This specification covers a corrosion and heat-resistant, work strengthened and aged cobalt-nickel-chromium alloy in the form of bars 2 inches (50.8 mm) and under in nominal diameter. These bars have been used typically for parts, such as fasteners, requiring a room temperature minimum tensile strength of 170 ksi (1172 MPa) for use up to 850 °F (454 °C) in applications requiring high ductility to promote toughness and resistance to cracking under shock loading conditions, but usage is not limited to such applications. This alloy exhibits exceptionally good resistance to corrosion, crevice corrosion, and stress-corrosion cracking.
SAE AMS 5920A-2013由美国机动车工程师协会 US-SAE 发布于 2013-02-07。
SAE AMS 5920A-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: 49.025.99 其他材料。
SAE AMS 5920A-2013 由 SAE AMS 5920-2003 变更而来。
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