| 摘要 |
FIELD: aircraft engineering.SUBSTANCE: aircraft power plant containing circular gas intake channel located between aircraft body and gas intake shell, as well as magnetic system, inducing radial magnetic field in channel. In channel MHD-generators box-shaped modules are arranged, in walls of which separating gas flows blades are built-in, but conducting circular electric current by inter-blade gaps, and rocket chamber with nozzle upwards is installed between module lower walls. Rocket fuel combustion products cross magnetic field and generate circular electric current in gases, which creates electrodynamic force in presence of same magnetic field, accelerating atmospheric mass, moving between MHD-generators modules, which creates thrust exceeding rocket chambers thrust in MHD-generators.EFFECT: higher thrust at atmospheric flight part in hypersonic mode.2 cl, 1 dwg |
