FIELD: aviation.
SUBSTANCE: proposed flying vehicle is made in form of body of revolution at vertical axis. Proposed flying vehicle is provided with axial-flow rotary compressor, engine with fuel and heat-insulated receiver connected with compressor. Flat back bottom of receiver has through holes of small diameter which are inclined to side opposite to takeoff and rotation of compressor rotor-propeller. Receiver is provided with four flaps for closing the holes for creation of trim of flying vehicle. Compressor rotor-propeller takes air in front of flying vehicle and delivers heated air to heat-insulated receiver. Air is expanded into surrounding medium through holes made in receiver bottom used as load-bearing area for flying vehicle surface. For performing horizontal flight, trim shall be formed by means of flaps in the direction of motion.
EFFECT: increased cargo carrying capacity.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ATMOSPHERIC COMPRESSOR JET-POWERED VEHICLE | 2016 |
|
RU2617863C1 |
| AXIAL-FLOW ROTARY COMPRESSOR | 2003 |
|
RU2243414C1 |
| METHOD OF CREATING A TRAIL AND POWER INSTALLATION FOR ITS IMPLEMENTATION | 2017 |
|
RU2680214C1 |
| SUBSONIC AIRCRAFT HYBRID POWER PLANT AND KRISHTOP MULTIPURPOSE AIRCRAFT (VERSIONS) | 2018 |
|
RU2698276C1 |
| AXISYMMETRIC AIRCRAFT | 2022 |
|
RU2789464C1 |
| COMBINATION BLADE OF FLYING VEHICLE MAIN ROTOR AND METHOD OF FLIGHT OF FLYING VEHICLE | 1998 |
|
RU2149799C1 |
| ROTARY COMPRESSOR | 2004 |
|
RU2273768C1 |
| CONVERTIPLANE | 2008 |
|
RU2369525C2 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2019 |
|
RU2708516C1 |
| VTOL AIRCRAFT AND VTOL RADIAL-FLOW AIR PROPULSOR | 2010 |
|
RU2437801C1 |
