宇航材料工艺2012，Vol.42Issue(5)：55-58,4.
PM-TiAl基合金热处理及其性能
Heat Treatment and Performance of PM-TiAl Base Alloy
摘要
Abstract
In order to optimize the usability, microstructure and mechanical property of TiAl based alloy after hot isostatic pressing and hot treatment was studied. After heat-treatment of 1 355℃ , organization of TiAl based alloy transformed to full lamellar microstructure. After heat-treatment of 1 335℃ , organization of TiAl based alloy transformed to double pattern microstructure. Tensile strength of full lamellar TiAl under room temperature is 446 Mpa, and will increase with temperature; yield strength of full lamellar TiAl under room temperature is 386 Mpa, and will increase with temperature.关键词
TiAl/热处理/全片层组织/相变Key words
TiAl/ Heat treatment/ Full lamellar organization/ Phase transition引用本文复制引用
马明珠,黄源殉,薛志勇,李冬青,李双寿..PM-TiAl基合金热处理及其性能[J].宇航材料工艺,2012,42(5):55-58,4.基金项目
航天科技创新基金重点资助项目(20094030090) （20094030090）
中央高校基本科研业务费资助(09MG27) （09MG27）
航天创新基金重点项目(CASC200906) （CASC200906）
