FIELD: combined flying vehicles. SUBSTANCE: flying vehicle has an aerostat shell from a gas-proof material filled with a carrying gas, and a nacelle which is aircraft 4. The aerostat shell is made from two positioned one inside the other disk balloons 1, 2 from a heat-resistant material rigidly fastened to the upper surface of aircraft 4 by annular tubular frame 3. Inner balloon 1 is made multisectional and is filled with helium and compensates for 80-90% of the flight vehicle weight. The space between outer and inner balloons 2 and 1 is filled with a hot air heated by main engines of aircraft 4. The relative thickness of balloons 1, 2 is about 10% of their diameter. EFFECT: improved operational characteristics. 3 cl, 1 dwg
| Title | Year | Author | Number | 
|---|---|---|---|
| TWO-MODE AEROSTATIC COMBINED FLYING VEHICLE | 2001 | 
 | RU2222471C2 | 
| CONTROLLABLE AEROSTATIC FLYING CRANE | 1995 | 
 | RU2098318C1 | 
| FIRE AIRSHIP | 2003 | 
 | RU2250122C1 | 
| FLYING VEHICLE WITH MUSCULAR DRIVE | 0 | 
 | SU1804413A3 | 
| COMBINATION FLYING VEHICLE | 1996 | 
 | RU2114765C1 | 
| POWERED GLIDER | 0 | 
 | SU1799335A3 | 
| AERO-SPACE TRANSPORT SYSTEM | 1994 | 
 | RU2111147C1 | 
| LIGHTER-THAN AIR SEMIRIGID COMBINED CONTROLLABLE FLYING VEHICLE | 1999 | 
 | RU2141911C1 | 
| HIGH-ALTITUDE GUIDED AEROSTATIC FLYING VEHICLE | 1994 | 
 | RU2111146C1 | 
| FOLDING AIRSHIP-AIRPLANE | 2020 | 
 | RU2752326C1 | 
Authors
Dates
1994-03-15—Published
1989-12-19—Filed