Form: This specification covers a titanium alloy in the form of heat treated bars@ wire@ forgings@ and flash welded rings and stock for forging and flash welded rings. Application: Primarily for parts which are machined after solution and precipitation heat treatment. Suitable for parts@ such as pressure vessels and other aerospace structures@ requiring high strength-to-weight ratios at@ or near@ room temperature. Certain processing procedures and service conditions may cause this material to be subject to stress-corrosion cracking; ARP 982 recommends practices to minimize such conditions.
AMS4965B-1971由SAE - SAE International 发布于 1971-11-15,并于 2012-12-15 实施。
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