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碳化硅纤维和层状结构对Ti-Al层状复合材料力学性能的影响

Effects of SiC Fibers and Laminated Structure on Mechanical Properties of Ti-Al Laminated Composites.

作者信息

Hou Chenyang, Zhang Shouyin, Ma Zhijian, Lu Baiping, Wang Zhenjun

机构信息

School of Aeronautic Manufacturing Engineering, Nanchang Hangkong University, Nanchang 330063, China.

出版信息

Materials (Basel). 2021 Mar 10;14(6):1323. doi: 10.3390/ma14061323.

Abstract

Ti/Ti-Al and SiC-reinforced Ti/Ti-Al laminated composites were fabricated through vacuum hot-pressure using pure Ti foils, pure Al foils and SiC fibers as raw materials. The effects of SiC fiber and a laminated structure on the properties of Ti-Al laminated composites were studied. A novel method of fiber weaving was implemented to arrange the SiC fibers, which can guarantee the equal spacing of the fibers without introducing other elements. Results showed that with a higher exerted pressure, a more compact structure with fewer Kirkendall holes can be obtained in SiC-reinforced Ti/Ti-Al laminated composites. The tensile strength along the longitudinal direction of fibers was about 400 ± 10 MPa, which was 60% higher compared with the fabricated Ti/Ti-Al laminated composites with the same volume fraction (60%) of the Ti layer. An in situ tensile test was adopted to observe the deformation behavior and fracture mechanisms of the SiC-reinforced Ti/Ti-Al laminated composites. Results showed that microcracks first occurred in the Ti-Al intermetallic layer.

摘要

以纯钛箔、纯铝箔和碳化硅纤维为原料,通过真空热压法制备了钛/钛铝和碳化硅增强钛/钛铝层状复合材料。研究了碳化硅纤维和层状结构对钛铝层状复合材料性能的影响。采用一种新颖的纤维编织方法来排列碳化硅纤维,该方法可以保证纤维等间距排列且不引入其他元素。结果表明,在碳化硅增强钛/钛铝层状复合材料中,施加更高的压力可获得结构更致密、柯肯达尔孔洞更少的材料。沿纤维纵向的拉伸强度约为400±10兆帕,与相同体积分数(60%)钛层的制备钛/钛铝层状复合材料相比,提高了60%。采用原位拉伸试验观察了碳化硅增强钛/钛铝层状复合材料的变形行为和断裂机制。结果表明,微裂纹首先出现在钛铝金属间化合物层中。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/a549/7998442/1545af06234d/materials-14-01323-g001.jpg

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