| 摘要 |
An invention relates to aircrafts, more specifically - to the development of the design of aircraft that can conduct a vertical take-off and landing, horizontal flying and changing of the flying direction. Its aim is to make the design of the aircraft simpler, to ensure the maneuvering capacity while being in horizontal motion, as well as to ensure security in case of emergency landing. The aim is achieved providing the aircraft (fig. 1), which comprises the hull (1), the cabin with the control system (2), the engines (4), e.g. the propeller-type engines, by flat discoid hull with at least five engines located in the seats of the hull. Four engines are connected in pairs with the horizontal axles (6, 7), which are mutually firmly connected by the hawser (8). Said horizontal axles (6, 7) are fixed in the hull in such a way that they can be turned around its axis, and they are mutually interacting with the control system by help of hydraulic system (5). The fifth engine ensuring the maneuvering capacity of aircraft is connected with the control system by help of the sliding hawser (11) and axle (10), which is fixed to the engine by revolving ring (9). The engine is, in addition, equipped with pair of worm gearings for its turning into horizontal plane.
|
