A method for fabricating a composite wing structural component for an aircraft is described. The method comprises extruding a filler material into each mold channel of a plurality of mold channels of a die to form a plurality of filler segments, removing the plurality of filler segments from the plurality of mold channels of the die, and arranging the plurality of filler segments in a space in the composite structural component, the space being defined by a radius of the composite structural component, such that the filler segments are in end-to-end contact. The method further comprises curing the plurality of filler segments in the space to fuse the plurality of filler segments.
Aircraft comprising composite structural component, and method for forming composite structural component
Patent
Electronic Resource
European Patent Office | 2021
|European Patent Office | 2023
|European Patent Office | 2023
|European Patent Office | 2021
|European Patent Office | 2021
|