A tilting folding wing mechanism is composed of a fuselage, a tilting mechanism and a folding mechanism. The tilting mechanism is composed of a translation device, a limiting device and a driving device, and through combined movement of the translation device, the limiting device and the driving device, the wing spar can translate relative to the fuselage while tilting. The folding mechanism is composed of an inner-section wing, a folding device and an outer-section wing, the outer-section wing can be folded relative to the inner-section wing around a shaft parallel to the chord line of the wing through the combined movement of the inner-section wing, and the wing can be turned over towards the rear side of the fuselage in cooperation with the movement of the tilting mechanism. According to the tilting folding wing mechanism, through reasonable matching and connection, the tilting wing unmanned aerial vehicle can have static stability when flying in a fixed wing state, and the space occupied by the tilting wing unmanned aerial vehicle when the tilting wing unmanned aerial vehicle is parked on the ground is reduced.
一种倾转折叠翼机构,由机身、倾转机构、折叠机构组成。所述的倾转机构由平移装置、限位装置、驱动装置组成,通过它们的组合运动,可实现翼梁在倾转的同时相对机身平移。所述的折叠机构由内段机翼、折叠装置、外段机翼组成,通过它们的组合运动,外段机翼可绕平行于机翼弦线的轴相对内段机翼折叠,配合倾转机构的运动,可实现机翼向机身后侧翻折。本发明的倾转折叠翼机构通过合理的配合与连接,可使倾转翼无人机在固定翼状态飞行时具备静稳定性,并降低倾转翼无人机在地面停放时所占用的空间。
Tilting folding wing mechanism
一种倾转折叠翼机构
2023-07-25
Patent
Electronic Resource
Chinese
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