The invention relates to the technical field of unmanned aerial vehicles, in particular to a hybrid power tilt rotor unmanned aerial vehicle comprising a fuselage, an empennage and two wings which are arranged on the fuselage, wherein a ducted fan is arranged at the lower part of the front end of the fuselage; each wing comprises an inner wing section and a tilting outer wing section, one end of each inner wing section is fixedly connected with the fuselage, the other end of each inner wing section is rotatably connected with the tilting outer wing section, and the empennage is of a V-shaped structure. The ducted fan is installed on the front lower portion of the fuselage, a lifting force can be provided, and the longitudinal balancing characteristic of the unmanned aerial vehicle can be remarkably improved; the unmanned aerial vehicle can take off and land vertically, can take off and land without being limited by a site, can cruise at a high speed during long endurance, and meets the requirements of surveying and mapping, patrol, transportation, police and the like.
本发明涉及无人飞行器技术领域,特别涉及一种混合动力倾转旋翼无人飞行器。包括机身及设置于机身上的尾翼和两个机翼,其中机身的前端下部设有涵道风扇;机翼包括内翼段和倾转外翼段,内翼段的一端与机身固定连接,另一端与倾转外翼段转动连接,尾翼为V型结构。本发明的机身前下部装有涵道风扇,可提供升力,并且能显著的提升飞行器的纵向配平特性;该飞行器可垂直起降,不受限于场地即可起飞降落,同时可长航时高速巡航,满足测绘、巡逻、运输、警用等需求。
Hybrid power tilt rotor unmanned aerial vehicle
一种混合动力倾转旋翼无人飞行器
2022-02-18
Patent
Electronic Resource
Chinese
CONTROL METHOD OF TILT ROTOR UNMANNED AERIAL VEHICLE, AND TILT ROTOR UNMANNED AERIAL VEHICLE
European Patent Office | 2021
|