FIELD: aerostation.
SUBSTANCE: proposed aerostat has nacelle, external envelope for warm air, internal envelope for light gas and hot air source in form of vortex tube with air blower. Solar batteries are used as energy source for air blower. Hot air pipe line running from vortex tube is brought out to upper part of external envelope and cold air pipe line is directed downward. Discharge pipe line from lower part of external envelope is directed downward. Aerostat is provided with storage batteries.
EFFECT: increased flying range.
3 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| JET AIRSHIP | 2005 |
|
RU2284947C1 |
| JET AIRSHIP (DIRIGIBLE) | 2005 |
|
RU2300482C1 |
| THERMAL BALLOON | 2011 |
|
RU2453470C1 |
| THERMOBALANCED DIRIGIBLE | 2010 |
|
RU2457149C2 |
| SEMI-RIGID DIRIGIBLE AEROSTAT | 2000 |
|
RU2230686C2 |
| THERMAL MULTI-CHAMBER AEROSTAT | 2000 |
|
RU2197409C2 |
| AEROSTAT | 1990 |
|
RU2005647C1 |
| GLIDING AEROSTAT | 1993 |
|
RU2104214C1 |
| SOLAR AEROSTAT | 2000 |
|
RU2184679C2 |
| TWO-MODE AEROSTATIC COMBINED FLYING VEHICLE | 2001 |
|
RU2222471C2 |
