FIELD: operation of aircraft in regions under various climatic and geographic conditions, as well as in some Northern regions. SUBSTANCE: aircraft wing is bent in root portion, engines are arranged inside fuselage behind passenger cabin and propellers are mounted on wing in area where wing outer panel changes to center section Drive to propellers is effected by means of transmission located in center section of wing and connected with engines and with propeller shaft on other side; it is enclosed in metal casing connected to wing. Engines are interconnected by means of mechanical device through reduction gears. Fuel system includes several fuel tanks. Engine compartment is isolated from passenger cabin by means of fireproof noise-absorbing bulkheads. Aircraft has several modifications for performing aerial photography, forest control, communications, tourism and personal air transport. EFFECT: enhanced reliability. 8 cl, 21 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LIGHT AMPHIBIAN | 1992 |
|
RU2111150C1 |
| LIGHT TWIN-ENGINED MULTI-PURPOSE AIRCRAFT LADOGA-9 FOR GROUND AND WATER BASES | 1994 |
|
RU2132290C1 |
| MULTI-PURPOSE TWIN-ENGINED SEA-BASED AND LAND- BASED AIRCRAFT OF SHORT TAKEOFF AND LANDING | 2001 |
|
RU2196707C2 |
| MULTI-PURPOSE LIGHT AIRCRAFT | 1992 |
|
RU2111151C1 |
| PROPELLER-DRIVEN FLYING VEHICLE "VISTLA-01" | 2005 |
|
RU2313472C2 |
| TWIN-ENGINE MULTI-PURPOSE AIRCRAFT "CHOLOD-1" (VERSIONS) | 2005 |
|
RU2297368C1 |
| FIREFIGHTING AIRCRAFT | 2010 |
|
RU2483981C2 |
| EMERGENCY RESCUE SYSTEM FOR RESCUE OF PASSENGERS, CREW AND CARGOES IN CASE OF IN-FLIGHT ACCIDENT | 1998 |
|
RU2152335C1 |
| MAIN LINE PASSENGER PLANE USING CRYOGENIC FUEL | 2015 |
|
RU2614443C1 |
| AMPHIBIOUS WITH INCREASED CARRYING CAPACITY | 2020 |
|
RU2739451C1 |
