Interfacial fatigue crack propagation in Ni-base superalloy protective coatings

被引:7
|
作者
Okazaki, M
Okamoto, M
Harada, Y
机构
[1] Univ Tokyo, Sch Engn, Dept Met, Bunkyo Ku, Tokyo 1138656, Japan
[2] Nagaoka Univ Technol, Nagaoka, Niigata 94021, Japan
[3] TOCALO Co, Kobe, Hyogo, Japan
关键词
adhesion strength; fatigue threshold; interface crack; long-term thermal ageing; MCrAlY alloy; Ni-base superalloy coatings; surface finishing of substrate;
D O I
10.1046/j.1460-2695.2001.00452.x
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
It is important to control the interface strength of coatings and composite materials; a feature that has been noted for many years. However, how can interface strength be evaluated and controlled? In order to explore this aspect, subcritical fatigue crack growth behaviour was investigated along the interface of a CoNiCrAlY coated Ni-Base superalloy. According to the traditional fatigue test methodology, fatigue crack propagation tests were carried out, using double cantilever beam specimens. The resistance to the fatigue crack propagation was successfully evaluated by a fracture mechanics approach. Particular attention was given to the effects of surface finish of the substrate as a coating parameter, the test temperature, and long-term thermal ageing after the coating.
引用
收藏
页码:855 / 865
页数:11
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