发明名称 TITANIUM ALUMINIDE USABLE AT HIGH TEMPERATURE
摘要 PROBLEM TO BE SOLVED: To obtain a Ti2 AlX (titanium aluminide) type alloy increased in tensile strength and creep strength, usable at high temp., and having sufficient ductility at ordinary temp. by providing a composition which contains Ti, Al, Nb, Ta, and Mo and in which respective relative quantities of the above elements and Si are regulated to values in specific ranges, respectively. SOLUTION: This alloy has a composition consisting of 20-25% Al, 10-14% Nb, 1.4-5% Ta, 2-4% Mo, 0-0.5% Si, and Ti as the balance on the basis of 100%. The alloy with this composition is subjected to pressure extrusion treatment at a temp. suited to form a creep-resistant single-phase structure and then to annealing treatment at 800 to 920 deg.C for at least 4 hr, by which a stable two-phase structure ofβ0 +O2 capable of advantageously contributing to ductility is formed and transformation is carried out. In this case, prior to the pressure extrusion treatment, isothermal forging treatment can be performed at a temp. below theβ-transus temp. of the alloy. The alloy transformed in this way can be suitably used for turbomachinery parts.
申请公布号 JPH1121642(A) 申请公布日期 1999.01.26
申请号 JP19980053584 申请日期 1998.03.05
申请人 OFFICE NATL ETUD RECH AEROSPAT <ONERA> 发明人 THOMAS MARC;MARTY MICHEL;NAKA SHIGEHISA
分类号 C22F1/00;C22C14/00;C22F1/18;(IPC1-7):C22C14/00 主分类号 C22F1/00
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