| 摘要 |
An aircraft comprises a system of azimuth, roll, pitch control, a propulsion system, a fuselage, a tail, upper and lower cell-type all-moving wings with negative sweep with shorter rear semiwimgs with semicircular tips, hinges for turning wings, which are displaced from each other in the transverse direction. At the ends of cells of short semiwings across their span by a hinged joint these tips of a wing with drives are secured, the drives are connected to the roll control system of the aircraft at angles with sweep of short semiwings X = 55° -75°. |
