Method for producing composite elements and composite element
View Patent ↗A method is proposed for producing composite elements which have at least one core and cover layers containing two fibres, with the following steps: coating of open-pored, semi-finished products comprising fibre materials with fine-grained, pulverulent, cross-linking resin, in such a manner that the open porosity remains, forming of an arrangement of at least one open-pored core and two coated semi-finished products in a forming tool which is heated to the cross-linking temperature of the pulverulent resin.
1. A composite element having at least one core and cover layers containing two fibers in a sandwich layer, wherein the core comprises an open-pored material and the cover layers comprise fiber materials provided with a coating and present in the form of semi-finished products, the coating having reactive resin, which is a powder matrix of cross-linking ethylene-propylene copolymers, unsaturated polyesters and/or polyurethanes and cetyl-methylcellulose, vinylacetate dispersions, PVA solutions, starch or polysaccharides as a thickening agent.
2. A composite element according to claim 1 , wherein the semi-finished product is formed as one of: a glass fiber mat, glass fiber layering, continuous or staple fiber glass fiber mat, synthetic fiber mat made of PET, PA or the like with a melting point of higher than 160° C., as a natural fiber mat made of jute, hemp, sisal, flax, kenaf, cotton or as metal fiber knitted material or mat.
3. A composite element according to claim 1 , wherein the core comprises an open-pored material which cannot melt at a temperature up to 200° C.
4. A composite element according to claim 3 , wherein the core has embedded mineral fibers, MF foam and/or silicate fibers.
5. A composite element according to claim 1 , wherein a plurality of open-pored cores is provided with different materials and properties with respective interposition of a coated semi-finished product.
6. A composite element according to claim 1 , wherein it has a relative airflow resistance of 150-450 kNs/m 4 .
7. A composite element according to claim 3 , wherein the core comprises a foamed or fiber material, or honeycomb structure produced from beamed or unsaturated paper or perforated aluminum, or knitted materials produced by textile techniques.
8. A composite element according to claim 5 , wherein the cover layers have different flow resistances.