Design and investigation of a pneumatic atomizer as applied to a low emission combustion chamber of a promising gas-turbine engine

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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 Federation

O. G. Chelebyan

Central Institute of Aviation motors, Moscow

Email: oganeschelebyan@mail.ru

Post-graduate Student

Instrumentation Engineer

Russian Federation

V. I. Yagodkin

Central Institute of Aviation motors, Moscow

Email: yagodkin@ciam.ru

Candidate of Technical Sciences

Head of the Sector

Russian Federation

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