BURNER OF GAS-TURBINE ENGINE COMBUSTION CHAMBER Russian patent published in 1998 - IPC

Abstract RU 2107869 C1

FIELD: combustion chambers of gas-turbine engines working mainly on gaseous fuel. SUBSTANCE: each burner of combustion zone and pilot combustion zone. Combustion process in pilot zone is organized at excess air coefficient of α = 1.2 to 1.4 and in main combustion zone at excess air coefficient of α = 1.8 to 2.0. EFFECT: enhanced efficiency. 2 cl, 2 dwg

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RU 2 107 869 C1

Authors

Postnikov A.M.

Markushin A.N.

Denisov I.S.

Savchenko V.P.

Dates

1998-03-27Published

1993-07-01Filed