FIELD: hybrid reactive detonation combustion power plants.
SUBSTANCE: invention of the HDRPPK relates to the field of hybrid reactive detonation combustion power plants with an MHD generator that generates electricity by rotating the electrically conductive products of detonation combustion in the circular channel of the MHD generator, and the reactive thrust of which is formed by the supersonic exit of the detonation combustion products from the main jet nozzle at the output of the circular channel of the MHD generator. HRDCPP can be used highly efficiently for hybrid aircraft operating in a wide range - from zero to supersonic speeds of several Machs, which can be used for long-range supersonic highly efficient and reliable aviation.
EFFECT: invention allows use of natural gas as the most preferred low-cost and lightweight fuel for aircraft; HDRPPK can also be used with high efficiency for any type of land or water-sea transport, as well as for hybrid amphibians of aeroamphibious structures.
3 cl, 2 dwg
