System and method for producing composite component

1. A system for continuous production of a composite component, comprising:

a feeding device for feeding a plurality of layers of reinforcing material from a material supply as elongate strip or sheet along a process path;

two cover layer applicators for applying two film or foil layers to cover both sides of the reinforcing material as the reinforcing material is fed or conveyed along the process path;

a resin application device comprising the two cover layer applicators and a nozzle for applying a resin to the reinforcing material fed along the process path in liquid form to provide a resin matrix;

a forming device configured to shape or mould a profile of the reinforcing material and the resin matrix to form the composite component as the reinforcing material is fed along the process path; and

one or more vacuum port for generating an under-pressure between the two film or foil layers as the reinforcing material is fed or conveyed along the process path so that the layers are pressed by external pressure into contact with the resin over the reinforcing material,

wherein the reinforcing material and the resin matrix are supported between and covered by the two film or foil layers and the resin is injected into contact with the reinforcing material via the nozzle.

2. The system according to claim 1 , wherein the forming device is configured to form and to at least partially cure the resin matrix to produce the composite component.

3. The system according to claim 1 , wherein the feeding device is configured to feed the plurality of layers of reinforcing material as an elongate strip or sheet in a longitudinal direction along the process path, wherein the forming device is configured to shape or mould a cross-sectional profile of the composite component transverse to the longitudinal direction, wherein the forming device includes a rotary frame having at least one form or mould on a periphery thereof in or upon which a cross-sectional profile of the component is shaped or moulded.

4. The system according to claim 3 , wherein the rotary frame comprises a plurality of forms or moulds arranged around the circumference thereof, and wherein the plurality of forms or moulds are separately detachable from the rotary frame.

5. The system according to claim 1 , wherein the resin application device is configured to apply the resin at or adjacent to the forming device, whereby the resin is applied immediately upstream of a point at which the reinforcing material contacts the forming device on at least one film or foil.

6. The system according to claim 5 , wherein the resin is applied between two film layers.

7. The system according to claim 1 , wherein the resin application device is configured to apply the resin to the reinforcing material upstream of the forming device.

8. A method for continuous production of a composite component, for an aircraft or spacecraft, comprising:

feeding a plurality of layers of reinforcing material from a material supply as elongate strip or sheet along a process path;

applying film or foil layers to two sides of the reinforcing material as the reinforcing material is fed or conveyed along the process path;

infusing a polymer resin into the reinforcing material fed or conveyed along the process path to provide a resin matrix;

forming or shaping a profile of the reinforcing material and resin matrix infused thereto to form a composite component as the reinforcing material is fed or conveyed along the process path;

applying the polymer resin to the reinforcing material fed along the process path between a pair of film or foil layers; and

applying a vacuum to a space between the pair of film or foil layers as the reinforcing material is fed or conveyed along the process path to press the polymer resin into the reinforcing material,

wherein the resin is applied between the film or foil layers as a liquid via a nozzle.

9. The method according to claim 8 , further comprising:

at least partially curing the resin matrix to produce the composite component, wherein the curing is performed or carried out during and/or directly following the forming or shaping.

10. The method according to claim 9 , comprising fully curing the resin matrix to produce the composite component.

11. The method according to claim 8 , wherein the forming or shaping includes pressing the layers of reinforcing material and the resin matrix into a form or mould by any one or more of an inflatable pressure member or vacuum-assisted pressure application or at least one roller member.