TURBO-MACHINE CONTAINING DETONATION CHAMBER AND AIRCRAFT EQUIPPED WITH SUCH TURBO-MACHINE Russian patent published in 2016 - IPC F02C3/14 F02K7/08 F23R7/00 

FIELD: engines and pumps.

SUBSTANCE: turbo-machine comprises at least, in the direction of the gas stream compressor, chamber containing a means ensuring formation of hot gases from the air mixture formed from the captured air flow and of fuel, and turbine rotated by means of hot gases and thus actuating the compressor. Said chamber comprises engine with continuous detonation wave equipped with circular detonation chamber and connected devices, providing continuous formation of hot gases from flammable fuel-air mixture. Engine with continuous detonation wave is designed to form the first flow of captured air entering the detonation chamber and used in engine, and the second flow bypassing the chamber. Turbo machine additionally comprises auxiliary means for mixing of hot gases leaving the detonation chamber, with the second air flow before turbine and carrying out several detonation chambers concentrically located relative to each other about turbo-machine axis, thus providing optimum operating conditions in a wide range of concentrations and limiting impacts at start-up.

EFFECT: invention is aimed at turbo-machine improvement, particularly increase of its effective power.

10 cl, 1 dwg