FIELD: aircraft engineering.
SUBSTANCE: aircraft comprises fuselage, control cabin, delta wing, tail plane, engines arranged above said wing and undercarriage. Head parts of the wing and fuselage are connected by hollow prop equipped with rudder arranged between said wing and fuselage. Wig head section hangs over control cabin. Outer wing is arranged above fuselage to retain rear landing gear. Cavities accommodating flywheels running in opposite directions are made in the wing on both sides from central line.
EFFECT: higher lift, mobility and stability.
2 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRBORNE VEHICLE | 2013 |
|
RU2533933C1 |
AIRBORNE VEHICLE | 2013 |
|
RU2536154C1 |
AIRCRAFT | 2013 |
|
RU2530354C1 |
AIRCRAFT FUSELAGE | 2013 |
|
RU2544055C1 |
AIRCRAFT | 2009 |
|
RU2407671C1 |
AIRCRAFT | 2012 |
|
RU2503590C1 |
AIRCRAFT | 2009 |
|
RU2407672C1 |
AIRCRAFT (VERSIONS) | 2011 |
|
RU2462392C1 |
AIRCRAFT | 2015 |
|
RU2581970C1 |
AIRCRAFT | 2009 |
|
RU2407674C1 |
Authors
Dates
2015-03-10—Published
2013-12-12—Filed