The concept of matching the joint operation of the combustion chamber, the compressor and the turbine

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Abstract

The paper presents scientifically grounded requirements on the values of corrected velocity of gas flow at the input and output of the combustion chamber aimed at providing stability and the required  uniformity of the gas temperature field at the turbine input while maintaining the optimal mode of chamber operation with regard to stability and efficiency of combustion and emission.

About the authors

A. V. Grigoriev

JSC Klimov

Author for correspondence.
Email: klimov@klimov.ru

General Designer

Russian Federation

P. P. Golubchikov

Saint-Petersburg State Polytechnical University

Email: kadet_spb@mail.ru

Student

Russian Federation

M. Yu. YIlushin

Klimov JSC, Saint-Petersburg

Email: klimov@klimov.ru

Engineer-designer

Russian Federation

O. A. Rudakov

Klimov JSC, Saint-Petersburg

Email: klimov@klimov.ru

Scientific Consultant

Russian Federation

A. V. Solovieva

Klimov JSC, Saint-Petersburg

Email: anastasia.solovjeva@gmail.com

Engineer-designer

Russian Federation

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