FIELD: aviation.
SUBSTANCE: devices for gyroscopic stabilization of aircraft. The aircraft contains a turbine and/or an electric motor connected to the aerodynamic body through the frame of the aircraft to provide thrust to the aircraft. The jet turbine has a fuel source, an air intake for air supply, and an outlet for exhausting the burnt air-fuel mixture. The jet turbine is connected to the gyroscopic stabilization unit by means of a shaft. The gyroscopic stabilization unit contains a gyroscopic fan with alternating rotary blades to provide controlled stable flight. The aircraft is preferably capable of vertical take-off so that it can be used in a wide range of situations.
EFFECT: ability to fight large fires using exhaust gases.
33 cl, 21 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COMPOUND HELICOPTER | 1994 |
|
RU2089456C1 |
| FIREFIGHTING AIRCRAFT | 2010 |
|
RU2483981C2 |
| MULTI-PURPOSE VERTICAL TAKEOFF AND LANDING FLYING VEHICLE | 2004 |
|
RU2272751C1 |
| INTEGRATED TECHNOLOGY OF OPERATION AND PRODUCTION "MAXINIO" TRANSPORT FACILITIES: VTOL ELECTRIC AIRCRAFT (VERSIONS), ELECTRIC AIRCRAFT UNITS AND METHODS OF EMPLOYMENT ELECTRIC AIRCRAFT AND ITS PARTS | 2010 |
|
RU2466908C2 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT | 2014 |
|
RU2574873C1 |
| AUTOGYRO FOR AVIA FOREST PROTECTION | 2020 |
|
RU2728950C1 |
| PROPELLER-DRIVEN FLYING VEHICLE "VISTLA-01" | 2005 |
|
RU2313472C2 |
| HELICOPTER | 2018 |
|
RU2710839C1 |
| FIRE CRANE HELICOPTER | 2022 |
|
RU2797539C1 |
| AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING AND/OR VERTICAL TAKEOFF AND LANDING WITH SHORTENED RUN | 2021 |
|
RU2764311C1 |
