FIELD: transport, aviation.
SUBSTANCE: proposed aircraft comprises a fuselage representing a rigid casing with fixed-geometry slots, a skin, wings, a tail unit, an engine and a landing gear. The wings can reciprocate across the fuselage casing. The said casing incorporates a wall built therein and furnished with a crosswise slot. Every wing arranged on the fuselage sides features an end face plate with a cantilever attached horizontally thereto to penetrate into the said wall slot. Note that the said end face plate is skintight with respect to the wall. Also, note that the said cantilever is linked up with the drive fitted inside the fuselage.
EFFECT: accelerated production of flight vehicle.
4 cl, 3 dwg
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AIRCRAFT | 2008 |
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RU2380275C1 |
AIRCRAFT (VERSIONS) | 2011 |
|
RU2462392C1 |
AIRCRAFT | 2009 |
|
RU2407671C1 |
AIRCRAFT | 2012 |
|
RU2503590C1 |
AIRCRAFT | 2009 |
|
RU2407674C1 |
AIRBORNE VEHICLE | 2013 |
|
RU2536154C1 |
AIRBORNE VEHICLE | 2013 |
|
RU2544036C1 |
AIRBORNE VEHICLE | 2013 |
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RU2533933C1 |
AIRCRAFT FUSELAGE | 2013 |
|
RU2544055C1 |
AIRCRAFT | 2009 |
|
RU2397107C1 |
Authors
Dates
2009-02-27—Published
2007-10-02—Filed