METHOD FOR PRODUCING A FIBRE COMPOSITE COMPONENT FIBRE COMPOSITE COMPONENT AND A FIBRE COMPOSITE FUSELAGE COMPONENT OF AN AIRCRAFT

摘要

The invention relates to a method for producing a fibre composite component (1) with a skinning field (2) and a primary component (8) for reinforcing the fibre composite component (1), comprising the steps: application of a pre-preg (4) to a tool form to form the skinning field (2), wherein fibres, corresponding to an assumed force flow path in the skinning field (2) of the component (1) for production, run partly non-linearly in the pre-preg (4), curing the pre-preg (4), application of layers of a textile semi-finished product (10) to the cured pre-preg (4) to form the primary component (8), impregnating the textile semi-finished product (10) with matrix material and curing the assembly of pre-cured pre-preg (4) and textile semi-finished product (10). The invention further relates to a fibre composite component comprising at least one support component and a skin section having a recess and a fibre composite fuselage section with a shell piece having at least one recess and support component built in the form of a frame piece.