SAE AMS 4035L-2011
含4.4Cu 1.5Mg 0.60Mn(2024-0)的退火铝合金薄板和板材.或加工制品(2024-F)(若有规定)

Aluminum Alloy, Sheet and Plate 4.4Cu 1.5Mg 0.60Mn (2024-0) Annealed; or when specified, As Fabricated (2024-F)

SAE AMS 4035L-2011 发布历史

This specification covers an aluminum alloy in the form of sheet and plate supplied in the annealed (0) condition. When specified, product shall be supplied in the "as fabricated" (F) temper. These products have been used typically for formed structural parts which will be subsequently heat treated, but usage is not limited to such applications. Certain design and processing procedures may cause these products to be susceptible to stress-corrosion cracking after heat treatment; SAE ARP 823 recommends practices to minimize such conditions.

SAE AMS 4035L-2011由美国机动车工程师协会 US-SAE 发布于 2011-12-19。

SAE AMS 4035L-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 4035L-2011的历代版本如下：

• 2011年12月19日 SAE AMS 4035L-2011 含4.4Cu 1.5Mg 0.60Mn(2024-0)的退火铝合金薄板和板材.或加工制品(2024-F)(若有规定)

SAE AMS 4035L-2011 由 SAE AMS 4035K-2003 变更而来。

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标准号

SAE AMS 4035L-2011

发布日期

2011年12月19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 660-2008 ASTM B 666/B 666M-2008 SAE AMS 2355 SAE AMS 2772-1997 SAE ARP 823 SAE AS 1990-1990

被代替标准

SAE AMS 4035K-2003

适用范围

This specification covers an aluminum alloy in the form of sheet and plate supplied in the annealed (0) condition. When specified, product shall be supplied in the "as fabricated" (F) temper. These products have been used typically for formed structural parts which will be subsequently heat treated, but usage is not limited to such applications. Certain design and processing procedures may cause these products to be susceptible to stress-corrosion cracking after heat treatment; SAE ARP 823 recommends practices to minimize such conditions.