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WO1996013617B1 - Machineable aluminum alloys containing in and sn and process for producing the same - Google Patents

Machineable aluminum alloys containing in and sn and process for producing the same

Info

Publication number
WO1996013617B1
WO1996013617B1 PCT/US1995/014023 US9514023W WO9613617B1 WO 1996013617 B1 WO1996013617 B1 WO 1996013617B1 US 9514023 W US9514023 W US 9514023W WO 9613617 B1 WO9613617 B1 WO 9613617B1
Authority
WO
WIPO (PCT)
Prior art keywords
indium
tin
alloy
machining
free
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.)
Ceased
Application number
PCT/US1995/014023
Other languages
French (fr)
Other versions
WO1996013617A1 (en
Filing date
Publication date
Priority claimed from US08/330,514 external-priority patent/US5587029A/en
Application filed filed Critical
Priority to EP95938979A priority Critical patent/EP0793734B1/en
Priority to DE69520798T priority patent/DE69520798T2/en
Priority to JP8514804A priority patent/JPH11511806A/en
Priority to AU40163/95A priority patent/AU697178B2/en
Publication of WO1996013617A1 publication Critical patent/WO1996013617A1/en
Publication of WO1996013617B1 publication Critical patent/WO1996013617B1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Abstract

Free-machining aluminum alloys are disclosed containing effective amounts of tin and indium. The tin and indium additions are especially adapted for use as free-machining constituents in aluminum alloys, such as AA2000 and AA6000 series aluminum alloys. The additions can be used in place of bismuth and lead in currently available free machining alloys. In alloys containing bismuth and tin, the indium can be used to replace the bismuth. A method of producing a free-machining aluminum alloy product also is described.

Claims

AMENDED CLAIMS[received by the International Bureau on 26 April 1996 (26.04.96); original claims 1-23 replaced by amended claims 1-18 (4 pages)]
1. A free-machining aluminum alloy comprising an aluminum alloy including an effective amount of tin and an effective amount of indium, the effective amounts of tin and indium being those amounts of tin and indium that when combined with each other and with other elements in the alloy form low melting point constituents that melt during a machining operation to facilitate formation of proper size machine chips for effective machining, the amount of tin and indium in the alloy ranging from 0.04 to 1.5 wt. % and the alloy having copper as a major alloying element.
2. The free-machining alloy of claim 1 wherein said tin and indium further comprise an eutectic ratio of tin to indium.
3. The free-machining alloy of claim 1 wherein said tin and indium further comprise a tin-rich ratio of tin to indium.
4. The free-machining alloy of claim 1 wherein said tin and indium range from 0.05 to 0.8 wt %.
5. The free-machining alloy of claim 1 wherein said indium ranges between 0.22 and 0.38 wt. % and said tin ranges between 0.20 and 0.52 wt. %.
6. The free-machining alloy of claim 1 wherein said tin and indium are substituted for a low melting point constituent containing lead.
7. A free-machining aluminum alloy comprising an aluminum alloy including an effective amount of tin and an effective amount of indium, the effective amounts of tin and indium being those amounts of tin and indium that when combined with each other and with other elements in the alloy form low melting point constituents that melt during a machining operation to facilitate formation of proper size machine chips for effective machining, the amount of tin and indium in the alloy ranging from 0.04 to 1.5 wt . % and the alloy having magnesium and silicon as major alloying elements .
8. A free-machining aluminum alloy comprising an aluminum alloy including an effective amount of tin and an effective amount of indium, the effective amounts of tin and indium being those amounts of tin and indium that when combined with each other and with other elements in the alloy form low melting point constituents that melt during a machining operation to facilitate formation of proper size machine chips for effective machining, said aluminum alloy consisting essentially in weight percent of: between 0.4 and 0.8% silicon; up to 0.7% iron; between 0.15 and 0.40% copper; up to 0.15% manganese; between 0.8 and 1.2 wt. % magnesium; between 0.04 and 0.35% chromium; up to 0.25% zinc; up to 0.15% titanium; between 0.05 and 1.5% indium; and between 0.05 and 1.5% tin; with the balance aluminum and inevitable impurities .
9. The free-machining alloy of claim 8 wherein said tin and indium are in a eutectic ratio.
10. The free-machining alloy of claim 8 wherein said tin and indium each range from 0.05 to 0.8 wt. %.
11. The free-machining alloy of claim 8 wherein said indium ranges between 0.22 and 0.38 wt . % and said tin ranges between 0.20 and 0.52 wt. %.
12. A free-machining aluminum alloy comprising an aluminum alloy including an effective amount of tin and an effective amount of indium, the effective amounts of tin and indium being those amounts of tin and indium that when combined with each other and with other elements in the alloy form low melting point constituents that melt during a machining operation to facilitate formation of proper size machine chips for effective machining, said alloy in weight percent consisting essentially of: between 0.05 and 1.5% indium; between 0.05 and 1.5% tin; up to 0.40 wt . % silicon; up to 0.70 wt. % iron; between 4.0 and 6.0 wt. % copper; up to 0.30 wt. % zinc; up to 0 . 15 wt . % titanium; 617 2 £ PCI7US95/14023
with the balance aluminum and inevitable impurities.
13. The free-machining alloy of claim 12 wherein said tin and indium each range from 0.05 to 0.8% wt .
14. The free-machining alloy of claim 13 wherein said indium ranges between 0.22 and 0.38 wt . % and said tin ranges between 0.20 and 0.52 wt. %.
15. The free-machining alloy of claim 1, wherein said alloy has greater than 0.10 wt. % indium.
16. The free-machining alloy of claim 7, wherein said alloy has greater than 0.10 wt. % indium.
17. The free-machining alloy of claim 8, wherein said alloy has greater than 0.10 wt. % indium.
18. The free-machining alloy of claim 12, wherein said alloy has greater than 0.10 wt. % indium.
PCT/US1995/014023 1994-10-27 1995-10-27 Machineable aluminum alloys containing in and sn and process for producing the same Ceased WO1996013617A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
EP95938979A EP0793734B1 (en) 1994-10-27 1995-10-27 Machineable aluminum alloys containing in and sn and process for producing the same
DE69520798T DE69520798T2 (en) 1994-10-27 1995-10-27 EDITABLE INDIUM AND TIN-CONTAINING ALUMINUM ALLOYS AND PRODUCTION METHODS
JP8514804A JPH11511806A (en) 1994-10-27 1995-10-27 Machinable aluminum alloy containing In and Sn and method for producing the same
AU40163/95A AU697178B2 (en) 1994-10-27 1995-10-27 Machineable aluminum alloys containing in and sn and process for producing the same

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/330,514 1994-10-27
US08/330,514 US5587029A (en) 1994-10-27 1994-10-27 Machineable aluminum alloys containing In and Sn and process for producing the same

Publications (2)

Publication Number Publication Date
WO1996013617A1 WO1996013617A1 (en) 1996-05-09
WO1996013617B1 true WO1996013617B1 (en) 1996-06-20

Family

ID=23290102

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1995/014023 Ceased WO1996013617A1 (en) 1994-10-27 1995-10-27 Machineable aluminum alloys containing in and sn and process for producing the same

Country Status (7)

Country Link
US (1) US5587029A (en)
EP (1) EP0793734B1 (en)
JP (1) JPH11511806A (en)
AU (1) AU697178B2 (en)
CA (1) CA2202857A1 (en)
DE (1) DE69520798T2 (en)
WO (1) WO1996013617A1 (en)

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US5725694A (en) * 1996-11-25 1998-03-10 Reynolds Metals Company Free-machining aluminum alloy and method of use
US6065534A (en) * 1998-05-19 2000-05-23 Reynolds Metals Company Aluminum alloy article and method of use
US6409966B1 (en) 1998-05-19 2002-06-25 Reynolds Metals Company Free machining aluminum alloy containing bismuth or bismuth-tin for free machining and a method of use
EP0964070A1 (en) * 1998-06-12 1999-12-15 Alusuisse Technology & Management AG Lead free Aluminium alloy based on AlCuMg with good machinability
US6361741B1 (en) 1999-02-01 2002-03-26 Alcoa Inc. Brazeable 6XXX alloy with B-rated or better machinability
US6315947B1 (en) 2000-05-23 2001-11-13 Reynolds Metals Company Free-machining aluminum alloy and method of use
US20060021211A1 (en) * 2004-07-28 2006-02-02 Ang Carolina C Dry machinable aluminum castings
US9890443B2 (en) * 2012-07-16 2018-02-13 Arconic Inc. 6XXX aluminum alloys, and methods for producing the same
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JP2016141841A (en) * 2015-02-02 2016-08-08 富士ゼロックス株式会社 Cylindrical support, electrophotographic photoreceptor, process cartridge, image forming apparatus, method of manufacturing cylindrical support
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US20190078179A1 (en) * 2017-09-14 2019-03-14 United States Of America As Represented By The Secretary Of The Navy Aluminum Anode Alloy
KR20250086646A (en) * 2022-10-20 2025-06-13 아르코닉 테크놀로지스 엘엘씨 New 6xxx Aluminum Alloy

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