WO2005106057B1 - Heat treatable al-zn-mg alloy for aerospace and automotive castings - Google Patents

Heat treatable al-zn-mg alloy for aerospace and automotive castings

Info

Publication number
WO2005106057B1
WO2005106057B1 PCT/US2005/013766 US2005013766W WO2005106057B1 WO 2005106057 B1 WO2005106057 B1 WO 2005106057B1 US 2005013766 W US2005013766 W US 2005013766W WO 2005106057 B1 WO2005106057 B1 WO 2005106057B1
Authority
WO
WIPO (PCT)
Prior art keywords
aluminum alloy
concentration
shaped casting
less
zinc
Prior art date
Application number
PCT/US2005/013766
Other languages
French (fr)
Other versions
WO2005106057A3 (en
WO2005106057A2 (en
Filing date
Publication date
Priority claimed from US11/111,585 external-priority patent/US20050238529A1/en
Application filed filed Critical
Priority to MXPA06012242A priority Critical patent/MXPA06012242A/en
Priority to CA002564078A priority patent/CA2564078A1/en
Priority to EP05743381A priority patent/EP1759028A4/en
Priority to JP2007509666A priority patent/JP2007534839A/en
Priority to AU2005238478A priority patent/AU2005238478A1/en
Publication of WO2005106057A2 publication Critical patent/WO2005106057A2/en
Publication of WO2005106057A3 publication Critical patent/WO2005106057A3/en
Publication of WO2005106057B1 publication Critical patent/WO2005106057B1/en
Priority to NO20065386A priority patent/NO20065386L/en

Links

Abstract

A heat treatable aluminum alloy for shaped castings includes from about 3.5-5.5 % Zn, from about 1-1.5 % Mg, less than about 1 % Si, less than about 0.30 % Mn, and less than about 0.3 % Fe and other incidental impurities.

Claims

AMENDED CLAIMS[received by the International Bureau on 09 December 2005 (09.12.05), original claims 1, 13, 14 and 21 amended; original claim 12 cancelled; remaining claims unchanged (4 pages)]
1. A heat treatable aluminum alloy for shaped castings, said aluminum alloy comprising, in weight percent:
Zn; about 3.5-5.5%;
Mg: about 0.8-1.5%;
Si: less than about 1%;
Mn: no more than about 0.04%; and
Fe and other incidental impurities: less than about 0.30%.
2. An aluminum alloy according to claim 1 further comprising at least one grain refiner selected from the group consisting of boron, carbon and combinations thereof.
3. An aluminum alloy according to claim 2, wherein said at least one grain refiner includes boron in a range from about 0.0025 to about 0.05%.
4. An aluminum alloy according to claim 2, wherein said at least one grain refiner includes carbon in a range from about 0.0025 to about 0.05%.
5. An aluminum alloy according to claim 1 further comprising at least one anti-recrystallization agent selected from the group consisting of zirconium, scandium and combinations thereof,
6. An aluminum alloy according to claim 5 wherein said at least one anti-recrystallization agent includes zirconium in a range below 0.2%,
7. An aluminum alloy according to claim 5 wherein said at least one aπti-recrystallization agent includes scandium in a range below 0.3%. 8. An aluminum alloy according to claim 1 wherein said zinc is at a concentration of about 4.2 to 4.
8%,
9. An aluminum alloy according to claim 1 wherein said zinc is at a concentration of about 4.4 to 4.6%.
10. An aluminum alloy according to claim 1 wherein said magnesium is at a concentration of about 1.0 to 1,4%.
11. An aluminum alloy according to claim 10 wherein said magnesium is at a concentration of about 1.1 to 1.3%,
12. An aluminum alloy according to claim 1 wherein a concentration of manganese in said alloy is less than about 0.01%.
13. A shaped casting of an aluminum alloy, wherein said alloy comprises:
Zn: about 3.5-5, 5%;
Mg: about 0.8-1.5%;
Si: less than about 1%;
Mn: no more than about 0,04%; and
Fe and other incidental impurities: less than about 0,30%.
14. A shaped casting according to claim 13 after T5 heat treatment,
15. A shaped casting according to claim 13 after T6 heat treatment,
16. A shaped casting according to claim 13 wherein said zinc is at a concentration of about 4,2 to 4.8%.
17. A shaped casting according to claim 13 wherein said zinc is at a concentration of about 4.4 to 4.6%.
18. A shaped casting according to claim 13 wherein said magnesium is at a concentration of about 1.0 to 1.4%.
19. A shaped casting according to claim 13 wherein said magnesium is at a concentration of about 1.1 to 1.3%.
20. A method of making an aluminum alloy shaped casting, said method comprising: preparing a molten mass of an aluminum alloy, said alloy comprising:
Zn: about 3,5-5.5%;
Mg: about 0.8-1.5%;
Si: less than about 1%;
Mn: no more than about 0,40%;
Fe and other incidental impurities: less than about 0.30%; casting at least a portion, of said molten mass in a mold configured to produce said shaped casting; permitting said molten mass in said mold to solidify; and removing said shaped casting from said mold,
21. A method according to claim 20 further comprising subjecting said shaped casting to a T5 heat treatment
22. A method according to claim 20 further comprising subjecting said shaped casting to a T6 heat treatment.
23. A method according to claim 20 wherein said zinc is at a concentration of about 4.2 to 4.8%.
24. A method according to claim 20 wherein said zinc is at a concentration of about 4,4-4.6%.
25 , A method according to claim 20 wherein said magnesium is at a concentration of about 1.0 to 1.4%.
26, A method according to claim 20 wherein said magnesium is at a concentration of about 1.1 to 1.3%.
PCT/US2005/013766 2004-04-22 2005-04-22 Heat treatable al-zn-mg alloy for aerospace and automotive castings WO2005106057A2 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
MXPA06012242A MXPA06012242A (en) 2004-04-22 2005-04-22 Heat treatable al-zn-mg alloy for aerospace and automotive castings.
CA002564078A CA2564078A1 (en) 2004-04-22 2005-04-22 Heat treatable al-zn-mg alloy for aerospace and automotive castings
EP05743381A EP1759028A4 (en) 2004-04-22 2005-04-22 Heat treatable al-zn-mg alloy for aerospace and automotive castings
JP2007509666A JP2007534839A (en) 2004-04-22 2005-04-22 Heat-treatable Al-Zn-Mg alloys for aerospace and automotive castings
AU2005238478A AU2005238478A1 (en) 2004-04-22 2005-04-22 Heat treatable AL-ZN-MG alloy for aerospace and automotive castings
NO20065386A NO20065386L (en) 2004-04-22 2006-11-22 Heat-treated Al-Zn-Mg alloy for stuffing for the aviation and automotive industry

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US56481304P 2004-04-22 2004-04-22
US60/564,813 2004-04-22
US11/111,585 2005-04-21
US11/111,585 US20050238529A1 (en) 2004-04-22 2005-04-21 Heat treatable Al-Zn-Mg alloy for aerospace and automotive castings

Publications (3)

Publication Number Publication Date
WO2005106057A2 WO2005106057A2 (en) 2005-11-10
WO2005106057A3 WO2005106057A3 (en) 2006-01-26
WO2005106057B1 true WO2005106057B1 (en) 2006-03-02

Family

ID=35136636

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/013766 WO2005106057A2 (en) 2004-04-22 2005-04-22 Heat treatable al-zn-mg alloy for aerospace and automotive castings

Country Status (9)

Country Link
US (1) US20050238529A1 (en)
EP (1) EP1759028A4 (en)
JP (1) JP2007534839A (en)
KR (1) KR20070009719A (en)
AU (1) AU2005238478A1 (en)
CA (1) CA2564078A1 (en)
MX (1) MXPA06012242A (en)
NO (1) NO20065386L (en)
WO (1) WO2005106057A2 (en)

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US20060289093A1 (en) * 2005-05-25 2006-12-28 Howmet Corporation Al-Zn-Mg-Ag high-strength alloy for aerospace and automotive castings
US8083871B2 (en) 2005-10-28 2011-12-27 Automotive Casting Technology, Inc. High crashworthiness Al-Si-Mg alloy and methods for producing automotive casting
EP1978120B1 (en) * 2007-03-30 2012-06-06 Technische Universität Clausthal Aluminium-silicon alloy and method for production of same
ES2330713B2 (en) * 2008-06-11 2010-04-19 Abinash Banerji ALUMINUM BASED GRAIN TUNER.
US8349462B2 (en) 2009-01-16 2013-01-08 Alcoa Inc. Aluminum alloys, aluminum alloy products and methods for making the same
FR2968675B1 (en) 2010-12-14 2013-03-29 Alcan Rhenalu 7XXX THICK-ALLOY PRODUCTS AND METHOD OF MANUFACTURE
CN105339515A (en) * 2013-09-30 2016-02-17 苹果公司 Aluminum alloys with high strength and cosmetic appeal
DE102014224229A1 (en) 2014-11-27 2016-06-02 Federal-Mogul Nürnberg GmbH Method for producing an engine component, engine component and use of an aluminum alloy
US11345980B2 (en) 2018-08-09 2022-05-31 Apple Inc. Recycled aluminum alloys from manufacturing scrap with cosmetic appeal
CN114214547B (en) * 2021-09-30 2022-08-23 中国航发北京航空材料研究院 Aluminum-zinc-magnesium-scandium alloy and preparation method thereof

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