Wind turbine blade

Patent metadata

Field	Value
Publication number	US-12546285-B2
Application number	US-202017923719-A
Country	US
Kind code	B2
Filing date	May 8, 2020
Priority date	May 8, 2020
Publication date	Feb 10, 2026
Grant date	Feb 10, 2026

Abstract

A method of manufacturing a wind turbine blade, comprising the steps of:
placing one or more shell fibre layers on a mould surface of a blade mould, placing a plurality of separately provided preforms directly on the one or more shell fibre layers in a stacked arrangement, infusing and curing the stacked preform arrangement, the one or more shell fibre layers together via a resin in mould cavity of the blade mould to form a wind turbine blade part with a spar cap integrated in a shell part providing part of the aerodynamic shape of the wind turbine blade.

First claim

The invention claimed is:

1 . A method of manufacturing a wind turbine blade extending along a longitudinal direction from a blade root through a root region and an airfoil region to a tip region with a blade tip, the wind turbine blade having a profiled contour including a pressure side, a suction side and a chord line extending between a leading edge and a trailing edge, the wind turbine blade comprising a shell providing an aerodynamic shape of the wind turbine blade and a spar cap forming a load carrying structure of the wind turbine blade, the method comprising the steps of:
providing a blade mould for a wind turbine blade part having a mould cavity with a mould surface; placing one or more shell fibre layers and optionally an exterior coat on the blade mould surface; placing a plurality of separately provided preforms directly on the one or more shell fibre layers in a stacked arrangement, wherein each of the preforms comprises a mixture of fibre material and a binding agent, wherein the fibre material of each preform is at least partially joined together by means of the binding agent; infusing the stacked preform arrangement, the one or more shell fibre layers and, optionally the exterior coat, with a resin in mould cavity of the blade mould, each of the preforms plastically conforming to the mould surface during the infusing; and curing the stacked preform arrangement, the one or more shell fibre layers and, optionally the exterior coat, together via the resin to form a wind turbine blade part with a spar cap integrated in a shell part providing part of the aerodynamic shape of the wind turbine blade.

2 . The method according to claim 1 , wherein the stacked preform arrangement, the one or more shell fibre layers and, optionally the exterior coat, are infused in a vacuum pressure environment, optionally in a vacuum-assisted resin transfer moulding process.

3 . The method according to claim 1 , wherein the stacked preform arrangement comprises:
two or more of the preforms in a chordwise direction ; two or more of the preforms in a thickness direction; and two or more of the preforms in a spanwise direction.

4 . The method according to claim 3 , wherein the plurality of preforms are arranged in a staggered manner or an offset manner in the stacked preform arrangement.

5 . The method according to claim 1 , wherein a core insert is placed directly on an exterior shell and adjacent to the stacked preform arrangement in a chordwise direction.

6 . The method according to claim 5 , wherein an end of the stacked preform arrangement facing the leading edge or the trailing edge of the wind turbine blade is beveled and an end of the stacked preform arrangement facing the interior of the wind turbine blade defines an acute angle with a beveled side, wherein the core insert has a beveled side, the method further comprises:
placing the core insert directly on the exterior shell and subsequently placing the plurality of preforms directly on the exterior shell in the stacked arrangement so that, after infusion, the beveled side of the core insert and the beveled side of the stacked preform arrangement form a scarf joint.

7 . The method according to claim 5 , wherein an end of the stacked preform arrangement facing the leading edge or the trailing edge of the wind turbine blade is beveled and an end of the stacked preform arrangement facing the exterior of the wind turbine blade defines an acute angle with the beveled side, wherein the core insert has a beveled side, the method further comprises:
placing the plurality of preforms directly on the exterior shell in the stacked arrangement and subsequently placing the core insert directly on the exterior shell so that, after infusion, the beveled side of the core insert and the beveled side of the stacked preform arrangement form a scarf joint.

8 . A wind turbine blade obtainable by a method according to claim 1 .

9 . The method according to claim 4 , wherein the plurality of preforms are arranged in the staggered manner or the offset manner in the stacked preform arrangement in a plane defined by a thickness direction and a chordwise direction.

10 . A wind turbine blade with a profiled contour including a pressure side and a suction side with a thickness direction extending therebetween, and a leading edge and a trailing edge with a chord having a chordwise direction extending therebetween, the wind turbine blade extending in a spanwise direction between a root end and a tip end, a spar cap extending in the spanwise direction, the chordwise direction, and the thickness direction, the wind turbine blade comprising:
an exterior shell providing the profiled contour of the wind turbine blade and comprising one or more shell fibre layers; and the spar cap being a sandwich-structured composite including one or more inner fibre layers and a core portion sandwiched between the one or more inner fibre layers and the exterior shell, the core portion comprising a plurality of separately provided preforms arranged in a stacked preform arrangement, wherein each of the preforms comprises a mixture of fibre material and a binding agent, wherein the fibre material is at least partially joined together by means of the binding agent, wherein the plurality of preforms and the exterior shell are joined together by means of a resin, wherein each of the preforms plastically conforms to the exterior shell, wherein an end of the stacked preform arrangement facing the leading edge or the trailing edge of the wind turbine blade is beveled and an end of the stacked preform arrangement facing the interior of the wind turbine blade defines an acute angle with a beveled side, wherein the beveled side of the stacked preform arrangement and a beveled side of the core insert form a scarf joint.

11 . The wind turbine blade according to claim 10 , wherein at least two adjacent preforms in a layer of the stacked preform arrangement are joined by a joint.

12 . The wind turbine blade according to claim 10 , wherein the core portion of the spar cap further comprises a core insert arranged directly on the exterior shell and adjacent to the stacked preform arrangement in a chordwise direction, wherein the core insert is of a different material than the preform arrangement.

13 . The wind turbine blade according to claim 11 , wherein the joint comprises a scarf joint or a butt joint.

14 . A wind turbine blade with a profiled contour including a pressure side and a suction side with a thickness direction extending therebetween, and a leading edge and a trailing edge with a chord having a chordwise direction extending therebetween, the wind turbine blade extending in a spanwise direction between a root end and a tip end, a spar cap extending in the spanwise direction, the chordwise direction, and the thickness direction, the wind turbine blade comprising:
an exterior shell providing the profiled contour of the wind turbine blade and comprising one or more shell fibre layers; and the spar cap being a sandwich-structured composite including one or more inner fibre layers and a core portion sandwiched between the one or more inner fibre layers and the exterior shell, the core portion comprising a plurality of separately provided preforms arranged in a stacked preform arrangement, wherein each of the preforms comprises a mixture of fibre material and a binding agent, wherein the fibre material is at least partially joined together by means of the binding agent, wherein the plurality of preforms and the exterior shell are joined together by means of a resin, wherein each of the preforms plastically conforms to the exte

Assignees

• Blade Dynamics Ltd
• Lm Wind Power As

Inventors

• Razeghi Rama
• Hayden Paul Trevor
• Jespersen Klavs
• Lund-Laverick Michael

Classifications

• B29C70/443 Primary

  and impregnating by vacuum or injection · CPC title

• B29C70/30

  Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core · CPC title

• B29C70/682

  Preformed parts characterised by their structure, e.g. form · CPC title

• F03D1/0682

  incorporated into the shell structure · CPC title

• F03D1/065

  characterised by their construction elements (F03D13/10 takes precedence) · CPC title