The invention relates to a co-rotating vertical take-off and landing membrane-wing aircraft, in particular to a power spar and membrane-wing co-rotating mechanism of the co-rotating vertical take-off and landing membrane-wing aircraft, which comprises an aircraft body, a control box body, a first power spar mechanism, a membrane-wing mechanism and a second power spar mechanism, the first power spar mechanism, the membrane wing mechanism and the second power spar mechanism are all rotationally connected with the fuselage, a transmission assembly is arranged on the control box body, and a connecting assembly is in transmission connection with one end of the transmission assembly, the first power spar mechanism, the membrane wing mechanism, the second power spar mechanism and the other end of the transmission assembly. The power spar and membrane wing co-rotation mechanism realizes single control and synchronous co-rotation, so that an engine and a membrane wing are always in an optimal cooperative state, the operation and control are simple, the association that a taxiing take-off and landing aircraft adopts a fixed wing and a vertical take-off and landing aircraft adopts a propeller wing is broken, and the aircraft can take off and land like a helicopter and climb and cruise like a fixed wing aircraft, and slides down like a power glider.
本发明涉及一种共转垂直起降膜翼飞机,尤其涉及一种共转垂直起降膜翼飞机的动力翼梁、膜翼共转机构,包括机身、控制箱体、第一动力翼梁机构、膜翼机构、第二动力翼梁机构,第一动力翼梁机构、膜翼机构和第二动力翼梁机构均与机身转动连接,所述控制箱体上设置有传动组件,所述传动组件的一端、第一动力翼梁机构、膜翼机构、第二动力翼梁机构和所述传动组件的另一端之间传动连接有连接组件。本发明的动力翼梁、膜翼共转机构实现了单一控制、同步共转,使发动机与膜翼永远处在最佳协同状态、操控简单,打破了滑跑起降飞机采用固定翼,垂直起降飞机采用旋桨翼的关联,可做到像直升机一样起降,像固定翼飞机一样爬升和巡航,像动力滑翔机一样滑降。
Power spar and membrane wing co-rotating mechanism of co-rotating vertical take-off and landing membrane wing aircraft
共转垂直起降膜翼飞机的动力翼梁、膜翼共转机构
03.09.2021
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Co-rotating vertical take-off and landing membrane wing aircraft
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