IP Library › Granted Patent US 10,378,505
Granted Patent B2
US 10,378,505 · App. 15/127,795 · Granted Aug 13, 2019

Hydrokinetic energy conversion system and use thereof

Inventor: Anders Holm (Arendal, NO)
Assignee: Flumill AS
F03B13/264F03B17/06F05B2240/243F05B2250/25F05B2250/711F05B2250/712Y02E10/28
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Quick Facts
Patent No.
US 10,378,505
App. No.
15/127,795
Granted
Aug 13, 2019
Kind
B2
Abstract

A hydrokinetic energy conversion system ( 1 ) comprising a turbine device ( 2 ) comprising a rotor ( 3 ) displaying a rotational axis (O), which turbine device is arranged to operate with the rotational axis in an inclined orientation vis-à-vis an incoming body of water (W), and which rotor comprises a blade ( 10 ) which is arranged to interact with the incoming body of water such that rotational energy is imparted to the rotor. The blade comprises a first, convex surface ( 12 ), a second, concave surface ( 13 ) and a free, distal edge (E) where the first surface and the second surface meet. The curvature of the second surface, when viewed in a plane orthogonal to the rotational axis, is such that a maximum depth (Dmax) of the second surface, when measured from a straight line intersecting the rotational axis and the distal edge, is at least 35% of the distance between the rotational axis and the distal edge.

Claims (16)

1. A hydrokinetic energy conversion system comprising a turbine device comprising a rotor displaying a rotational axis, which turbine device is arranged to operate with the rotational axis in an inclined orientation vis-à-vis an incoming body of water, and which rotor comprises at least one helical blade which is arranged to interact with the incoming body of water such that rotational energy is imparted to the rotor, which at least one helical blade comprises a first, convex surface, a second, concave surface and a free, distal edge where the first surface and the second surface meet, wherein the curvature of the second surface, when viewed in a plane orthogonal to the rotational axis, is such that a maximum depth of the second surface, when measured from a straight line intersecting the rotational axis and the distal edge, is at least 35% of the distance between the rotational axis and the distal edge and in that the at least one helical blade, at the position of the maximum depth, displays a thickness which is less than 15% of the distance between the rotational axis and the distal edge.

2. The system according to claim 1 , wherein said maximum depth is at least 40% of the distance between the rotational axis and the distal edge.

3. The system according to claim 2 , wherein said maximum depth is at least 50% of the distance between the rotational axis and the distal edge.

4. The system according to claim 1 , wherein the at least one helical blade, at the position of the maximum depth (D max ), displays a thickness which is less than 10% of the distance between the rotational axis and the distal edge.

5. The system according to claim 1 wherein a cross-section of the second surface, when viewed in a plane orthogonal to the rotational axis, displays a constant curvature between the position of the maximum depth and the distal edge.

6. The system according to claim 1 , wherein the at least one helical blade displays a continuously decreasing thickness from the position of the maximum depth to the distal edge.

7. The system according to claim 1 , wherein the at least one helical blade displays a pitch ratio within the interval of 1-4.

8. The system according to claim 1 , wherein the rotor displays a diameter-length ratio within the interval of 0.1-1.7.

9. The system according to claim 1 , wherein said at least one helical blade comprises a first helical blade and a second helical blade which is offset 180 degrees in relation to the first helical blade.

10. The system according to claim 1 , wherein it comprises a support device for supporting the turbine device, and in that the turbine device comprises a first, proximal end and a second, distal end, which proximal end is pivotally connected to the support device about a pivot axis.

11. The system according to claim 10 , wherein the pivot axis is orthogonal to the rotational axis.

12. The system according to claim 11 , wherein the pivot axis has an orientation which is any one of horizontal, vertical and diagonal.

13. The system according to any one of claims 1 - 9 , wherein it comprises a first support device for supporting a first end ( 8 ) and a second support device for supporting a second end of the turbine device, which first and second ends are fixedly connected to the support devices.

14. The system according to claim 1 , wherein the rotational axis, when the system is in operation, forms an angle (α) to the incoming body of water which is within the interval of 80-20 degrees.

15. The system according to claim 14 , wherein the rotational axis, when the system is in operation, forms an angle (α) to the incoming body of water which is within the interval of 70-30 degrees.

16. The system according to claim 15 , wherein the rotational axis, when the system is in operation, forms an angle (α) to the incoming body of water which is within the interval of 60-40 degrees.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 15, 2016
From: HOLM, ANDERS
To: FLUMILL AS
Reel/Frame 040739/0274 →
Priority Claims (1)
GB 1405119.7 · Mar 21, 2014 · national
Continuity (1)
Related Publication 20170096981A1 · Apr 6, 2017
Cited By (1)
US 1,130,315