Abstract: A method for production of fiber composite components, particularly suitable for the production of profiles of complicated shape with varying profile cross-section and/or with at least parts with curved lines, such as used for the production of aircraft, for example. The method (a) produces plural core components, (b) separates application of a first fiber material to each of the core components, (c) assembles the core components provided with the first fiber material to form a sequence of core components, (d) applies a second fiber material common to the core component sequence along at least one side of the core component sequence, provided with the first fiber material, (e) impregnates and hardens the first and second fiber materials to form a fiber-reinforced component body, and (f) separates the component body into plural sections as represented by the fiber composite components.

Abstract: A fiber composite component is at least partially produced by braiding. It comprises a core element which has at least one concavely constructed face that is adjoined by a passage opening. Respective opposite transverse or longitudinal sides of the core element and the side of the passage opening not bounded by the core element are enclosed by a braided fiber composite loop element.

Abstract: A fiber composite component is at least partially produced by braiding. It comprises a core element which has at least one concavely constructed face that is adjoined by a passage opening. Respective opposite transverse or longitudinal sides of the core element and the side of the passage opening not bounded by the core element are enclosed by a braided fiber composite loop element.

Abstract: A method for production of fiber composite components, particularly suitable for the production of profiles of complicated shape with varying profile cross-section and/or with at least parts with curved lines, such as used for the production of aircraft, for example. The method (a) produces plural core components, (b) separates application of a first fiber material to each of the core components, (c) assembles the core components provided with the first fiber material to form a sequence of core components, (d) applies a second fiber material common to the core component sequence along at least one side of the core component sequence, provided with the first fiber material, (e) impregnates and hardens the first and second fiber materials to form a fiber-reinforced component body, and (f) separates the component body into plural sections as represented by the fiber composite components.

Abstract: A fiber composite component is at least partially produced by braiding. It comprises a core element which has at least one concavely constructed face that is adjoined by a passage opening. Respective opposite transverse or longitudinal sides of the core element and the side of the passage opening not bounded by the core element are enclosed by a braided fiber composite loop element.

Abstract: A fiber composite component is at least partially produced by braiding. It comprises a core element which has at least one concavely constructed face that is adjoined by a passage opening. Respective opposite transverse or longitudinal sides of the core element and the side of the passage opening not bounded by the core element are enclosed by a braided fiber composite loop element.

Abstract: A process for repairing a framework (1) composed of profile members, in particular for repairing the body structure of a vehicle in which a damaged subassembly (10) composed of several profile members (11-15) is removed by cutting through the profile members at locations which are still undamaged and replaced by a corresponding replacement subassembly (10E). For flush fitting of the replacement subassembly against the free ends of the cut profile members of the framework (1), a fitting case (20) is slidably inserted into the end of the respective profile members of the replacement subassembly or of the profile members of the framework. After positioning the replacement assembly the fitting cases are slidably displaced such that they extend partially into the abutting ends of the profile members. The profile members are then permanently secured to the fitting cases.