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Heat transfer at various methods of thermal protection in the systems of power-driven gas turbine plants (GTP)

  • Aircraft and Rocket Engine Design and Development
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Abstract

The scheme variants of implementing the thermal protection against heat flows being generated by the body of a high-temperature stationary gas turbine engine (GTE) are presented. The scheme of the experimental bench with a working section is given. Methodical approaches to the heat transfer calculation at different variants of forced and natural convection organization and under various operating conditions are described. The generalized results of the experiments carried out using a heat curtain being generated by porous injection are presented.

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Authors and Affiliations

  1. Tupolev Kazan National Research Technical University, Kazan, Russia

    A. V. Gimbitskii, S. G. Dezider’ev & A. G. Karimova

Authors
  1. A. V. Gimbitskii
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  2. S. G. Dezider’ev
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  3. A. G. Karimova
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Additional information

Original Russian Text © A.V. Gimbitskii, S.G. Dezider’ev, A.G. Karimova, 2011, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2011, No. 3, pp. 63–66.

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Gimbitskii, A.V., Dezider’ev, S.G. & Karimova, A.G. Heat transfer at various methods of thermal protection in the systems of power-driven gas turbine plants (GTP). Russ. Aeronaut. 54, 322–327 (2011). https://doi.org/10.3103/S1068799811030159

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  • DOI: https://doi.org/10.3103/S1068799811030159

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