Calculation of the Fuel Gas Heating in the Flame Tube Head of Multi-Injector Combustion Chamber of the Gas Turbine Engine
- Authors: Baklanov A.V.1, Malyukov A.V.2
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Affiliations:
- Tupolev Kazan National Research Technical University
- AO KMPO
- Issue: Vol 62, No 1 (2019)
- Pages: 66-73
- Section: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230832
- DOI: https://doi.org/10.3103/S1068799819010094
- ID: 230832
Cite item
Abstract
The flame tube head design is presented of the multi-injector combustion chamber of the gas turbine engine. The technique is described of determining the temperature of fuel gas flowing in the header, which is placed in the combustion chamber flame tube head. The calculation results of the fuel heating in the flame tube head are given.
Keywords
About the authors
A. V. Baklanov
Tupolev Kazan National Research Technical University
Author for correspondence.
Email: andreybaklanov@bk.ru
Russian Federation, ul. Karla Marksa 10, Kazan, Tatarstan, 420111
A. V. Malyukov
AO KMPO
Email: andreybaklanov@bk.ru
Russian Federation, ul. Dement’eva 1, Kazan, 420036