Evaluation, degradation and life assessment of coatings for land based combustion turbines

Abstract Use of metallic and thermal barrier coatings to protect hot section blades and vanes of combustion turbines for power generation has been common practice for the past three and one decades respectively. Because these coatings must be optimised with respect to both different forms of corrosion and modes of operation (base load versus peak load), their performance may be machine specific. Industrial end users generally do not have detailed knowledge of the failure mechanisms of the coatings and the basis for selecting coatings to suit specific requirements, topics the present review seeks to address. The evolution of protective coatings, coating failure mechanisms and a methodology for selecting machine specific coatings are described. The methodology, which can be used to rank and optimise coating systems and to predict the remaining life of coatings, forms the basis of a computer code known as COATLIFE. The ingredients of this methodology, i.e. degradation modelling and thermomechanical fatigue life prediction, are reviewed.

[1]  T. A. Cruse,et al.  Thermal Barrier Coating Life Prediction Model Development , 1988 .

[2]  R. Viswanathan,et al.  COMBUSTION TURBINE (CT) HOT SECTION COATING LIFE MANAGEMENT , 2002 .

[3]  E. Jordan,et al.  Thermal Barrier Coatings for Gas-Turbine Engine Applications , 2002, Science.

[4]  D. Clarke,et al.  Measurement of the stress in oxide scales formed by oxidation of alumina-forming alloys , 1996 .

[5]  G. G. Stokes "J." , 1890, The New Yale Book of Quotations.

[6]  Ramaswamy Viswanathan,et al.  Damage Mechanisms and Life Assessment of High Temperature Components , 1989 .

[7]  W. Lih,et al.  Effect of pre-aluminization on the properties of ZrO2-8wt.% Y2O3/Co-29Cr-6Al-1Y thermal-barrier coatings , 1992 .

[8]  N. S. Cheruvu,et al.  Degradation of MCrAlY Coating and Substrate Superalloy During Long Term Thermal Exposure , 1995 .

[9]  G. Wallwork,et al.  Mapping of the oxidation products in the ternary Co-Cr-Al system , 1971 .

[10]  N. S. Cheruvu,et al.  Coating Life Prediction for Combustion Turbine Blades , 1999 .

[11]  C. Barrett,et al.  Resistance of Ni-Cr-Al alloys to cyclic oxidation at 1100 and 1200°C , 1977 .

[12]  N. S. Cheruvu,et al.  Coating Life Prediction Under Cyclic Oxidation Conditions , 1998 .

[13]  W. Quadakkers,et al.  Long-term oxidation tests on a re-containing MCrAlY coating , 1997 .

[14]  B. Wu,et al.  Effects of bond coat preoxidation on the properties of ZrO2-8wt.% Y2O3/Ni-22Cr-10Al-1Y thermal-barrier coatings , 1991 .

[15]  N. Dahotre,et al.  Elevated Temperature Coatings: Science and Technology IV , 2001 .

[16]  R. Ohtani Creep and Fatigue at Elevated Temperature , 1980 .

[17]  K. Chan,et al.  Development of a Thermal Barrier Coating Life Model , 2003 .

[18]  Robert A. Miller,et al.  Oxidation‐Based Model for Thermal Barrier Coating Life , 1984 .

[19]  R. Viswanathan,et al.  Combustion Turbine Hot Section Life Management , 2002 .

[20]  R. A. Miller Progress Toward Life Modeling of Thermal Barrier Coatings for Aircraft Gas Turbine Engines , 1987 .

[21]  K. Chan A mechanics-based approach to cyclic oxidation , 1997 .