FIELD: engines and pumps.
SUBSTANCE: engine comprises several detonation tubes, each including independent discharge outlet, interconnected in the common air-fuel intake inlet. Air-fuel mix detonates in detonation tubes simultaneously while common air-fuel mix inlet minimises the back pressure caused by said detonation by sending several shock waves toward each other at application of back pressures as reactive fronts and reduction of the effects of shock waves propagating backward and upstream. Said detonation tubes can be curved.
EFFECT: uniform power feed to the turbine.
22 cl, 12 dwg
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