| 摘要 |
A method for producing a fiber composite component, in particular for aerospace, the method comprising the following steps: forming a mold core from a material comprising cork by a molding tool to establish an outer geometry of said mold core; arranging the so formed mold core adjacent to an at least partly hardened stiffening element on a base element of said composite component to be produced for the shaping of at least one molded portion of said fiber composite component to be produced; and multistage exposure of at least said molded portion to heat and/or pressure to produce said fiber composite component; a corresponding mold core and a corresponding fiber composite component. |
