초록 ▼

Composite tubes may be fabricated by filament winding a layer of resin impregnated carbon fiber with a near-axial fiber orientation over a mandrel and over end-fittings. Bands of resin-impregnated fibers are then wound circumferentially around this near-axial layer in a position that coincides with

Composite tubes may be fabricated by filament winding a layer of resin impregnated carbon fiber with a near-axial fiber orientation over a mandrel and over end-fittings. Bands of resin-impregnated fibers are then wound circumferentially around this near-axial layer in a position that coincides with a circumferential groove in the underlying end-fittings. The ends of the near-axial layer are folded back over the bands, resulting in a double layer of intact near-axial fibers locked into the groove on the end-fittings by the bands of intact circumferential fibers. Testing has shown this arrangement to be effective for introducing very high axial loads onto the composite tube.

대표청구항 ▼

1. A method of forming a join in a composite tube between an end-fitting and a composite material, including: i. forming a layer of composite material having a tubular structure extending over at least part of an end-fitting, fibers of the layer reversing direction on a ring;ii. forming a band aroun

1. A method of forming a join in a composite tube between an end-fitting and a composite material, including: i. forming a layer of composite material having a tubular structure extending over at least part of an end-fitting, fibers of the layer reversing direction on a ring;ii. forming a band around the end-fitting and the layer of composite material;iii. folding the layer of composite material back over the band by moving the ring relative to the end-fitting; andiv. cutting the layer free from the ring. 2. A method as claimed in claim 1 wherein the layer of composite material is an axial or near-axial layer. 3. A method as claimed in claim 1 wherein the band is formed from a composite material. 4. A method as claimed in claim 1 wherein step ii) includes forming the band around a peripheral surface feature so as to press the layer of composite material into or against the surface feature. 5. A method as claimed in claim 4 wherein the peripheral surface feature is a peripheral groove. 6. A method as claimed in claim 4 wherein the peripheral surface feature is a peripheral shoulder. 7. A method as claimed in claim 1 including: v. mounting an end-fitting, a mandrel and the ring in fixed relation to each other; andvi. carrying out step i) by winding fibers impregnated with resin over the mandrel and end-fitting, and around the pins in the ring. 8. A method as claimed in claim 1, wherein the layer of composite material is formed by laying or winding fibers impregnated with resin over a mandrel and the end-fitting. 9. A method as claimed in claim 1, wherein the layer of composite material is formed by laying fibers over a mandrel and the end-fitting and subsequently impregnating the fibers with resin. 10. A method as claimed in claim 1, including forming a further layer of composite material having a tubular structure extending over at least part of an end-fitting; forming a further band around the end-fitting and the further layer of composite material; andfolding the further layer of composite material back over the further band. 11. A method as claimed in claim 10 wherein the further band is formed around a further peripheral surface feature so as to press the layer of composite material into or against the further surface feature. 12. A method of forming a composite tube, including forming a first join at a first end of a tube between a first end-fitting and a composite material, and forming a second join at a second end of the tube between a second end-fitting and the composite material, each join being formed by the method of claim 1. 13. A method as claimed in claim 12 wherein step iii) is performed in respect of each join such that the ends of the composite layer meet or overlap at a point along the length of the tube. 14. A method as claimed in claim 1 including forming a further layer of composite material over the outside of the tube. 15. A method as claimed in claim 4 wherein the peripheral surface feature is a protrusion.