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The thermal fatigue behaviour of an air plasma sprayed thermal barrier coating wasinvestigated. And also the interfacial strengths of thermal barrier coated specimens subjected to thermal fatigue, as well as a retired TBC vane were also evaluated bymeans of an instrumented indentation machine. The results indicated that, (1) theTGO grew at the interface during thermal fatigue cycle as a function of the exposure time at elevated temperature; (2) the microcracks were initiated in the top coating and at the interface after thermal cycle tests; (3) the interfacial strength of TBC,which was evaluated by the indentation method, increased with the thermal cycles;(4) the interfaciai strength of the retired TBC vane was almost equal with that of theas-sprayed TBC specimen.

参考文献

[1] A K RAY;N ROY;K M GODIWALLA .Crack propagation studies and bond coat properties in thermal barrier coatings under bending[J].Bulletin of Materials Science,2001(2):203-209.
[2] D. Renusch;H. Echsler;M. Schutze .Progress in life time modeling of APS-TBC Part I: residual, thermal and growth stresses including the role of thermal fatigue[J].Materials at High Temperatures,2004(2):65-76.
[3] Y. Yamazaki;T. Kinebuchi;H. Fukanuma;N. Ohno;K. Kaise .Deformation and Fracture Behaviors in the Freestanding APS-TBC: Effects of Process Parameters and Thermal Exposure[J].Key engineering materials,2007(3):1935-1938.
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