Method of making a root end joint of a wind turbine blade and a root segment for such a joint

Patent metadata

Field	Value
Publication number	US-9897066-B2
Application number	US-201414261224-A
Country	US
Kind code	B2
Filing date	Apr 24, 2014
Priority date	Oct 25, 2011
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

A method of making a root end joint for a wind turbine. A plurality of root segments ( 10 ) are formed of a composite material. Each has an arcuate end face ( 11 ) which subtends an angle of 90° or less and has a plurality of connection holes ( 12 ). The segments are joined together side-by-side to build up the circular profile of the root end. The segments include a proportion of uni-axial to multiaxial fiber which decreases from the arcuate end face towards the opposite end.

First claim

What is claimed is:

1. A method of making a root end joint of a wind turbine blade, the method comprising:
forming a plurality of root segments of a composite material, each root segment being generally the shape of a segment of a hollow cylinder having at least one arcuate end face subtending an angle of 90° or less with a plurality of connection holes, an opposite end, and a pair of side faces extending axially from the arcuate end face to the opposite end;
arranging a plurality of the root segments side-by-side into a root tool, wherein the root segments include uniaxial and multi-axial fibers, wherein the relative proportion of uni-axial to multi-axial fiber decreases from the arcuate end face towards the opposite end, and wherein each root segment comprises a fixed length between the arcuate end face and the opposite end;
aligning the connection holes of the arranged root segments with through holes of an alignment frame that abuts against the root tool;
securing the arranged root segments to the alignment frame via a plurality of bolts positioned through the aligned connection holes and through holes;
laying up a plurality of laminate layers atop the fixed lengths of each root segment; and
securing the laminate layers and the root segments together so as to form the root end joint.

2. A method according to claim 1 , wherein adjacent side faces of adjacent root segments have a complementary keying configuration.

3. A method according to claim 1 , wherein a thickness of the fixed lengths of the root segments tapers from the arcuate end face towards the opposite end.

4. A method according to claim 1 , wherein the root segments are joined together to form a substantially semi-circular configuration.

5. A method according to claim 1 , further comprising drilling the connection holes after the root segments are formed.

6. A method according to claim 1 , further comprising forming the connection holes as the root segments are formed.

7. A method according to claim 6 , wherein the step of forming the connection holes is achieved by forming the root segments with inserts having female screw threads in situ.

8. A method according to claim 6 , comprising the steps of inserting disposable inserts into the root segment during the forming step and removing the disposable inserts to form the connection holes.

9. A method according to claim 3 , further comprising laying up the plurality of laminate layers atop the tapering fixed lengths of each root segment until a thickness of the root end joint is uniform.

10. A method according to claim 1 , wherein securing the laminate layers and the root segments together so as to form the root end joint further comprises infusing the laminate layers and the root segments together via at least one resin material.

11. A method according to claim 1 , wherein securing the laminate layers and the root segments together so as to form the root end joint further comprises curing the laminate layers and the root segments together.

Assignees

• Blade Dynamics Ltd

Inventors

• Hayden Paul Trevor
• Broome Peter Anthony

Classifications

• B29D99/0028

  hollow blades · CPC title

• F05B2230/50

  Building or constructing in particular ways · CPC title

• F03D3/064

  Fixing wind engaging parts to rest of rotor · CPC title

• B29C70/865

  completely encapsulated · CPC title

• Y10T29/49336

  Blade making · CPC title