FIELD: aviation.
SUBSTANCE: invention relates to the aviation equipment. Aircraft comprises a frame, branch pipes with outlet holes for passage of working substance, creating reactive forces, central and flexible shells in form of separate sections, having cavities for working substance and for carrier gas, separated by elastic walls, power source and injector of working substance, made with possibility to supply working substance to each said cavity for working substance and the above branch pipes. Cavities for bearing gas of shells are made with possibility of their connection to each other.
EFFECT: invention is aimed at expansion of capabilities of aircraft movement along the ground.
1 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT | 2014 |
|
RU2578911C1 |
| AIRCRAFT | 2011 |
|
RU2475416C2 |
| HEAT ENGINE | 2017 |
|
RU2666708C1 |
| SPRINKLER | 0 |
|
SU1109088A1 |
| THERMAL WIND ENGINE | 2023 |
|
RU2816343C1 |
| THERMAL ENGINE | 2007 |
|
RU2367818C1 |
| ENGINE | 2011 |
|
RU2467203C1 |
| THERMAL WIND MOTOR | 2013 |
|
RU2542167C2 |
| SEMI-RIGID CONTROLLABLE AEROSTATIC FLYING VEHICLE AT VARYING CONFIGURATION OF CASE | 2004 |
|
RU2249536C1 |
| COMBINATION FLYING VEHICLE | 1996 |
|
RU2114765C1 |
