Drive mechanism, drive system, aerodynamic surface and aircraft

The present invention provides a drive mechanism, a drive system, and an aerodynamic structure for an aircraft, each comprising at least one articulated module comprising four links, where each link comprises three coupling points distributed to form a triangular geometry, where each coupling point comprises a first coupling point and a second coupling point, where each coupling point comprises a first coupling point and a second coupling point, where each coupling point comprises a first coupling point and a second coupling point. The links are coupled to each other such that articulation with only one degree of freedom is provided. 本发明提供了驱动机构、驱动系统、空气动力学表面和飞行器，驱动机构、驱动系统和用于飞行器的空气动力学结构各自包括包含四个连杆的至少一个铰接式模块，其中，每个连杆包含分布成形成三角形几何形状的三个联接点，其中，连杆彼此联接成使得提供仅具有一个自由度的铰接。