Offset perpendicular axis turbine

Patent metadata

Field	Value
Publication number	US-10844835-B2
Application number	US-201715639792-A
Country	US
Kind code	B2
Filing date	Jun 30, 2017
Priority date	Jun 30, 2017
Publication date	Nov 24, 2020
Grant date	Nov 24, 2020

Abstract

A perpendicular axis turbine having at least two blades, wherein the blades are longitudinally offset with respect to one another, reducing the effects of blade-vortex interaction and providing increased power generation. In one embodiment, the blades are longitudinally offset such that the attachment point of one blade is halfway between the attachment points for the other blade.

First claim

We claim:

1. A perpendicular axis turbine comprising:
a central turbine shaft;
a first blade attached to the central turbine shaft, the first blade having an airfoil cross-section and a first blade shape comprising at least one arcing segment having different radii at different longitudinal positions, the first blade shape defining a first path as said first blade revolves about a central axis of said central turbine shaft; and
a second blade attached to the central turbine shaft, the second blade having an airfoil cross-section and a second blade shape that is the same as the first blade shape, said second blade defining a second path as said second blade revolves about said central axis of said central turbine shaft;

wherein the first and second blades are longitudinally offset with respect to each other so that at each longitudinal position where the first and second blades overlap, the first and second blades are disposed at different radii from the central axis; and the perpendicular axis turbine has no blade other than the first blade, that follows the first path.

2. The perpendicular axis turbine according to claim 1 , comprising at least one additional blade having an airfoil cross-section, said at least one additional blade being attached to the central turbine shaft and defining an additional path as said additional blade revolves about said central axis of said central turbine shaft, wherein said additional path partially longitudinally intersects said first path and said second path.

3. The perpendicular axis turbine according to claim 1 , wherein the first and second blades are each attached to the central turbine shaft using at least two attachment points.

4. The perpendicular axis turbine according to claim 3 , wherein the at least two attachment points are at a longitudinal positions near opposite ends of the central turbine shaft, where a radial distance to the blade is minimum.

5. The perpendicular axis turbine according to claim 4 , wherein the first and second blades are each attached to the central turbine shaft by rigid linear members with smooth surfaces, wherein said linear members are substantially perpendicular to the central turbine shaft.

6. The perpendicular axis turbine according to claim 4 , wherein the first and second blades are each attached to the central turbine shaft by rigid linear members with smooth surfaces, wherein said linear members are oriented at a fixed angle of 20°-90° relative to the central turbine shaft.

7. The perpendicular axis turbine according to claim 6 , wherein the linear members are oriented at a fixed angle of 40°-80° relative to the central turbine shaft.

8. The perpendicular axis turbine according to claim 7 , wherein the linear members are oriented at a fixed angle of 50°-75° relative to the central turbine shaft.

9. The perpendicular axis turbine according to claim 1 , wherein an attachment point for said first blade is on the central turbine shaft at a percentage distance of 1%-80% of the distance between attachment points for said second blade and an attachment point for said second blade is on the central turbine shaft at a percentage distance of 1%-80% of the distance between attachment points for said first blade, and wherein the percentage distance of the first blade is equal to the percentage distance of the second blade.

10. The perpendicular axis turbine according to claim 1 , wherein one of a pair of attachment points an attachment point for said first blade is midway between a pair of attachment points for said second blade and one of said pair of attachment points an attachment point for said second blade is midway between said pair of attachment points for said first blade.

11. The perpendicular axis wind turbine according to claim 1 , wherein angles between the blades are equal for even distribution.

12. The perpendicular axis wind turbine according to claim 1 , wherein said first blade approximates a troposkein curve.

13. The perpendicular axis turbine according to claim 1 , wherein said first blade is helical.

14. The perpendicular axis turbine according to claim 1 , wherein the airfoil cross-sections of the blades are designed to be primarily driven by lift.

15. A perpendicular axis turbine comprising:
a central turbine shaft having first and second ends;
a first blade having an airfoil cross-section, the first blade having a first blade shape comprising at least one arcing segment having different radii at different longitudinal positions; and
a second blade having an airfoil cross-section, the second blade having a second blade shape that is the same as the first blade shape;
wherein:
both the first and second blades are attached to the central turbine shaft at respective first end proximal and second end proximal attachment points;
the first blade's attachment points are longitudinally offset from corresponding second blade's attachment points by 1%-80% of a distance between the first blade's base attachment points; and
the first blade's attachment points relative to the first blade shape are the same as the second blade's attachment points to the second blade shape.

16. The perpendicular axis turbine according to claim 15 , comprising at least one additional blade having an airfoil cross-section, said at least one additional blade being attached to the central turbine shaft and defining an additional path as said additional blade revolves about said central axis of said central turbine shaft, wherein said additional path partially longitudinally intersects said first said second path.

17. The perpendicular axis turbine according to claim 15 , wherein the first and second blades are each attached to the central turbine shaft by rigid linear members with smooth surfaces, wherein said linear members are: substantially perpendicular to the central turbine shaft; or oriented at a fixed angle of 20°-90° relative to the central turbine shaft.

18. The perpendicular axis wind turbine according to claim 15 , wherein:
angles between the blades are equal for even distribution; said first blade approximates a troposkein curve; or said first blade is helical.

19. The perpendicular axis turbine according to claim 15 , wherein for each blade, the attachment points are longitudinally aligned with positions of the blade shape where a radial distance to the blade is minimum.

20. The perpendicular axis turbine according to claim 15 , wherein the airfoil cross-sections of the blades are designed to be primarily driven by lift.

Assignees

• Nat Res Council Canada

Inventors

• Fereidooni Amin
• Seleman Hilewit Doma
• Matida Edgar A
• Nitzsche Fred

Classifications

• F03D3/061

  characterised by their aerodynamic shape, e.g. aerofoil profiles · CPC title

• F03B13/264

  using the horizontal flow of water resulting from tide movement · CPC title

• F05B2220/32

  in water turbines · CPC title

• F05B2240/212

  of the Darrieus type · CPC title

• F03B17/063

  the flow engaging parts having no movement relative to the rotor during its rotation · CPC title