This specification covers a titanium alloy in the form of bars, forgings, and stock for forging. This material has been used typically for parts to be fabricated in the solution heat treated and aged condition, requiring high strength-to-weight ratio and stability up to 550 °F (288 °C), but usage is not limited to such applications. Certain processing procedures and service conditions may cause these products to become subject to stress-corrosion cracking; SAE ARP 982 recommends practices to minimize such conditions.
SAE AMS 6926A-2011由美国机动车工程师协会 US-SAE 发布于 2011-06-23。
SAE AMS 6926A-2011 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: 77.120.50 钛和钛合金。
SAE AMS 6926A-2011 经过热溶解处理和老化 13V 11Cr 3Al 的钛合金条材,锻件和锻坯 由 SAE AMS 6926-2004 变更而来。
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