Camber changing and low drag wing for vertical axis wind turbine

Abstract

A camber changing wing for a vertical axis wind turbine includes a main body, a pivoting slat, a first beam member, and a second beam member. The main body has front, rear, top and bottom portions. The pivoting slat is disposed adjacent to the front portion. The pivoting slat has a leading edge, and a top and bottom sides. Each of the beam members has a front end, a rear end, and a pivot point. The front end of the first beam member is coupled to the top side of the pivoting slat. The front end of the second beam member is coupled to the bottom side of the pivoting slat. The first beam member is rotatably attached to the top portion of the main body at the pivot point. The second beam member is rotatably attached to the bottom portion of the main body at the pivot point.

Claims

1. A camber changing wing for a vertical axis wind turbine, comprising: a main body having a front portion, a rear portion, a top portion, and a bottom portion; a pivoting slat disposed adjacent the front portion of the main body, the pivoting slat having a leading edge, a top side and a bottom side, the pivoting slat freely pivoting about an axis of rotation disposed through the main body from the top portion to the bottom portion; and a first beam member and a second beam member, each of the first beam member and the second beam member having a front end, a rear end, and a pivot point disposed between the front end and the rear end, the front end of the first beam member coupled to the top side of the pivoting slat, the front end of the second beam member coupled to the bottom side of the pivoting slat, the first beam member rotatably attached to the top portion of the main body at the pivot point of the first beam member, and the second beam member rotatably attached to the bottom portion of the main body at the pivot point of the bottom beam member.

2. The camber changing wing of claim 1, wherein the front portion of the main body is rounded.

3. The camber changing wing of claim 1, wherein the rear portion of the main body is tapered relative to the front portion of the main body.

4. The camber changing wing of claim 1, wherein the leading edge of the pivoting slat is tapered relative to a remainder of the pivoting slat.

5. The camber changing wing of claim 1, wherein the pivoting slat has a trailing surface that is disposed adjacent to the front portion of the main body, the trailing surface having a shape corresponding substantially to a shape of the front portion of the main body.

6. The camber changing wing of claim 5, wherein the trailing surface of the pivoting slat is concave.

7. The camber changing wing of claim 1, further comprising a first master wing and a second master wing, the first master wing coupled to the rear end of the first beam member, and the second master wing coupled to the rear end of the second beam member.

8. The camber changing wing of claim 7, wherein the first master wing is disposed on one side of the first beam member and extends upwardly from the first beam member, and the second master wing is disposed on one side of the second beam member and extends downwardly from the second beam member.

9. The camber changing wing of claim 7, wherein the first master wing and the second master wing are each spaced apart from a rearward edge of the rear portion of the main body.

10. The camber changing wing of claim 1, further comprising a top axle disposed on the top portion of the main body, and a bottom axle disposed on the bottom portion of the main body, the top axle and the bottom axle together defining the axis of rotation through the main body.

11. The camber changing wing of claim 10, wherein the pivot point of the first beam member is defined by a hole formed through the first beam member, and the pivot point of the second beam member is defined by a hole formed through the second beam member, the top axle disposed through the hole in the first beam member and the bottom axle disposed through the hole in the second beam member.

12. The camber changing wing of claim 9, wherein the top axle and the bottom axle are provided by opposite ends of an elongate axle member disposed through an entirety of the main body from the top portion to the bottom portion of the main body.

Description

DRAWINGS

(1) The above, as well as other advantages of the present disclosure, will become readily apparent to those skilled in the art from the following detailed description, particularly when considered in the light of the drawings described hereafter.

(2) FIG. 1 is a side elevational view of a camber changing wing for a vertical axis wind turbine, according to one embodiment of the present disclosure;

(3) FIG. 2 is a top plan view of the camber changing wing depicted in FIG. 1;

(4) FIG. 3 is a top plan view of a vertical axis wind turbine with a plurality of camber changing wings, according to one embodiment of the present disclosure;

(5) FIG. 4 is a side elevational view of the vertical axis wind turbine depicted in FIG. 3, the wings shown in one rotational position;

(6) FIG. 5 is a side elevational view of the vertical axis wind turbine depicted in FIGS. 3-4, the wings shown in another rotational position;

(7) FIG. 6 is a schematic top plan view of a single one of the camber changing wings at various rotational positions relative to a directional wind and at a low number of revolutions per minute around a central axis; and

(8) FIG. 7 a schematic top plan view of a single one of the camber changing wings at various rotational positions relative to a directional wind and at a high number of revolutions per minute around a central axis to illustrate a self-regulation of the speed of the chamber changing wings in operation.

DETAILED DESCRIPTION

(9) The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses. It should also be understood that throughout the drawings, corresponding reference numerals indicate like or corresponding parts and features. In respect of the methods disclosed, the order of the steps presented is exemplary in nature, and thus, is not necessary or critical.

(10) As used herein, relative terms such as up, down, upper, lower, top, bottom, above, and beneath are made with reference to the direction of gravity.

(11) A camber changing wing 100 according to one embodiment is shown in FIGS. 1-7. The camber changing wing 2 may be used with a substantially vertical axis wind turbine 100, for example, as illustrated in FIGS. 3-5. In a particular embodiment, the camber changing wing 2 includes a main body 4, a pivoting slat 6, a first beam member 8, a second beam member, 10, a first master wing 12, and a second master wing 14.

(12) The main body 4 of the camber changing wing 2 has a front portion 16, a rear portion 18, a top portion 20, and a bottom portion 22. The main body 4 may further have an attachment point feature 24 configured to mate with a corresponding attachment feature (not shown) on an arm of the vertical axis wind turbine 100. As shown in FIG. 1, the attachment point feature 24 may be disposed on a side portion 26 of the main body 4 between the front portion 16 and the rear portion 18. Other suitable locations for the attachment point feature 24 may be selected by a skilled artisan, as desired.

(13) As shown in FIG. 2, the front portion 16 of the main body 4 of the camber changing wing 2 may be rounded. The rear portion 18 of the main body 4 of the camber changing wing 2 may also be tapered relative to the front portion 16 of the main body 4. One of ordinary skill in the art may also select other suitable shapes for the main body 4 within the scope of the present disclosure.

(14) The pivoting slat 6 of the camber changing wing 2 is disposed adjacent to the front portion 16 of the main body 4. The pivoting slat 6 has a leading edge 32, a top side 35 and a bottom side 37, The pivoting slat 6 is configured to freely pivot about an axis of rotation 28 disposed through the main body 4 from the top portion 20 to the bottom portion 22. For example, as shown in FIG. 2, there may also be a gap 30 disposed between the front portion 16 of the main body 4 and the pivoting slat 6 that allows for the free movement of the pivoting slat 6 relative to the main body 4.

(15) The leading edge 32 of the pivoting slat 6 may be tapered relative to a remainder of the pivoting slat 6. A skilled artisan may select other suitable shapes for the pivoting slat 6 and the leading edge 32, as desired.

(16) With continued reference to FIG. 2, the pivoting slat 6 has a trailing surface 34 that is disposed adjacent to the front portion 16 of the main body 4. In one example, the trailing surface 34 has a shape corresponding substantially to a shape of the front portion 16 of the main body 4. In certain embodiments, the trailing surface 34 of the pivoting slat 6 is concave and conforms to a rounded or convex outer surface of the front portion 16 of the main body 5.

(17) It should be appreciated that the trailing surface 34 of the pivoting slat 6 is also configured to contact the main body 4, and militate against a rotation of the pivoting slat 6 about the axis of rotation 28 at a predetermined angle. For example, the predetermine angle may be approximately 45 degrees relative to an elongate axis 36 of the main body 4. Other suitable predetermined angles may also be selected by the skilled artisan within the scope of the present disclosure.

(18) Referring to FIGS. 1-5, the camber changing wing 2 of the present disclosure further has the first beam member 8 and the second beam member 10. Each of the first beam member 8 and the second beam member 10 has a front end 38, 39, a rear end 40, 41, and a pivot point 42, 43. The pivot point 42, 43 is disposed between the front end 38, 39 and the rear end 40, 41. The front end 38 of the first beam member 8 is coupled to the top side 33 of the pivoting slat 6. The front end 39 of the second beam member 10 is coupled to the bottom side 35 of the pivoting slat 6. The first beam member 8 is rotatably attached to the top portion 20 of the main body 4 at the pivot point 42 of the first beam member 8. The second beam member 10 is rotatably attached to the bottom portion 22 of the main body 4 at the pivot point 43 of the bottom beam member 10.

(19) Although described herein as having two beam members 10, 12, it should be appreciated that a single beam member or more than two beam members for connecting the pivoting slat 6 to the main body may also be used, as desired.

(20) In a particular embodiment, the first beam member 8 may be rotatably attached to the main body 4 with a top axle 44 disposed on the top portion 20 of the main body 4. Likewise, the second beam member 10 may be rotatably attached to the main body 4 with a bottom axle 46 disposed on the bottom portion 22 of the main body 4. In this embodiment, the top axle 44 and the bottom axle 46 together define a location of the axis of rotation 28 that is disposed through the main body 4.

(21) Additionally, the pivot point 42 of the first beam member 8 may be defined by a hole 48 formed through the first beam member 8. Likewise, the pivot point 43 of the second beam member 10 may be defined by a hole 50 formed through the second beam member 10. In this example, the top axle 44 is disposed through the hole 48 in the first beam member 8 and the bottom axle 46 is disposed through the hole 50 in the second beam member 10.

(22) It should be appreciated that the top axle 44 and the bottom axle 46 are free rotating within the holes 48, 50, respectively. Rotation facilitating means such as bearings and the like may also be employed to facilitate the free rotation.

(23) As non-limiting example, the top axle 44 and the bottom axle 46 may be formed directly on the main body 4, separately formed and attached to the main body 4, or provided as a single unitary structure disposed through the main body 4. In a particular example, the top axle 44 and the bottom axle 46 are provided by opposite ends of an elongate axle member disposed through an entirety of the main body 4 from the top portion 20 to the bottom portion 22 of the main body 4. Other means for providing a rotatable attachment of the first beam member 8 and the second beam member 10 to the main body 4 of the camber changing wing 2 may also be used within the scope of the present disclosure.

(24) The camber change wing 2 may further have the first master wing 12 and the second master wing 14. The first master wing 12 is coupled to the rear end 40 of the first beam member 8. The second master wing 14 is coupled to the rear end 41 of the second beam member 10. In a particular example, the first master wing 12 is disposed on one side of the first beam member 8 and extends upwardly from the first beam member 8. Similarly, the second master wing 14 may be disposed on one side of the second beam member 41 and extends downwardly from the second beam member 41.

(25) The first master wing 12 and the second master wing 14 may be spaced apart from a rearward edge 52 of the rear portion 18 of the main body 4. Each of the first master wing 12 and the second master wing 14 may have a substantially streamlined shape, for example. Suitable shapes, configurations, and locations for the first master wing 12 and the second master wing 14 may be selected by one ordinary skill in the art, as desired.

(26) As shown in FIGS. 3-5, the camber changing wing 2 of the present disclosure may be used with the vertical axis wind turbine 100. The vertical axis wind turbine 100 includes at least one substantially vertical rotating shaft 102 to which at least one of the camber changing wing 2 is secured, for example, using the attachment point feature 24. The rotation shaft 102 has a rotational movement 103 in operation. The rotating shaft 102 may be in communication with an electrical generator, a pump, or the like for purposes of supplying movement or power by means of the rotational movement 103.

(27) The at least one camber changing wing 2 may have a substantially vertical orientation, and therefore be oriented substantially parallel with the substantially vertical rotating shaft 102. The camber changing wing 2 may be secured to an arm 104 of, and spaced apart from, the vertical axis wind turbine 100, for example. In particular, the arm 104 is configured to hold the camber changing wing 2 at a substantially fixed distance from the rotation shaft 102.

(28) In a particular embodiment, the vertical axis wind turbine 100 includes a plurality of the camber changing wings 2. The camber changing wings 2 may be positioned substantially equidistant about the rotating shaft 102, for example. In a most particular example, the vertical axis wind turbine 100 includes three to five camber changing wings 2. One of ordinary skill in the art may select other numbers of the camber changing wings 2, as desired.

(29) In operation, the camber changing wing 2 of the present disclosure maintains an optimum driving force and minimum drag regardless of its position around the rotating shaft 102. This occurs because the of movement of the leading edge 32 of the pivoting slat 6 that is driven by the first and second master wings 12, 14 that follow the relative wind, as shown in FIGS. 3-7.

(30) For example, as shown in FIGS. 3-7, the leading edge 32 of the pivoting slat 6 changes position based on relative wind and is a slave to the first and second master wings 12, 14 that are always in the relative wind. This causes the pivoting slat 6 to move to an opposite side of the main body 4 relative to the first and second master wings 12, 14, and place the cambers of the camber changing wing 2 on an optimum sided based on the relative wind and the direction of movement of the camber changing wing 2. This in turn reduces the drag on the camber changing wing 2 from the direct head wind by lining up the relative wind through the streamlined first and second master wings 12, 14.

(31) With reference to FIGS. 6-7, it should also be understood that the camber changing wing 2 is self-regulating in speed during operation. In FIG. 6, which shows the operation of the wing at various locations during a low speed rotation around the vertical wind turbine 100, an angle of the combined pivoting slat 6, the first and second beam members 8, 10, and the first and second master wings 12, 14 relative to main body 4 aligns substantially with the relative wind. However, during a high speed rotation as shown in FIG. 7, the angle of the combined pivoting slat 6, the first and second beam members 8, 10, and the first and second master slats 12, 14 relative to main body 4 does not align substantially with the relative wind. The result of this change in angle with the rotational speed is that the camber changing wing 2 never exceeds a maximum rotational speed.

(32) Advantageously, the camber changing wing 2 of the present disclosure is more efficient than many known wings when used with the vertical axis wind turbine 100. Unlike the prior art wings, which may change the angle of attack, the wing 2 of the present disclosure changes the camber, and thereby better minimizes drag. Additionally, the wing 2 is camber changing with minimal mechanical complexity, as it does not require gears, linkages or motors in order to change the camber. Also, as established above, the wing 2 is self-regulating in speed during an operation of the vertical wind turbine 100, without requiring any sensors or other mechanical or electromechanically governors to monitor or adjust the rotational speed.

(33) While certain representative embodiments and details have been shown for purposes of illustrating the invention, it will be apparent to those skilled in the art that various changes may be made without departing from the scope of the disclosure, which is further described in the following appended claims.