IP Library › Granted Patent US 11,969,959
Granted Patent B2
US 11,969,959 · App. 17/312,766 · Granted Apr 30, 2024

Methods for manufacturing blade components for wind turbine rotor blades

Inventor: Andrew Mitchell Rodwell (Greenville, SC)
Assignee: GE Infrastructure Technology LLC
B29C70/42B29C59/14F03D1/0675B29L2031/085F05B2230/50F05B2280/6003F05B2280/6015
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Quick Facts
Patent No.
US 11,969,959
App. No.
17/312,766
Granted
Apr 30, 2024
Kind
B2
Abstract

A method of manufacturing a blade component of rotor blade of a wind turbine includes providing a plurality of pultrusions constructed of one or more fibers or fiber bundles cured together via a resin material. The method also includes placing a protective cap over at least one end of one or more of the plurality of pultrusions. Further, the method includes heat treating a surface of the plurality of pultrusions while the protective cap remains over the at least one end. Moreover, the method includes removing the protective cap from the at least one end. The method further includes arranging the plurality of pultrusions in a mold of the blade component. In addition, the method includes infusing the plurality of pultrusions together so as to form the rotor blade component.

Claims (33)

1. A method of manufacturing a blade component of rotor blade of a wind turbine, the method comprising:

providing a plurality of pultrusions constructed of one or more fibers or fiber bundles cured together via a resin material;

placing a protective cap over at least one end of one or more of the plurality of pultrusions, the protective cap conforming to a shape of the at least one end;

heat treating a surface of the plurality of pultrusions while the protective cap remains over the at least one end;

removing the protective cap from the at least one end;

arranging the plurality of pultrusions in a mold of the blade component; and,

infusing the plurality of pultrusions together so as to form the rotor blade component.

2. The method of claim 1 , wherein the at least one end of one or more of the plurality of pultrusions is tapered, the protective cap being placed over the at least one tapered end.

3. The method of claim 1 , wherein heat treating the surface of the plurality of pultrusions further comprises plasma treating the surface of the plurality of pultrusions.

4. The method of claim 1 , wherein the protective cap is constructed of a metal material.

5. The method of claim 1 , wherein the protective cap is placed over each end of the one or more plurality of pultrusions.

6. The method of claim 1 , wherein the protective cap comprises a substantially V-shaped cross-section.

7. The method of claim 1 , wherein the blade component comprises at least one of a spar cap, a shear web, or a root ring.

8. The method of claim 1 , wherein the fibers or fiber bundles comprise at least one of glass fibers, carbon fibers, polymer fibers, wood fibers, bamboo fibers, ceramic fibers, nanofibers, metal fibers.

9. The method of claim 1 , wherein the at least one resin material further comprises at least one of a thermoset material or a thermoplastic material.

10. The method of claim 1 , further comprising arranging the tapered pultrusions in the mold of the rotor blade component such that tapered ends of the plurality of pultrusions extend in a substantially span-wise direction when installed on the rotor blade of the wind turbine.

11. The method of claim 10 , wherein the at least one resin material further comprises at least one of a thermoset material or a thermoplastic material.

12. The method of claim 1 , wherein the protective cap is placed over each end of the one or more plurality of pultrusions.

13. A method of forming a pultrusion for use in manufacturing a blade component of rotor blade of a wind turbine, the method comprising:

forming the pultrusion of one or more fibers or fiber bundles cured together via a resin material;

placing a protective cap over at least one end of the pultrusion, the protective cap conforming to a shape of the at least one end;

heat treating a surface of the pultrusion while the protective cap remains over the at least one end; and,

removing the protective cap from the at least one end.

14. The method of claim 13 , further comprising tapering the at least one end of pultrusion and placing the protective cap over the at least one tapered end.

15. The method of claim 13 , wherein heat treating the surface of the plurality of pultrusions further comprises plasma treating the surface of the plurality of pultrusions.

16. The method of claim 13 , wherein the blade component comprises at least one of a spar cap, a shear web, or a root ring.

17. The method of claim 13 , wherein the protective cap is constructed of a metal material.

18. The method of claim 13 , wherein the protective cap comprises a substantially V-shaped cross-section.

19. The method of claim 13 , wherein the fibers or fiber bundles comprise at least one of glass fibers, carbon fibers, polymer fibers, wood fibers, bamboo fibers, ceramic fibers, nanofibers, metal fibers.

20. A method of controlling a plasma heat treating process for forming a pultrusion for use in manufacturing a blade component of rotor blade of a wind turbine, the method comprising:

providing the pultrusion of one or more fibers or fiber bundles cured together via a resin material;

placing a protective cap over at least one end of the pultrusion, the protective cap conforming to a shape of the at least one end; and,

applying a plasma treating process to at least one surface of the pultrusion while simultaneously blocking heat to the at least one end of the pultrusion with the protective cap during the plasma treating process, the at least one end of the pultrusion defining a cross-sectional thickness that is less than an overall cross-sectional thickness of the pultrusion.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 17, 2023
From: GENERAL ELECTRIC COMPANY
To: GE INFRASTRUCTURE TECHNOLOGY LLC
Reel/Frame 065727/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 10, 2021
From: RODWELL, ANDREW MITCHELL
To: GENERAL ELECTRIC COMPANY
Reel/Frame 056502/0860 →
Continuity (1)
Related Publication 20220055319A1 · Feb 24, 2022
Cited By (1)
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