Modular wind turbine rotor blades and methods of assembling same

Patent metadata

Field	Value
Publication number	US-9897065-B2
Application number	US-201514753142-A
Country	US
Kind code	B2
Filing date	Jun 29, 2015
Priority date	Jun 29, 2015
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

The present disclosure is directed to a method for assembling a modular rotor blade of a wind turbine. The method includes providing a pre-formed blade root section and a pre-formed blade tip section of the rotor blade. Further, the blade root section includes one or more spar caps extending in a generally span-wise direction. Another step includes providing at least one pre-formed blade segment of the rotor blade. The method also includes mounting the at least one blade segment around the one or more spar caps of the blade root section, wherein the at least one blade segment includes a chord-wise cross-section having multiple joints, wherein at least one joint is located on at least one of a pressure side surface or a suction side surface. In addition, the method also includes joining the blade tip section to at least one of the one or more spar caps or the at least one blade segment.

First claim

What is claimed is:

1. A method for assembling a modular rotor blade of a wind turbine; the method comprising:
providing a pre-formed blade root section and a pre-formed blade tip section of the rotor blade, at least one of the blade root section or the blade tip section comprising one or more spar caps extending in a generally span-wise direction therefrom, the one or more spar caps being integral with at least one of the blade root section or the blade tip section;
providing a plurality of blade segments of the rotor blade;
arranging the plurality of blade segments with the one or more spar caps of the blade root section between the blade root section and the blade tip section, wherein, when arranged with the one or more spar caps; at least one of the plurality of blade segments comprises a chord-wise cross-section having multiple joints, wherein at least one joint is located on at least one of a pressure side surface or a suction side surface; and,
joining the blade tip section to at least one of the one or more spar caps and one of the plurality of blade segments.

2. The method of claim 1 , further comprising:
securing a pre-formed structural component to the blade root section in a generally span-wise direction, and
mounting the plurality of b segments to the structural component.

3. The method of claim 1 , herein arranging the plurality of blade segments further comprises;
securing the plurality of blade segments to at least one of the blade root section, the blade tip section, the structural component, the one or more spar caps, or adjacent blade segments via at least one of adhesive, welding, or one or more fasteners.

4. The method of claim 1 , further comprising mounting one or more shear webs between the one or more spar caps of the blade root section or the blade tip section before arranging the plurality of blade segments between the blade root section and the blade tip section.

5. The method of claim 1 , wherein the plurality of blade segments further comprise at least one leading edge blade segment and at least one trailing edge blade segment, the method further comprising:
mounting the at least one leading edge blade segment and the at least one trailing edge blade segment between the blade root section and the blade tip section, and
securing the leading edge blade segment and the trailing edge blade segment together at a pressure side seam and a suction side seam.

6. The method of claim 5 , further comprising supporting the blade root section via a main fixture assembly during mounting of the at least one leading edge blade segment and the at least one trailing blade segment between the blade root section and the blade tip section.

7. The method of claim 6 , further comprising supporting the at least one leading and trailing edge blade segments during mounting via a leading edge fixture assembly and a trailing edge fixture assembly, respectively.

8. The method of claim 7 , further comprising:
placing the at least one leading blade segment onto a leading edge fixture assembly,
installing the leading edge fixture assembly onto the main fixture assembly below the blade root section when the blade root section is installed onto the main fixture assembly, and
mounting the at least one leading edge blade segment between the blade root section and the blade tip section while the leading edge blade segment is on the leading edge fixture assembly.

9. The method of claim 8 , further comprising:
placing the at least one trailing edge blade segment onto a trailing edge fixture assembly,
installing the trailing edge blade segment fixture assembly onto the main fixture assembly above the blade root section when the blade root section is installed onto the main fixture assembly.

10. The method of claim 9 , further comprising installing the trailing edge fixture assembly above the blade root section via a crane.

11. The method of claim 10 , further comprising mounting the at least one trailing edge blade segment between the blade root section and the blade tip section while the trailing edge blade segment is on the trailing edge fixture assembly.

12. A method for assembling a modular rotor blade of a wind turbine, the method comprising:
providing a pre-formed blade root section and a pre-formed blade tip section of the rotor blade, at least one of the blade root section or the blade tip section comprising one or more spar caps extending in a generally span-wise direction therefrom, the one or more spar caps being integral with at least one of the blade root section or the blade tip section;
providing at least one pre-formed blade segment of the rotor blade;
arranging the at least one blade segment with the one or more spar caps of the blade root section, wherein the at least one blade segment comprises a chord-wise cross-section defining a continuous blade surface; and,
joining the blade tip section at one of the one or more spar caps and the at least one blade segment.

13. The method of claim 12 , wherein the continuous blade surface comprises a single joint at a trailing edge of the blade segment, wherein the continuous blade surface comprises a pressure side surface and a suction side surface, and wherein the method further comprises:
separating the pressure and suction side surfaces at the single joint,
mounting the continuous blade segment over the one or more spar caps,
joining the pressure and suction side surfaces at the single joint, and
securing the continuous blade segment between the blade root section and the blade tip section.

14. The method of claim 12 , wherein the continuous blade surface is non-jointed, wherein the method further comprises:
installing the non-jointed blade surface around the one or more spar caps.

Assignees

• Gen Electric

Inventors

• Caruso Christopher Daniel
• Yarbrough Aaron A
• Hynum Daniel Alan
• Tobin James Robert

Classifications

• F05B2230/60

  Assembly methods · CPC title

• B23P15/04

  turbine or like blades from several pieces · CPC title

• F03D1/001 Primary

  Mechanical Engineering · mapped topic

• F03D1/0675 Primary

  of the blades · CPC title

• F05B2240/302

  Segmented or sectional blades · CPC title