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Hypersonic, jet engine With PULSE DETONATION the combustion chamber, with a combined HYPERSONIC jet stream with supersonic ramjet 'one another'
Hypersonic, jet engine With PULSE DETONATION the combustion chamber, with a combined HYPERSONIC jet stream with supersonic ramjet 'one another'
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机译：高超音速喷气发动机带有脉冲爆震的燃烧室，结合了超音速喷气流和超音速冲压喷气机“彼此”
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1. Hypersonic air jet engine is detonation-pulsing cone-circular combustion chamber an enveloping propulsive jet working channel, thereby combining hypersonic jet flow of the working cone-circular combustion chamber with a supersonic jet stream of a working channel uniflow "one another" konusno- circular detonation-pulsating combustion chamber has an annular nozzle supply explosive vapor-fuel mixture has an increased formation portion EMA discharge and suction of the first explosion volume has a portion forming a second blast volume, a braking portion ahead running of the shock wave at the output of cone-circular combustion chambers, has coincidence outer conical surface of cone-circular combustion chamber with an inlet nozzle portion of the first nozzle Lovaglio sealingly connected second, there is a combination of supersonic and hypersonic jet streams working happens like in the mixing chamber in place joining two nozzles Lovaglio having means zazhi Hassium ensures ignition of the explosive fuel mixture in the initial period of engine start, has a thermal charge for heating and purging of the combustion chamber, the ram channel and setting an ejection air thrust has detonation starting charge for the formation of triple shock wave with the required interval for engine startup has two feed flow air to form a fuel mixture operating due to overpressure outside air during motion of the aircraft, the first flow from the tail
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