Fibre-reinforced components

Patent metadata

Field	Value
Publication number	US-11214025-B2
Application number	US-201515524921-A
Country	US
Kind code	B2
Filing date	Nov 9, 2015
Priority date	Nov 7, 2014
Publication date	Jan 4, 2022
Grant date	Jan 4, 2022

Abstract

A method for forming a composite component, comprising: locating a rigid composite element comprising a matrix interspersed with long fibre reinforcement in a mould that is shaped to define a cavity about the rigid element; loading a material comprising a matrix precursor interspersed with short fibre reinforcement into the cavity; and curing the matrix precursor.

First claim

The invention claimed is:

1. A method for forming a composite component, comprising:
locating a rigid composite element comprising a matrix interspersed with long fibre reinforcement in a mould that is shaped to define a cavity about the rigid element;
loading a material comprising a matrix precursor interspersed with short fibre reinforcement into the cavity; and
curing the matrix precursor;
wherein a first part of the mould is shaped to fit to the contours of the rigid composite element and a second part of the mould is shaped to define the cavity around part of the rigid composite element, the rigid composite element comprising at least one projection integrally formed with the rigid composite element; and
wherein the step of locating comprises locating the at least one projection at an edge of the cavity of the second part of the mould, where the mould is shaped to fit against the contours of the surfaces of the at least one projection facing away from the cavity such that the mould seals against the at least one projection to substantially inhibit flow of the matrix precursor out of the cavity.

2. A method as claimed in claim 1 , wherein a first part of the mould is shaped to fit to the contours of the rigid element and a second part of the mould is shaped to define the cavity around the rigid element, and the step of locating comprises closing the mould against the rigid element without substantially altering the shape of the rigid element.

3. A method as claimed in claim 1 , wherein the rigid element is hollow in the region adjacent to the cavity.

4. A method as claimed in claim 1 , wherein the method comprises, prior to the loading step, heating the mould to a temperature at which the matrix of the rigid element will soften.

5. A method as claimed in claim 4 , wherein the temperature to which the mould is heated is between the glass transition temperature of the matrix of the rigid element and 20° C. above that temperature.

6. A method as claimed in claim 4 , wherein the rigid element is hollow in the region adjacent the cavity, and wherein the step of closing the mould comprises indenting the mould into the surface of the rigid element so as to seal the cavity.

7. A method as claimed in claim 1 , wherein the mould comprises a first part of the mould and a second part of the mould, the first part of the mould comprising a mould body and at least one mould slider moveable between an extended position and a retracted position relative to the mould body, and the step of locating comprises closing the mould against the rigid element by: bringing the at least one mould slider, in the extended position, into contact with a second part of the mould, closing the first part of the mould and the second part of the mould around the rigid composite element so that the mould slider moves between the extended position and the retracted position.

8. A method as claimed in claim 7 , wherein the step of bringing the at least one mould slider into contact with a second part of the mould comprises securing the rigid composite element in the second part of the mould by the at least one mould slider.

9. A method as claimed in claim 1 , wherein the projection extends away from the exterior surface of the rigid composite element.

10. A method as claimed in claim 1 , wherein the method comprises, heating the said material to a temperature at which the matrix of the rigid element will soften.

11. A method as claimed in claim 10 , wherein the temperature to which the said material is heated is between the glass transition temperature of the matrix of the rigid element and 20° C. above that temperature.

12. A method as claimed in claim 10 , wherein the method comprises heating the said material to the said temperature after loading it into the cavity.

13. A method as claimed in claim 10 , wherein the method comprises heating the said material to the said temperature before loading it into the cavity.

14. A method as claimed in claim 1 , wherein the long fibre reinforcement comprises fibres longer than 50 cm.

15. A method as claimed in claim 1 , wherein the said material comprises fibres shorter than 10 cm.

16. A method as claimed in claim 1 , wherein the said material comprises no fibres longer than 10 cm.

17. A method as claimed in claim 1 , comprising the step of forming the rigid composite element by resin transfer moulding.

18. A method as claimed in claim 1 , wherein the rigid composite element is a tub for a vehicle.

19. A method as claimed in claim 18 , wherein the cavity is adjacent to a portion of the tub forming part of a crash structure.

20. A method as claimed in claim 19 , wherein the material injected into the cavity defines a structural feature of the crash structure.

21. A method as claimed in claim 18 , wherein the cavity is adjacent to an A-pillar of the tub.

22. A method as claimed in claim 21 , wherein the material injected into the cavity defines a feature running lengthwise along the A-pillar.

23. A method as claimed in claim 22 , wherein the feature is one of a flange for carrying a door seal and a flange for bonding glass to.

24. A method as claimed in claim 1 , comprising, prior to the step of loading, coating at least a part of the surface of the rigid element with an adhesive, wherein that part of the surface is overlain by the cavity.

25. A method as claimed in claim 24 , wherein the adhesive is applied as a peelable film.

Assignees

• Mclaren Automotive Ltd

Inventors

• Meeks Graham
• Santoni Claudio

Classifications

• B29C70/76 Primary

  Moulding on edges or extremities of the preformed part · CPC title

• B62D29/046

  Combined superstructure and frame, i.e. monocoque constructions · CPC title

• B29C70/081

  Combinations of fibres of continuous or substantial length and short fibres · CPC title

• B29C70/86 Primary

  Incorporated in coherent impregnated reinforcing layers, {e.g. by winding} · CPC title

• B29C43/18

  incorporating preformed parts or layers, e.g. compression moulding around inserts or for coating articles {(B29C43/206 takes precedence)} · CPC title