| 摘要 |
The present invention provides an apparatus and a method for producing a lar ge- area fibre-composite structural component, in particular for the aircraft sector, comprising a predetermined shaping element (1) , a controllable layi ng device (4, 5, 6) for the defined laying of at least one fibrous sheet (15) over or into the predetermined shaping element (1) , a controllable turning device (10) for a defined turning of the predetermined shaping element (1) a nd of the laying device (4, 5, 6} in relation to each other by a predetermined turning angle, and a central control device, which is connected to the layin g device (4, 5, 6) and the turning device (10) for controlling of the same.</S DOAB> |
