FIELD: aerostation.
SUBSTANCE: proposed airship has gondola, envelope with rigid framework made in form of ball segment and vortex tube. Solar panels are secured on envelope surface. Jet engines are provided with swivel nozzles connected with vortex tube cold air pipe line. End of vortex tube hot air pipe line is brought out to the upper part of envelope inside which ballonet filled with light gas is located.
EFFECT: possibility of operation without fuel.
3 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| JET AIRSHIP | 2005 |
|
RU2284947C1 |
| THERMOBALANCED DIRIGIBLE | 2010 |
|
RU2457149C2 |
| AEROSTAT | 2005 |
|
RU2284279C1 |
| AIRSHIP | 2015 |
|
RU2580385C1 |
| AIRSHIP | 2016 |
|
RU2644813C1 |
| METHOD OF FLIGHT AND AIRCRAFT TO THIS END | 2009 |
|
RU2410284C1 |
| POWER PROPULSION SYSTEM FOR AIRSHIP | 2014 |
|
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| COMBINATION LIGHTER-THAN-AIR FLYING VEHICLES (VERSIONS) | 2006 |
|
RU2318697C2 |
| AIRSHIP WITH SOLAR BATTERIES | 2009 |
|
RU2404903C1 |
| AEROSTAT | 2009 |
|
RU2390466C1 |
