Method of producing a continuous fibre reinforcement layer from individual fibre mats

Patent metadata

Field	Value
Publication number	US-10513810-B2
Application number	US-201415318398-A
Country	US
Kind code	B2
Filing date	Jun 16, 2014
Priority date	Jun 16, 2014
Publication date	Dec 24, 2019
Grant date	Dec 24, 2019

Abstract

A method of producing a single assembled longitudinally extending fibre layer for use in a later resin infusion process for manufacturing a fibre-reinforced composite structure is described including steps: a) providing a first fibre mat comprising unidirectional reinforcement fibres oriented in a longitudinal direction of the first fibre mat, b) providing a second fibre mat comprising unidirectional reinforcement fibres oriented in a longitudinal direction of the second fibre mat, c) arranging the first fibre mat and the second fibre mat so that unidirectional fibres of one end of the first fibre mat adjoin one end of the second fibre mat in a single plane at a common boundary, and d) splicing unidirectional fibres of the first fibre mat at one end of the first fibre mat to unidirectional fibres of the second fibre mat at one end of the second fibre mat in order to form a splicing joint.

First claim

The invention claimed is:

1. A method of manufacturing a wind turbine blade part producing a single assembled longitudinally extending fibre layer for use in a later resin infusion process, the method comprising the following steps:
a) providing a first fibre mat comprising unidirectional reinforcement fibres oriented in a longitudinal direction of the first fibre mat between two ends;
b) providing a second fibre mat comprising unidirectional reinforcement fibres oriented in a longitudinal direction of the second fibre mat between two ends;
c) arranging the first fibre mat and the second fibre mat so that unidirectional fibres of one end of the first fibre mat adjoin one end of the second fibre mat in a single plane at a common boundary; and
d) splicing unidirectional fibres of the first fibre mat at said one end of the first fibre mat to unidirectional fibres of the second fibre mat at said one end of the second fibre mat in order to form a splicing joint, the first fibre mat and the second fibre mat forming a spliced mat, the spliced mat consisting of a single layer of longitudinally extending fibres.

2. The method according to claim 1 , wherein said one end of the first fibre layer and said one end of the second fibre layer are cut taperingly, and wherein said fibre layers in step c) are arranged so that the common boundary forms a tapering transition between unidirectional fibres of the first fibre mat and unidirectional fibres of the second fibre mat in the longitudinal direction of the single continuous, longitudinally extending fibre layer.

3. The method according to claim 2 , wherein the tapering transition has a thickness-to-length ratio between 1:50 and 1:5.

4. The method according to claim 1 , wherein step d) comprises the use of an adhesive for providing said splicing.

5. The method according to claim 4 , wherein the adhesive is powder based.

6. The method according to claim 1 , wherein the splicing joint is heated.

7. The method according to claim 1 , wherein step d) comprises the step of stitching the first fibre mat and the second fibre mat together for providing said splicing.

8. The method according to claim 1 , wherein further unidirectional fibres of the first fibre mat are pressed against unidirectional fibres of the second fibre mat in order to form a frictional connection between said unidirectional fibres.

9. The method according to claim 1 , wherein step d) comprises the use of rollers for pressing the unidirectional fibres of the first mat and the second fibre mat against each other.

10. The method according to claim 1 , wherein unidirectional fibres at said one ends of the first fibre mat and the second fibre mat are unstitched at a longitudinal zone at said one ends prior to step d).

11. The method according to claim 1 , wherein unidirectional fibres at said one ends of the first fibre mat and the second fibre mat are aligned in the longitudinal direction via alignment means.

12. A method of manufacturing a wind turbine blade part, comprising the steps of:
laying up fibre layers in a mould, wherein at least one of the fibre layers is produced according to the method of claim 1 ;
supplying a resin to said fibre layers; and
forming the fibre layers into a composite structure.

13. The method of manufacturing a wind turbine blade part according to claim 12 , wherein the layup of the fibre layers involves stacking a plurality of the fibre layers, and wherein said at least one fibre layer is sandwiched between two fibre layers which do not have a splicing joint at the splicing joint of said at least one fibre layer.

14. The method of manufacturing a wind turbine blade part according to claim 12 , wherein the wind turbine blade part is a load carrying structure.

15. The method of manufacturing a wind turbine blade part according to claim 12 , wherein the step of forming the fibre layers into the composite structure comprises formation selected from the group consisting of hardening and curing.

16. The method of manufacturing a wind turbine blade part according to claim 12 , wherein the wind turbine blade part comprises a blade shell part.

17. The method according to claim 3 , wherein the thickness-to-length ratio is approximately 1:30.

18. The method according to claim 6 , wherein the splicing joint is ironed.

19. The method according to claim 11 , wherein the alignment means comprise a comb.

Assignees

• Lm Wp Patent Holding As

Inventors

• Ramachandran Dhinagaran
• Thadathazhath Shalu
• Madurai Sathiyagopi
• Sushil Rohin
• Aithal Rajesh
• Priyadarshini B Hannah
• Basha Mohammad Imdad
• Lundsgaard-Larsen Christian
• Østergaard Rasmus C
• Jacobsen Torben Krogsdal

Classifications

• F03D1/0675

  of the blades · CPC title

• B29C65/72

  by combined operations {or combined techniques}, e.g. welding and stitching · CPC title

• D04H3/04 Primary

  in rectilinear paths, e.g. crossing at right angles · CPC title

• B29D99/0025

  Producing blades or the like, e.g. blades for turbines, propellers, or wings · CPC title

• F05B2230/60

  Assembly methods · CPC title