The invention discloses a wing body fusion layout aircraft which comprises a traditional propulsion system and an auxiliary electric propulsion system, the auxiliary electric propulsion system comprises a first auxiliary electric propulsion system and a second auxiliary electric propulsion system which are independently controlled and symmetrically arranged in the outer side or the inner side of the traditional propulsion system, and the traditional propulsion system comprises two basic engines. Each of the first auxiliary electric propulsion system and the second auxiliary electric propulsionsystem comprises a motor using electric power as a power source, a controller controlling the motor, a generator set supplying power to the motor, and an auxiliary thrust generator connected with themotor and driven by the motor. According to the wing body fusion layout aircraft disclosed by the invention, when the single engine of the basic engine fails, the differential high-speed propeller fan or ducted fan can be used for providing additional yaw control for the aircraft, so that the problem of insufficient yaw moment of the wing body fusion layout aircraft due to vertical fin layout limitation is solved; and the characteristics of energy conservation and emission reduction are achieved, and dependence on a traditional propelling system can be reduced.
本发明公开了一种翼身融合布局飞机,该飞机包括传统推进系统和辅助电推进系统,辅助电推进系统包括彼此独立控制且对称布置于传统推进系统外侧或内侧的第一和第二辅助电推进系统,传统推进系统包括两台基础发动机,第一和第二辅助电推进系统分别包括:使用电力作为动力源的电动机、控制电动机的控制器、为电动机供电的发电机组、与电动机连接并由电动机驱动的辅助推力产生器。根据本发明的翼身融合布局飞机,当基础发动机单发失效时,能够利用差动的高速桨扇或涵道风扇为飞机提供额外的偏航控制,从而解决翼身融合布局飞机由于垂尾布局限制而导致的偏航力矩不足的问题;并且具有节能减排的特征,可减少对传统推进系统的依赖。
Wing body fusion layout aircraft
一种翼身融合布局飞机
2021-02-26
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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