The invention discloses a distributed electric propulsion box type wing ground effect aircraft which comprises a main fuselage, the two sides of the main fuselage are connected with one ends of sweepback wing main wings, one ends of two empennages above the tail of the main fuselage are connected with the main fuselage through vertical tails, and the other ends of the two empennages are connected with the other ends of the two main wings through end plates respectively. The empennage is connected with a plurality of high ducted fans directly driven by a motor, an elevator and an aileron are arranged at the rear part of the empennage, a rudder is arranged at the rear part of the vertical fin, and the elevator, the aileron and the rudder are controlled by a flight control system and are mutually independent. The ground-effect aircraft provided by the invention adopts a box-type wing structure formed by combining the sweepback main wing and the sweepforward empennage, has better aerodynamic performance in a take-off and climbing low-speed flight state, and can provide larger lift force and better maneuvering characteristics.
本发明公开了一种分布式电推进盒式翼地效飞行器,包括主机身,主机身两侧连接后掠翼主翼一端,主机身尾部上方的两尾翼一端通过垂尾连接主机身,另一端分别通过端板连接两主翼另一端,尾翼上连接若干由电机直接驱动的高置涵道风扇,尾翼的后部设置升降舵和副翼,垂尾的后部设置方向舵,所述的升降舵、副翼和方向舵由飞行控制系统进行控制且升降舵、副翼和方向舵互相独立。本发明提供的地效飞行器采用后掠式主翼加前掠式尾翼组合的盒式翼构型,在起飞和爬升低速飞行状态下具有更好的气动性能,能够提供更大的升力和更好的机动性能。
Distributed electric propulsion box type wing ground effect aircraft
一种分布式电推进盒式翼地效飞行器
2025-02-07
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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