WO2005106057B1 - Heat treatable al-zn-mg alloy for aerospace and automotive castings - Google Patents
Heat treatable al-zn-mg alloy for aerospace and automotive castingsInfo
- 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
Links
- 229910000861 Mg alloy Inorganic materials 0.000 title 1
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract 17
- 229910052749 magnesium Inorganic materials 0.000 claims abstract 7
- 229910052725 zinc Inorganic materials 0.000 claims abstract 7
- 239000012535 impurity Substances 0.000 claims abstract 4
- 229910052748 manganese Inorganic materials 0.000 claims abstract 2
- 238000005266 casting Methods 0.000 claims 13
- 239000011777 magnesium Substances 0.000 claims 9
- 239000011701 zinc Substances 0.000 claims 9
- FYYHWMGAXLPEAU-UHFFFAOYSA-N magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 claims 6
- HCHKCACWOHOZIP-UHFFFAOYSA-N zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims 6
- 238000010438 heat treatment Methods 0.000 claims 4
- 239000011572 manganese Substances 0.000 claims 4
- 229910045601 alloy Inorganic materials 0.000 claims 3
- 239000000956 alloy Substances 0.000 claims 3
- REDXJYDRNCIFBQ-UHFFFAOYSA-N aluminium(3+) Chemical class [Al+3] REDXJYDRNCIFBQ-UHFFFAOYSA-N 0.000 claims 3
- 239000003795 chemical substances by application Substances 0.000 claims 3
- 238000001953 recrystallisation Methods 0.000 claims 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims 2
- 229910052796 boron Inorganic materials 0.000 claims 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims 2
- 229910052799 carbon Inorganic materials 0.000 claims 2
- 239000000203 mixture Substances 0.000 claims 2
- SIXSYDAISGFNSX-UHFFFAOYSA-N scandium Chemical compound [Sc] SIXSYDAISGFNSX-UHFFFAOYSA-N 0.000 claims 2
- 229910052706 scandium Inorganic materials 0.000 claims 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims 2
- 229910052726 zirconium Inorganic materials 0.000 claims 2
- PWHULOQIROXLJO-UHFFFAOYSA-N manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 claims 1
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
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%.
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) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE502005001724D1 (en) | 2005-01-19 | 2007-11-29 | Fuchs Kg Otto | Quench-resistant aluminum alloy and method for producing a semifinished product from this alloy |
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 |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR917559A (en) * | 1945-11-20 | 1947-01-15 | Aluminum-zinc-magnesium alloys | |
US3616420A (en) * | 1968-11-25 | 1971-10-26 | British Aluminium Co Ltd | Aluminium base alloys and anodes |
JPS61186445A (en) * | 1985-02-12 | 1986-08-20 | Riyouka Keikinzoku Kogyo Kk | Metallic mold for molding resin |
JPS61227143A (en) * | 1985-03-29 | 1986-10-09 | Sumitomo Light Metal Ind Ltd | Aluminum alloy for high pressure casting excelling in strength and suitable for welding structures |
JPS62250149A (en) * | 1986-04-24 | 1987-10-31 | Kobe Steel Ltd | Aluminum alloy for bicycle |
US4873054A (en) * | 1986-09-08 | 1989-10-10 | Kb Alloys, Inc. | Third element additions to aluminum-titanium master alloys |
JP3594272B2 (en) * | 1995-06-14 | 2004-11-24 | 古河スカイ株式会社 | High strength aluminum alloy for welding with excellent stress corrosion cracking resistance |
JPH10280081A (en) * | 1997-04-08 | 1998-10-20 | Sky Alum Co Ltd | Frame-shaped member with high strength and high precision, made of al-zn-mg alloy, and its production |
JPH10298692A (en) * | 1997-04-22 | 1998-11-10 | Sky Alum Co Ltd | Frame-shaped member with high strength and high precision, and its production |
US20010028861A1 (en) * | 1997-12-17 | 2001-10-11 | Que-Tsang Fang | High strength Al-Zn-Mg alloy for making shaped castings including vehicle wheels and structural components |
JP4818509B2 (en) * | 2000-12-04 | 2011-11-16 | 新日本製鐵株式会社 | Paint bake hardening and press forming aluminum alloy plate and method for producing the same |
EP1229141A1 (en) * | 2001-02-05 | 2002-08-07 | ALUMINIUM RHEINFELDEN GmbH | Cast aluminium alloy |
JP3852915B2 (en) * | 2001-11-05 | 2006-12-06 | 九州三井アルミニウム工業株式会社 | Method for producing semi-melt molded billet of aluminum alloy for transportation equipment |
-
2005
- 2005-04-21 US US11/111,585 patent/US20050238529A1/en not_active Abandoned
- 2005-04-22 CA CA002564078A patent/CA2564078A1/en not_active Abandoned
- 2005-04-22 EP EP05743381A patent/EP1759028A4/en not_active Withdrawn
- 2005-04-22 WO PCT/US2005/013766 patent/WO2005106057A2/en active Application Filing
- 2005-04-22 MX MXPA06012242A patent/MXPA06012242A/en unknown
- 2005-04-22 KR KR1020067024487A patent/KR20070009719A/en not_active Application Discontinuation
- 2005-04-22 AU AU2005238478A patent/AU2005238478A1/en not_active Abandoned
- 2005-04-22 JP JP2007509666A patent/JP2007534839A/en active Pending
-
2006
- 2006-11-22 NO NO20065386A patent/NO20065386L/en not_active Application Discontinuation
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