Jointed wind turbine rotor blade having varying material combinations along its span for pin reinforcement

Patent metadata

Field	Value
Publication number	US-11680555-B2
Application number	US-201917290308-A
Country	US
Kind code	B2
Filing date	Oct 30, 2019
Priority date	Oct 31, 2018
Publication date	Jun 20, 2023
Grant date	Jun 20, 2023

Abstract

A jointed rotor blade includes a first blade segment and a second blade segment extending in opposite directions from a chord-wise joint. Each of blade segments has at least one shell member defining an airfoil surface and an internal support structure. The internal support structure of the first blade segment includes a beam structure extending lengthwise that structurally connects with the internal support structure of the second blade segment via a receiving section. The rotor blade further includes one or more pin joints positioned on at least one of internal support structures of the first blade segment or the second blade segment. Thus, at least one of internal support structures of the first blade segment or the second blade segment includes varying material combinations along a span of the rotor blade at locations of the one or more pin joints so as to reinforce the one or more pin joints.

First claim

What is claimed is:

1. A rotor blade for a wind turbine, comprising:
a first blade segment and a second blade segment extending in opposite directions from a chord-wise joint, each of the first and second blade segments comprising at least one shell member defining an airfoil surface and an internal support structure, the internal support structure of the first blade segment comprising a beam structure extending lengthwise that structurally connects with the internal support structure of the second blade segment via a receiving section; and
one or more pin joints positioned on at least one of internal support structures of the first blade segment or the second blade segment,
wherein at least one of internal support structures of the first blade segment or the second blade segment comprises varying material combinations along a span of the rotor blade at locations of the one or more pin joints so as to reinforce the one or more pin joints,
wherein the varying material combinations further comprise one or more reinforcement members at the locations of the one or more pin joints, and wherein the one or more reinforcement members comprise a core material that is different than a core material from remaining portions of the internal support structures.

2. The rotor blade of claim 1 , wherein at least one of the internal support structures of the first and second blade segments comprise at least one shear web connected with a suction side spar cap and a pressure side spar cap, the shear web comprising the varying material combinations along the span of the rotor blade at the locations of the one or more pin joints.

3. The rotor blade of claim 2 , wherein the varying material combinations comprises at least one of varying resin materials, varying metal materials, varying fiber materials, varying fiber orientations, and/or combinations thereof.

4. The rotor blade of claim 3 , wherein the varying resin materials comprise at least one of a thermoset resin or a thermoplastic resin.

5. The rotor blade of claim 3 , wherein the varying fiber materials comprise at least one of glass fibers, carbon fibers, polymer fibers, wood fibers, bamboo fibers, ceramic fibers, nanofibers, metal fibers, or combinations thereof.

6. The rotor blade of claim 3 , wherein a fiber orientation at the locations of the one or more bolts joints comprises a quasi-isotropic fiber orientation.

7. The rotor blade of claim 3 , wherein a thickness of the shear web at the locations of the one or more pin joints is greater than a thickness of remaining portions of the shear web.

8. The rotor blade of claim 1 , wherein the one or more reinforcement members comprise at least one tapered transition feature at an edge thereof.

9. The rotor blade of claim 1 , wherein the one or more pin joints comprises, at least, one or more first pin joints located at a first end of the beam structure for connecting with a receiving end of the receiving section of the second blade segment, the one or more first pin joints comprising at least one pin tube embedded in a first material combination of the varying material combinations.

10. The rotor blade of claim 9 , wherein the first blade segment comprises at least one chord-wise extending pin joint slot located on the beam structure proximate to the chord-wise joint, the at least one pin joint slot surrounded by a second material combination of the varying material combinations, wherein the first and second material combinations differ from a primary material combination of the shear web.

11. A method of assembling a rotor blade of a wind turbine, the method comprising:
arranging a first blade segment and a second blade segment in opposite directions from a chord-wise joint, each of the blade segments having a shell member defining an airfoil surface and an internal support structure, at least one of the internal support structures of the blade segments comprising a shear web;
inserting the beam structure extending lengthwise from the first blade segment into a receiving section of the second blade segment;
attaching a free end of the beam structure with a receiving end of the receiving section of the second blade segment using one or more first pin joints; and
connecting the first and second blade segments using one or more second pin joints located at the chord-wise joint, wherein, when the first and second blade segments are connected, a thickness of the shear web at locations of at least one of the one or more first pin joints or the one or more second pin joints is greater than a thickness of remaining portions of the shear web so as to reinforce at least one of the one or more first pin joints or the one or more second pin joints, and
wherein at least one of the beam structure or the receiving section comprises varying material combinations along a span of the rotor blade at locations of the one or more first and second pin joints so as to reinforce the one or more first and second pin joints,
wherein the varying material combinations further comprise one or more reinforcement members at the locations of the one or more first and second pin joints, and wherein the one or more reinforcement members comprise a core material that is different than a core material from remaining portions of the internal support structures.

12. The method of claim 11 , wherein the varying material combinations comprises at least one of varying resin materials, varying metal materials, varying fiber materials, varying fiber orientations, and/or combinations thereof, the varying resin materials comprising at least one of a thermoset resin or a thermoplastic resin, the varying fiber materials comprising at least one of glass fibers, carbon fibers, polymer fibers, wood fibers, bamboo fibers, ceramic fibers, nanofibers, metal fibers, or combinations thereof.

13. The method of claim 11 , further comprising at least one of infusing or bonding the varying material combinations to the shear web.

14. The method of claim 11 , further comprising forming at least one tapered transition feature into an edge of the one or more reinforcement members.

15. The method of claim 11 , wherein the one or more first pin joints further comprise at least one pin tube embedded in a first material combination of the varying material combinations, the first blade segment comprising at least one chord-wise extending pin joint slot located on the beam structure proximate to the chord-wise joint, the at least one pin joint slot surrounded by a second material combination of the varying material combinations, wherein the first and second material combinations differ from a primary material combination of the shear web.

Assignees

• Gen Electric

Inventors

• Merzhaeuser Thomas
• Yarbrough Aaron A
• Rodwell Andrew Mitchell
• KUMAR Rishikesh

Classifications

• F05B2230/604

  using positioning or alignment devices for aligning or centering, e.g. pins · CPC title

• F05B2260/30

  Retaining components in desired mutual position · CPC title

• F03D1/0675 Primary

  of the blades · CPC title

• F05B2280/6003

  Composites; e.g. fibre-reinforced · CPC title

• F05B2240/302

  Segmented or sectional blades · CPC title