Microstructure control and mechanical properties from isothermal forging and heat treatment of Ti-22Al-25Nb (at.%) orthorhombic alloy

被引:106
作者
Wang, Wei [1 ]
Zeng, Weidong [1 ]
Xue, Chen [1 ]
Liang, Xiaobo [2 ]
Zhang, Jianwei [2 ]
机构
[1] Northwestern Polytech Univ, State Key Lab Solidificat Proc, Xian 710072, Peoples R China
[2] Beijing Iron & Steel Res Inst, Beijing 100081, Peoples R China
基金
高等学校博士学科点专项科研基金;
关键词
Titanium aluminides; based on Ti3Al; Creep; Isothermal forging; Electron microscopy; scanning; Aero-engine components; TI2ALNB BASED ALLOY; TENSILE BEHAVIOR; QUANTITATIVE-ANALYSIS; INTERMETALLIC ALLOY; CREEP-BEHAVIOR; EVOLUTION; PHASE;
D O I
10.1016/j.intermet.2014.07.011
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
The microstructural evolution, creep, and tensile deformation behavior of an orthorhombic Ti-22Al -25Nb (at.%) alloy was investigated by thermo-mechanical processing, including common forging, isothermal forging, and heat treatment. Three different microstructures were obtained by varying the isothermal forging temperatures and heat-treatment schedule. Tensile-creep experiments were conducted from 650 to 700 degrees C and over a stress range of 100-200 MPa. The alloy tensile strengths at room temperature and 650 degrees C were also determined. As the isothermal forging temperature increases from 1040 degrees C to 1080 degrees C, three alloy microstructures result, including equiaxial, duplex, and bimodal-size lamellar orthorhombic microstructures. Of the three, the bimodal-size lamellar orthorhombic microstructures have the highest strength but worst ductility, whereas the equiaxial microstructures have the highest ductility but worst strength. The equiaxial microstructures have the worst creep resistance, whereas the duplex microstructures and bimodal-size lamellar orthorhombic microstructures have a similar creep resistance. (c) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:79 / 86
页数:8
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