FIELD: lighter- than-air flying vehicles. SUBSTANCE: energy of translational motion of air flow before entering wind motor 7 mounted on aerostat is converted into energy of rotary motion by swirling air flow in spiral narrowing passages of annular air intake forming vortex whose peripheral layer is exhausted to aerostat envelope; after interaction of central mass of vortex with wind motor 7, energy of translational motion of carrier gas is used for creating the control forces. EFFECT: enhanced reliability. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF SUPPLY OF POWER TO AEROSTAT | 2001 |
|
RU2196072C2 |
| WINDMILL | 1994 |
|
RU2118704C1 |
| WINDMILL | 1994 |
|
RU2098657C1 |
| WINDMILL OPERATION | 1994 |
|
RU2101555C1 |
| METHOD OF OPERATION OF SYSTEM OF GAS TURBINE SUPERCHARGING OF INTERNAL COMBUSTION ENGINE | 1994 |
|
RU2084651C1 |
| METHOD OF OPERATION OF POWER-GENERATING SEMI- SUBMERSIBLE PLATFORM | 2001 |
|
RU2213882C2 |
| METHOD FOR DRIVING MULTISTAGE VANE COMPRESSOR | 1993 |
|
RU2074979C1 |
| WIND-DRIVEN MOTOR | 0 |
|
SU1765492A2 |
| WIND MOTOR | 0 |
|
SU1657723A1 |
| THERMAL AIRSHIP | 0 |
|
SU1735117A1 |
