FIELD: machine building.
SUBSTANCE: invention relates to electrical machine building and can be used in electric supply system of hypersonic and detonation aircrafts. Aircraft power supply system comprises drive aircraft engine, generator, lead-out terminals of which are electrically connected to rectifier device, output ends of rectifier device are connected with inverter. Inverter is connected to electric energy consumer. Aircraft engine is made in the form of detonation engine, on the nozzle of which there installed is magnetic field source and winding, which is electrically connected to rectifier device.
EFFECT: higher reliability and energy efficiency, simplified design of aircraft power supply.
1 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| GUIDED MISSILE OF COMBINED ACTION | 2023 |
|
RU2816419C1 |
| METHOD FOR GENERATING ELECTRICAL ENERGY ON BOARD HYPERSONIC FLYING VEHICLE AND MHD GENERATOR USED FOR THE PURPOSE | 2005 |
|
RU2290736C1 |
| AIRCRAFT POWER UNIT | 2013 |
|
RU2601690C2 |
| HYBRID AIR-JET MAGNETOGASDYNAMIC ENGINE | 1998 |
|
RU2138668C1 |
| METHOD AND DEVICE FOR CONTROL OF FLOW IN NOZZLE OF FLYING VEHICLE JET ENGINE | 2006 |
|
RU2323137C1 |
| ENGINE INSTALLATION FOR HYPERSONIC AND AIR SPACE FLYING VEHICLES | 1997 |
|
RU2133863C1 |
| HYBRID DETONATING REACTIVE POWER PLANT OF KRISHTOP (HDRPPK) AND METHOD OF FUNCTIONING OF HDRPPK (OPTIONS) | 2022 |
|
RU2784128C1 |
| METHOD OF CREATING THRUST OF HYPERSONIC FLYING VEHICLE IN CRUISING ATMOSPHERE FLIGHT CONDITIONS | 1993 |
|
RU2042577C1 |
| DRONE AIRCRAFT | 2010 |
|
RU2432301C2 |
| INTERMITTENT DETONATION ENGINE | 2010 |
|
RU2435059C1 |
