FIELD: hypersonic and air space flying vehicles with electrode-free technical means on principle of magnetodynamics. SUBSTANCE: proposed engine installation is designed to increase velocity limit of serviceability of hypersonic ramjet engines by prevention of separation of boundary layer from walls of diffuser. Magnetic field is formed by current-carrying windings laid behind walls of gas circuits of hypersonic ramjet engines transverse to their central axes. Hypersonic ramjet engines are formed near one or both side surfaces of fuel tanks made in the form of torus that forms appearance of flying vehicle. EFFECT: improved design and operational characteristics. 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HYBRID AIR-JET MAGNETOGASDYNAMIC ENGINE | 1998 |
|
RU2138668C1 |
| AIRCRAFT POWER UNIT | 2013 |
|
RU2601690C2 |
| METHOD AND AIR VEHICLE FOR MOVING IN PLANETARY ATMOSPHERE WITH SPEEDS ABOVE THE FIRST SPACE AND HIGHLY INTEGRATED HYPERSONIC VEHICLE APPARATUS (VERSIONS) FOR IMPLEMENTATION OF THE METHOD | 2012 |
|
RU2618831C2 |
| HYPERSONIC RAMJET ENGINE | 2017 |
|
RU2691702C2 |
| HYPERSONIC RAMJET ENGINE AND METHOD OF ORGANIZATION OF COMBUSTION | 2003 |
|
RU2262000C2 |
| AIRCRAFT RAMJET ENGINE | 2004 |
|
RU2269022C2 |
| HYPERSONIC FLYING VEHICLE | 1999 |
|
RU2172278C2 |
| COMPOSITE RAMJET ENGINE | 1993 |
|
RU2076829C1 |
| METHOD OF IGNITION AND COMBUSTION OF FUEL IN ATHODYD | 2013 |
|
RU2550209C1 |
| HYPERSONIC PROPULSIVE JET ENGINE, AND COMBUSTION ARRANGEMENT METHOD | 2012 |
|
RU2511921C1 |
