Email this article Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection
- Authors: Baklanov A.V.1, Gimbitskii A.V.2
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Affiliations:
- AO KMPO
- Tupolev Kazan National Research Technical University
- Issue: Vol 62, No 3 (2019)
- Pages: 463-468
- Section: Aircraft and Rocket Engine Design and Development
- URL: https://journals.rcsi.science/1068-7998/article/view/231059
- DOI: https://doi.org/10.3103/S1068799819030140
- ID: 231059
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Abstract
The paper presents the results of determining the temperature of gas turbine plant shell. The total heat transfer from the engine is calculated. The thermal protection scheme by blowing air through the porous screen is proposed to reduce the temperature of the gas turbine plant shell as well as to reduce the total heat transfer from the engine to the surrounding compartment space.
About the authors
A. V. Baklanov
AO KMPO
Author for correspondence.
Email: andreybaklanov@bk.ru
Russian Federation, ul. Dement’eva 1, Kazan, Tatarstan, 420036
A. V. Gimbitskii
Tupolev Kazan National Research Technical University
Email: andreybaklanov@bk.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
