Wind turbine blades and method of manufacturing the same

Patent metadata

Field	Value
Publication number	US-10105913-B2
Application number	US-201314646219-A
Country	US
Kind code	B2
Filing date	Nov 18, 2013
Priority date	Nov 20, 2012
Publication date	Oct 23, 2018
Grant date	Oct 23, 2018

Abstract

Method of making a spar cap includes: providing a plurality of composite strips, each strip being of constant cross section defined by first and second sides and edges, the first and second sides comprising first and second abutment surfaces, the strip being of uniform thickness between the abutment surfaces, a first edge region of the strip comprising a first edge being of relatively reduced thickness, the first side of the strip comprising an edge surface, and the strip having a peel ply layer at least partially covering the first abutment surface and the edge surface; removing the peel ply layers; stacking the strips such that the first abutment surface abuts an abutment surface of an adjacent strip to define an interface region, such that a clearance region is defined; supplying resin to the respective clearance regions and causing the resin to infiltrate into the interface regions; and curing the resin.

First claim

The invention claimed is:

1. A method of making a spar cap for a wind turbine blade, the method comprising:
(a) providing a plurality of elongated pultruded fibrous composite strips, each strip being of essentially constant cross section taken transverse to a longitudinal axis of the strip and defined by first and second mutually opposed and longitudinally extending sides and by first and second longitudinal edges, the first and second sides comprising, respectively, first and second substantially planar abutment surfaces, a separation between the first and second sides defining a thickness of the strip, the strip being of essentially uniform thickness between the first and second abutment surfaces, a first edge region of the strip comprising a first edge of the strip being of relatively reduced thickness compared to a thickness of the strip between the first and second abutment surfaces, the first side of the strip comprising a first edge surface adjacent the first abutment surface in the first edge region of the strip, and the strip having a first peel ply layer at least partially covering the first abutment surface and at least partially covering the first edge surface;
(b) removing the first peel ply layers from the plurality of strips;
(c) stacking the strips in a mould such that the first abutment surface of each strip faces an abutment surface of an adjacent strip in the stack to define an interface region between the strips, and such that a clearance region is defined between the first edge region of each strip and an edge region of an adjacent strip in the stack;
(d) supplying resin to the plurality of clearance regions and causing the resin to infiltrate into the interface regions between adjacent strips from the plurality of clearance regions; and
(e) curing the resin to bond the strips together.

2. The method of claim 1 , wherein the first abutment surface of each of the plurality of strips abuts an abutment surface of an adjacent strip in the stack to define the interface region between the strips.

3. The method of claim 1 , wherein an interlayer is disposed in the interface region between the first abutment surface of each strip and the abutment surface of the adjacent strip in the stack.

4. The method of claim 1 , wherein each of the plurality of strips is of tapering thickness in the first edge region, such that when the strips are stacked in step (c), the clearance region becomes progressively narrower moving from the first edge towards the interface region.

5. The method of claim 1 , wherein the first edge surface is inclined relative to the first abutment surface.

6. The method of claim 1 , wherein the first edge is a longitudinal edge of the strip.

7. The method of claim 1 , wherein each strip has a second edge region of relatively reduced thickness, the second edge region comprising the second edge of the strip, and step (c) of the method comprises stacking the strips in the mould such that a clearance region is defined between the second edge region of each strip and an edge region of an adjacent strip in the stack.

8. The method of claim 7 , wherein the first side of each strip comprises a second edge surface between the second edge and the first abutment surface, the second edge surface being inclined relative to the first abutment surface, and the first peel ply layer at least partially covers the second edge surface, and step (b) of the method comprises removing the first peel ply layer from the second edge surface.

9. The method of claim 1 , wherein the second abutment surface of each strip is at least partially covered by a second peel ply layer, and step (b) of the method comprises removing the second peel ply layers from the respective strips to expose fibres on the respective second abutment surfaces; and step (c) of the method comprises stacking the strips in the mould such that the second abutment surface of each strip faces an abutment surface of an adjacent strip in the stack to define an interface region between the strips.

10. The method of claim 1 , further comprising, prior to step (a), forming the strips by a pultrusion process comprising drawing a bundle of resin-coated fibres and the first peel ply layer through a pultrusion die having a cross section corresponding to the cross section of at least one of the plurality of strips taken transverse to a longitudinal axis thereof.

11. The method of claim 1 , wherein step (c) comprises stacking the strips in a wind turbine blade mould.

12. The method of claim 1 , wherein the first side of the strip comprises an outwardly extending step adjacent the first edge surface in the first edge region of the strip, wherein the first edge surface is arranged between the step and the first abutment surface.

13. The method of claim 12 , wherein the step has a height that is essentially equal to a thickness of the first peel ply layer.

14. The method of claim 12 , wherein the step is essentially orthogonal to the first edge surface.

15. The method of claim 1 , wherein step (c) of the method comprises stacking the strips in the mould such that all of the strips stacked in the mould are aligned with each other.

Assignees

• Vestas Wind Sys As

Inventors

• Sandercock Stephen

Classifications

• Y10T29/49339

  Hollow blade · CPC title

• Y02E10/721

  Cross-Sectional Technologies · mapped topic

• B29C70/547

  using channels or porous distribution layers incorporated in or associated with the product · CPC title

• B29D99/0028

  hollow blades · CPC title

• B29C65/70

  by moulding (using a particular moulding technique, see the relevant technique {, e.g. by injection B29C45/14467}) · CPC title