Segmented airfoil design for guide wires

Abstract

The present invention is an improved wind turbine comprising: a wind turbine wheel having a hub, a rim and a cable extending between the hub and the rim; a set of airfoils rotatably carried by the cable and disposed between the hub and the rim; a cinch attached to the cable and disposed between adjacent airfoils; and, an upturned section included in at least one airfoil in the set of airfoils and disposed at a trailing edge of the airfoil wherein each airfoil has a different angle of attack relative to an adjacent airfoil.

Claims

1. An improved wind turbine comprising: a wind turbine wheel having a hub, a rim and a cable extending between the hub and the rim; a set of airfoils rotatably carried by the cable and disposed between the hub and the rim; a cinch attached to the cable and disposed between adjacent airfoils; said airfoils having symmetrical convex top and bottom surfaces with said top surface transitioning into an upturned section defined by an upward slope of a surface contour along a trailing edge portion of said top surface of said airfoils relative to a horizontal plane extending from a leading edge to a trailing edge, wherein said upturned section does not extend above a plane defined by an apex of the convex top surface, and wherein each airfoil has a different angle of attack relative to an adjacent airfoil; and, a vane mounted directly to at least one of said airfoils, wherein said vane includes a shaft extending beyond said trailing edge of said airfoil and a fin disposed at a distal end of said shaft, wherein said vane causes rotation of said airfoil to an optimal angle of attack relative to a wind direction.

2. The improved wind turbine of claim 1 including: an inner cable extending between a proximal end of the hub and the rim; and, a set of inner airfoils carried by the inner cable.

3. The improved wind turbine of claim 2 including: an outer cable extending between a distal end of the hub and the rim; and, a set of outer airfoils carried by the outer cable.

4. The improved wind turbine of claim 1 including: a first airfoil adjacent to the hub having a first length; a second airfoil adjacent to the rim having a second length; and, wherein the first length is less than the second length.

5. The improved wind turbine of claim 4 including an intermediate airfoil having a length between the first length and the second length.

6. The improved wind turbine of claim 1 including a spacer assembly disposed between adjacent airfoils.

7. The improved wind turbine of claim 6 including a resilient member included in the spacer assembly.

8. The improved wind turbine of claim 6 including a washer included in the spacer assembly.

9. The improved wind turbine of claim 1 wherein an airfoil in the set of airfoils has a length in a range of 2 feet to 12 feet.

10. The improved wind turbine of claim 1 including sailets attached to the rim extending from an exterior of the rim.

11. The improved wind turbine of claim 10 wherein the sailets include a variable pitch.

12. The improved wind turbine of claim 1 said airfoils include material selected from the group consisting of high performance vinyl ester resin, 40% unidirectional fiberglass reinforcement, 17% continuous fiberglass mat, resin mixture, UV inhibitors, pigments, surfacing coatings and combinations thereof.

13. The improved wind turbine of claim 1 including a cable opening defined in each airfoil in the set of airfoils for receiving the cable.

14. The improved wind turbine of claim 1 including a generator having a generator wheel configured to engage the rim and disposed below the rim.

15. An improved wind turbine comprising: a wind turbine wheel having a rim; a hub included in the wind turbine wheel having a proximal end and a distal end; an inner set of cables extending between the proximal end of the hub and the rim; a set of inner airfoils rotatably attached to the inner set of cables; an outer set of cables extending between the distal end of the hub and the rim; a set of outer airfoils rotatably attached to the outer set of cables; said airfoils having symmetrical convex top and bottom surfaces with said top surface transitioning into an upturned section defined by an upward slope of a surface contour along a trailing edge portion of said top surface of said airfoils relative to a horizontal plane extending from a leading edge to a trailing edge, wherein said upturned section does not extend above a plane defined by an apex of the convex top surface; and, a vane mounted directly to at least one of said airfoils, wherein said vane includes a shaft extending beyond said trailing edge of said airfoil and a fin disposed at a distal end of said shaft, wherein said vane causes rotation of said airfoil to an optimal angle of attack relative to a wind direction.

16. The improved wind turbine of claim 15 including a spacer assembly disposed between adjacent airfoils.

17. The improved wind turbine of claim 16 including a cinch included in the spacer assembly.

18. An improved wind turbine comprising: a wind turbine wheel having a rim and a hub; a set of cables extending between the hub and the rim; a set of airfoils independently rotatably attached to the set of cables and extending between the rim and the hub; and, said airfoils having symmetrical convex top and bottom surfaces with said top surface transitioning into an upturned section defined by an upward slope of a surface contour along a trailing edge portion of said top surface of said airfoils relative to a horizontal plane extending from a leading edge to a trailing edge, wherein said upturned section does not extend above a plane defined by an apex of the convex top surface; and, a vane mounted directly to at least one of said airfoils, wherein said vane includes a shaft extending beyond said trailing edge of said airfoil and a fin disposed at a distal end of said shaft, wherein said vane causes rotation of said airfoil to an optimal angle of attack relative to a wind direction.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The construction designed to carry out the invention will hereinafter be described, together with other features thereof. The invention will be more readily understood from a reading of the following specification and by reference to the accompanying drawings forming a part thereof, wherein an example of the invention is shown and wherein:

(2) FIG. 1 shows a rear view of aspects of the invention;

(3) FIG. 2 is an elevated view of aspects of the invention;

(4) FIG. 3 is a side perspective view of aspects of an airfoil;

(5) FIG. 4 is a perspective view of aspects of an airfoil;

(6) FIG. 5 shows a side view of aspects of the invention;

(7) FIG. 6 shows a side view of aspects of the invention;

(8) FIGS. 7A and 7B are top views of aspects of the invention;

(9) FIG. 8A is an upward perspective view of aspects of the invention;

(10) FIG. 8B is a downward perspective view of aspects of the invention; and,

(11) FIG. 9 is a side view of aspects of the invention.

(12) It will be understood by those skilled in the art that one or more aspects of this invention can meet certain objectives, while one or more other aspects can meet certain other objectives. Each objective may not apply equally, in all its respects, to every aspect of this invention. As such, the preceding objects can be viewed in the alternative with respect to any one aspect of this invention. These and other objects and features of the invention will become more fully apparent when the following detailed description is read in conjunction with the accompanying figures and examples. However, it is to be understood that both the foregoing summary of the invention and the following detailed description are of a preferred embodiment and not restrictive of the invention or other alternate embodiments of the invention. In particular, while the invention is described herein with reference to a number of specific embodiments, it will be appreciated that the description is illustrative of the invention and is not constructed as limiting of the invention. Various modifications and applications may occur to those who are skilled in the art, without departing from the spirit and the scope of the invention, as described by the appended claims. Likewise, other objects, features, benefits and advantages of the present invention will be apparent from this summary and certain embodiments described below, and will be readily apparent to those skilled in the art. Such objects, features, benefits and advantages will be apparent from the above in conjunction with the accompanying examples, data, figures and all reasonable inferences to be drawn therefrom, alone or with consideration of the references incorporated herein.

DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT

(13) With reference to the drawings, the invention will now be described in more detail. Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood to one of ordinary skill in the art to which the presently disclosed subject matter belongs. Although any methods, devices, and materials similar or equivalent to those described herein can be used in the practice or testing of the presently disclosed subject matter, representative methods, devices, and materials are herein described.

(14) Referring to FIGS. 1 and 2, a wind turbine 10 is shown having a mast 12. The wind turbine includes a rim 14 that has cables extending from the rim to a hub 18. A plurality of airfoils 20 can be carried by cables extending from the hub to the rim. In one embodiment, the wind turbine can include 80 cables that can be 80 feet or more in length and made from inch steel. A plurality of airfoils can include an opening that receives the cable and allows the airfoil to be slidable attached to and rotate about the cable. The opening can be circular, oval or other shape. Each airfoil on a cable can rotate independently of the other airfoils. For example, airfoil 22a can rotate about the cable independently of airfoil 22b. The airfoil can be of different lengths along a cable. For example, an airfoil disposed adjacent to the rim can have a shorter length that one disposed adjacent to the rim. When rotating, the airfoils are moving through the air at differing speed, due to the fact that the distance traveled for one airfoil is along a difference circumferential path. This travel distance can be represented by the travel distance=2r.sup.2 where r is the distance of the airfoil from the hub. Because each airfoil can rotate about the cable independently, the angle of attack of each airfoil can decrease from the hub to the rim. Further, the airfoil section can be longer at the rim than the hub as the angle of attack dies not change as much the farther the distance from the hub (e.g. r). The angle of attack can stay relative the same while the pitch of each airfoil can vary from hub to rim.

(15) In operation, the rim can engage a generator wheel 24 of generator 26 so that rotational energy from the rim can be transferred to the generator wheel and therefore turn the generator to produce electricity.

(16) Referring to FIG. 3, an example of a section of an airfoil 40 is shown. The airfoil can include a leading edge 28 and a trailing edge 30. A cable opening 32 can be included in the airfoil to receive the cable and allow the airfoil to rotate about the cable. A forward opening 34 can be included and have a generally pyramid cross section and reduce the weight of the airfoil. A rear opening 36 can be included having a tear drop cross section. In one embodiment, the airfoil is symmetrical along bisect 38. In one embodiment, the trailing edge of the airfoil can include an upturned section 39 that can increase the camber line resulting in a high lift coefficient producing more rotational speed for the wind turbine. With this upturned section, the angle of attack can be less for the same amount of rotational force created. In one embodiment, the upturned section can be in the range of 5 degrees to 15 degrees.

(17) Referring to FIG. 4, one embodiment of the airfoil can include an upper surface 60 and a lower surface 62 having a cable opening 64 disposed in a space defined between the upper and the lower surface. Support ribs 66 can be disposed between the upper and lower surface to provide support and maintain the shaped of the airfoil. The cable opening can extend through one or more ribs. The end of the airfoil can be closed with an end cap 68. The ribs can include rib openings.

(18) Referring to FIG. 5, one embodiment of the airfoil 40 is shown carried by cable 16 so that the airfoil can rotate about the cable. A vane 42 can be attached to the airfoil extending toward the trailing edge and include a shaft 44 and fin 46. When the air flow in a direction shown as 48, the vane causes the leading edge to face the wind direction causing the airfoil to rotate toward the optimal angle of attack. As this configuration reacts to the relative wind direction, each airfoil along the cable may have a slightly different angle of attack providing an advantageous configuration of the plurality of airfoils along the cable. In one embodiment, the achieved angle of attack is in the range of 9 to 13 degrees. In one embodiment, the airfoil is in the range of 5 to 10 inches in width, 1 to 2 inches at its thickest portion and 8 to 12 feet in length. In one embodiment, the shaft is about 2 feet. The vane can be included in the end cap and on one or both ends of the airfoil.

(19) Referring to FIG. 6, a plurality of airfoils are shown carried by cable 16 wherein each airfoil can independent rotate about the cable 16. The airfoil can include an opening 32 (FIG. 2) that received the cables and attached the airfoil to the wind turbine. Given that each airfoil can have a different angle of attack, the airfoil assembly 50 can act as a blade with a twist. As each airfoil can rotate independently to each other, the airfoil assembly can result in a twist resulting from the true wind speed, a twist that is not possible with the transitional single blade. Therefore, an airfoil can automatically adjust to changes in the relative positions of the wind when the cable opening 32 location is placed between the leading edge and trailing edge allowing the airfoil to automatically position itself at an optimum angle of attack regardless of true wind or apparent wind direction.

(20) Referring to FIG. 7A, several airfoils are shown with airfoil 52a being positioned above airfoil 52b which it in turn positioned over airfoil 52c. Given that the vanes position each airfoil with different angles of attack, we see that .sub.a.sub.b.sub.c so that the assembly creates a twist along the length of the cable. In one embodiment, .sub.a, .sub.b, and .sub.c can all be positive relative to horizontal line 41. FIG. 5B shows the plurality of the airfoils superimposed as they would be along the cable.

(21) The invention can provide for automatic blade pitch control with no blade pitch drive system or software. The airfoil sections can automatically adjust to the optimum 80-foot blade twist. The automatic blade twist can also adjust itself for the true wind speed which current blades cannot do. Maintenance will be significantly less than what is required with the traditional designs. Completely changing an airfoil assembly will take significantly less time than current blade exchanges. Transportation of the wind turbine is simplified with a much more compact and simpler design that with the traditional blade systems. When parked, the airfoil assembly can accommodate higher wind than the traditional blade designs. When the wind turbine is parked, the airfoil assembly will provide no lift as the wind can automatically turns the wheel downwind from the mast since the airfoils can be configured so they can only rotate 90. The vane can be fixed to the airfoil, so it always keeps airfoil at an ideal angle of attack eliminating a blade pitch drive. When the capacity of the generator is reached, and the wind speed increases the electric output can be limited by yawing out of perpendicular to the sailets.

(22) Referring to FIGS. 8A and 8B, the mast 12 supporting the wind turbine support the hub. Cables extending between the hub and the rim 14 as shown carrying a plurality of airfoils. An inner set of cables can extend from the proximal end of the hub 70 to rim 14. An outer set of cables can extend from the distal end of the hub 72 to rim 14. A cable of the inner set of cables can include a set of inner airfoils 74 extending from the hub to the rim. An outer cable in the outer set of cables can include an outer set of airfoils 76 extending from the hub to the rim.

(23) Referring to FIG. 9, the airfoil 40 is shown rotatable carried by cable 16. An adjacent airfoil 80 is shown disposed closer to the hub with airfoil 40 disposed closer to the rim. When rotating, inertia forces due to the rotation of the turbine wheel force the airfoil toward the rim away from the hub. This force can cause adjacent airfoils to bind against each other and restrict the ability of the airfoil to rotates about the cable interfering with the airfoils ability to optimize the angle of attack. The airfoils can be separated from each other by gaps 82 that are created by a spacer assembly 84. The spacer assembly can be secured to the cable and prevents the airfoil inwardly adjacent to the spacer assembly from applying pressure to the outwardly adjacent airfoil. The spacer assembly can include an inward washer 82 that can include lubricity, high temperature tolerance, UV resistance, salt water resistance and crush resistance. In one embodiment, the lower washer can be made from polytetrafluoroethylene (PTFE). A cinch 84 can be can secured to a fixed position on the cable preventing the cinch from sliding along the cable. In one embodiment, the cinch can include two components that are placed on either side of the cable and secured together such as with screws that can extend through cinch openings 88. Therefore, when the lower adjacent airfoil 80 is force toward an upward adjacent airfoil, the cinch and washer prevent the lower adjacent airfoil from contacting the upper adjacent airfoil and therefore can prevent the airfoils from binding. The spacer assembly can include an upper washer 86 disposed between the cinch and the upper adjacent airfoil so that when the turbine wheel is as rest, the upper airfoil contacts the upper washer and not the cinch. In one embodiment, a resilient member such as a spring or other tensioned member can be disposed between the cinch and the lower washer or the lower washer and lower airfoil.

(24) Unless specifically stated, terms and phrases used in this document, and variations thereof, unless otherwise expressly stated, should be construed as open ended as opposed to limiting. Likewise, a group of items linked with the conjunction and should not be read as requiring that each and every one of those items be present in the grouping, but rather should be read as and/or unless expressly stated otherwise. Similarly, a group of items linked with the conjunction or should not be read as requiring mutual exclusivity among that group, but rather should also be read as and/or unless expressly stated otherwise.

(25) Furthermore, although items, elements or components of the disclosure may be described or claimed in the singular, the plural is contemplated to be within the scope thereof unless limitation to the singular is explicitly stated. The presence of broadening words and phrases such as one or more, at least, but not limited to or other like phrases in some instances shall not be read to mean that the narrower case is intended or required in instances where such broadening phrases may be absent.

(26) While the present subject matter has been described in detail with respect to specific exemplary embodiments and methods thereof, it will be appreciated that those skilled in the art, upon attaining an understanding of the foregoing may readily produce alterations to, variations of, and equivalents to such embodiments. Accordingly, the scope of the present disclosure is by way of example rather than by way of limitation, and the subject disclosure does not preclude inclusion of such modifications, variations and/or additions to the present subject matter as would be readily apparent to one of ordinary skill in the art using the teachings disclosed herein.