| 摘要 |
The invention relates to a method for production of fibre composite compo nents (10), particularly suitable for the production of profiles of complica ted 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, wit h the following steps: (a) production of several core components (12), (b) s eparate application of a first fibre material (16) to each of the core compo nents (12), (c) assembling the core components (12) provided with the first fibre material (16) to form a sequence of core components (18), (d) applicat ion of a second fibre material (20) common to the core component sequence (1 8) along at least one side of the core component sequence (18), provided wit h the first fibre material (16), (e) impregnating and hardening the first an d second fibre materials (16, 20) to form a fibre-reinforced component body and (f) separation of the component body into several sections as represente d by the fibre composite components (10). |
