FEATURES OF ORGANIZATION OF FILM COOLING OF HIGH TEMPERATURE GAS TURBINES BLADES


  • A. A. Khalatov Institute of Engineering Thermophysics of the National Academy of Sciences of Ukraine
  • A. S. Kovalenko NTUU «Kyiv Politechnic Inztitute»
  • S. B. Reznik SE IVCHENKO-PROGRESS
DOI: https://doi.org/10.31472/ihe.4.2017.02
Keywords: high temperature turbine, cooling air, convective-film cooling, front edge of blade

Abstract

The features of the release of the cooling air in the interscapular channel high temperature gas turbines at the film cooling are considered. Possibilities of its local distribution on contour of an entrance edge of the perforated blades are investigated. The presented calculations show that the substantial increase in the cooling efficiency can be attained due to channels of small dimension in the blade wall.

 

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Published
2017-03-24
How to Cite
Khalatov, A., Kovalenko, A., & Reznik, S. (2017). FEATURES OF ORGANIZATION OF FILM COOLING OF HIGH TEMPERATURE GAS TURBINES BLADES. Thermophysics and Thermal Power Engineering, 39(4), 11-20. https://doi.org/https://doi.org/10.31472/ihe.4.2017.02
Issue
Vol 39 No 4 (2017): Industrial Heat Engineering
Section
Heat and Mass Exchange Processes
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