SAE AMS 5771E-2004
74Ni 7.0Cr 16.5Mo溶解热处理的镍合金耐腐蚀和耐热棒材、锻件和环材

Nickel Alloy, Corrosion and Heat -esistant, Bars, Forgings and Rings 74Ni 7.0Cr 16.5Mo Solution Heat Treated

SAE AMS 5771E-2004 发布历史

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts, such as turbine air-sealing components, requiring moderate strength up to 1400 degrees F (760 degrees C) and oxidation resistance up to 1600 degrees F (871 degrees C), particularly where a low coefficient of expansion is desirable, but usage is not limited to such applications.

SAE AMS 5771E-2004由美国机动车工程师协会 US-SAE 发布于 2004-01-13。

SAE AMS 5771E-2004 在中国标准分类中归属于: J32 锻压。

SAE AMS 5771E-2004的历代版本如下：

• 2004年01月13日 SAE AMS 5771E-2004 74Ni 7.0Cr 16.5Mo溶解热处理的镍合金耐腐蚀和耐热棒材、锻件和环材

SAE AMS 5771E-2004 74Ni 7.0Cr 16.5Mo溶解热处理的镍合金耐腐蚀和耐热棒材、锻件和环材 于 2009-04-14 变更为 SAE AMS 5771F-2009 74Ni 7.0Cr 16.5Mo溶解热处理,耐腐蚀和耐热镍合金棒材,锻件和环材。

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标准号

SAE AMS 5771E-2004

发布日期

2004年01月13日

实施日期

废止日期

无

中国标准分类号

J32

发布单位

US-SAE

代替标准

SAE AMS 5771F-2009

适用范围

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings. These products have been used typically for parts, such as turbine air-sealing components, requiring moderate strength up to 1400 degrees F (760 degrees C) and oxidation resistance up to 1600 degrees F (871 degrees C), particularly where a low coefficient of expansion is desirable, but usage is not limited to such applications.