Segmented wind turbine rotor blade with welded joint

Patent metadata

Field	Value
Publication number	US-10605227-B2
Application number	US-201715485359-A
Country	US
Kind code	B2
Filing date	Apr 12, 2017
Priority date	Apr 12, 2017
Publication date	Mar 31, 2020
Grant date	Mar 31, 2020

Abstract

The present disclosure is directed to a rotor blade assembly for a wind turbine having a first rotor blade segment with a first spar cap segment and a second rotor blade segment with a second spar cap segment. The first and second spar cap segments are arranged together at an interface and are constructed of a composite material. Further, the rotor blade assembly includes a joint assembly at the interface of the first and second spar cap segments. The joint assembly is constructed of a first metal joint secured to the first spar cap segment and a second metal joint secured to second spar cap segment. Moreover, the first and second metal joints are welded together at a weld area.

First claim

What is claimed is:

1. A method for joining rotor blade segments of a rotor blade of a wind turbine, the method comprising:
forming first and second rotor blade segments having first and second spar cap segments, respectively, the first and second spar cap segments being constructed of a composite material;
forming the first and second rotor blade segments with first and second shear web segments, respectively, the first and second shear web segments comprising first and second interlocking ends, respectively;
securing first and second metal joints to the first and second spar cap segments of the first and second rotor blade segments, respectively;
arranging the first and second interlocking ends together;
arranging the first and second metal joints together at an interface;
welding the first and second metal joints together; and
welding the first and second interlocking ends concurrently with the first and second metal joints of the first and second spar cap segments.

2. The method of claim 1 , wherein the composite material of the first and second spar cap segments comprises one or more pultrusions, the method further comprising forming at least one of beveled ends or stepped ends into the one or more pultrusions of the first and second spar cap segments at the interface.

3. The method of claim 1 , further comprising staggering ends of the one or more pultrusions of the first and second spar cap segments at the interface.

4. The method of claim 1 , wherein the first and second metal joints each comprises a plurality of metal plates.

5. The method of claim 4 , wherein securing the first and second metal joints to the first and second spar cap segments, respectively, further comprises bonding the plurality of metal plates of each of the first and second metal joints to the one or more pultrusions of the first and second spar cap segments, respectively, via an adhesive.

6. The method of claim 4 , wherein securing the first and second metal joints to the first and second spar cap segments, respectively, further comprises infusing the plurality of metal plates of each of the first and second metal joints to the one or more pultrusions of the first and second spar cap segments, respectively, via a resin material.

7. The method of claim 4 , further comprising:
forming a sloped area into a side of each of the plurality of metal plates; and, placing a filler material within each of the sloped areas of the plurality of metal plates.

8. The method of claim 1 , further comprising providing additional features at the interface to secure the first and second rotor blade segments together in addition to welding, the additional features comprising at least one of placing additional pultrusions or metal components between the first and second metal joints, placing a metallic mesh between the first and second metal joints, or utilizing a joint plate and a plurality of bolts at the interface.

9. A method for joining rotor blade segments of a rotor blade of a wind turbine, the method comprising: forming first and second rotor blade segments of a composite material; forming the first and second rotor blade segments with first and second shear web segments, respectively, the first and second shear web segments comprising first and second interlocking ends, respectively; securing first and second metal joints to the first and second rotor blade segments, respectively; arranging the first and second interlocking ends together; aligning the first and second metal joints together at an interface; and, welding the first and second metal joints together; and welding the first and second interlocking ends concurrently with the first and second metal joints of the first and second rotor blade segments.

10. The method of claim 9 , wherein securing the first and second metal joints to the first and second rotor blade segments, respectively, further comprises bonding the first and second metal joints to the first and second rotor blade segments via at least one of an adhesive or a resin material.

11. The method of claim 9 , wherein aligning the first and second metal joints together at the interface further comprises aligning corresponding interlocking components of the first and second metal joints together before welding.

12. The method of claim 9 , wherein the interface is located away from at least one of a spar cap or a shear web of the rotor blade.

Assignees

• Gen Electric

Inventors

• Johnson Stephen Bertram
• Chen Xu
• Walker Alan M

Classifications

• B29C66/73941

  characterised by the materials of both parts being thermosets · CPC title

• B29C65/48

  using adhesives {, i.e. using supplementary joining material; solvent bonding} · CPC title

• B29C66/54

  Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles · CPC title

• B29C66/12463

  being tapered · CPC title

• F03D1/0675 Primary

  of the blades · CPC title