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现行 SAE AMS4237B
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Aluminum Alloy, Castings, Sand, 4.6Cu - 0.35Mn - 0.25Mg - 0.22Ti (206.0-T71), Solution Heat Treated and Naturally Aged 铝合金 铸件 砂 4.6Cu-0.35Mn-0.25Mg-0.22Ti(206.0-T71) 固溶热处理和自然时效
发布日期: 2007-04-13
自2007年4月起,SAE航空航天材料部已宣布本规范“取消”。通过这一行动,本文件将保留在航空航天材料规范索引的数字部分,表明其已被“取消”。本规范涵盖砂铸件形式的铝合金。主要用于需要结合高强度、良好延展性和冲击强度的部件。某些设计和加工程序可能会导致这些铸件容易发生应力腐蚀开裂。
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of April 2007. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been "CANCELLED".This specification covers an aluminum alloy in the form of sand castings. Primarily for components requiring a combination of high strength 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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