SAE AMS 4416-2008
2.9Cu-1.7Li-0.4Mg-0.4Ag-0.10Zr溶解热处理,使用拉伸和人工老化应力释放的铝合金挤压轮廓(2196-T8511)

Aluminum Alloy, Extruded Profiles (2196-T8511) 2.9Cu-1.7Li-0.4Mg-0.4Ag-0.10Zr Solution Heat Treated, Stress Relieved by Stretching and Artificially Aged

SAE AMS 4416-2008 发布历史

This specification covers an aluminum-lithium alloy in the form of extruded profiles.1.2 ApplicationThese extrusions have been used typically for machined parts requiring dimensional stability during machining processes,and high strength, but usage is not limited to such applications.1.2.1 Certain processing procedures may cause this product to become susceptible to stress-corrosion cracking;ARP823 recommends practices to minimize such conditions.

SAE AMS 4416-2008由美国机动车工程师协会 US-SAE 发布于 2008-07-31。

SAE AMS 4416-2008 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 4416-2008的历代版本如下：

• 2008年07月31日 SAE AMS 4416-2008 2.9Cu-1.7Li-0.4Mg-0.4Ag-0.10Zr溶解热处理,使用拉伸和人工老化应力释放的铝合金挤压轮廓(2196-T8511)

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标准号

SAE AMS 4416-2008

发布日期

2008年07月31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

代替标准

SAE AMS 4416A-2012

适用范围

This specification covers an aluminum-lithium alloy in the form of extruded profiles.1.2 ApplicationThese extrusions have been used typically for machined parts requiring dimensional stability during machining processes,and high strength, but usage is not limited to such applications.1.2.1 Certain processing procedures may cause this product to become susceptible to stress-corrosion cracking;ARP823 recommends practices to minimize such conditions.