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现行 SAE AMS5856B
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Alloy Billets and Preforms, Corrosion and Heat Resistant, 59.5ni 12cr 10co 3.0mo 6.0w 3.0ti 1.5ta 4.5al 0.015b 0.10zr (0.30-0.35c), Powder-Metallurgy Product 耐腐蚀耐热合金坯料和预制件 59.5ni 12cr 10co 3.0mo 6.0w 3.0ti 1.5ta 4.5al 0.015b 0.10zr(0.30-0.35c) 粉末冶金产品
发布日期: 1998-10-01
本规范涵盖了以锻件坯料和预制件形式存在的耐腐蚀和耐热镍合金粉末冶金产品。主要用于要求高强度高达1500华氏度(815摄氏度)以及耐腐蚀和抗氧化性高达1700华氏度(925摄氏度)的零件。自1986年10月16日起,SAE航空航天材料部已宣布本规范为“非现行”。建议本规范不适用于新设计。
This specification covers a corrosion and heat resistant nickel alloy powder-metallurgy product in the form of billets and preforms for forgings. Primarily for parts requiring high strength up to 1500 degrees F (815 degrees C) and corrosion and oxidation resistance up to 1700 degrees F (925 degrees C). This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of October 16, 1986. It is recommended that this specification not be specified for new designs.
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