FIELD: engines and pumps.
SUBSTANCE: intermittent detonation engine consists of housing, circular air duct with central body, semi-closed detonation combustion chamber, detonation initiator, nozzle set, fuel system and control system. Circular air duct has sharp saw-toothed inlet edge. There is a system of magneto-hydrodynamic control of output detonation wave front located in nozzle sett at the output of semi-closed detonation chamber.
EFFECT: invention improves the uniformity of pressure field along the section of air duct circular channel, increases engine operating stability and its thrust.
1 dwg
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