SAE AMS 4236C-2013
溶解热处理和天然老化4.6Cu 0.35Mn 0.25Mg 0.22Ti (A206.0-T4)铝合金铸件

Aluminum Alloy Castings 4.6Cu 0.35Mn 0.25Mg 0.22Ti (A206.0-T4) Solution Heat Treated and Naturally Aged


SAE AMS 4236C-2013 发布历史

This specification covers an aluminum alloy in the form of sand, investment, permanent mold, and composite mold castings. Primarily for components requiring high strength combined with good ductility and impact strength. Certain design and processing procedures may cause these castings to become susceptible to stress-corrosion cracking.

SAE AMS 4236C-2013由美国机动车工程师协会 US-SAE 发布于 2013-02-12。

SAE AMS 4236C-2013 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 4236C-2013 发布之时,引用了标准

SAE AMS 4236C-2013的历代版本如下:

  • 2013年02月12日 SAE AMS 4236C-2013 溶解热处理和天然老化4.6Cu 0.35Mn 0.25Mg 0.22Ti (A206.0-T4)铝合金铸件

 

 

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标准号
SAE AMS 4236C-2013
发布日期
2013年02月12日
实施日期
废止日期
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
ASTM B 557-2010 ASTM B 660-2008 ASTM E 10-2012 ASTM E 29-2008 ASTM E 34-2011 ASTM E 716-2010 ASTM E 1251-2011 ASTM E 1417-2005 ASTM E 1742-2008 ASTM G 44-1999 SAE AMS 2175-2003 SAE AMS 2360 SAE AMS 2694 SAE AMS 2771 SAE AMS 2804 SAE AS 1990-1990
被代替标准
SAE AMS 4236B-2007
适用范围
This specification covers an aluminum alloy in the form of sand, investment, permanent mold, and composite mold castings. Primarily for components requiring high strength combined with good ductility and impact strength. Certain design and processing procedures may cause these castings to become susceptible to stress-corrosion cracking.




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