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Monday, June 23, 2008 - 4:30 PM

Improving Understanding of Failure Mechanisms of Thermal Barrier Coatings

A. Atkinson, D. S. Balint, A. Luz, K. M. Nikbin, N. J. Vecchione, X. Wang, R. Wu, Imperial College, London, United Kingdom; L. Chirivi, J. R. Nicholls, Cranfield University, Cranfield, United Kingdom

Thermal barrier coatings (TBCs) are crucial for increasing the turbine inlet temperature (and hence efficiency) of gas turbine engines.  This paper describes a UK collaborative project (funded by EPSRC and MoD) aimed at improving understanding of the thermal cycling failure mechanisms of electron beam physical vapour deposited (EBPVD) yttria stabilised zirconia (YSZ) TBCs on CMSX4 superalloys. 

The project involves the production of TBCs with different bond coats and with controlled surface morphologies, measurement of residual stress in the alumina thermally grown oxide (TGO) using luminescence, and measurement of YSZ mechanical properties and inter-layer adhesion by indentation.  Generation of stress in the coating on thermal cycling, and its relief by plastic deformation and fracture, was studied by finite element modelling (FEM).  The bond coats studied include two beta-structured Pt-Al types (differing in their aluminising temperature, LT and HT)) and a gamma-gamma prime structure produced by Pt diffusion without aluminising. 

In this contribution we describe some of the key findings of the project.  The TBCs with the LTPt-Al bond coat fail by a rumpling mechanism that generates isolated cracks at the interface between the TGO and the YSZ.  This reduces adhesion at this interface and the TBC delaminates when it can no longer resist the release of stored elastic energy of the YSZ, which stiffens with time due to sintering.  By contrast, the TBCs with Pt diffusion bond coats do not rumple, and the adhesion of interfaces in the coating does not significantly degrade.  These TBCs fail at the bond coat/TBC interface driven by release of stored elastic energy in both the TGO and YSZ.  The TBCs with HTPt-Al bond coats show mixtures of both failure mechanisms.  It is shown that the different failure mechanisms are caused by the different high temperature mechanical properties of the bond coats.


Summary: This contribution describes a UK collaborative project aimed at improving understanding of the thermal cycling failure mechanisms of EBPVD YSZ TBCs on CMSX4 superalloys. The project involves production of TBCs with different bond coats and surface finishes, measurement of residual stress and mechanical properties of coating layers, and finite element modelling of stress generation and relief (including failure). Some key project results are described with emphasis on the role of the bond coat mechanical properties and stiffening of the YSZ in controlling the ultimate delamination of the coating.