COMBUSTION CHAMBER WITH ACOUSTIC ABSORBER Russian patent published in 2000 - IPC

Abstract RU 2161262 C2

FIELD: rocketry; liquid-propellant rocket engines. SUBSTANCE: combustion chamber includes gas passage, center injector face and unit of injector faces with gas and gas-and-liquid injectors. Injectors connect gas passage cavity with injector face cavity. Perforated diaphragm is mounted in gas passage above injector face unit forming resonance cavity of acoustic absorber. Inlet end faces of gas injectors are located at level of or above upper surface of diaphragm. EFFECT: enhanced operational reliability and stability of combustion at minor amount of additional parts. 7 cl, 8 dwg

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Authors

Gritsenko E.A.

Anisimov V.S.

Danil'Chenko V.P.

Mikhajlov S.V.

Jaroslavtsev V.G.

Dates

2000-12-27Published

1999-01-25Filed