Effects of WC-17Co Coating Combined with Shot Peening Treatment on Fatigue Behaviors of TC21 Titanium Alloy

被引:14
|
作者
Du, Dongxing [1 ,2 ]
Liu, Daoxin [1 ]
Zhang, Xiaohua [1 ]
Tang, Jingang [2 ]
Meng, Baoli [3 ]
机构
[1] Northwestern Polytech Univ, Inst Corros & Protect, Sch Aeronaut, Xian 710072, Peoples R China
[2] China Acad Engn Phys, Inst Machinery Mfg Technol, Mianyang 621999, Peoples R China
[3] Xian Aircraft Int Corp, Xian 710089, Peoples R China
来源
MATERIALS | 2016年 / 9卷 / 11期
基金
中国国家自然科学基金;
关键词
WC-Co coating; TC21 titanium alloy; fatigue; shot peening; residual stress; toughness; HVOF THERMAL SPRAY; FRETTING FATIGUE; WEAR; STRENGTH; STEEL;
D O I
10.3390/ma9110865
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 improvement and mechanism of the fatigue resistance of TC21 high-strength titanium alloy with a high velocity oxygen fuel (HVOF) sprayed WC-17Co coating was investigated. X-ray diffraction (XRD) and the corresponding stress measurement instrument, a surface roughness tester, a micro-hardness tester, and a scanning electron microscope (SEM) were used to determine the properties of the HVOF WC-17Co coating with or without shot peening. The fatigue behavior of the TC21 titanium alloy with or without the WC-17Co coating was determined by using a rotating bending fatigue testing machine. The results revealed that the polished HVOF sprayed WC-17Co coating had almost the same fatigue resistance as the TC21 titanium alloy substrate. This resulted from the polishing-induced residual surface compressive stress and a decrease in the stress concentration on the surface of the coating. Moderate-intensity shot peening of the polished WC-17Co coatings resulted in significant improvement of the fatigue resistance of the alloy. Furthermore, the fatigue life was substantially higher than that of the substrate, owing to the deep distribution of residual stress and high compressive stress induced by shot peening. The improved surface toughness of the coating can effectively delay the initiation of fatigue crack propagation.
引用
收藏
页数:14
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