Method for manufacturing a structural element of a wind turbine blade, method for manufacturing a wind turbine blade, structural element of a wind turbine blade and wind turbine blade

Patent metadata

Field	Value
Publication number	US-12078143-B2
Application number	US-202017764255-A
Country	US
Kind code	B2
Filing date	Sep 30, 2020
Priority date	Oct 9, 2019
Publication date	Sep 3, 2024
Grant date	Sep 3, 2024

Abstract

A method for manufacturing a structural element of a wind turbine blade including forming of at least one injection hole in at least one laminate provided on a top side of a core material of a first portion and a second portion of the structural element and a bottom side of a core material of the first portion and the second portion, so that the at least one injection hole is fluidically connected to the cavity. Further, injecting adhesive through the injection hole into the cavity, curing the adhesive injected into the cavity and thereby forming a joint between an end of the core material of the first portion and an end of the core material of the second portion. Further, a method for manufacturing a wind turbine blade and the structural element, the wind turbine blade is also provided.

First claim

The invention claimed is:

1. A method for manufacturing a structural element of a wind turbine blade, the method comprising:
(a) providing a first portion of the structural element and a second portion of the structural element, whereby each of the first portion and the second portion comprise a core material;
(b) arranging an end of the core material of the first portion to face an end of the core material of the second portion, whereby a gap is formed between the end of the core material of the first portion and the end of the core material of the second portion;
(c) providing laminates on top sides of the core materials of the first portion and the second portion and on bottom sides of the core materials of the first portion and the second portion, whereby a cavity enclosing the gap is formed between the end of the core material of the first portion, the end of the core material of the second portion and at least two of the laminates;
(d) forming at least one injection hole in at least one of the laminates, so that the at least one injection hole is fluidically connected to the cavity;
(e) injecting adhesive through the at least one injection hole into the cavity, curing the adhesive injected into the cavity and thereby forming a structural joint between the end of the core material of the first portion and the end of the core material of the second portion; and
(f) arranging at least one intermediate piece connecting the end of the core material of the first portion with the end of the core material of the second portion, wherein the at least one intermediate piece comprises spacers on a surface, whereby the spacers create space for the cavity between the intermediate piece and the end of the core material of the first portion and between the intermediate piece and the end of the core material of the second portion.

2. The method according to claim 1 , wherein the joint is a scarf joint or a butt joint.

3. The method according to claim 1 , wherein at least one of the laminates is tapered at an end to form a lip.

4. The method according to claim 1 , wherein at least one of the laminates extends beyond the end of the core material on which the at least one of the laminates is provided.

5. The method according to claim 1 , wherein during the injection of the adhesive, an adhesive stopper is provided adjacent to the laminate provided on the bottom side of the core material of the first portion and the laminate provided on the bottom side of the core material of the second portion.

6. The method according to claim 1 , wherein the step of providing the laminates includes
overlaminating a laminate on the laminates provided on the top sides of the core materials of the first portion and the second portion, so that the overlaminated laminate connects the laminates provided on the top sides of the core materials of the first portion and the second portion with each other, and/or
overlaminating a laminate on the laminates provided on the bottom sides of the core materials of the first portion and the second portion, so that the overlaminated laminate connects the laminates provided on the bottom sides of the core materials of the first portion and the second portion with each other.

7. The method according to claim 1 , wherein the at least one intermediate piece is tapered at ends, and that the end of the core material of the first portion and the end of the core material of the second portion are tapered correspondingly to the ends of the intermediate piece for fitting therewith.

8. The method according to claim 1 , wherein two separate intermediate pieces are being arranged to connect the end of the core material of the first portion with the end of the core material of the second portion.

9. The method according to claim 1 , wherein the first portion and the second portion are shell portions, spar web portions and/or spar cap portions.

10. A method for manufacturing a wind turbine blade, whereby the method comprises the method for manufacturing a structural element of the wind turbine blade according to claim 1 , by means of which at least two of a shell, a spar web and a spar cap of the wind turbine blade are manufactured and joined together using overlamination and/or adhesive injection.

11. A structural element of a wind turbine blade manufactured by means of the method according to claim 1 , whereby the structural element is a shell, a spar web or a spar cap.

12. A wind turbine blade comprising at least one structural element according to claim 11 .

13. A method for manufacturing a structural element of a wind turbine blade, the method comprising:
(g) providing a first portion of the structural element and a second portion of the structural element, whereby each of the first portion and the second portion comprise a core material;
(h) arranging an end of the core material of the first portion to face an end of the core material of the second portion, whereby a gap is formed between the end of the core material of the first portion and the end of the core material of the second portion;
(i) providing laminates on top sides of the core materials of the first portion and the second portion and on bottom sides of the core materials of the first portion and the second portion, whereby a cavity enclosing the gap is formed between the end of the core material of the first portion, the end of the core material of the second portion and at least two of the laminates;
(j) forming at least one injection hole in at least one of the laminates, so that the at least one injection hole is fluidically connected to the cavity;
(k) injecting adhesive through the at least one injection hole into the cavity, curing the adhesive injected into the cavity and thereby forming a structural joint between the end of the core material of the first portion and the end of the core material of the second portion; and
arranging at least one intermediate piece connecting the end of the core material of the first portion with the end of the core material of the second portion, wherein the at least one intermediate piece comprises spacers on a surface, wherein ends of the at least one intermediate piece are being fitted into corresponding recesses of the end of the core material of the first portion and the end of the core material of the second portion.

14. The method according to claim 13 , wherein the joint is a scarf joint or a but joint.

15. The method according to claim 13 , wherein at least one of the laminates is tapered at an end to form a lip.

16. The method according to claim 13 , wherein at least one of the laminates extends beyond the end of the core material on which the at least one of the laminates is provided.

17. The method according to claim 13 , wherein during the injection of the adhesive, an adhesive stopper is provided adjacent to the laminate provided on the bottom side of the core material of the first portion and the laminate provided on the bottom side of the core material of the second portion.

18. The method according to claim 13 , wherein the step of providing the laminates includes
overlaminating a laminate on the laminates provided on the top sides of the core materials of the first portion and the second portion, so that the overlaminated laminate connects the laminates provided on the top sides of the core materials of the first portion and the second portion with each other, and/or
overlaminating a laminate on the laminates provided on the bottom sides of the core materials of the first portion and the second portion, so that the overlaminated laminate

Assignees

• Siemens Gamesa Renewable Energy As

Inventors

• Buchbjerg Bjarke
• Chiesura Gabriele

Classifications

• F05B2230/23

  by permanently joining parts together · CPC title

• B29L2031/085

  Wind turbine blades · CPC title

• B29K2105/0097

  Glues or adhesives, e.g. hot melts or thermofusible adhesives · CPC title

• B29C65/542 Primary

  by injection · CPC title

• Y02P70/50

  Manufacturing or production processes characterised by the final manufactured product · CPC title