METHOD FOR REINFORCING A FIBRE COMPOSITE COMPONENT AND ARRANGEMENT FOR PRODUCING A REINFORCED FIBRE COMPOSITE COMPONENT

The invention relates to a method for reinforcing a fiber composite component (1) for aerospace, wherein a reinforcing element (3) having a receiving area (9) and a compression element (4) adapted to the geometry of the receiving area (9) are provided. The compression element (4) is inserted into the receiving area (9) of the reinforcing element (3). The reinforcing element (3) and the inserted compression element (4) are thereby reproducibly affixed to each other by means of a reversible fixator device (5). The reversible fixator device (5) comprises at least one first fixator segment (6) applied to the compression element (4) and at least one second fixator segment (7) that can be applied to the reinforcing element (3). The reinforcing element (3), together with the compression element (4) affixed thereto, is then reproducibly applied to the fiber composite component (1) to be reinforced in order to form a molded segment (8). The molded segment so formed (8) is cured to the fiber composite component (1) in order to bind the reinforcing element (3) thereto. The reversible fixator device (5) and the compression element (4) are then removed from the reinforced fiber composite component (1).