FIELD: aviation industry.
SUBSTANCE: engines for aviation industry and other industries. Invention relates to the fields of: aircraft engines for aircrafts, energy industry, mechanical engineering and engine building, and specifically to devices and installations in which the working fluid is used to create a supersonic high-temperature plasma jet in the process of detonation combustion of a mixture of fuel with air for universal and highly efficient use in various designs of reactive detonation combustion devices, for example: aircraft engines using the Krishtop detonating intermittent air-jet engine, rotary detonation engines, the torque on the shaft of which is formed by jet thrust, located at the edges of the Krishtop detonating intermittent air-jet engine rotor, hybrid detonation air-breathing systems, as well as in the designs of devices for detonation highly efficient fuel combustion in power CCGTs of high efficiency and ecological efficiency, as well as other devices for various purposes and in various fields of application. The invention can be attributed to a completely new scheme, conditionally called "gate scheme" - in addition to the known detonation combustion schemes - conditionally called "spin scheme", "valve scheme" and "valveless scheme" for pulsating jet engines.
EFFECT: high efficiency and ecological efficiency.
4 cl, 4 dwg
