WO2005111413A1 - Wind turbine rotor projection - Google Patents

Wind turbine rotor projection Download PDF

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Publication number
WO2005111413A1
WO2005111413A1 PCT/CA2005/000766 CA2005000766W WO2005111413A1 WO 2005111413 A1 WO2005111413 A1 WO 2005111413A1 CA 2005000766 W CA2005000766 W CA 2005000766W WO 2005111413 A1 WO2005111413 A1 WO 2005111413A1
Authority
WO
WIPO (PCT)
Prior art keywords
wind
turbine
rotor
wind turbine
blades
Prior art date
Application number
PCT/CA2005/000766
Other languages
French (fr)
Inventor
Bud T. J. Johnson
Original Assignee
Envision Corportion
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Envision Corportion filed Critical Envision Corportion
Priority to CA002567174A priority Critical patent/CA2567174A1/en
Priority to JP2007516914A priority patent/JP2007538189A/en
Priority to AU2005243553A priority patent/AU2005243553A1/en
Priority to EP05745332A priority patent/EP1766230A1/en
Priority to US11/569,340 priority patent/US7726935B2/en
Publication of WO2005111413A1 publication Critical patent/WO2005111413A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/04—Wind motors with rotation axis substantially parallel to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D3/00—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/10—Stators
    • F05B2240/12—Fluid guiding means, e.g. vanes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/74—Wind turbines with rotation axis perpendicular to the wind direction

Definitions

  • the inventor has studied examples of present state of the art wind turbines of the propeller type, in particular, as they are now in common use. At their apparently low levels of efficiency, another approach had to be made, to better utilize presently well known and commonly applied principles of fluid mechanics and aerodynamics, to improve our ability to extract maximum energy potential from the wind.
  • First is the matter of concentrating wind pressure over the entire addressable frontal exposure of its turbine blades, and directing all of the available wind energy toward driving the turbine blades.
  • Second is to have the main driven surfaces of its turbine blades situated within the outer thirty percent of the radius between axle center and the outer tips of its turbine blades. This feature greatly increases torque, and ultimate recovery of energy.
  • the first improvement over present state of the art is the matter of concentrating the wind energy driving force within the outer 30 percent of the radius between axle center and the outer tips of our turbine rotor blades.
  • a half sphere shape including the outer surface of the turbine rotor extends forward from the rear of the turbine rotor, in line with axle center, and displaces more than seventy percent of the frontal area of the wind turbine.
  • a second improvement is achieved by deployment of the said half sphere shape, including the outer face of the turbine rotor, centered in line with axle center, beginning at the rear face of the said rotor, and extending forward of the turbine rotor from axle center, to front dead center of the said half sphere shape.
  • the portion of the said half sphere shape extending forward from the turbine rotor is mounted in a fixed stationary position, and does not rotate.
  • This increases incoming wind speed as the wind spreads over the said half sphere shape, and that is a common principle of physics.
  • the wind speed increase lowers the operating wind speed threshold quite significantly, as a clear advantage over present state of the art.
  • the wind speed increase at the surface of the said half sphere shape is % C x R, and that ratio is 1.5707 to 1. That figure is reduced due to surface tension, drag, or friction against flow, and the well known system referred to as Reynolds numbers could be used to determine the approximate drag factor.
  • the inventor's engineering consultants suggest that the net velocity increase is 46%, and the resulting increase in available kinetic energy amounts to 1.46 cubed, or 311%.
  • the third improvement over present state of the art is the matter of using as many as twenty four comparatively short and properly curved turbine blades of adequate front to back depth, and pitch angle, to achieve maximum torque drive, and further assure that no wind is going to get past the blades, and must drive them all. Blade length must be adequate to catch or encounter all of the wind mass that has been speeded up. This consideration should be rather exact, as a blade length reaching beyond the faster moving wind mass, is going to be entering a slower moving wind mass, which will create drag, resulting in some efficiency loss. This situation provides maximum capture of wind energy, which is converted to the highest amount of torque at our driven axle.
  • a fifth, or further potential improvement over present state of the art is the placement of a series of radially and evenly spaced thin airfoils on the periphery of the stationary forward portion of the half sphere, beyond the turbine rotor.
  • the said airfoils would curve incoming wind in a spiral fashion around the half sphere stationary head, in the same direction that the turbine rotor is turning.
  • the advantage to be gained is that a more open turbine blade pitch can be used with much the same effect as a more closed off blade pitch. This can eliminate the necessity for mechanical means of changing blade pitch when higher speed winds are encountered.
  • the blade pitch is an average of forty degrees
  • the said airfoils can be retracted inward, to zero effect, and the wind turbine rotor blades will then operate at their forty degree pitch.
  • the airfoils can also be made of flexible material which can be progressively curved or bent like a spring. In that case the airfoils would not be retractable, and would remain in place at zero curvature, longitudinally, which would be much the same as being retracted to the point of no affect.
  • the said airfoils are an improvement over present state of the art, where mechanical means are used to vary blade pitch to access incoming wind more efficiently and safely, and to go to neutral, in the case of excessive wind speeds.
  • mechanical pitch control or failure of a governor system could lead to serious damage to the wind turbine.
  • Figure 1 is a side view of a preferred embodiment of the invention, as mounted on the rotatable top of its support tower platform, with turbine rotor and 24 rotor blades.
  • the turbine rotor has a curved face, being the rearward portion of what would be a completed half sphere shape, including a stationary front portion, separately supported, and mounted closely in front of the said turbine rotor.
  • a close general outline of the outside edge of the path of the wind mass displaced by the spherical head is shown in its broadening arc form, and as it would address a complete cross section of the blades of the wind turbine. This is shown as a broken line arc, from the front center of the stationary portion of the spherical head shape, to the outer tips of the turbine rotor blades.
  • Figure 2 is a frontal view of the same preferred embodiment of the invention, as mounted on the rotatable top of its support tower platform, with turbine rotor and 24 rotor blades.
  • Figure 3 is a side view of the wind turbine, showing relative positions of 12 curved airfoils on the stationary frontal projection of its spherical head, which can be recessed to full closure, and zero effect. They would serve the purpose of curving the oncoming direction of the wind, in the rotational direction of the turbine rotor blades, to add the effect of 20 or more degrees to fixed turbine rotor blades for the purpose of eliminating any necessity for pitch control.
  • Figure 4 is a frontal view of the wind turbine, showing relative positions of the same 12 curved airfoils as illustrated in figure 3.
  • Figure 1 is a side view of a preferred embodiment of the invention, as mounted on the rotatable top of its support tower platform, where we have the stationary portion of its spherical head 1 , and the rotating portion of its spherical head 2, which is also the outer facing of its rotor 3.
  • airfoil shaped structural support beams 8 for the stationary portion of its spherical head section and its front end axle bearing, then we have the stationary portion of its structural support tower (column) 9, and broken line representing the outer periphery of the volume expansion area of wind displaced by the said spherical head 10, and undulating lines 11, to indicate turbulence expected behind turbine rotor 3, which would be common to exhausted wind behind the blades of the wind turbine.
  • Figure 2 is a frontal view of the wind turbine, showing the stationary front section of the half sphere shape 1 , rotating curved outer circumferential surface 2, of turbine rotor 3, being the remainder of the said half sphere shape. Then we have turbine blades 4, of which there are twenty four in this embodiment. Also shown are support struts 8, for the stationary frontal portion of the said half sphere shape and front axle bearing, and rotatable top base mount 7, for the wind turbine, and then stationary support tower 9, which would extend to ground level.
  • Figure 3 is an angularly offset side view of another preferred embodiment of the wind turbine, showing relative positions of twelve comparatively thin and retractable airfoils 12, placed upon and within the stationary frontal projection 1, of the half spherical shape of more than seventy percent of the radius from axle center to the inside edges or bottom ends of its comparatively short turbine blades 4.
  • the conical projection of its rear body or encasement 5, segmented, as may be necessary for purposes of efficient manufacturing of such projection and then the somewhat cylindrical and aerodynamically shaped lower extension 6, of its outer body and wall surrounding its supporting structural elements and internal entry port, and extending downward to its rotatable base 7, on top of its supporting tower structure 9.
  • Figure 4 is a direct frontal view of the same preferred embodiment as described in figure 3, where we can observe curved retractable airfoils 12, and their relationship to the turbine blades 4, and we can further see the essential struts 8, supporting the front axle bearing of the turbine, and carrying the stationary frontal portion of half spherical shape 1 , at the front of the wind turbine. Then we can see further the aerodynamically shaped front end of the bottom extension of the rear housing or embodiment of the wind turbine 6, and then we have rotatable base support 7, and stationary support tower 9.

Abstract

An horizontal axis wind turbine having a rotor (3) with a frontal projection comprising a stationary spherical head (1) upstream of its multibladed turbine rotor (3) displaces and increases the speed of wind addressed over 70% of the total frontal area. A series of thin airfoils (12) radially and evenly placed on said spherical haead (1) to direct wind towards the turbine short blades (4).

Description

WIND TURBINE SPEEDBALL CONFIGURATION BACKGROUND OF THE INVENTION
The inventor has studied examples of present state of the art wind turbines of the propeller type, in particular, as they are now in common use. At their apparently low levels of efficiency, another approach had to be made, to better utilize presently well known and commonly applied principles of fluid mechanics and aerodynamics, to improve our ability to extract maximum energy potential from the wind.
Based on principles of physics and aerodynamics known to the inventor, some serious possibilities were apparent, with numerous novel ways and means of embodying what he has seen as the best combinations of those principles to apply toward greater efficiency in the capture of wind energy. At the present time, there is a fast growing demand for electrical energy in particular, to be produced by means which do not damage the environment. This situation now provides adequate incentive toward the invention and development of wind power based generation of electrical energy, where individual unit capacity might range from a low of 20 kilowatts to as much as 5 megawatts per single unit. OBJECTS OF THE INVENTION
The objects of this invention are as follows:
First is the matter of concentrating wind pressure over the entire addressable frontal exposure of its turbine blades, and directing all of the available wind energy toward driving the turbine blades.
Second is to have the main driven surfaces of its turbine blades situated within the outer thirty percent of the radius between axle center and the outer tips of its turbine blades. This feature greatly increases torque, and ultimate recovery of energy.
Thirdly, since usual present state of the art wind turbines are quite limited as to being able to provide useable power output at wind speeds below 15 kilometers
(9.32 miles) per hour, it is of great advantage to be able to significantly increase oncoming wind speed, to lower the bottom threshold of the operating wind speed range of the wind turbine. The affect of a wind speed increase is cubic in nature, greatly increasing available kinetic energy (wattage per square meter).
Fourthly, it would be desirable to create or generate a continuously increasing vacuum or a lower pressure induction area behind the turbine blades.
Fifthly, there would be serious advantage in being able to create the effect of coarser pitch of and to the turbine blades without having to apply any mechanical devices to the rotor or drive axle of the wind turbine. BASIC DESCRIPTION AND IMPROVEMENTS OVER PRESENT STATE OF THE ART
Based on the objects of this invention, the first improvement over present state of the art is the matter of concentrating the wind energy driving force within the outer 30 percent of the radius between axle center and the outer tips of our turbine rotor blades. A half sphere shape including the outer surface of the turbine rotor, extends forward from the rear of the turbine rotor, in line with axle center, and displaces more than seventy percent of the frontal area of the wind turbine.
A second improvement is achieved by deployment of the said half sphere shape, including the outer face of the turbine rotor, centered in line with axle center, beginning at the rear face of the said rotor, and extending forward of the turbine rotor from axle center, to front dead center of the said half sphere shape. The portion of the said half sphere shape extending forward from the turbine rotor, is mounted in a fixed stationary position, and does not rotate. The remainder, continuing rearward, as it represents the outer surface of the turbine rotor, rotates as part of the said rotor. This increases incoming wind speed as the wind spreads over the said half sphere shape, and that is a common principle of physics. The wind speed increase lowers the operating wind speed threshold quite significantly, as a clear advantage over present state of the art. The wind speed increase at the surface of the said half sphere shape is % C x R, and that ratio is 1.5707 to 1. That figure is reduced due to surface tension, drag, or friction against flow, and the well known system referred to as Reynolds numbers could be used to determine the approximate drag factor. The inventor's engineering consultants suggest that the net velocity increase is 46%, and the resulting increase in available kinetic energy amounts to 1.46 cubed, or 311%.
The third improvement over present state of the art, is the matter of using as many as twenty four comparatively short and properly curved turbine blades of adequate front to back depth, and pitch angle, to achieve maximum torque drive, and further assure that no wind is going to get past the blades, and must drive them all. Blade length must be adequate to catch or encounter all of the wind mass that has been speeded up. This consideration should be rather exact, as a blade length reaching beyond the faster moving wind mass, is going to be entering a slower moving wind mass, which will create drag, resulting in some efficiency loss. This situation provides maximum capture of wind energy, which is converted to the highest amount of torque at our driven axle. It will also be of some further advantage to indent the surface of the stationary spherical head, in front of the turbine rotor, much the same as a golf ball. This could significantly reduce surface tension, resulting in a smoother and faster expanding arc of accelerated wind mass to drive the turbine blades. The fourth improvement over present state of the art is where we now have as many as twenty four turbine blades which are generating a significant vacuum induction effect behind the said blades. Three bladed propeller types of wind turbines of present state of the art, are only doing so by means of three blades. In the case of this invention, we are gaining the effect of twenty four blades rather than three blades, and further enhancing the advantage, by assuring there is no effective open area between the blades where that vacuum induction effect can be broken, diminished or lost.
A fifth, or further potential improvement over present state of the art is the placement of a series of radially and evenly spaced thin airfoils on the periphery of the stationary forward portion of the half sphere, beyond the turbine rotor. The said airfoils would curve incoming wind in a spiral fashion around the half sphere stationary head, in the same direction that the turbine rotor is turning. The advantage to be gained, is that a more open turbine blade pitch can be used with much the same effect as a more closed off blade pitch. This can eliminate the necessity for mechanical means of changing blade pitch when higher speed winds are encountered. For example, if the blade pitch is an average of forty degrees, we can curve the wind coming over the stationary portion of the spherical head by twenty degrees in the direction of rotation, and the turbine blades will operate as though they had a coarser pitch. In the case of rather high wind speeds, the said airfoils can be retracted inward, to zero effect, and the wind turbine rotor blades will then operate at their forty degree pitch. The airfoils can also be made of flexible material which can be progressively curved or bent like a spring. In that case the airfoils would not be retractable, and would remain in place at zero curvature, longitudinally, which would be much the same as being retracted to the point of no affect. The said airfoils are an improvement over present state of the art, where mechanical means are used to vary blade pitch to access incoming wind more efficiently and safely, and to go to neutral, in the case of excessive wind speeds. With state of the art wind turbines, failure of mechanical pitch control, or failure of a governor system could lead to serious damage to the wind turbine.
In addition to the foregoing improvements over present state of the art, other options are intended, such as utilizing a smaller number of deeper turbine blades, or using a stationary complete half sphere in front of a turbine rotor. The turbine rotor would then have a flat faced purely cylindrical outer surface. It is also likely that we will be able to utilize a form of constant speed or step down transmission, as well as adding more load in the form of further generator capacity, and perhaps magnetic friction heating, to slow down and stabilize the turbine impeller when higher wind speeds are encountered. Since such options could be quite obvious to someone skilled in the art, they are not further included in either the detailed description or drawings to follow. It is also apparent to the inventor, that a version of this invention could easily be applied as a wind power drive system for water craft, including ships on the ocean. Its basic features could also be applied as an under water front drive system for water craft. Highly efficient air circulation fans and aircraft propellers are further possibilities. DETAILED DESCRIPTION
Figure 1 is a side view of a preferred embodiment of the invention, as mounted on the rotatable top of its support tower platform, with turbine rotor and 24 rotor blades. The turbine rotor has a curved face, being the rearward portion of what would be a completed half sphere shape, including a stationary front portion, separately supported, and mounted closely in front of the said turbine rotor. A close general outline of the outside edge of the path of the wind mass displaced by the spherical head is shown in its broadening arc form, and as it would address a complete cross section of the blades of the wind turbine. This is shown as a broken line arc, from the front center of the stationary portion of the spherical head shape, to the outer tips of the turbine rotor blades.
Figure 2 is a frontal view of the same preferred embodiment of the invention, as mounted on the rotatable top of its support tower platform, with turbine rotor and 24 rotor blades.
Figure 3 is a side view of the wind turbine, showing relative positions of 12 curved airfoils on the stationary frontal projection of its spherical head, which can be recessed to full closure, and zero effect. They would serve the purpose of curving the oncoming direction of the wind, in the rotational direction of the turbine rotor blades, to add the effect of 20 or more degrees to fixed turbine rotor blades for the purpose of eliminating any necessity for pitch control.
Figure 4 is a frontal view of the wind turbine, showing relative positions of the same 12 curved airfoils as illustrated in figure 3.
With all of the foregoing in view, and such other and further purposes, advantages or novel features as may become apparent from consideration of this disclosure and specifications, the present invention consists of the inventive concept which is comprised, embodied embraced or included in various specific embodiments of such concept, reference being made to the accompanying figures, in which: Figure 1 is a side view of a preferred embodiment of the invention, as mounted on the rotatable top of its support tower platform, where we have the stationary portion of its spherical head 1 , and the rotating portion of its spherical head 2, which is also the outer facing of its rotor 3. Then turbine blades 4, and the conical shape of its rear outer encasement 5, and the aerodynamically shaped lower extension 6, of its outer body and wall, surrounding its supporting structure and internalized access entry port, extending downward to its rotatable base 7, on top of its tower column, 9.
Then we have airfoil shaped structural support beams 8, for the stationary portion of its spherical head section and its front end axle bearing, then we have the stationary portion of its structural support tower (column) 9, and broken line representing the outer periphery of the volume expansion area of wind displaced by the said spherical head 10, and undulating lines 11, to indicate turbulence expected behind turbine rotor 3, which would be common to exhausted wind behind the blades of the wind turbine.
Figure 2 is a frontal view of the wind turbine, showing the stationary front section of the half sphere shape 1 , rotating curved outer circumferential surface 2, of turbine rotor 3, being the remainder of the said half sphere shape. Then we have turbine blades 4, of which there are twenty four in this embodiment. Also shown are support struts 8, for the stationary frontal portion of the said half sphere shape and front axle bearing, and rotatable top base mount 7, for the wind turbine, and then stationary support tower 9, which would extend to ground level.
Figure 3 is an angularly offset side view of another preferred embodiment of the wind turbine, showing relative positions of twelve comparatively thin and retractable airfoils 12, placed upon and within the stationary frontal projection 1, of the half spherical shape of more than seventy percent of the radius from axle center to the inside edges or bottom ends of its comparatively short turbine blades 4. Then we have the conical projection of its rear body or encasement 5, segmented, as may be necessary for purposes of efficient manufacturing of such projection, and then the somewhat cylindrical and aerodynamically shaped lower extension 6, of its outer body and wall surrounding its supporting structural elements and internal entry port, and extending downward to its rotatable base 7, on top of its supporting tower structure 9.
Figure 4 is a direct frontal view of the same preferred embodiment as described in figure 3, where we can observe curved retractable airfoils 12, and their relationship to the turbine blades 4, and we can further see the essential struts 8, supporting the front axle bearing of the turbine, and carrying the stationary frontal portion of half spherical shape 1 , at the front of the wind turbine. Then we can see further the aerodynamically shaped front end of the bottom extension of the rear housing or embodiment of the wind turbine 6, and then we have rotatable base support 7, and stationary support tower 9.

Claims

CLAIMSBased on the foregoing detailed description, together with further related comments and explanations, the objects of the subject invention, as set forth herein above have been addressed adequately, and are easily achievable. Also, while there is shown and described, preferred embodiments of the invention, it is understood that the invention is not limited thereto, but may be otherwise variously embodied and applied within the scope of the following claims. Accordingly,What is claimed is:
1. A wind turbine with a stationary half spherical projection including the outer surface of its turbine rotor, and extending forward, as a stationary extension thereof, beyond its rotor, for the purpose of speeding up wind addressed by its turbine blades, to improve the efficiency of the said wind turbine, by speeding up wind addressed, by as much as fifty seven percent, subject to probable drag losses of 10 to 20 percent.
2. A wind turbine with a stationary half spherical projection, not including the outer surface of its turbine rotor, and extending forward, as a stationary extension thereof, beyond its rotor, for the purpose of speeding up wind addressed by its turbine blades, to improve the efficiency of the said wind turbine, by speeding up the wind addressed, by as much as fifty seven percent, subject to probable drag losses of 10 to 20 percent.
3. A wind turbine with a stationary half spherical projection including the outer surface of its rotor, and extending forward beyond the said rotor, as a stationary extension of the said sphere, which effectively displaces a major portion of the total frontal area of the wind turbine, including that of its entire rotational arc, to the extent of 70 percent or more, of the radius of the said rotational arc from axle center to its blade tips, to access a greater amount of the energy from all of the wind directly addressed by the blades of the said wind turbine.
4. A wind turbine which utilizes a larger number of comparatively short turbine blades, mounted on a relatively large diameter rotor, to access a maximum percentage of oncoming wind, as displaced by a half sphere head directly in front of the said rotor, where all of the said displaced wind must address all of the said turbine blades.
5. A wind turbine with comparatively short turbine blades, solidly mounted on a comparatively large rotor, which can withstand the effects of the said rotor turning at a much faster rotational speed than can be tolerated by present state of the art propeller types of wind turbines.
6. A wind turbine with comparatively short turbine blades solidly mounted on a comparatively large rotor, placed behind a frontally projecting stationary spherical head, with a series of thin airfoils radially, proportionately and evenly placed on the said spherical head, bendable into a curvature, to spiral oncoming wind, as it proceeds toward the said turbine rotor's blades in their direction of rotation, thereby creating the effect of a coarser pitch blade angle at lower wind speeds, and where the said airfoils can be recessed, uncurved or straightened out to longitudinal zero effect in the case of higher wind velocity.
7. A wind turbine with a comparatively large turbine rotor, which has a round, tapered or conical housing extending rearward from the rear outer edge of its rotor surface, to serve as a protective covering for all of its then internalized mechanical components and electrical generator(s) or other driven devices, and further, to provide a more secure, spacious, walled and contained area where personnel servicing the wind turbine are safe and protected from the elements while servicing or repairing the wind turbine.
PCT/CA2005/000766 2004-05-19 2005-05-17 Wind turbine rotor projection WO2005111413A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
CA002567174A CA2567174A1 (en) 2004-05-19 2005-05-17 Wind turbine rotor projection
JP2007516914A JP2007538189A (en) 2004-05-19 2005-05-17 Wind turbine speedball configuration
AU2005243553A AU2005243553A1 (en) 2004-05-19 2005-05-17 Wind turbine rotor projection
EP05745332A EP1766230A1 (en) 2004-05-19 2005-05-17 Wind turbine rotor projection
US11/569,340 US7726935B2 (en) 2004-05-19 2005-05-17 Wind turbine rotor projection

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CA2,467,199 2004-05-19
CA002467199A CA2467199A1 (en) 2004-05-19 2004-05-19 Wind turbine

Publications (1)

Publication Number Publication Date
WO2005111413A1 true WO2005111413A1 (en) 2005-11-24

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Country Status (9)

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US (1) US7726935B2 (en)
EP (1) EP1766230A1 (en)
JP (1) JP2007538189A (en)
KR (1) KR20070028426A (en)
CN (2) CN101014765A (en)
AU (1) AU2005243553A1 (en)
CA (1) CA2467199A1 (en)
RU (1) RU2386854C2 (en)
WO (1) WO2005111413A1 (en)

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