Hollow composite products and method for making same
View Patent ↗The invention concerns a hollow composite product comprising over 20% glass in the form of long fibres, the thickness of the product walls further ranging between 1 and 10 mm about. The invention also concerns a method for making said product, which consists in inserting in a mould ( 10 ) a preheated assembly ( 9 ) comprising in its core at least an inflatable pocket covered with at least a composite structure, the composite structure including at least a filler material in the form of long fibres and the preheated assembly including a material capable of creeping, and in inflating the inflatable pocket under pressure higher than 40 bars.
1. A method for manufacturing a hollow composite product, comprising:
forming a preheated liner;
forming a preheated composite structure, the composite structure comprising at least one reinforcing substance in a form of fibers of at least 1 mm in length and at least one material configured to flow;
combining the preheated composite structure and the preheated liner to form a preheated assembly;
placing the preheated assembly in a mold; and
inflating the liner to a pressure in excess of 40 bar so that the preheated assembly adopts a shape of the mold to produce a product.
2. A method according to claim 1 , wherein the liner is inflated using a gas, the gas being removed after the product produced has solidified and before the mold is opened.
3. A method according to claim 1 , wherein the liner remains incorporated with the composite structure in the product produced after solidification.
4. A method according to claim 1 , wherein the liner is made of a material of a same kind as the at least one material configured to flow of the composite structure.
5. A method according to claim 1 , wherein the composite structure is formed of at least one array of criss-crossed yarns.
6. A method according to claim 1 , wherein the composite structure comprises reinforcing filaments or yarns at least one of intermingled with and inserted among filaments or yarns made of organic substance.
7. A method according to claim 1 , wherein the composite structure comprises at least one organic thermoplastic substance or thermoset.
8. A method according to claim 1 , wherein the liner is in a form of a tube around which the composite structure is wrapped after the liner tube and the composite structure have been heated, to obtain the preheated assembly.
9. A method for manufacturing a hollow composite product, comprising:
forming a preheated assembly, the preheated assembly comprising (a) a liner film and (b) a composite structure comprising at least one reinforcing substance in a form of fibers of at least 1 mm in length and at least one material configured to flow;
rolling up the preheated assembly so that the liner film is on an inside of the rolled-up structure;
placing the preheated assembly in a mold; and
inflating the liner to a pressure in excess of 40 bar so that the preheated assembly adopts a shape of the mold to produce a product.
10. A method according to claim 9 , wherein the liner is inflated using a gas, the gas being removed after the product produced has solidified and before the mold is opened.
11. A method according to claim 9 , wherein the liner remains incorporated with the composite structure in the product produced after solidification.
12. A method according to claim 9 , wherein the liner is made of a material of a same kind as the at least one material configured to flow of the composite structure.
13. A method according to claim 9 , wherein the composite structure is formed of at least one array of criss-crossed yarns.
14. A method according to claim 9 , wherein the composite structure comprises reinforcing filaments or yarns at least one of intermingled with and inserted among filaments or yarns made of organic substance.
15. A method according to claim 9 , wherein the composite structure comprises at least one organic thermoplastic substance or thermoset.
16. A method for manufacturing a hollow composite product, comprising:
forming first and second preheated assemblies, each preheated assembly comprising (a) a liner film and (b) a composite structure comprising at least one reinforcing substance in a form of fibers of at least 1 mm in length and at least one material configured to flow;
combining the first and second preheated assemblies such that the respective liner films thereof face each other to form a final preheated assembly;
placing the final preheated assembly in a mold; and
inflating the liner to a pressure in excess of 40 bar so that the final preheated assembly adopts a shape of the mold to produce a product.
17. A method according to claim 16 , wherein the liner is inflated using a gas, the gas being removed after the product produced has solidified and before the mold is opened.
18. A method according to claim 16 , wherein the liner remains incorporated with the composite structures in the product produced after solidification.
19. A method according to claim 16 , wherein the liner is made of a material of a same kind as the at least one material configured to flow of the composite structures.
20. A method according to claim 16 , wherein the composite structures are formed of at least one array of crisscrossed yarns.
21. A method according to claim 16 , wherein the composite structures comprise reinforcing filaments or yarns at least one of intermingled with and inserted among filaments or yarns made of organic substance.
22. A method according to claim 16 , wherein the composite structures comprise at least one organic thermoplastic substance or thermoset.