FIELD: reaction engine.
SUBSTANCE: proposed method comes to delivery of on-coming flows of preliminarily compressed air into combustion chamber of reaction engine and combustion of fuel. Said air is compressed in compressor driven by gas turbine on-coming flows of compressed air getting from compressor are formed in combustion chamber provided with solid bottom arranged at opposite side from its outlet hole. Said on-coming flows collide in central part of combustion chamber with complete braking and converting of kinematic energy into additional compression directly in combustion chamber. Fuel is combusted in said volume of additionally compressed air.
EFFECT: increased engine power and reactive thrust.
4 cl, 1 dwg
