The present invention relates to a vertical axis wind turbine, and how to make its blades perform better. Drag and lift blades each have their own benefits and drawbacks; the possibility of combining them for better total performance is presented. Drag blades operate from the push of the wind; lift blades operate like the wing of an aircraft by inducing circulation changes.
The invention is herein described, by way of example only, with reference to the accompanying drawings, wherein:
The present invention shows vertical axis turbine blades that deliver solutions to the problem of providing maximal power and maximal quiet at the same time. Vertical axis blades are less powerful when working in a drag configuration (being pushed by the wind) and noisier but more powerful when working in a lift configuration (with an airfoil-type effect). Lift configurations also have more trouble starting. Therefore, this application attempts to bridge the gap between the two types of configuration by presenting several solutions that increase power to a basically drag configuration or decrease the noise of a lift configuration.
Definitions: The environment of the inventions can be any fluid. The term “wind” is often used because it is most common, but the inventions mentioned are adaptable to any fluid, whether gas or liquid. Foils are as generally known in the aircraft industry. If a non-blade foil shape is close enough to a blade to affect its performance, it is functionally adjacent to it. Any reference to such a structure is distinct from foil shapes that may be on the blade.
The principles and operation of a vertical axis turbine according to the present invention may be better understood with reference to the drawings and the accompanying description.
Referring now to the drawings,
In summary, (1) and (2) are different types of lift type blades, (1) being a complete foil. (3) illustrates how the geometry of (2) involves crossing the chord midline part way. (4) is an example of a drag type of blade. (5) shows how they can be combined vertically. In this case, the lower and upper parts are drag, and the middle part of the blade is lift. The opposite is also possible. (6) illustrates a tapering shape. The reason for this is that a turbine with a lower or upper foil produces a distribution of higher velocity air even a little in front of the foil shape (8), so that a tapered shape that bulges at the middle can contact that area of higher velocity. This bulge shape of blade is claimed for drag and lift varieties, and for association with a foil. For orientation, (7) is the shaft.
While the invention has been described with respect to a limited number of embodiments, it will be appreciated that many variations, modifications and other applications of the invention may be made.
The present invention successfully addresses the shortcomings of the presently known configurations by providing devices for obtaining simultaneous drag and lift effects with a vertical axis turbine.
It is now disclosed for the first time a blade (defined as including a blade segment) of a vertical axis turbine, comprising:
a. at least two regions of different shapes in a vertical distribution along the blade. (Note that this does not refer to a different shape at the very edge, such as a winglet, which is known art. All these descriptions refer to more than minimal changes or purely esthetic curves added to the blade design. The regions of two different shapes as described here include the possibility that there may be an area of gradual transition from one shape to another.)
In one embodiment, the blade further comprises:
b. a foil shape (not the blade) functionally adjacent to the blade.
According to another embodiment, one region is a predominantly drag shape, and one region is a predominantly lift shape.
According to another embodiment, at least one region is a mixed drag and lift shape.
According to another embodiment, the turbine is in a liquid.
According to another embodiment, the different shape is one of different dimension of the same shape.
In one embodiment, the blade further comprises:
b. a third vertically distinct region of lift or drag.
According to another embodiment, one of the regions is a partial foil shape.
According to another embodiment, the line from the external edge to the endpoint of the partial foil is in the direction of the internal curve of the blade on one side.
According to another embodiment, the line from the external edge on the second side to the endpoint of the partial foil is in the direction of the internal curve of the blade.
According to another embodiment, one of the regions is a full foil.
In one embodiment, the blade further comprises:
b. a foil shape (not the blade) functionally adjacent to the blade.
It is now disclosed for the first time a blade (defined as including a blade segment) for a vertical axis turbine, wherein the line from the external edge to the endpoint of the partial foil, is in the direction of the internal curve of the blade on at least one side.
According to another embodiment, the turbine is in a liquid.
In one embodiment, the blade further comprises:
a foil shape (not the blade) functionally adjacent to the blade.
It is now disclosed for the first time a blade (defined as including a blade segment) of a vertical axis turbine, comprising:
a. shape that bulges peripherally and/or centrally in a vertical distribution.
In one embodiment, the blade further comprises:
b. a foil shape (not the blade) functionally adjacent to the blade.
It is now disclosed for the first time an arm holding a vertical axis turbine blade, comprising:
a. a streamlined arm facing the direction of movement of the turbine with a collector shape on the opposite side.
According to another embodiment, the streamlined arm comes to a point in front.
According to another embodiment, the streamlined arm is rounded in front.
According to another embodiment, the turbine is in a liquid.
Filing Document | Filing Date | Country | Kind | 371c Date |
---|---|---|---|---|
PCT/IB09/53610 | 8/17/2009 | WO | 00 | 2/7/2011 |
Number | Date | Country | |
---|---|---|---|
61089914 | Aug 2008 | US |