FIELD: aeronautical engineering. SUBSTANCE: proposed flying vehicle has cone-shaped fuselage, four stabilizers autonomous power supply source, two engines for creation of thrust, elevators and rudders. Flying vehicle is provided with water reactor with collector-type heating elements for forming steam in heating water, turbine for generation of electric power, rotors with blades for suction of air and aeromaneuverable tubes with air intakes. Said rotors, elevators and rudders are located in aeromaneuverable tubes. Each engine is made in form of jet engine arranged in tail fuselage for creation of thrust due to steam formed in electric batteries. EFFECT: increased flying range. 2 cl, 6 dwg _
| Title | Year | Author | Number |
|---|---|---|---|
| FLYING VEHICLE | 2004 |
|
RU2312796C2 |
| FLOATING DEVICE | 2007 |
|
RU2416546C2 |
| AIRCRAFT | 2008 |
|
RU2466907C1 |
| COMBINED DYNAMICALLY SCALED AERODYNAMIC MODEL FOR DIFFERENT TYPES OF AERODYNAMIC TESTS | 2023 |
|
RU2808290C1 |
| METHOD OF CREATING AIRCRAFT LIFT (VERSIONS), METHOD OF FLIGHT, NON-AERODYNAMIC ALL-WEATHER VTOL AIRCRAFT "MAXINIO" (VERSIONS), METHODS OF TAKE-OFF AND LANDING, AICRAFT CONTROL METHOD AND SYSTEM, FUSELAGE, WING (VERSIONS), THRUST REVERSE AND METHOD OF ITS OPERATION, LANDING GEAR SYSTEM, GAS SEPARATION AND DISTRIBUTION SYSTEM | 2007 |
|
RU2349505C1 |
| ROTOROPLANE | 2001 |
|
RU2245824C2 |
| ELECTRON-LASER ACCORDION | 1998 |
|
RU2197758C2 |
| HOVERCRAFT WITH WATER-JET PROPULSOR | 2015 |
|
RU2582505C1 |
| METHOD OF CREATION OF VEHICLE PROPULSIVE FORCE AND PROPULSION DEVICE BASED THEREON | 2006 |
|
RU2334116C1 |
| CONVERTIPLANE | 2008 |
|
RU2369525C2 |
