US Patent 11878794 Aircraft wing trailing edge section assembly

An aircraft wing trailing edge section assembly is disclosed having an upper skin structure providing an upper external aerodynamic trailing edge surface, a lower skin structure providing a lower external aerodynamic trailing edge surface, and a movement mechanism including a first portion attached to an internal surface of the upper skin structure, a second portion attached to an internal surface of the lower skin structure, and a rotationally mounted connector member connected between the first and second portions, such that rotational movement of the connector member causes simultaneous movement of both first and second portions and therefore both upper and lower skin structures, such that the camber of the trailing edge section is changed. An aircraft wing section assembly, an aircraft and methods of operating an aircraft are disclosed.