The effects of the formation of a multi-scale reinforcing phase on the microstructure evolution and mechanical properties of a Ti2AlC/TiAl alloy

被引:61
作者
Fang, Hongze [1 ]
Wang, Shu [1 ]
Chen, Ruirun [1 ]
Xu, Qin [2 ]
Yan, Yongda [3 ]
Su, Yanqing [1 ]
Guo, Jingjie [1 ]
机构
[1] Harbin Inst Technol, Natl Key Lab Precis Hot Proc Met, Harbin 150001, Heilongjiang, Peoples R China
[2] Henan Univ Technol, Sch Mech & Elect Engn, Zhengzhou 450001, Peoples R China
[3] Harbin Inst Technol, Robot Inst, State Key Lab Robot & Syst, Harbin 150080, Heilongjiang, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
CARBON ADDITION; LAMELLAR STRUCTURE; FATIGUE PROPERTIES; TIAL ALLOYS; BEHAVIOR; CREEP; TRANSFORMATION; MO; NB;
D O I
10.1039/d1nr02435c
中图分类号
O6 [化学];
学科分类号
0703 ;
摘要
In order to acquire TiAl composites with a multi-scale reinforcing phase, and to improve the microstructure and tensile properties at elevated temperatures, TiAl alloys have been prepared with different added carbon content levels via vacuum arc melting. The results show that when the carbon content is greater than or equal to 1.0 at%, then Ti2AlC forms and the microstructure changes from having a dendrite morphology to an equiaxed crystal morphology. The B2 phase disappears in the Ti2AlC-containing alloys. As the carbon content increases from 0 to 3.0 at%, the lamellar colony size decreases from 148.4 to 32.8 mu m and the lamellar width decreases from 441.2 to 117.6 nm. More nanoscale Ti2AlC particles form in the alpha(2) lamellae at a higher carbon content, and there are a lot of dislocations around them. As the carbon content, the Ti2AlC content increases from 0 to 16.8 vol% and the length-diameter ratio decreases from 9.2 to 1.8. The reason for the microstructure refinement is that carbon and carbide act as heterogeneous particles during solidification, and carbide dissolves some alloy elements, improving the microstructure uniformity. Compressive testing shows that the maximum compressive strength is 2324.3 MPa at a carbon content of 1.5%. At a carbon content of 2.5%, the compression strain is higher (28.1%). Tensile testing at elevated temperatures shows that upon increasing the temperature from 750 to 850 degrees C, the tensile strength increases from 398 to 541 MPa, and the strain increases from 6.1 to 12.2% with a temperature increase from 750 to 950 degrees C. The increase in the mechanical properties is attributed to the refined lamellar colonies and lamellar width, the solid solution of elements, and the formation of nanoprecipitates.
引用
收藏
页码:12565 / 12576
页数:12
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