The invention relates to the technical field of aircrafts, in particular to a four-duct tilting layout aircraft. The aircraft comprises an aircraft body, and a front tilting duct power device and a tail tilting duct power device are arranged on the front portion and the tail portion of the aircraft body respectively. The front tilting duct power device and the tail tilting duct power device are switched between a horizontal advancing position and a vertical lifting position; wings are arranged on the fuselage, supporting rods parallel to the length direction of the fuselage are fixedly arranged on the wings, and empennages are arranged at the rear ends of the supporting rods. Through the combination of the tilting duct power devices on the supporting rod power assemblies, the actions of vertical take-off and landing, level flight and the like of the aircraft can be achieved, the space needed by take-off of the aircraft can be greatly reduced, and the overall resistance borne in the level flight process is reduced. Through the aircraft structure provided by the invention, the control stability and flight performance of the aircraft are greatly improved, and the use flexibility of the aircraft is improved.
本发明涉及飞行器技术领域,具体涉及一种四涵道倾转布局的飞行器,包括机身,机身前部和尾部分别设置有前部倾转涵道动力装置和尾部倾转涵道动力装置,所述的前部倾转涵道动力装置与尾部倾转涵道动力装置均在水平前进位置和垂直提升位置两个位置之间切换;机身上设置机翼,机翼上固定设置有平行于机身长度方向的撑杆,撑杆的后端设置有尾翼。本发明通过撑杆动力组件上的倾转涵道动力装置的组合,能够实现飞行器的垂直起降,平飞等动作,不仅能够大大的减小飞行器起飞所需的空间,还减小了平飞过程中受到的整体阻力。通过本发明提供的飞行器结构,大大地提高了飞行器的操控平稳性和飞行性能,提高了飞行器的使用灵活度。
Four-duct tilting layout aircraft
一种四涵道倾转布局的飞行器
2021-06-04
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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