This specification covers a titanium alloy in the form of sheet, strip, and plate through 4.000 inches (101.60 mm).. This material has been used typically for parts to be formed or machined in the solution heat treated condition and subsequently precipitation heat treated requiring high strength-to-weight ratio and stability up to 550 °F (288 °C) in the precipitation heat treatment condition, 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 4939B-2013由美国机动车工程师协会 US-SAE 发布于 2013-03-01。
SAE AMS 4939B-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: 49.025.30 钛。
SAE AMS 4939B-2013 由 SAE AMS 4939A-2008 变更而来。
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