Patent ID: 8088236

Claim:
Method for producing a large-area fibre-composite structural component, in particular for the aircraft sector, comprising: providing of a predetermined shaping element; advance rolling up of a fibrous sheet to be laid on two fibrous sheet rolls, which are received by means of a controllable laying device; defined laying of the fibrous sheet over or onto the predetermined shaping element by adjusting the two fibrous sheet rolls both in the vertical direction and in the transverse direction by means of the controllable laying device having four synchronously controllable lifting columns which are arranged in pairs around the shaping element for adjusting the fibrous sheet rolls in the vertical direction, each pair of lifting columns being respectively assigned a vertically adjustable cross member, wherein in each cross member there are respectively integrated two receiving carriages for receiving the fibrous sheet rolls that can be displaced synchronously along the respective cross member for adjusting the fibrous sheet rolls in the transverse direction, and guiding the two fibrous sheet rolls uniformly and synchronously from the centre of the predetermined shaping element to the edge of the same by means of the controllable laying device; turning of the predetermined shaping element and the controllable laying device in relation to each other by a predetermined turning angle by means of a controllable turning device; and defined laying of a further fibrous sheet on top of the already laid fibrous sheet by means of the controllable laying device.