Actuator-link assembly manufacturing method, actuator-link assembly designing method, and actuator-link assembly

An actuator-link assembly comprising an actuator that can be attached pivotably, at one end thereof, to a control surface of an aircraft or to a horn arm member attached to the control surface in order to drive the control surface, and a link that is coupled to the actuator,

• wherein the link comprises:
• a pair of linear portions disposed alongside each other and each extending linearly;
• a coupling portion connecting to one end of each of the pair of linear portions on the same side via a bent portion and extending so as to couple the one end of each of the pair of linear portions on the same side to each other;
• a fulcrum shaft attachment portion that is provided so as to protrude from a center portion of the coupling portion and that can be attached pivotably to a fulcrum shaft for rotatably supporting the control surface;
• and
• an actuator attachment portion that is provided as the other end of each of the pair of linear portions and that can be attached pivotably to the other end of the actuator via a pivot shaft, and
• a material constituting the pair of linear portions and the coupling portion contains fiber reinforced plastic.