FIELD: aviation.
SUBSTANCE: proposed flying vehicle has fuselage with stabilizers, two jet engines for creating the thrust, two aero-maneuverable tubes with air intake and rotors with blades for suction of air, elevators, lateral controls and rudder and turbine for generation of electric power. Provision is also made for self-contained power supply source and electric starter with adjustable starting rheostats. Flying vehicle is provided with two thermo-dynamic tubes each of which is provided with air electric heating elements arranged in thermo-compressor chamber, pneumatic pump which has piston connected with shaft of controllable reversible induction motor by means of gear train with clutch and revolving worm screw. Both jet engines are mounted in fuselage tail.
EFFECT: wide range of technical means.
2 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLYING VEHICLE | 1997 |
|
RU2214348C2 |
| FLOATING DEVICE | 2007 |
|
RU2416546C2 |
| ELECTRON-LASER ACCORDION | 1998 |
|
RU2197758C2 |
| REGISTER-TYPE ACCORDION | 1993 |
|
RU2097839C1 |
| GROUND-EFFECT CRAFT | 2002 |
|
RU2254250C2 |
| ACCORDION | 0 |
|
SU1744710A1 |
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| MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS | 1996 |
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| TAKEOFF-AND-LANDING COMPLEX FOR GROUND-EFFECT CRAFT AND METHOD OF PERFORMING TAKEOFF AND LANDING OF SUCH CRAFT | 2002 |
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RU2254251C2 |
