PULSEJET ENGINE Russian patent published in 2013 - IPC F02K7/20 

Abstract RU 2488711 C2

FIELD: engines and pumps.

SUBSTANCE: pulsejet engine comprises housing with combustion chamber and nozzle, fuel feed and ignition system. Said nozzle is composed of annular slot, either discontinuous or solid closed. Engine housing is composed of, at least, two discs with disc-shape combustion chamber arranged there between. Discs are fixed relative to each other by crossbars arranged in circle. Lower disc is secured to generator while top disc is fitted on axle engaged with generator rotor shaft to revolve relative to bottom disc.

EFFECT: better engine cooling, expanded range of jet engines.

4 cl, 1 dwg

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RU 2 488 711 C2

Authors

Telesov Anton Aleksandrovich

Telesov Aleksandr Nikolaevich

Telesov Pavel Aleksandrovich

Dates

2013-07-27Published

2011-02-14Filed