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首页|粉末Ti-22Al-24Nb-0.5Mo合金热变形能力的对比研究

粉末Ti-22Al-24Nb-0.5Mo合金热变形能力的对比研究

omparative Study on HotWorkability of Powder Metallurgy Ti-22Al-24Nb-0.5Mo Alloy

中文摘要英文摘要

采用预合金粉末热等静压工艺制备名义成分为Ti-22Al-24Nb-0.5Mo(原子百分数)的粉末Ti2AlNb 合金, 对粉末合金、经热处理的粉末合金和同种成分的熔铸Ti2AlNb合金进行了压缩实验。结果表明, 粉末Ti2AlNb合金具有与熔铸变形合金相当的变形能力, 热处理对粉末Ti2AlNb 合金的变形能力没有明显的影响, 粉末合金在低温和高应变速率下的变形抗力更低,不易开裂。采用典型粉末成型工艺制备粉末Ti2AlNb热变形坯料, 在两相区进行了不同变形量的墩粗和拔长热变形。结果表明, 粉末Ti2AlNb坯料变形后没有宏观裂纹, 变形均匀。拉伸实验结果表明, 变形后经热处理的粉末Ti2AlNb合金表现出更好的拉伸性能。

Powder metallurgy (PM) Ti2AlNb alloy of Ti-22Al-24Nb-0.5Mo (atomic fraction, %) was prepared from pre-alloyed powder using hot isostatic pressing (HIPing). Compression tests of PM Ti2AlNb alloy, heat treated PM Ti2AlNb alloy and wrought Ti2AlNb alloy with the same chemical composition were conducted on Gleeble-3800 testing machine. The testing temperatures were from 930oC to 1050oC, strain rates varied from 0.001 s-1 to 10 s-1, and engineering strain was about 50% for each compression. The results show that the deformability of PM Ti2AlNb alloy is comparable to that of wrought alloy, and heat treatment has no obvious effect on the hot workability of PM Ti2AlNb alloy. The high temperature flow behavior of Ti2AlNb alloys prepared by different fabrication routes is similar in this work, while processing windows for PM Ti2AlNb alloy is broader than casting alloys especially at low temperature or relative high strain rate. PM Ti2AlNb billets for hot deformation were prepared by a typical powder metallurgy process, and were upset or drawn out to different deformation in two-phase region. Macrostructure of deformed PM Ti2AlNb billets were observed, no macro crack was found in deformed PM Ti2AlNb billets and the deformation was uniform. The results of tensile tests show that the deformed PM Ti2AlNb alloy after heat treatment presents better tensile properties.

卢正冠、卢斌、雷家峰、杨锐、徐磊、吴杰

10.12074/202303.00281V1

有色金属冶炼

金属材料Ti2AlNb合金粉末冶金热等静压热机械加工

卢正冠,卢斌,雷家峰,杨锐,徐磊,吴杰.粉末Ti-22Al-24Nb-0.5Mo合金热变形能力的对比研究[EB/OL].(2023-03-18)[2025-08-24].https://chinaxiv.org/abs/202303.00281.点此复制

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