发明名称 METHOD OF FORMING METALLIC MEMBER, HEAT-TREATING TITANIUM-BASED ALLOY AND PRODUCING AIRCRAFT, AND AIRCRAFT COMPRISING LOAD-APPLIED STRUCTURAL MEMBER
摘要 PROBLEM TO BE SOLVED: To provide a method of heat-treating a Ti-based alloy and various improvements that can be realized using such heat treatment. SOLUTION: In one exemplary implementation, a method of forming a metallic member is provided that comprises the steps of: forming an alloy into a utile shape; cooling the alloy from a first temperature higher than the beta transus temperature of the alloy to a second temperature lower than the beta transus temperature at a cooling rate of about≤30°F/min. If so desired, the alloy may be treated at about 700 to 1,100°F for about 1 to 12 hr. The titanium alloy treated in accordance with the aspect of the invention may have higher tensile strength and higher fracture toughness than conventional wrought, mill-annealed Ti64 alloy. COPYRIGHT: (C)2005,JPO&NCIPI
申请公布号 JP2005002473(A) 申请公布日期 2005.01.06
申请号 JP20040171188 申请日期 2004.06.09
申请人 BOEING CO:THE 发明人 BRIGGS ROBERT D
分类号 C22F1/18;C22C14/00;C22F1/00;(IPC1-7):C22F1/18 主分类号 C22F1/18
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