SAE AMS 4601-2011
固溶热处理,冷加工和自然老化(2219-T31/T-351)含6.3Cu-0.30Mn-0.06Ti-0.10V-0.18Zr铝合金薄板和板材

Aluminum Alloy, Sheet and Plate 6.3Cu 0.30Mn 0.06Ti 0.10V 0.18Zr Solution Heat Treated, Cold Worked and Naturally Aged (2219-T31/T-351)

SAE AMS 4601-2011 发布历史

This specification covers an aluminum alloy in the form of sheet and plate. This product form has been used typically for structural parts requiring high strength up to 500 °F (260 \mCD)after proper precipitation heat treatment and which may require forming or welding during fabrication, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.

SAE AMS 4601-2011由美国机动车工程师协会 US-SAE 发布于 2011-07-22。

SAE AMS 4601-2011 在中国标准分类中归属于: V11 航空与航天用金属铸锻材料，在国际标准分类中归属于: 49.025.20 铝。

SAE AMS 4601-2011的历代版本如下：

• 2011年07月22日 SAE AMS 4601-2011 固溶热处理,冷加工和自然老化(2219-T31/T-351)含6.3Cu-0.30Mn-0.06Ti-0.10V-0.18Zr铝合金薄板和板材

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标准号

SAE AMS 4601-2011

发布日期

2011年07月22日

实施日期

废止日期

无

中国标准分类号

V11

国际标准分类号

49.025.20

发布单位

US-SAE

引用标准

ANSI H 35.2-2009 ANSI H 35.2M-2009 ASTM B 594-2009 ASTM B 666/B 666M-2008 SAE AMS 2355 SAE AMS 2770 SAE AMS 2772-1997 SAE ARP 1990

适用范围

This specification covers an aluminum alloy in the form of sheet and plate. This product form has been used typically for structural parts requiring high strength up to 500 °F (260 \mCD)after proper precipitation heat treatment and which may require forming or welding during fabrication, but usage is not limited to such applications. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; ARP823 recommends practices to minimize such conditions.