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Journal ArticleOPEN ACCESS

Current Status of Thermal Barrier Coating System for Aero-Engines

  • SATO A
  • MATSUNAGA Y
  • YOSHIZAWA H
  • et al.
Journal of High Temperature Society (2007) 33(5) 252-256
DOI: 10.7791/jhts.33.252
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Abstract

The turbine inlet temperature of aero engines has increased progressively to improve the specific fuel consumption of engines. The Thermal Barrier Coating ( TBC ) system for high pressure turbine blades has now become essential to overcome the severe operating conditions. This article introduces development progress and some issues with the TBC system for aero engines, and discusses recent research on bond coats.

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APA

SATO, A., MATSUNAGA, Y., YOSHIZAWA, H., TAKAHASHI, K., & MORI, N. (2007). Current Status of Thermal Barrier Coating System for Aero-Engines. Journal of High Temperature Society, 33(5), 252–256. https://doi.org/10.7791/jhts.33.252

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