The invention relates to the technical field of aircrafts, in particular to a composite wing vertical take-off and landing aircraft which comprises an aircraft body, a front wing and an empennage. Propeller mounting frames are arranged on the front wings on the two sides of the fuselage, and each propeller mounting frame comprises a middle rod, an inner rod and an outer rod; lift propeller mechanisms are mounted on the middle rod, the inner rod and the outer rod; the propeller mounting frames are arranged on the front wings on the two sides of the fuselage, so that a plurality of lift propeller mechanisms are convenient to mount, and the aircraft can be transported in a heavy load manner; the propeller mounting frame is provided with a middle rod connected with the front wing and the rear empennage respectively, and an inner rod and an outer rod are distributed on the two sides of the middle rod, so that the aircraft is good in flying stability, meanwhile, the stress of the front wing is reduced, the stress is relatively balanced, and the service life is prolonged.
本发明涉及飞行器技术领域,尤其是指一种复合翼垂直起降飞行器,包括机身、前机翼及尾翼;所述机身两侧的前机翼上均设置有螺旋桨安装架,所述螺旋桨安装架包括中杆、内杆和外杆;所述中杆、内杆和外杆上均安装有升力螺旋桨机构;本发明采用在机身两侧前机翼上设置螺旋桨安装架,便于安装多个升力螺旋桨机构,使得飞行器能够大载重运输;所述螺旋桨安装架设置有分别与前机翼和后尾翼连接中杆,并且在中杆的两侧分布有内杆和外杆,使得飞行器飞行时平稳性好,同时减小了前机翼受力且受力较为均衡,提高使用的寿命。
Composite wing vertical take-off and landing aircraft
一种复合翼垂直起降飞行器
2023-08-08
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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