OPTIMIZATION OF PREMIUM FIBER MATERIAL USAGE IN WIND TURBINE SPARS

• US 20100296941A1
• Filed: 05/21/2009
• Published: 11/25/2010
• Est. Priority Date: 05/21/2009
• Status: Active Grant

• Current Assignee: Michael D. Zuteck
• Original Assignee: Michael D. Zuteck
• Inventors: Zuteck, Michael D.
• Granted Patent: US 8,079,819 B2
• Time in Patent Office: Days
• US Class Current: 416/226
• CPC Class Codes: F03D 1/0675 of the blades
• CPC Class Codes: F05B 2280/2006 Carbon, e.g. graphite
• CPC Class Codes: F05B 2280/6003 Composites; e.g. fibre-reinforced
• CPC Class Codes: F05C 2253/04 Composite, e.g. fibre-reinforced
• CPC Class Codes: Y02E 10/72 Wind turbines with rotation axis in wind direction

Abstract

The use of premium material in the construction of wind turbine blades may provide increases in blade efficiency and enable the use of thinner blades. By providing a spar cap having a section of premium material having a constant thickness, the use of the premium material may be optimized to provide a more effective use of premium material. Additional material, which may be less expensive as well as heavier, may be added near the blade root to provide additional strength and stiffness to the blade.

Claims

1. A wind turbine blade, comprising:

a blade shell; and

a main spar located at least partially within the blade shell, the main spar comprising a first spar cap, a second spar cap, and at least one shear web extending between the first spar cap and the second spar cap, wherein the first spar cap comprises;

a first component comprising a first material, wherein the first component has a substantially constant thickness over a section of the spar cap which extends along at least half the length of the blade shell; and

a second component located adjacent the first component and comprising a second material, wherein the second material is different from the first material.

2. The blade of claim 1, wherein the section of substantially constant thickness of the first component comprises a plurality of plies of said first material extending along the length of said section of substantially constant thickness.

3. The blade of claim 1, wherein the first material has a strength to weight ratio greater than a strength to weight ratio of the second material.

4. The blade of claim 1, wherein the first material has a stiffness to weight ratio greater than a stiffness to weight ratio of the second material.

5. The blade of claim 1, wherein the first component of the first spar cap extends along an inner surface of the blade shell, and wherein the first component is disposed between at least a part of the second component of the first spar cap and said inner surface of the blade shell.

6. The blade of claim 1, wherein at least part of the second component of the first spar cap extends along an inner surface of the blade shell, and wherein said at least part of the second component is disposed between the first component of the first spar cap and said inner surface of the blade shell.

7. The blade of claim 1, wherein the first material comprises carbon fiber.

8. The blade of claim 1, wherein the second material comprises fiberglass.

9. The blade of claim 1, wherein an outboard end of the first component of the spar cap is located outboard of an outboard end of the second component of the first spar cap

10. A wind turbine blade, comprising:

a blade shell; and

a main spar located at least partially within the blade shell, the main spar comprising a first spar cap, a second spar cap, and at least one shear web extending between the first spar cap and the second spar cap, wherein the first spar cap comprises a first component comprising a first material and a second component comprising a second material, the second material being different than the first material, wherein the first component comprises a plurality of plies of said first material extending at least between a first point in an inboard region of the blade and a second point located more than 50% of the blade length away from the first point.

11. The wind turbine blade of claim 10, wherein the first point is located near the blade root.

12. The wind turbine blade of claim 10, wherein the first point is located within a root buildup section of the blade.

13. A spar, comprising:

a first spar cap, wherein the first spar cap comprises a first component comprising a constant thickness section having a substantially constant thickness of a first material, and a second component having thickness which varies over the length of the second component, wherein the length of the substantially constant thickness section of the first component is greater than the length of the second component;

a second spar cap; and

at least one shear web extending between an inner surface of the first spar cap and an inner surface of the second spar cap.

14. The spar of claim 13, wherein the second spar cap comprises a first component comprising a constant thickness section having a substantially constant thickness of a first material, and a second component having thickness which varies over the length of the second component, wherein the length of the substantially constant thickness section of the first component is greater than the length of the second component.

15. The spar of claim 14, wherein the constant thickness section of the first component of the first spar cap has a thickness which is substantially equal to a thickness of the constant thickness section of the first component of the second spar cap.

16. The spar of claim 13, wherein the first component of the first spar cap comprises a tapering section located outboard of the constant thickness section.

17. The spar of claim 13, wherein the first component of the first spar cap comprises a section of substantially constant width.

18. The spar of claim 13, wherein the constant thickness section of the first component of the first spar cap extends at least 66% of the length of the first component.

19. The spar of claim 13, wherein the constant thickness section of the first component of the first spar cap extends at least 80% of length of the first component.