FIELD: aerostatic flying vehicles. SUBSTANCE: proposed flying vehicle includes disk-shaped lifting balloon filled with helium and hot air and nacelle made in form of civil aeroplane. Located inside said balloon is disk-shaped multi-sectional container whose sections are filled with helium for carrying the cargoes. Flying vehicle is provided with air temperature control unit for regulation of temperature from 200 C to 20 C. Balloon has form of wing round in plan at controllable angle of attack for forming additional aerostatic lifting force; ratio of thickness of balloon to diameter is 20-25%. Flying vehicle is provided with storage batteries for supply of electrical equipment , solar cells located on upper plane of balloon, clearance limit lights, light designations of number and search-lights for landing at night. EFFECT: improved technical and operational characteristics. 5 cl, 1 dwg, 1 tbl
| Title | Year | Author | Number | 
|---|---|---|---|
| AEROSTAT COMBINED FLYING VEHICLE | 1989 | 
 | RU2009073C1 | 
| METHOD OF FLIGHT AND AIRCRAFT TO THIS END | 2009 | 
 | RU2410284C1 | 
| CONTROLLABLE AEROSTATIC FLYING CRANE | 1995 | 
 | RU2098318C1 | 
| SEARCH-AND-RESCUE AIRCRAFT | 2007 | 
 | RU2337855C1 | 
| FIRE AIRSHIP | 2003 | 
 | RU2250122C1 | 
| AERONAUTICAL VEHICLE | 2016 | 
 | RU2659147C1 | 
| POWERED GLIDER | 0 | 
 | SU1799335A3 | 
| RECONNAISSANCE UNMANNED AERIAL VEHICLE | 2023 |  | RU2806574C1 | 
| AERO-SPACE TRANSPORT SYSTEM | 1994 | 
 | RU2111147C1 | 
| MULTI-MISSION HIGHLY-MANEUVERABLE VERTICAL TAKEOFF AND LANDING AIRCRAFT | 1997 | 
 | RU2127693C1 | 
Authors
Dates
2004-01-27—Published
2001-03-11—Filed