Мақаланы E-mail арқылы жіберу Study of Heat Transfer from the Shell of Gas Turbine Plant and Methods of Its Thermal Protection
- Авторлар: Baklanov A.1, Gimbitskii A.2
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Мекемелер:
- AO KMPO
- Tupolev Kazan National Research Technical University
- Шығарылым: Том 62, № 3 (2019)
- Беттер: 463-468
- Бөлім: 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
Дәйексөз келтіру
Ашық рұқсат
Рұқсат берілді
Тек жазылушылар үшін
Аннотация
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.
Негізгі сөздер
Авторлар туралы
A. Baklanov
AO KMPO
Хат алмасуға жауапты Автор.
Email: andreybaklanov@bk.ru
Ресей, ul. Dement’eva 1, Kazan, Tatarstan, 420036
A. Gimbitskii
Tupolev Kazan National Research Technical University
Email: andreybaklanov@bk.ru
Ресей, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
