IP Library › Granted Patent US 11,215,161
Granted Patent B2
US 11,215,161 · App. 16/186,876 · Granted Jan 4, 2022

Retrofit winglets for wind turbines

Inventors: Leonard Scott Miller (Wichita, KS); Vijay Matheswaran (Wichita, KS)
Assignee: Wichita State University
F03D1/0675F03D1/0633F05B2230/80F05B2240/301F05B2280/2001F05B2280/4002F05B2280/6003F05B2280/6012
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Quick Facts
Patent No.
US 11,215,161
App. No.
16/186,876
Granted
Jan 4, 2022
Kind
B2
Abstract

A winglet is provided for retrofitting to a wind turbine. Aerodynamic and centrifugal forces for winglets having a range of configurations including winglet height, taper ratio, twist, and cant angle are modeled, wherein the winglet height, taper ratio, twist, and cant angle are used to define a grid in a Vector Lattice. An increase in a coefficient of power C p of each winglet design when applied to a predetermined main blade of the wind turbine can be determined. A winglet configuration can then be selected wherein the coefficient of power C p of the main blade and winglet is at least 2% greater than the coefficient of power C p of the main blade alone, and wherein a ratio of normal aerodynamic force generated by the winglet to centrifugal force generated by the winglet during rotation at a nominal rated speed is in a range between 0.75 and 2.

Claims (39)

1. A wind turbine comprising:

a main blade arranged for wind-driven rotation in a vertical plane; and

a winglet extending from a tip of the main blade away from the vertical plane, wherein a coefficient of power Cp of the main blade and winglet is at least 2% greater than a coefficient of power Cp of the main blade alone, and wherein a ratio of normal aerodynamic force generated by the winglet to centrifugal force generated by the winglet during rotation at a nominal speed is in a range between 0.75 and 2;

wherein the winglet has a twist of 0°;

where the winglet has a taper ratio of 1.

2. The wind turbine of claim 1 wherein the winglet has a height between 1.7 meters and 2.1 meters and a radius of curvature between 0.45 meters and 0.55 meters.

3. The wind turbine of claim 1 wherein an increased thrust generated by the winglet is less than about 1%.

4. The wind turbine of claim 1 wherein the winglet is comprised of:

a load bearing balsa spar;

a foam core embedded with the spar; and

a fiberglass skin over the spar.

5. The wind turbine of claim 4 wherein the fiberglass skin provides a sleeve adapted to slip onto an end of the main blade to be adhesively bonded.

6. The wind turbine of claim 4 wherein the main blade is configured to receive an adapter bolted to the main blade and providing male connector extensions, wherein the winglet further comprises female sockets for receiving the male connector extensions.

7. A winglet for retrofitting to a main blade of a wind turbine, comprising:

a load bearing balsa spar;

a foam core embedded with the spar; and

a fiberglass skin over the spar;

wherein the winglet is configured to extend from a tip of the main blade away from a vertical plane of the main blade, wherein a coefficient of power Cp of the main blade and winglet is at least 2% greater than a coefficient of power Cp of the main blade alone, and wherein a ratio of normal aerodynamic force generated by the winglet to centrifugal force generated by the winglet during rotation at a nominal speed is in a range between 0.75 and 2;

wherein the winglet has a taper ratio in an inclusive range of from 0.5 to 1.

8. The winglet of claim 7 wherein the winglet has a twist of 0° and the taper ratio is 1.

9. The winglet of claim 8 wherein the winglet has a height between 1.7 meters and 2.1 meters and a radius of curvature between 0.45 meters and 0.55 meters.

10. The winglet of claim 7 wherein an increased thrust generated by the winglet is less than about 1%.

11. The winglet of claim 7 wherein the fiberglass provides a sleeve adapted to slip onto an end of the main blade to be adhesively bonded.

12. The winglet of claim 7 wherein the main blade is configured to receive an adapter bolted to the main blade and providing male connector extensions, wherein the winglet further comprises female sockets for receiving the male connector extensions.

13. A wind turbine comprising:

a main blade arranged for wind-driven rotation in a vertical plane; and

a winglet extending from a tip of the main blade away from the vertical plane, wherein a coefficient of power Cp of the main blade and winglet is at least 2% greater than a coefficient of power Cp of the main blade alone, and wherein a ratio of normal aerodynamic force generated by the winglet to centrifugal force generated by the winglet during rotation at a nominal speed is in a range between 0.75 and 2;

wherein the winglet has a taper ratio in an inclusive range of from 0.5 to 1.

14. The wind turbine of claim 13 wherein the winglet has a twist of 0°.

15. The wind turbine of claim 13 wherein the taper ratio is 1.

16. The wind turbine of claim 13 wherein the winglet has a height between 1.7 meters and 2.1 meters.

17. The wind turbine of claim 13 wherein the winglet has a radius of curvature between 0.45 meters and 0.55 meters.

18. The wind turbine of claim 13 wherein an increased thrust generated by the winglet is less than about 1%.

19. The wind turbine of claim 13 wherein the winglet is comprised of:

a load bearing balsa spar;

a foam core embedded with the spar; and

a fiberglass skin over the spar.

20. The wind turbine of claim 19 wherein the fiberglass skin provides a sleeve adapted to slip onto an end of the main blade to be adhesively bonded.

21. The wind turbine of claim 13 wherein the main blade is configured to receive an adapter bolted to the main blade and providing male connector extensions, wherein the winglet further comprises female sockets for receiving the male connector extensions.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 12, 2018
From: MILLER, LEONARD SCOTT; MATHESWARAN, VIJAY
To: WICHITA STATE UNIVERSITY
Reel/Frame 047502/0580 →
Continuity (2)
Provisional Application 62585179 · Nov 13, 2017
Related Publication 20190145375A1 · May 16, 2019