Design and investigation of a pneumatic atomizer as applied to a low emission combustion chamber of a promising gas-turbine engine
- Authors: Vasilyev A.Y.1, Chelebyan O.G.1, Yagodkin V.I.1
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Affiliations:
- Central Institute of Aviation motors, Moscow
- Issue: Vol 10, No 5 (2011)
- Pages: 65-71
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/2739
- DOI: https://doi.org/10.18287/2541-7533-2011-0-5(29)-65-71
- ID: 2739
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Abstract
A new injector module has been developed that meets all the requirements made. The module proposed makes it possible to improve the structure of the field of flow of fuel-air mixture and to ensure high quality of fuel atomization, which, in turn, will make it possible to obtain a wide range of starting and steady operation of the combustion chamber under the terrestrial and high – altitude conditions. The degree of homogenization of the mixture is increased, and, as a consequence, we can expect lower emission of harmful impurities at the output of the gas turbine engine.
About the authors
A. Yu. Vasilyev
Central Institute of Aviation motors, Moscow
Author for correspondence.
Email: vasiliev@ciam.ru
Candidate of Technical Sciences
Head of the Sector
Russian FederationO. G. Chelebyan
Central Institute of Aviation motors, Moscow
Email: oganeschelebyan@mail.ru
Post-graduate Student
Instrumentation Engineer
Russian FederationV. I. Yagodkin
Central Institute of Aviation motors, Moscow
Email: yagodkin@ciam.ru
Candidate of Technical Sciences
Head of the Sector
Russian Federation