The invention discloses a wing deformation mechanism for a water-air cross-medium ornithopter. The wing deformation mechanism comprises a fuselage; the first front swing rod is rotationally connected to the front side of the machine body, and the first front swing rod can swing up and down relative to the machine body; the flapping wing driving mechanism is arranged on the fuselage and used for driving the first front swing rod to swing up and down; the first side of the airfoil is connected with the fuselage, and the second side of the airfoil is rotationally connected with the first front swing rod; the deformation driving mechanism is used for driving the wing surface to rotate backwards relative to the first front swing rod and driving the wing surface to deform; by applying the mechanism, the flight performance of the aircraft under different working conditions can be improved.
本发明公开了一种用于水空跨介质扑翼飞行器的机翼变形机构,包括:机身;第一前摆杆,转动连接于机身的前侧,第一前摆杆能够相对于机身上下摆动;扑翼驱动机构,设置在机身上,扑翼驱动机构用于驱动第一前摆杆上下摆动;翼面,翼面的第一侧连接机身,翼面的第二侧转动连接第一前摆杆;变形驱动机构,用于驱动翼面相对于第一前摆杆向后转动并驱动翼面变形;应用上述机构能够提高飞行器在不同工况下飞行的性能。
Wing deformation mechanism for water-air cross-medium ornithopter
一种用于水空跨介质扑翼飞行器的机翼变形机构
2022-11-01
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |