Abstract: An apparatus for the forming of a lay-up of fiber composite material, in particular in the aerospace sector is provided. In this case, the apparatus has at least one forming tool, which has a surface contour corresponding to a desired geometry of the lay-up after the forming, and a tool carrier, to which the at least one forming tool is releasably fastened. From a further viewpoint, the invention makes available an apparatus with a modular structure, it then being possible for any desired forming tools to be combined with the tool carrier according to requirements. This leads in particular to less laborious handling, since it obviates the need for handling of the comparatively large tool carrier.

Abstract: The invention relates to a method for producing a fiber composite component, comprising the steps: introduction of a first body (12), consisting of fibers and a matrix material, into a mold (10), said first body (12) having a continuous first body edge (18); the first body (12) is irradiated with microwaves (28) to produce a fiber-composite component. According to the invention, the first body (12) is introduced into the mold (10) in such a way that at least parts of the first body edge (18) are brought into contact with the mold (10).

Abstract: Methods and apparatus for manufacturing an FC parison out of a laminate with at least two prepreg layers provide for: mounting at least a first edge section of the laminate in a first clamping device that can be moved relative to a fitting by means of a mechanical gearing, and a second edge section of the laminate lying opposite the first edge section in another clamping device, exerting a tensile stress via the first clamping device relative to the second clamping device over the area of the laminate lying between the clamping devices, while simultaneously moving the first clamping device in a direction directed away from the second clamping device up to a location where a rounded surface area of a fitting imparts to the laminate a curvature between the first clamping device and second clamping device as viewed in its longitudinal direction.

Abstract: The invention relates to a method for producing a fibre composite component, comprising the steps: introduction of a first body (12), consisting of fibres and a matrix material, into a mould (10), said first body (12) having a continuous first body edge (18); the first body (12) is irradiated with microwaves (28) to produce a fibre-composite component. According to the invention, the first body (12) is introduced into the mould (10) in such a way that at least parts of the first body edge (18) are brought into contact with the mould (10).

Abstract: An apparatus for the forming of a lay-up of fibre composite material, in particular in the aerospace sector is provided. In this case, the apparatus has at least one forming tool, which has a surface contour corresponding to a desired geometry of the lay-up after the forming, and a tool carrier, to which the at least one forming tool is releasably fastened. From a further viewpoint, the invention makes available an apparatus with a modular structure, it then being possible for any desired forming tools to be combined with the tool carrier according to requirements. This leads in particular to less laborious handling, since it obviates the need for handling of the comparatively large tool carrier.