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High strength Ti alloy material having improved workability and process for producing the same

机译:具有改善的可加工性的高强度钛合金材料及其制造方法

摘要

Herein disclosed are a high-strength Ti alloy material having improved workability which contains 2-5% Al, 5-12% V and 0.5-8% Mo (the percents being on a weight basis) and which satisfies the relation: 14%≦1.5. times.(V content)+(Mo content)≦21%, with the balance being Ti and incidental impurities, and a process for producing such high - strength Ti alloy material.PPThe process comprises: preparing a Ti alloy ingot having the above specified composition; hot working the ingot at a temperature wihtin the range of 600°-950° C.; subjecting the work to solid solution treatment at a temperature in the range of 700°-800° C.; and age-hardening the work at a temperatrue between 300° and 600° C. The reesulting Ti alloy material is suitable for use in the fabrication of parts of aircraft where high specific strength and heat resistance are required.
机译:本文公开了具有改善的可加工性的高强度Ti合金材料,该材料包含2-5%的Al,5-12%的V和0.5-8%的Mo(百分比基于重量)并且满足以下关系:14%&lE 1.5。 (V含量)+(Mo含量)≥21%,其余为Ti和附带杂质,以及制备这种高强度Ti合金材料的方法。

该方法包括:具有上述规定组成的钛合金锭;在600°-950°C的温度范围内对铸锭进行热加工;在700°-800°C的温度下对所述工件进行固溶处理;所得的钛合金材料适用于制造要求高比强度和耐热性的飞机零件。

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