This specification covers a titanium alloy in the form of bars, wire, forgings, and flash welded rings 4.000 inches (101.60 mm) and under in nominal diameter or least distance between parallel sides and of stock for forging and flash welded rings. These products have been used typically for parts which are machined after solution and precipitation heat treatment and aging and are suitable for parts requiring high strength-to-weight ratios up to moderately elevated temperatures, 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; ARP 982 recommends practices to minimize such conditions.
SAE AMS 4965J-2007由美国机动车工程师协会 US-SAE 发布于 2007-06-01。
SAE AMS 4965J-2007 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 4965J-2007 6.0Al 4.0V溶解热处理和老化的钛合金棒材、线材、锻件和环材 于 2011-06-23 变更为 SAE AMS 4965K-2011 经过热溶解处理和老化的 6.0Al 4.0V 钛合金,栏杆,电线,锻件和圆环。
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