The invention belongs to the technical field of aviation aircrafts, and particularly relates to a vertical and horizontal dual-purpose aircraft based on tilting power. The vertical take-off and landing aircraft comprises a fuselage, two main wings, two front canards, a vertical empennage, N tilting ducted fans, an embedded lift ducted fan and an undercarriage. The vertical take-off and landing aircraft adopts a canard layout and a lift/thrust/control integrated power system, can realize the state conversion from vertical flight to horizontal flight, can take off and land in a smaller space, and is flexible to deploy. The power is separated from the wings, the canard layout is adopted, the aspect ratio can be effectively increased, the lift-drag ratio can be improved, and compared with a common vertical take-off and landing aircraft, the aircraft has the advantages of being high in voyage and low in energy consumption and has huge development prospects in the fields of aerial reconnaissance, surveying and mapping, monitoring and the like.
本发明属于航空飞行器技术领域,具体为一种基于倾转动力的垂平两用飞行器。该垂直起降飞机包括机身、两个主机翼、两个前置鸭翼、垂直尾翼、N个倾转涵道风扇、嵌入式升力涵道风扇和起落架。该垂直起降飞行器采用鸭翼布局和升/推/控一体化动力系统,可实现由垂直飞行到水平飞行的状态转换,可在较小的空间进行起降,部署灵活。动力与机翼分离且采用鸭翼布局,可有效增大展弦比提高升阻比,相比常见的垂直起降飞行器具有高航程和低能耗的优势,在空中侦察,测绘以及监视等领域有着巨大的发展前景。
Vertical and horizontal dual-purpose aircraft based on tilting power
一种基于倾转动力的垂平两用飞行器
2022-07-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
Aircraft saddle and self-tilting vertical take-off and landing aircraft
European Patent Office | 2022
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