The subject matter of the present disclosure broadly relates to the art of energy conversion systems and, more particularly, to a wind turbine capable of converting wind energy into rotational mechanical energy, such as may be used to operate a generator to produce electrical energy, for example, as well as a method of operating a wind turbine.
The subject matter of the present disclosure finds particular application and use in connection with wind turbine, and is shown and described herein with preference thereto. It will be appreciated, however, that the subject matter of the present disclosure is amenable to use in a variety of other applications and/or environments, such as air moving devices (e.g., fans) and other power generation systems (e.g., turbines), for example. As such, it is to be understood that the specific reference herein to use on and/or in association with wind turbines is merely one example of such use not intended to be limiting.
Wind turbines are well known and commonly used to convert wind energy into rotational mechanical output that can be used for any suitable purpose, such as to operate a generating system or device for the production of electrical power, for example. Current wind turbine designs typically include a base structure that supports a turbine housing at a level that is elevated with respect to the surrounding geography (i.e., land surface or water level). In many constructions, two or more turbine blades are supported on a hub of the turbine housing. The hub is capable of rotating in response to air currents (i.e., wind) that are acting on the blades. In this manner, wind energy can be converted to rotational mechanical energy for electrical power generation and/or other purposes.
Notwithstanding the overall success of modern wind turbine designs, one or more characteristics have been observed that may operate to limit the application and/or use of wind turbines. These characteristics may also reduce the overall cost effectiveness of wind turbines under certain conditions. As such, these issues may lead to a reduction in the installation and use of wind turbines, where increased installation and usage might be preferred.
One such characteristic involves the conditions of operation of wind turbines. That is, there are known to be minimum and maximum wind speed thresholds outside of which operation of a wind turbine is generally avoided. Of course, these minimum and maximum wind speed thresholds will vary from wind turbine to wind turbine and from situation to situation.
At one extreme, it is generally acknowledges that there is a minimum wind speed at which a wind turbine can effectively operate. In many cases, the minimum wind speed is within a range of from about 5 MPH to about 8 MPH. As such, wind turbines often remain idle in light wind conditions.
At the opposite extreme, it is generally recognized that there is a maximum wind speed at which a wind turbine may be operated. Often, the maximum wind speed is greater than 50 MPH. As expected, the maximum wind speed threshold will relate to the design and construction of the wind turbine as well as the operational limitations of the electrical components driven by the turbine. Nonetheless, wind turbines are commonly stopped during high wind conditions.
It is believed desirable to develop a wind turbine and method of operation that overcomes these and/or other disadvantageous characteristics of known wind turbines and that can operate under a greater range of wind speeds and/or conditions.
One example of a wind turbine in accordance with the subject matter of the present disclosure can include a base structure and a turbine body that includes first and second body portions. The first body portion is supported on the base structure and includes a first axis extending longitudinally along the first body portion. The second body portion is supported on the first body portion for rotation about the first axis. A turbine blade assembly is supported on the second turbine body for rotation therewith about the first axis. The turbine blade assembly includes a turbine blade that has a longitudinal length, a first longitudinal edge, a second longitudinal edge spaced laterally from the first longitudinal edge, a first side extending longitudinally along at least a portion of the length between the first and second longitudinal edges, and a second side extending longitudinally along at least a portion of the length between the first and second longitudinal edges and generally opposite the first side. The turbine blade includes a proximal end operatively connected to the second turbine body and a distal end spaced radially-outwardly from the proximal end. A first endless band includes a first outer surface and a first band width. The first endless band is oriented such that the first band width extends longitudinally along the turbine blade. The first endless band is supported on the turbine blade such that the first outer surface is exposed along at least a portion of at least one of the first and second sides of the turbine blade and is capable of lateral movement along the at least one of the first and second sides. In this manner, a relative velocity can be maintained between the first outer surface and the at least one of the first and second sides of the turbine blade.
One example of a wind turbine blade assembly in accordance with the subject matter of the present disclosure can include a wind turbine blade and an endless band. The wind turbine blade includes a longitudinal length extending between opposing first and second ends, a first edge extending longitudinally along the blade, a second edge extending longitudinally along the blade in laterally spaced relation to the first edge, a first side extending longitudinally along the blade and laterally between the first and second edges, and a second side extending longitudinally along the blade and laterally between the first and second edges generally opposite the first side. The first endless band includes a first outer surface and a first band width. The first endless band being oriented such that the first band width extends longitudinally along the blade. The first endless band being supported on the blade such that the first outer surface is exposed along at least a portion of at least one of the first and second sides of the blade and is capable of lateral movement along the at least one of the first and second sides such that a first relative velocity can be maintained between the first outer surface and the at least one of the first and second sides of the blade.
One example of a method of operating a wind turbine in accordance with the subject matter of the present disclosure can include providing a wind turbine and providing an endless band. The wind turbine can include a base structure, a turbine body supported on the base structure and at least one turbine blade. The turbine body can have a longitudinal-extending turbine body axis, and the at least one turbine blade can be supported on the turbine body for rotation about the turbine body axis. The at least one turbine blade includes a longitudinal length extending between opposing first and second ends, a first edge extending longitudinally along the blade, a second edge extending longitudinally along the blade in laterally spaced relation to the first edge, a first side extending longitudinally along the blade and laterally between the first and second edges, and a second side extending longitudinally along the blade and laterally between the first and second edges generally opposite the first side. The endless band includes a first outer surface and a first band width. The method also includes orienting the endless band such that the first band width extends longitudinally along the blade and supporting the endless band on the blade such that the first outer surface is exposed along at least a portion of at least one of the first and second sides of the blade. The method further includes driving the at least one endless band such that the outer surface moves laterally along at least one of the first and second sides of the blade between the first and second edges thereof.
Referring now in greater detail to the drawings, it is to be understood that the illustrations reference herein are for the purposes of demonstrating examples of embodiments of the subject matter of the present disclosure and that these illustrations and examples are not intended to be in any way limiting. Additionally, it should be recognized and appreciated that the drawings are not to scale and that the proportion of certain features and/or elements may be exaggerated for purposes of clarity and ease of understanding.
Support or base structure 102 is shown in
Base structure 102 is shown in
Turbine body 104 includes a first or front end 112, a second or tail end 114 and a longitudinal axis AX2 that extends generally between front and tail ends 112 and 114. As shown in
Turbine body 104 also includes a first body portion 116 that is supported on the base structure for rotation about axis AX1, as described above, and a second body portion 118 that is supported on the first body portion for rotation about axis AX2. It will be appreciated that second body portion 118 can be supported on first body portion 116 in any suitable manner, such as may be known by those of skill in the art.
With further reference to
Turbine blade assemblies 106 extend radially-outwardly from second body portion 116 between a first or proximal end 120 and a second or distal end 122. A longitudinal axis AX3 extends generally between the proximal and distal ends. In one preferred embodiment, the turbine blade assemblies are supported on second body portion 116 for rotation about axis AX3 respectively of each turbine blade assembly, as is generally indicated by arrows RT3 in
It will be recognized that turbine blades of a wide variety of different sizes, shapes, configurations and constructions have been developed, and that all such variations could not be shown and/or described in the subject disclosure. For example, turbine blades have been developed that include straight edges, tapered edges, curved edges, approximately planar sides, curved sides, symmetrically-shaped sides and asymmetrically-shaped sides. Additionally, many blades are twisted along the longitudinal length thereof such that the wind contacts the turbine blade at different angles at different points along the longitudinal extent of the turbine blade. Notwithstanding all of the many variations of turbine blades, it is to be understood that the subject matter of the present disclosure is broadly capable of use on or otherwise in association with turbine blades of any suitable type, kind, configuration and/or construction. As such, it is to be understood that the type, kind, size, shape, construction, configuration and/or arrangement of turbine blades shown and described herein are merely exemplary and not intended to be limiting.
A turbine blade assembly in accordance with the subject matter of the present disclosure, such as one of turbine blade assemblies 106, for example, includes a turbine blade and at least one surface that is disposed along at least one side of the turbine blade and is moveable relative to the side of the blade such that the relative speed of the moveable surface with respect to the wind is different than the relative speed of the side of the turbine blade would be at that same longitudinal location. In
Turning, now, to
Turbine blade 202 further includes opposing first and second sides 212 and 214 (
As mentioned above, a turbine blade assembly in accordance with the subject matter of the present disclosure includes at least one surface that is moveable in an approximately lateral direction along a side of the turbine blade. It will be appreciated that any suitable number of one or more moveable surfaces can be used, such as from one (1) to fifty (50) different surfaces, for example. Additionally, it will be appreciated that the at least one moveable surface can take any suitable form, configuration and/or construction and can be of any suitable size and/or shape that may be cooperative with the turbine blade on which the at least one moveable surface is operatively supported. As one example, the at least one moveable surface can take the form of at least one endless band that is operatively supported on the turbine blade for movement in an approximately lateral direction along at least one side of the turbine blade.
In the exemplary embodiment shown in
It will be appreciated that the influence a given moving surface may have on a turbine blade will vary depending upon the position of the moving surface along the longitudinal length of the turbine blade. This is due, at least in part, to the increased distance from axis Ax2 at which force variations attributable to the moving surface will act on the turbine blade. In one exemplary embodiment of a turbine blade assembly, the one or more moving surfaces could be provided along only a portion of the longitudinal length of the turbine blade, such as along the outermost one-third of the blade, for example. As another exemplary embodiment of a turbine blade assembly, a plurality of moving surfaces could be spaced longitudinally along the turbine blade with one or more dimensions (e.g., length and/or width) of the moving surfaces decreasing in the direction of the distal end of the turbine blade.
If one or more endless bands are used to form the at least one moving surface on the turbine blade, as illustrated in
One exemplary arrangement is shown in greater detail in
Another example of a support element that may be suitable for use in supporting an endless belt includes a plurality of bearing elements 222 spaced longitudinally along an edge of the turbine blade, such as along trailing edge 210, for example. In one exemplary arrangement, the plurality of bearing elements can be approximately aligned with fixed portions 224 of the turbine blade so that the plurality of bearing element together with the fixed portions at least partially form trailing edge 210. As one example, a plurality of wheels or roller elements could be longitudinally spaced along the leading or trailing edge of the turbine blade. Such a plurality of wheels or roller elements could rotate independently of one another to permit endless belts of a non-uniform length to be laterally conveyed about the turbine blade. As another example, plurality of bearing elements 222 can include one or more longitudinally-extending rows of spherical bearings 226 (i.e. ball bearings) that are suitably retained on the turbine blade, such as by using a ball bearing cage or other structure (not shown), for example.
The one or more endless bands (e.g., endless bands 216A-F) can be moved or otherwise conveyed along the one or more sides of the turbine blade in any suitable manner, such as by using one or more rotational motions sources operatively connected to the endless bands. As one example, a single drive shaft could extend longitudinally outwardly along the length of the turbine blade. The single drive shaft could be operatively connected to a drive element suitable for conveying the endless bands in a substantially synchronous manner. As another example, a plurality of motors or other rotational motion sources could be supported in longitudinally-spaced relation along the length of the turbine blade. Each of the plurality of motors could be operatively connected to a drive element suitable for conveying one or more of the endless bands. In such an arrangement, one or more of the endless bands could be independently controlled from the remaining one or more endless bands. As shown in
In the exemplary arrangement shown in
As indicated in
In the exemplary arrangement shown in
Another example of a turbine blade assembly 300 is shown in
Turbine blade assembly 300 also includes at least one surface that is moveable in an approximately lateral direction along a side of the turbine blade. As shown in the exemplary arrangement in
Endless bands 316A-F are shown extending between laterally spaced-apart support elements that permit the endless bands to be conveyed or otherwise moved with respect to one or more of the first and second sides of the turbine blade. As one example, the endless bands could be supported between rollers 318 and 320. Roller 318 drivably engaging the endless bands toward the leading edge of the turbine blade assembly and roller 320 being freely rotating to permit displacement of the endless band thereabout. It will be appreciated that cylindrical rollers, which are shown in
Rollers 318 or other support elements that may be suitable for drivably engaging one or more of endless bands 316A-F can be operatively connected to a rotational motion source in any suitable manner. As one example, one or more electric motors could be longitudinally spaced along the length of the turbine blade and operatively connected to one or more of the drive elements. As another example, a drive shaft 322 or other rotational motion source could extend longitudinally outwardly along the length of the turbine blade and be operatively connected to one or more of the drive elements (e.g., roller 318), such as by way of a suitable transmission element 324 (e.g., a transmission belt or gear set).
First side 312 of turbine blade 302 also includes first and second laterally-spaced openings 326 and 328. Similarly, second side 314 of the turbine blade includes first and second laterally-spaced openings 330 and 332. During operation, endless band 316F is conveyed around drive roller 318 and the first opening in one of the first and second sides, depending upon the direction in which the endless band is being displaced. The endless band is further displaced along the corresponding side of the turbine body and returns toward support roller 320 through the second opening in that first or second side. The endless band would continue to be displaced around support roller 320 and exit from the second opening in the opposing one of the first and second sides. The endless band is then further displaced along that opposing side toward the first opening therein through which the endless band returns to be drivably engaged by drive roller 318. It will be recognized that similar openings are provided along both sides of the longitudinal length of the turbine blade such that the one or more other endless bands can be similarly convey along at least a portion of the sides of the turbine blade.
Additionally, or in the alternative, a turbine blade assembly, such as turbine blade assembly 106, 200 and/or 300, for example, can optionally include a first endless band operatively disposed along a first side of the turbine blade and a second endless belt that is operatively disposed along a second side of the turbine blade.
Turbine blade assembly 400 also includes a first endless band 412 operatively disposed for movement along first side 408. It will be appreciated that first endless band 412 can be supported between laterally-spaced support elements, such as rollers 414 and 416. Additionally, roller 414 can be operatively connected to a suitable rotational motion source 418 (e.g., an electric motor or drive shaft), such as by way of a suitable transmission element 420 (e.g., a transmission belt or gear set). First side 408 can be adapted to permit egress and return of endless band 412, such as has been discussed above with regard to first side 312, for example.
Turbine blade assembly 400 further includes a second endless band 422 that is operatively disposed for movement along second side 410 of turbine blade 402. Second endless band 422 can be similarly supported for movement between laterally-spaced support elements, such as rollers 424 and 426, for example. Roller 424 can be operatively connected to a suitable rotational motion source, such as rotational motion source 418 by way of a separate transmission element, for example. Alternately, roller 424 could be operatively connected to a separate rotational motion source 428 (e.g., an electric motor or drive shaft), such as by way of a suitable transmission element 430 (e.g., a transmission belt or gear set). Second side 410 can also be adapted to permit egress and return of endless belt 422, such as has been discussed above with regard to second side 314, for example.
Though not shown in the drawings, it will be appreciated that any suitable number of endless bands, such as from one (1) to fifty (50), for example, could be longitudinally-spaced along the first and/or second sides of a turbine blade. Additionally, it will be appreciated that any combination of quantity, width, length and/or configuration of endless bands could be used.
The at least one moveable surface operatively disposed on or along a turbine blade, such as one of endless bands 126, 216A-F, 316A-F, 412 and/or 422, for example, can be formed from any suitable material or combination of materials, such as metal, plastic and/or fabric, for example. Metal material could include stainless steel sheet, for example. Plastic material could include any suitable polymeric film, such as polyester film, for example. Fabric material could include any suitable elastomeric or non-elastomeric, woven or non-woven material having one or more plies formed of filaments of one or more types and/or kinds of material.
Reference is now made to the general operation and use of a turbine blade assembly in accordance with the subject matter of the present disclosure that includes a turbine blade and at least one moveable surface supported on or along at least one side of the turbine blade. As mentioned above, turbine blades are typically disposed at an angle relative to the wind direction. This angle is often referred to in the art as the angle of attack and is represented in
It will be appreciated, however, that in current turbine blade designs, forces attributable to or otherwise associated with the angle of attack represent only a portion of the overall forces acting on a turbine blade. Another portion of the overall forces acting on a turbine blade are attributable to the use of turbine blades having an airfoil design or cross-section. As is well understood in the art, air currents flowing past a turbine blade having an airfoil design will generate a first air pressure acting on one side and a second, different air pressure acting on the opposing side of the turbine blade. The generation of these two different air pressures is generally believed to be due to air flowing across the two different sides of the turbine blade at two different speeds, as is well understood in the art. Accordingly, the air flowing at a first speed (e.g., a higher speed) across one side of the turbine blade would be expected to generate a different pressure (e.g., a lower pressure) on the surface than the air flowing at a second speed (e.g., a lower speed) across the opposing side of the turbine blade (e.g., a higher pressure side). As a result, one side of the turbine blade is often referred to as the pressure side of the turbine blade with the opposing side being referred to as the suction side.
Forces due to differential air pressures acting on a turbine blade (i.e., aerodynamic forces other than those associated with the angle of attack) can also be resolved into a first directional component that acts in the direction of the wind and a second directional component that acts approximately transverse (e.g., perpendicular) to the first directional component. It is generally desirable to orient a turbine blade such that the portion of the force attributable to the angle of attack (i.e., the second directional component thereof) and the portion of the force attributable to differential air pressures (i.e., the second directional component thereof) are acting in the same direction to cause displacement of the turbine blade about the axis of rotation.
Generally, it will be appreciated that the at least one moveable surface supported on a turbine blade is capable of displacement in either of two lateral directions with respect to the side of the turbine blade. One such lateral direction will be approximately the same as the direction in which the air current (i.e., the wind) is flowing. The second lateral direction will be generally opposite the direction in which the air current (i.e., the wind) is flowing. Displacement of the at least one moveable surface along a side of a turbine blade will increase or decrease the overall force acting on the turbine blade depending upon which direction (i.e., with the wind or against the wind) the at least one moveable surface is being displaced. The change in the overall force acting on the turbine blade will also depend upon whether the at least one surface is being displaced along the pressure side, the suction side or both sides, and which direction the at least one surface is being displacement on that side (or along those sides).
As a more specific example, endless band 216F is shown in
For purposes of illustration and ease of understanding, the forces attributable to the operation of the one or more moveable surfaces are shown in
Due to the displacement of the surface of the endless belt in first direction DIR1, the increase in force attributable to the displacement of the moveable surface, the portion of the force attributable to differential air pressures and the portion of the overall force attributable to the angle of attack are all acting in the same direction to cause displacement of the turbine blade about the axis of rotation. The increased force due to the sum of these directional components will generate a corresponding increase in torque at second body portion 118 (
Additionally, it will be appreciated that the one or moveable surfaces can be selectively operated to vary the magnitude and/or direction of the additional force acting on the turbine blade. It will be recognized that the distal end of a conventional turbine blade moves at a greater instantaneous linear velocity than does the proximal end of the turbine blade. As one example, one or more of the endless bands (e.g., endless bands 216A-F, 316A-F, 412 and/or 422) could be operated at surface speeds that decrease with outward longitudinal position along the turbine blade, such as to balance the forces acting on the turbine blade, for example. As another example, one or more of the endless bands could be operated at surface speeds that increase with outward longitudinal position along the turbine blade, such as to offset any change in effective wind direction due to the movement of the turbine blade. As a further example, one or more of the endless bands could be selectively operated such that some bands are displaced and other bands remain stationary, such as to minimize maintenance and repair cost while obtaining benefits associated with the use of the one or more moveable surfaces.
Returning to the previous example, endless band 216F is also shown in
It will also be appreciated that first directional force component FBD, which acts in the direction of the wind, can be accommodated in any suitable manner. As one example, the structure of a turbine blade, as well as the turbine body on which the turbine blade is supported, could simply be manufactured to be more robust to accommodate such increased load conditions. As another example, a blade support assembly or other structure could be provided to buttress the one or more turbine blade assemblies of the wind turbine. One example of a blade support assembly could include support structure that is operatively connected to the base structure and/or turbine body and a bearing structure that is supported on the support structure and is adapted to operatively engage the one or more turbine blade assemblies of the wind turbine.
In the arrangement shown in
Blade support assembly 128 can also, optionally, include one or more bearing elements that are supported on the one or more turbine blade assemblies and act to abuttingly engage the bearing structure and thereby minimize or at least reduce frictional losses between the bearing structure and the turbine blade assemblies, as the same rotate about axis AX2. The one or more bearing elements are schematically represented in
As another example, a magnetic bearing arrangement could be used to maintain the turbine blade assemblies in spaced relation to the bearing structure. In one exemplary arrangement, one or more magnets (not shown), such as permanent magnets and/or electromagnets, for example, could be supported on each of the turbine blade assemblies. A corresponding one or more magnets (not shown), such as permanent magnets and/or electromagnets, for example, could be disposed along bearing structure 132. In a preferred arrangement, at least the magnets disposed along the bearing structure are electromagnets that can be selectively operated by a suitable control system 136. Such a control system could be disposed in electrical communication with the electromagnets in any suitable manner, such as by way of electrical conductor 138, for example.
Method 500 further includes displacing the at least one moveable surface in one of the first and second lateral directions DIRSF and at a surface speed SPDSF, as is represented by box 506 in
As such, method 500 can also, optionally, include determining the wind conditions under which the wind turbine will be operating, as is represented by box 508 in
One example of a plurality of actions that could be used to make a determination of operating parameters, as is represented by reference number 510, is shown in
If a NO determination is made at box 512, however, the current wind speed conditions are above the theoretical minimum wind speed. As such, a further inquiry can be made as to whether wind speed condition WSP is greater than the theoretical maximum wind speed condition WMAX, as is indicated in decision box 518. IF a YES determination is made at box 518, the current wind speed conditions are above the theoretical maximum wind speed for operation of the wind turbine. In such case, direction of movement DIRSF of the at least one surface is determined to be second direction DIR2, as is represented by box 520. In a preferred arrangement, second direction DIR2 will correspond to movement of the surface in a direction with the wind on the pressure side of a turbine blade and/or in a direction opposite the wind on the suction side of a turbine blade. As discussed above, this expected to decrease the force acting on the turbine blade, which may permit the wind turbine to operate under wind speed conditions above the theoretical maximum wind speed. Again, a determination of a suitable surface speed SPDSF can optionally be made, as is represented by box 522. Thereafter, method 500 proceeds with displacement of the at least one moveable surface in the direction of movement and, optionally, at the surface speed that has been previously determined, as is indicated by box 506.
If a NO determination is made at box 518, the current wind speed conditions are within the desired range for operation of the wind turbine. In such case, direction of movement DIRSF of the at least one surface is determined to be first direction DIR1, as is represented by box 524. As described above, first direction DIR1 will preferably correspond to movement of the surface in a direction opposite the wind on the pressure side of a turbine blade and/or in a direction with the wind on the suction side of a turbine blade. This is expected to increase the force acting on the turbine blade, which may permit the wind turbine to generate greater output or provide other desirable operational and/or performance characteristics. Optionally, a determination of a suitable surface speed SPDSF could also be made, as is represented by box 526. Thereafter, method 500 proceeds with displacement of the at least one moveable surface in the direction of movement and, optionally, at the surface speed that has been previously determined, as is indicated by box 506.
While the subject matter of the present disclosure has been described with reference to the foregoing embodiments and considerable emphasis has been placed herein on the structures and structural interrelationships between the component parts of the embodiments disclosed, it will be appreciated that other embodiments can be made and that many changes can be made in the embodiments illustrated and described without departing from the principles hereof. Obviously, modifications and alterations will occur to others upon reading and understanding the preceding detailed description. Accordingly, it is to be distinctly understood that the foregoing descriptive matter is to be interpreted merely as illustrative of the subject matter of the present disclosure and not as a limitation. As such, it is intended that the subject matter of the present disclosure be construed as including all such modifications and alterations insofar as they come within the scope of the appended claims and any equivalents thereof.
This application is a continuation-in-part of U.S. application Ser. No. 12/157,104, filed on Jun. 5, 2008, which claims the benefit of U.S. Provisional Application Ser. No. 60/933,325, filed Jun. 6, 2007, the subject matter of each of which is hereby incorporated herein by reference in its entirety. U.S. Pat. Nos. 6,322,024 and 6,824,109, both to the inventor of the present application, disclose the use of moving bands in connection with fixed wing aircraft. The entire disclosure of each of these documents is hereby incorporated herein by reference.
Number | Date | Country | |
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60933325 | Jun 2007 | US |
Number | Date | Country | |
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Parent | 12157104 | Jun 2008 | US |
Child | 12372371 | US |