Component for aircraft, has reinforcement arranged in edge area such that edge area exhibits larger wall thickness than wall area, where wall area is attached to side that is turned away from component edge at edge area

摘要

The component has a wall area (110) comprising an edge area (120) and a component edge (130), and a reinforcement (121) arranged in the edge area such that the edge area exhibits larger wall thickness than the wall area. The wall area is attached to a side that is turned away from the component edge at the edge area. The wall area includes a fiber-reinforced plastic area (113), and the edge area is provided with an elongated cylindrical element (115) in an area of the reinforcement, where the cylindrical element extends up to the component edge. An independent claim is also included for a connecting system comprising a recess.