Rotor blade with a segmented supporting structure and method for manufacturing the rotor blade

Patent metadata

Field	Value
Publication number	US-9879541-B2
Application number	US-201414201885-A
Country	US
Kind code	B2
Filing date	Mar 9, 2014
Priority date	Mar 20, 2013
Publication date	Jan 30, 2018
Grant date	Jan 30, 2018

Abstract

A rotor blade with a supporting structure, wherein the rotor blade has a rotor blade base section and a rotor blade tip section, is provided. The supporting structure includes a first supporting segment for supporting the rotor blade base section and at least a second supporting segment for supporting the rotor blade tip section. Furthermore, the supporting structure includes the first supporting segment and the second supporting segment along the rotor blade longitudinal direction. The first supporting segment is joined to the second supporting segment in a supporting structure transition section, wherein the supporting structure transition section is located in between the rotor blade base section and the rotor blade tip section. Finally, the first supporting segment and/or the second supporting segment include a fiber material. A method for manufacturing the rotor blade is also provided.

First claim

The invention claimed is:

1. A rotor blade comprising:
a rotor blade base section, a rotor blade tip section, and a rearward swept shape; and
a supporting structure which comprises a first supporting segment for supporting the rotor blade base section, a second supporting segment for supporting the rotor blade tip section, and a supporting structure transition section where the first supporting segment and the second supporting segment each terminate and form a joint, wherein the first supporting segment is straight up to the supporting structure transition section, the second supporting segment is straight up to the supporting structure transition section, and the first supporting segment and the second supporting segment form an angle with each other of less than 180 degrees;
wherein the first supporting segment is joined directly to the second supporting segment in the supporting structure transition section, wherein the supporting structure transition section is configured to form the angle to be less than 180 degrees; and
wherein the first supporting segment and/or the second supporting segment comprises a fibre material, and
wherein the supporting segments cooperate to form the rearward swept shape.

2. The rotor blade according to claim 1 ,
wherein the first supporting segment comprises a first layer of fibre material and the second supporting segment comprises a second layer of fibre material.

3. The rotor blade according to claim 2 ,
wherein the first layer and/or the second layer comprises a planar shape.

4. The rotor blade according to claim 2 , wherein
the first layer comprises at least a first layer longitudinal surface section and at least a first layer transversal surface section, wherein the first layer longitudinal surface section is greater than the first layer transversal surface section;
the second layer comprises at least a second layer longitudinal surface section and at least a second layer transversal surface section, wherein the second layer longitudinal surface section is greater than the second layer transversal surface section; and
the first layer longitudinal surface section is directly joined to the second layer longitudinal surface section in the supporting structure transition section.

5. The rotor blade according to claim 2 ,
wherein the first layer and the second layer at least partly overlay in the supporting structure transition section.

6. The rotor blade according to claim 2 , wherein
the first supporting segment comprises a stack of additional layers for additionally supporting the first supporting segment,
the second supporting segment comprises a further stack of further additional layers for additionally supporting the second supporting segment,
the first layer and the stack of additional layers at least partly overlay,
the second layer and the further stack of further additional layers at least partly overlay, and
the stack of additional layers is joined to the further stack of further additional layers in the supporting structure transition section.

7. The rotor blade according to claim 2 ,
wherein the first layer of fibre material and/or the second layer of fibre material comprises a shape of a cuboid.

8. The rotor blade according to claim 1 ,
wherein the fibre material comprises a fabric with fibres.

9. The rotor blade according to claim 1 ,
wherein the fibre material comprises a composite material.

10. The rotor blade according to claim 1 ,
wherein the angle is smaller than 175 degrees.

11. The rotor blade according to claim 1 , wherein
the first supporting segment comprises a supplementary first supporting segment for additionally supporting the rotor blade,
the second supporting segment comprises a supplementary second supporting segment for additionally supporting the rotor blade, and
the first supporting segment is joined to the supplementary first supporting segment by a first connection component and/or the second supporting segment is joined to the supplementary second supporting segment by a second connection component.

12. The rotor blade according to claim 1 ,
wherein the rotor blade is a part of a wind turbine engine.

13. The rotor blade according to claim 1 ,
wherein the fibre material comprises a fabric with unidirectional fibres.

14. The rotor blade according to claim 1 ,
wherein the fibre material comprises a sheet with pre-impregnated composite material.

15. The rotor blade according to claim 1 ,
wherein the angle is smaller than 170 degrees.

16. The rotor blade according to claim 1 , wherein a rotor blade longitudinal direction extends from the rotor blade base section to the rotor blade tip section, wherein the supporting segments deviate from the rotor blade longitudinal direction by up to 20 degrees.

17. A method for manufacturing a rotor blade according to claim 2 , wherein the method comprises
joining the first supporting segment and the second supporting segment.

18. The method according to claim 17 , wherein the method comprises
a) arranging the first layer and the second layer in a mould;
b) applying a filling material into the mould and thus obtaining a composite comprised by the supporting structure and the filling material; and
c) curing the composite.

19. The method according to claim 18 , wherein the filling material is a liquid filling material.

Assignees

• Torgard Sigmund Wenningsted
• Siemens Ag

Inventors

• Torgard Sigmund Wenningsted

Classifications

• Y02P70/50

  Manufacturing or production processes characterised by the final manufactured product · CPC title

• Y02E10/72

  Wind turbines with rotation axis in wind direction · CPC title

• B23P15/04

  turbine or like blades from several pieces · CPC title

• F03D1/0675

  of the blades · CPC title

• F05B2280/6013

  Fibres · CPC title