SAE AMS 4248C-2012
通过加压释放应力和沉淀热处理的1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T652)溶液热处理铝合金手工铸件和卷形环材

Aluminum Alloy, Hand Forgings and Rolled Rings 1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T652) Solution Heat Treated, Stress Relief by Compression, and Precipitation Heat Treated

SAE AMS 4248C-2012 发布历史

This specification covers an aluminum alloy in the form of hand forgings and rolled rings. These products have been used typically for complex shaped parts requiring moderate strength and good forgeability of the alloy and where stability is required during machining, but usage is not limited to such applications. Corrosion resistance of this alloy is superior to that of aluminum alloys having copper as the principal alloying element.

SAE AMS 4248C-2012由美国机动车工程师协会 US-SAE 发布于 2012-01-09。

SAE AMS 4248C-2012 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 4248C-2012的历代版本如下：

• 2012年01月09日 SAE AMS 4248C-2012 通过加压释放应力和沉淀热处理的1.0Mg 0.60Si 0.28Cu 0.20Cr (6061-T652)溶液热处理铝合金手工铸件和卷形环材

SAE AMS 4248C-2012 由 SAE AMS 4248B-2006 变更而来。

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标准号

SAE AMS 4248C-2012

发布日期

2012年01月09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

ASTM B 594-2009 ASTM B 660-2008 ASTM E 1417-2005 SAE AMS 2355 SAE AMS 2772-1997 SAE AMS 2808 SAE AS 1990-1990

被代替标准

SAE AMS 4248B-2006

适用范围

This specification covers an aluminum alloy in the form of hand forgings and rolled rings. These products have been used typically for complex shaped parts requiring moderate strength and good forgeability of the alloy and where stability is required during machining, but usage is not limited to such applications. Corrosion resistance of this alloy is superior to that of aluminum alloys having copper as the principal alloying element.