Enviar artigo por via de e-mail Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection
- Autores: Baklanov A.1, Gimbitskii A.2
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Afiliações:
- AO KMPO
- Tupolev Kazan National Research Technical University
- Edição: Volume 62, Nº 3 (2019)
- Páginas: 463-468
- Seção: 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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Resumo
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.
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Sobre autores
A. Baklanov
AO KMPO
Autor responsável pela correspondência
Email: andreybaklanov@bk.ru
Rússia, ul. Dement’eva 1, Kazan, Tatarstan, 420036
A. Gimbitskii
Tupolev Kazan National Research Technical University
Email: andreybaklanov@bk.ru
Rússia, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
