FIELD: aviation industry.
SUBSTANCE: proposed aircraft contains fuselage, wing and engine. Fuselage and wing are built using two parabolas. Wing is provided with rods with damping devices in units of fastening to aerodynamic center of fuselage.
EFFECT: improved aerodynamic properties of aircraft.
2 cl, 11 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HELICOPTER | 2006 |
|
RU2309873C1 |
| PROPELLER BLADE | 2004 |
|
RU2278058C2 |
| FLAPPING-WING AIRCRAFT | 2006 |
|
RU2323129C2 |
| HELICOPTER | 2006 |
|
RU2333867C2 |
| TURBOJET ENGINE | 2007 |
|
RU2367798C2 |
| AXIAL-BLOW BLOWER | 2007 |
|
RU2362911C2 |
| AIR PROPELLER | 2006 |
|
RU2318698C1 |
| PROPELLER | 2006 |
|
RU2314968C1 |
| ROTOR MAST | 2007 |
|
RU2359862C2 |
| VANE-TYPE WIND-DRIVEN POWER PLANT | 2006 |
|
RU2309290C1 |
