foundry goods being formed by Al casting alloy, this casting alloy contains at least five following alloy compositions
Si:2.5 to 3.3, preferred 2.7 to 3.1 % by weight
Mg:0.2 to 0.7, preferred 0.3 to 0.6 % by weight
Fe:< 0.18, preferred 0.05 to 0.16 % by weight
Mn:< 0.5, preferred 0.05 to 0.4 % by weight
Ti:< 0.1, preferred 0.01 to 0.08 % by weight
Sr:< 0.03, preferred 0.01 to 0.03 % by weight
Cr:0.3 to 1.3, preferred 0.4 to 1.0, particularly preferably 0.5 to 0.8 % by weight
Other: < 0.1 % by weight,
And be supplemented to 100 % by weight with Al respectively, its medium casting is processed 15 to 120 minutes, preferably 15 to 60 minutes, particularly preferably 20 to 55 minutes, very particularly preferably 30 to 55 minutes and definitely particularly preferably between 30 to 45 minutes carrying out heat aging between 150 to 240 DEG C.
Can be advantageously, foundry goods is processed 15 to 120 minutes, preferably 15 to 60 minutes, particularly preferably 20 to 55 minutes, very particularly preferably 30 to 55 minutes and definitely particularly preferably between 30 to 45 minutes carrying out heat aging between 170 to 230 DEG C.
Can be suitable, foundry goods is processed 15 to 120 minutes, preferably 15 to 60 minutes, particularly preferably 20 to 55 minutes, very particularly preferably 30 to 55 minutes and definitely particularly preferably between 30 to 45 minutes carrying out heat aging between 200 to 220 DEG C.
Other advantage can be, foundry goods carried out solution annealing 1 to 10 hour, preferably 5 to 9 hours, particularly preferably 6 to 8 hours before heat aging is processed between 490 and 550 DEG C.
Can be advantageously, foundry goods carried out solution annealing 1 to 10 hour, preferably 5 to 9 hours, particularly preferably 6 to 8 hours before heat aging is processed between 530 and 550 DEG C.
Above-mentioned heat treatment causes further improving significantly the mechanical characteristics through cast member or foundry goods.
For chassis application, particularly, for the member of wheel guiding, improve generally mechanical characteristics value.
Can contain the impurity that is subject to restriction of production according to alloy of the present invention, such as Pb, Ni, Zn etc. are general known as those skilled in the art.These impurity belong to other described alloy compositions.
Foundry goods according to the present invention is with respect to the hot-cured foundry goods through traditional or have especially the intensity of improvement without hot-cured foundry goods at all, and also has intensity-stretch ratio ratio of improvement.
As according to the present invention through hot-cured, in particular as the manufacture method of the foundry goods of car chassis parts, it is main that what be suitable for is permanent mo(u)ld casting method.Because workpiece, member or the parts of high request need extraordinary mechanical characteristics, as manufacture method particularly suitable is gravity cast-in chills and low-pressure chill casting.
Particularly by the casting method being stressed, for example low pressure-back pressure casting (CPC method), semisolid casting and other casting methods being stressed are forged the low pressure sand casting process of (Cobapress) or cast molding device automation as high-pressure casting, cast, are obtained good mechanical technology performance by good cast structure.Here particularly preferably be back pressure-cast-in chills method (CPC method).
Except already described advantage, the advantage also having through hot-cured foundry goods according to the present invention is, owing to not existing alloy compositions Cu and Zn to significantly improve the corrosion stability of foundry goods.This foundry goods is also relatively cheap, because do not have to adopt more expensive equally alloy additive, for example SE metal, so can apply common melt process and not need the special consumption separating for circulating.
Detailed description of the invention
Embodiment
In order to detect the mechanical characteristics through hot-cured foundry goods, cast turntable bearing and manufacture tensile test bar by this turntable bearing according to DIN50125:2009-07 by alloy A lSi3Mg0.5Cr0.7 with low pressure-back pressure-cast-in chills method.Then carry out solution annealing 0.5 to 6 hour and carry out equally the heat aging processing of 0.5 to 6 hour at 200-220 DEG C at 545 DEG C.To mechanical characteristics tensile strength R m, yield limit R p0.2 and elongation at fracture A5 measure.This is adopted to DIN EN ISO6842-1:2009-12.The value recording is shown in Figure 1 with diagrammatic form.
There is shown, by heat aging is processed below 60 minutes, 30-59 minute particularly carrying out between 200 and 220 DEG C, can see significantly improving of elongation at fracture, the raising of this elongation at fracture is also accompanied by the raising of tensile strength.Here, yield limit has the same high grade of roughly maintenance.

Claims (6)

1. the foundry goods being formed by Al casting alloy, described casting alloy contains at least five following alloy compositions:
Si:2.5 to 3.3, preferred 2.7 to 3.1 % by weight
Mg:0.2 to 0.7, preferred 0.3 to 0.6 % by weight
Fe:< 0.18, preferred 0.05 to 0.16 % by weight
Mn:< 0.5, preferred 0.05 to 0.4 % by weight
Ti:< 0.1, preferred 0.01 to 0.08 % by weight
Sr:< 0.03, preferred 0.01 to 0.03 % by weight
Cr:0.3 to 1.3, preferred 0.4 to 1.0, particularly preferably 0.5 to 0.8 % by weight
Other: < 0.1 % by weight
And be supplemented to 100 % by weight with Al respectively, wherein said foundry goods carries out heat aging between 150 to 240 DEG C to be processed 15 to 120 minutes, preferably 15 to 60 minutes, particularly preferably 20 to 55 minutes and very particularly preferably 30 to 55 minutes.
2. foundry goods according to claim 1, is characterized in that, described foundry goods carries out heat aging between 170 to 230 DEG C to be processed 15 to 120 minutes, preferably 15 to 60 minutes, particularly preferably 20 to 55 minutes and very particularly preferably 30 to 55 minutes.
3. foundry goods according to claim 1 and 2, is characterized in that, described foundry goods carries out heat aging between 200 to 220 DEG C to be processed 15 to 120 minutes, preferably 15 to 60 minutes, particularly preferably 20 to 55 minutes and very particularly preferably 30 to 55 minutes.
4. according to the foundry goods described in any one in claims 1 to 3, it is characterized in that, described foundry goods carries out solution annealing 1 to 10 hour, preferably 5 to 9 hours, particularly preferably 6 to 8 hours between 490 and 550 DEG C.
5. according to the foundry goods described in any one in claim 1 to 4, it is characterized in that, described foundry goods carries out solution annealing 1 to 10 hour, preferably 5 to 9 hours, particularly preferably 6 to 8 hours between 530 and 550 DEG C.
6. according to the purposes of the foundry goods described in any one in the claims, described foundry goods is as member or the parts of car floor parts.
CN201280049889.1A 2011-10-11 2012-09-14 Casting Expired - Fee Related CN103889746B (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102011115511.6 2011-10-11
DE102011115511 2011-10-11
PCT/DE2012/100278 WO2013053354A2 (en) 2011-10-11 2012-09-14 Cast part

Publications (2)

Publication Number Publication Date
CN103889746A true CN103889746A (en) 2014-06-25
CN103889746B CN103889746B (en) 2018-09-18

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CN201280049889.1A Expired - Fee Related CN103889746B (en) 2011-10-11 2012-09-14 Casting

Country Status (5)

Country Link
US (1) US20140251508A1 (en)
EP (1) EP2766205A2 (en)
CN (1) CN103889746B (en)
DE (2) DE102012108590A1 (en)
WO (1) WO2013053354A2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110016593A (en) * 2018-01-10 2019-07-16 通用汽车环球科技运作有限责任公司 Aluminium alloy and preparation method thereof
CN110121566A (en) * 2016-12-22 2019-08-13 Ksm铸造集团有限公司 Ceralumin

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015111020A1 (en) * 2014-07-29 2016-02-04 Ksm Castings Group Gmbh Al-cast alloy
US20190055628A1 (en) 2016-03-01 2019-02-21 Ksm Castings Group Gmbh Al-casting alloy
DE102018128040A1 (en) 2017-11-17 2019-05-23 Ksm Castings Group Gmbh Al-cast alloy

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07310150A (en) * 1994-05-12 1995-11-28 Hitachi Metals Ltd Method for heat-treating aluminum alloy
DE10235529A1 (en) * 2002-08-03 2004-02-12 Daimlerchrysler Ag Cast part used as a crank housing in an I.C. engine comprises an aluminum alloy containing iron and manganese
US20040103964A1 (en) * 2002-09-09 2004-06-03 Takeyoshi Nakamura Process for thermally treating light alloy casting
WO2005007917A2 (en) * 2003-07-04 2005-01-27 Belte Ag Method and device for chilling a cast part
CN101709415A (en) * 2009-12-16 2010-05-19 中国科学院苏州纳米技术与纳米仿生研究所 Die-cast aluminum alloy material and method for preparing same
CN101855124A (en) * 2007-11-08 2010-10-06 Ksm铸造有限公司 The front axle carrier that is used for self-propelled vehicle
US20110126947A1 (en) * 2008-07-30 2011-06-02 Rio Tinto Alcan International Limited Casting made from aluminium alloy, having high hot creep and fatigue resistance

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5413407A (en) * 1977-07-01 1979-01-31 Kobe Steel Ltd High toughness aluminum alloy for casting and heat treatment method therefor
JP3669440B2 (en) * 2004-05-26 2005-07-06 アイシン軽金属株式会社 Wear resistant aluminum alloy
FR2890082B1 (en) 2005-08-31 2009-12-04 Ksm Castings Gmbh MOLDING ALLOYS ALUMINUM (A1).
DE102008055928A1 (en) 2007-11-08 2009-08-27 Ksm Castings Gmbh Al-cast alloys
ES2426226T3 (en) * 2009-06-30 2013-10-22 Hydro Aluminium Deutschland Gmbh AlMgSi band for applications with high conformation requirements

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07310150A (en) * 1994-05-12 1995-11-28 Hitachi Metals Ltd Method for heat-treating aluminum alloy
DE10235529A1 (en) * 2002-08-03 2004-02-12 Daimlerchrysler Ag Cast part used as a crank housing in an I.C. engine comprises an aluminum alloy containing iron and manganese
US20040103964A1 (en) * 2002-09-09 2004-06-03 Takeyoshi Nakamura Process for thermally treating light alloy casting
WO2005007917A2 (en) * 2003-07-04 2005-01-27 Belte Ag Method and device for chilling a cast part
CN101855124A (en) * 2007-11-08 2010-10-06 Ksm铸造有限公司 The front axle carrier that is used for self-propelled vehicle
US20110126947A1 (en) * 2008-07-30 2011-06-02 Rio Tinto Alcan International Limited Casting made from aluminium alloy, having high hot creep and fatigue resistance
CN101709415A (en) * 2009-12-16 2010-05-19 中国科学院苏州纳米技术与纳米仿生研究所 Die-cast aluminum alloy material and method for preparing same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110121566A (en) * 2016-12-22 2019-08-13 Ksm铸造集团有限公司 Ceralumin
CN110016593A (en) * 2018-01-10 2019-07-16 通用汽车环球科技运作有限责任公司 Aluminium alloy and preparation method thereof

Also Published As

Publication number Publication date
WO2013053354A3 (en) 2014-03-20
DE112012004236A5 (en) 2014-08-21
WO2013053354A2 (en) 2013-04-18
DE102012108590A1 (en) 2013-04-11
US20140251508A1 (en) 2014-09-11
EP2766205A2 (en) 2014-08-20
CN103889746B (en) 2018-09-18

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Granted publication date: 20180918