Fabrication of (TiB/Ti)-TiAl composites with a controlled laminated architecture and enhanced mechanical properties

被引:62
作者
Ding, Hao [1 ]
Cui, Xiping [1 ]
Gao, Naonao [1 ]
Sun, Yuan [2 ]
Zhang, Yuanyuan [1 ]
Huang, Lujun [1 ]
Geng, Lin [1 ]
机构
[1] Harbin Inst Technol, Sch Mat Sci & Engn, POB 433, Harbin 150001, Peoples R China
[2] Chinese Acad Sci, Inst Met Res, Div Superalloys, Shenyang 110016, Peoples R China
来源
JOURNAL OF MATERIALS SCIENCE & TECHNOLOGY | 2021年 / 62卷
基金
中国国家自然科学基金;
关键词
Titanium aluminide matrix composites; Laminated structure; High temperature properties; Strengthening-toughening; TITANIUM-ALLOY LAYERS; FRACTURE-BEHAVIOR; MICROSTRUCTURE EVOLUTION; VOLUME FRACTION; DEFORMATION; TOUGHNESS; STRENGTH; CLEAVAGE; DESIGN; SHEETS;
D O I
10.1016/j.jmst.2020.06.011
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The (TiB/Ti)-TiAl composites with a laminated structure composing of alternating TiB/Ti composite layers, alpha(2)-Ti3Al interfacial reaction layers of and gamma-TiAl layers were successfully prepared by spark plasma sintering of alternately stacked TiB2/Ti powder layers and TiAl powder layers. And the influence of thickness ratio of TiB2/Ti powder layers to TiAl powder layers on microstructure evolution and mechanical properties of the resulting (TiB/Ti)-TiAl laminated composites were investigated systemically. The results showed that the thickening of alpha(2)-Ti3Al layers which originated from the reaction of Ti and TiAl was significantly hindered by introducing TiB2 particles into starting Ti powders. As the thickness ratio of TiB2/Ti powder layers to TiAl powder layers increased, the bending fracture strength and fracture toughness at room temperature of the final (TiB/Ti)-TiAl laminated composites were remarkably improved, especially for the (TiB/Ti)-TiAl composites prepared by TiB2/Ti powder layers with thickness of 800 mu m and TiAl powder layers with thickness of 400 mu m, whose fracture toughness and bending strength were up to 51.2 MPa.m(1/2) and 1456 MPa, respectively, 293 % and 108 % higher than that of the monolithic TiAl alloys in the present work. This was attributed to the addition of high-performance network TiB/Ti composite layers. Moreover, it was noteworthy that the ultimate tensile strength at 700 degrees C of (TiB/Ti)-TiAl composites fabricated by 400 mu m thick TiB2/Ti powder layers and 400 mu m thick TiAl powder layers was as high as that at 550 degrees C of network TiB/Ti composites. This means the service temperature of (TiB/Ti)-TiAl laminated composites was likely raised by 150 degrees C, meanwhile a good combination of high strength and high toughness at ambient temperature could be maintained. Finally, the fracture mechanism of (TiB/Ti)-TiAl laminated composites was proposed. (C) 2020 Published by Elsevier Ltd on behalf of The editorial office of Journal of Materials Science & Technology.
引用
收藏
页码:221 / 233
页数:13
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