PULSEJET ENGINE DETONATION CHAMBER Russian patent published in 1997 - IPC

Abstract RU 2078969 C1

FIELD: pulsejet engines with resonance combustion chambers. SUBSTANCE: detonation chamber has housing with nozzle 3, coaxial semi-closed chamber 1, unit 4 for supply of gas generation products, shock wave generating device and air flow jet accelerator 5 made in form of axis-symmetrical passage terminating in supersonic nozzle changing to semiclosed chamber. EFFECT: enhanced efficiency. 1 dwg

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RU 2 078 969 C1

Authors

Porshnev V.A.

Fedorets O.N.

Sorokin V.N.

Kononenko R.P.

Dates

1997-05-10—Published

1993-06-10—Filed