Wind turbine blade manufacture

Patent metadata

Field	Value
Publication number	US-11760041-B2
Application number	US-201917298775-A
Country	US
Kind code	B2
Filing date	Dec 9, 2019
Priority date	Dec 10, 2018
Publication date	Sep 19, 2023
Grant date	Sep 19, 2023

Abstract

A method of forming a wind turbine blade shear web flange section (36) by resin transfer moulding comprises providing a mould assembly (84) comprising a mould surface (86) defining a mould cavity and arranging a plurality of elongate flange elements (46) with the mould surface in an array (80) such that the flange elements are positioned one on top of another with first and second longitudinal ends (56,60) of each flange element longitudinally offset from respective first and second longitudinal ends of a neighbouring flange element so as to form a tapered portion (58,62) at each of a first and second longitudinal end of the flange section (36). A The method further comprises injecting resin to the mould cavity and curing the array of flange elements in a resin matrix to form a cured flange section having a laminate construction.

First claim

The invention claimed is:

1. A method of forming a wind turbine blade shear web flange section by resin transfer moulding (RTM), the method comprising:
providing a mould assembly comprising a mould surface defining a mould cavity;
arranging a plurality of elongate flange elements with the mould surface in an array such that the flange elements are positioned one on top of another with first and second longitudinal ends of each flange element longitudinally offset from respective first and second longitudinal ends of a neighbouring flange element so as to form a tapered portion at each of a first and second longitudinal end of the flange section;
injecting resin to the mould cavity; and
curing the array of flange elements in a resin matrix to form a cured flange section having a laminate construction,
wherein the flange elements are arranged on a first portion of the mould surface so as to form a base of the flange section, and on a second portion of the mould surface, which extends substantially away from the first portion, so as to form an upstand of the flange section extending substantially away from the base of said flange section, and
arranging the plurality of elongate flange elements with the mould surface such that consecutive flange elements in the array are positioned with at least one longitudinal edge offset from a corresponding longitudinal edge of a neighbouring flange element such that the upstand tapers with increasing distance from the base.

2. The method of claim 1 , wherein the flange elements are pre-formed with a substantially L-shaped cross section prior to arranging the flange elements with the mould surface.

3. The method of claim 1 , wherein the flange elements comprise a +/−45 degree biaxial fabric.

4. The method of claim 1 , wherein the mould cavity has a substantially T-shaped profile in cross-section.

5. The method of claim 4 , wherein four or more flange elements are arranged in the array such that at least two flange elements form a first side of the flange section and at least two flange elements form a second side of the flange section resulting in a substantially T-shaped flange section.

6. The method of claim 5 , wherein the flange elements on the second side of the flange section are arranged such that first longitudinal ends of said flange elements are longitudinally offset from corresponding first longitudinal ends of the flange elements on the first side of the flange section.

7. The method according to claim 1 , wherein the base of the flange section tapers with increasing distance from the upstand.

8. The method according to claim 7 , wherein a base of a first flange element arranged with the mould surface extends a lesser distance from the upstand of the flange section compared to a base of a last flange element arranged with the mould surface.

9. The method according to claim 1 , wherein an upstand of a first flange element arranged with the mould surface extends a greater distance from the base of the flange section compared to an upstand of a last flange element arranged with the mould surface.

10. The method according to claim 1 , wherein the tapered portion at the first longitudinal end of the flange section defines an upward facing scarfed surface and the second longitudinal end of the flange section defines a downward facing scarfed surface.

11. The method according to claim 1 , wherein each flange element comprises a base and an upstand, the method further comprising arranging the plurality of elongate flange elements with the mould surface such that the base of each flange element of the array extends a different distance from the upstand of the flange section.

12. The method according to claim 11 , the method further comprising arranging the plurality of elongate flange elements with the mould surface such that the upstand of each flange element of the array extends a different distance from the base of the flange section.

13. A method of manufacturing a wind turbine blade shear web, the method comprising:
arranging an elongate panel;
arranging a plurality of flange sections along a longitudinal edge of the elongate panel, the flange sections being formed according to claim 1 ; and
integrating the plurality of flange sections and the elongate panel to form a wind turbine blade shear web.

14. The method according to claim 13 , wherein the tapered portions of longitudinally adjacent flange sections overlap to define at least one scarf joint between said adjacent flange sections.

Assignees

• Vestas Wind Sys As

Inventors

• Smith Jonathan
• Preston Robert Charles

Classifications

• B29C70/48 Primary

  and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM] {, e.g. by vacuum} · CPC title

• B29L2031/085

  Wind turbine blades · CPC title

• F03D1/0675

  of the blades · CPC title

• B29D99/0028

  hollow blades · CPC title

• Y02E10/72

  Wind turbines with rotation axis in wind direction · CPC title