The Evolution of Thermal Barrier Coatings in Gas Turbine Engine Applications

@article{Meier1994TheEO,
  title={The Evolution of Thermal Barrier Coatings in Gas Turbine Engine Applications},
  author={S. Meier and D. Gupta},
  journal={Journal of Engineering for Gas Turbines and Power-transactions of The Asme},
  year={1994},
  volume={116},
  pages={250-257}
}
  • S. Meier, D. Gupta
  • Published 1994
  • Engineering
  • Journal of Engineering for Gas Turbines and Power-transactions of The Asme
  • Thermal barrier coatings (TBCs) have been used for almost three decades to extend the life of combustors and augmentors and, more recently, stationary turbine components. Plasma-sprayed yttria-stabilized zirconia TBC currently is bill-of-material on many commercial jet engine parts. A more durable electron beam-physical vapor deposited (EB-PVD) ceramic coating recently has been developed for more demanding rotating as well as stationary turbine components. This ceramic EB-PVD is bill-of… CONTINUE READING
    Low Thermal Conductivity Coatings for Gas Turbine Applications
    41
    THERMAL BARRIER COATINGS (TBCs)
    20

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