US20140178189A1 - Vertical axis dual vortex downwind inward flow impulse wind turbine - Google Patents

Vertical axis dual vortex downwind inward flow impulse wind turbine Download PDF

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Publication number
US20140178189A1
US20140178189A1 US14/049,432 US201314049432A US2014178189A1 US 20140178189 A1 US20140178189 A1 US 20140178189A1 US 201314049432 A US201314049432 A US 201314049432A US 2014178189 A1 US2014178189 A1 US 2014178189A1
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United States
Prior art keywords
housing
turbine
outlet
array
stator
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
US14/049,432
Inventor
Joe C. Cassidy
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Zephyr International Inc
Original Assignee
Zephyr International Inc
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Filing date
Publication date
Priority claimed from US12/214,273 external-priority patent/US20080317582A1/en
Application filed by Zephyr International Inc filed Critical Zephyr International Inc
Priority to US14/049,432 priority Critical patent/US20140178189A1/en
Assigned to ZEPHYR INTERNATIONAL, INC. reassignment ZEPHYR INTERNATIONAL, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CASSIDY, JOE C.
Publication of US20140178189A1 publication Critical patent/US20140178189A1/en
Abandoned legal-status Critical Current

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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/04Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • F03D3/0427Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels with converging inlets, i.e. the guiding means intercepting an area greater than the effective rotor area
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/04Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • F03D3/0409Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels surrounding the rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06Rotors
    • F03D1/0608Rotors characterised by their aerodynamic shape
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D1/00Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/06Rotors
    • F03D1/065Rotors characterised by their construction elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D3/00Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/02Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  having a plurality of rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D5/00Other wind motors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D15/00Transmission of mechanical power
    • F03D15/10Transmission of mechanical power using gearing not limited to rotary motion, e.g. with oscillating or reciprocating members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D17/00Monitoring or testing of wind motors, e.g. diagnostics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D80/00Details, components or accessories not provided for in groups F03D1/00 - F03D17/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/10Combinations of wind motors with apparatus storing energy
    • F03D9/11Combinations of wind motors with apparatus storing energy storing electrical energy
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D9/00Adaptations of wind motors for special use; Combinations of wind motors with apparatus driven thereby; Wind motors specially adapted for installation in particular locations
    • F03D9/20Wind motors characterised by the driven apparatus
    • F03D9/25Wind motors characterised by the driven apparatus the apparatus being an electrical generator
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/10Stators
    • F05B2240/12Fluid guiding means, e.g. vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/10Stators
    • F05B2240/13Stators to collect or cause flow towards or away from turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/10Stators
    • F05B2240/14Casings, housings, nacelles, gondels or the like, protecting or supporting assemblies there within
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/24Rotors for turbines
    • F05B2240/241Rotors for turbines of impulse type
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/74Wind turbines with rotation axis perpendicular to the wind direction

Definitions

  • the subject invention relates to wind-powered turbines.
  • Wind has been used as a source of power for many years.
  • Windmills historically have been used to grind grain, pump water and provide other forms of mechanical energy. In recent times they have been used to generate electric power.
  • windmills typically utilize a blade or air foil which the wind passes over without significantly changing directions.
  • Water-powered turbines are often impulse turbines where the direction of the water is significantly changed as it interacts with the turbine blade.
  • a typical example of this is the pelton turbine.
  • impulse turbines have not been used to convert wind energy to electric power.
  • a wind-powered turbine has a housing with an inlet and an outlet. Mounted in the housing is a plurality of spaced-apart stators that are arranged in a fixed annular cylindrical stator array. A plurality of cupped rotors are arranged in an annular cylindrical rotor array which is rotatable about a central axis and fits inside of the stator array. The stators are positioned to cause air which flows around the outer periphery of the stator array to impinge on the rotors. An air handling system causes air entering the housing to flow around the outer periphery of the stator array.
  • FIG. 1 is a perspective view of a wind turbine embodying the subject invention.
  • FIG. 2 is a perspective view of the wind turbine of FIG. 1 with the housing in a different orientation.
  • FIG. 3 is a cross-sectional view, at an enlarged scale, taken along the lines 3 - 3 in FIG. 2 .
  • FIG. 4 is a cross-sectional view, at an enlarged scale, taken along the lines 4 - 4 in FIG. 3 .
  • FIG. 5 is an exploded fragmentary view showing how a rotor is attached to a rotor ring.
  • FIG. 6 is a cross-sectional view, at an enlarged scale, taken along the lines 6 - 6 in FIG. 3 .
  • FIG. 7 is an exploded fragmentary view showing how a stator is attached to a stator ring.
  • FIG. 8 is an exploded view showing portions of the turbine.
  • FIG. 9 is a cross-sectional view taken on the line 9 - 9 in FIG. 8 .
  • FIG. 10 is a cross-sectional view taken on the line 10 - 10 in FIG. 8 .
  • FIG. 11 is a cross-sectional view taken on the line 11 - 11 in FIG. 2 .
  • FIG. 12 is a perspective view, similar to FIG. 2 of an alternate embodiment of the invention.
  • FIG. 13 is a cross-sectional view, at an enlarged scale, taken along the lines 13 - 13 in FIG. 12 .
  • a wind-powered turbine 10 comprises a housing 12 with an inlet end 24 containing an inlet 14 and an outlet end 22 containing an outlet 16 .
  • the entire inlet end 12 a is open to provide the inlet 14
  • the entire outlet end 12 b is open to provide the outlet 16 .
  • the housing 12 is mounted on a turntable 18 which in turn is mounted on top of a tower 20 .
  • the turntable 18 has an outer ring 19 which is attached to the tower 20 .
  • the outer ring 20 has a slot 21 formed in its inner periphery.
  • the outer periphery 23 of a cylindrical plate 25 extends into the slot 21 .
  • Roller bearings 27 are located between the top, bottom and edge of the plate 25 and the ring 19 .
  • the housing 12 is attached to the plate through struts 29 .
  • the struts support the housing 10 sufficiently above the turntable 18 that the turntable has no effect on wind entering the housing.
  • the struts separate the housing from the turntable by an amount equal to 50% of the height of the inlet 14 .
  • the turntable allows complete rotation of the housing 12 so that the inlet can face into the wind.
  • the housing 12 has a larger cross-sectional shape at its outlet end 22 than at its inlet end 24 .
  • the housing is square in cross-section but it could have many other cross-sectional shapes.
  • the entire housing is symmetrical so that the distance from the inlet end to the outlet end is equal around its entire extent.
  • a cylindrical turbine assembly 26 is mounted in the housing between the inlet end and the outlet end.
  • the turbine assembly 26 best seen in FIGS. 4 , 6 and 8 includes a plurality of stators 28 which are arranged in an annular cylindrical stator array 30 .
  • the stator array is divided into a first section 30 a and a second section 30 b which are separated from one another.
  • the first stator section is located between an annular upper stator ring 32 and an annular middle stator ring 34 and the second stator section is located between the middle stator ring 34 and an annular lower stator ring 36 .
  • the outer periphery of the middle stator ring contains a rounded bull nose 37 which projects outwardly from the stators to assist in splitting air entering the turbine assembly 26 between the first and second Sections 30 a, 30 b.
  • Each stator 28 has a hole 38 extending centrally through it, and a rod 40 , which passes through the hole 38 , is attached to the upper, middle and lower stator rings.
  • the rod joins the stators and stator rings into an integral unit.
  • the stators are tear-drop shaped and are symmetrical side to side. They are angled to direct air entering the turbine in the desired manner, as will be explained later.
  • Pins 42 extend between the tops and bottoms of the stators into the stator rings to prevent the stators from rotating on the rods 40 , FIG. 7 .
  • the number of stators, and thus the spacing between them, is set to cause the air entering the turbine assembly 26 to be distributed relatively equally around the entire outer periphery of the stator array 30 .
  • the turbine assembly 26 also includes a plurality of cupped rotors 50 which are arranged in an annular rotor array 52 which fits immediately inside of the stator array 30 .
  • the rotors have an entry end and an opposed exit end such that air passing over each stator impinges on the entry end of an associated rotor, passes along the entire cupped face of the rotor and exits the exit end of this rotor.
  • the cupped shape of the rotors causes air striking them to change direction much as the rotors do in a pelton hydraulic turbine. In the embodiment illustrated, the air exits the rotors at approximately 164 degrees relative where it enters them, but increasing or decreasing this angle may increase the efficiency of the turbine.
  • each stator there is one rotor for each stator and the stators and rotors are positioned such that air directed by each stator impinges substantially on the cupped side of an associated rotor.
  • the rotors are oriented such that a line A, which connects their tips, extends through the center of the rotor array, FIG. 4 .
  • the rotor array also is divided into a first section 52 a and a second section 52 b, which are separated from one another.
  • the turbine assembly 26 also includes a plurality of cupped rotors 50 which are arranged in an annular rotor array 52 which fits immediately inside of the stator array 30 .
  • the rotor array also is divided into a first section 52 a and a second section 52 b, which are separated from one another.
  • the cupped shape of the rotors causes air striking them to change direction much as the rotors do in an pelton hydraulic turbine.
  • the air exits the rotors at approximately 164 degrees relative to where it enters them, but increasing or decreasing this angle may increase the efficiency of the turbine.
  • the rotors are oriented such that a line A which connects their tips extends through the center of the rotor array, FIG. 4 .
  • the first rotor section 52 a is located between an annular upper rotor ring 54 and a cylindrical cross-sectioned rotor plate 56
  • the second rotor section 52 b is located between the rotor plate 56 and an annular lower rotor ring 58 .
  • the rotor plate is wider proximate its center than at its periphery to assist in dividing air between the first and second sections 52 a, 52 b .
  • Each rotor 50 has a hole 60 extending centrally through it, and a rod 62 , which passes through the hole 60 , is attached to the upper and lower rotor rings and the rotor plate.
  • the rod joins the rotors, rotor rings and rotor plate into an integral unit.
  • Pins 63 extend between the tops and bottoms of the rotors into the rotor rings and rotor plate to prevent the rotors from rotating on the rods 62 , FIG. 5 .
  • An axle 66 which is attached to the center plate 56 , extends downwardly out of the housing to a driven device such as a generator, compressor, flywheel, etc. (not shown).
  • the axle 66 is journaled in stabilizer bearings 68 which are mounted in the housing 12 .
  • a thrust bearing 70 located on the ground at the bottom of the axle supports it.
  • a pulley 74 located on the axle 66 is connected through a belt 78 to a small alternator 76 , which is mounted on the housing.
  • the alternator keeps a battery 80 located in an isolation space 81 between the isolation walls 47 charged.
  • the battery powers a small computer 82 which monitors environmental conditions and shuts the turbine down when conditions, such as high wind or ice, dictate.
  • a rectangular nozzle 72 located in the inlet end 22 of the housing directs wind-driven air entering the housing onto the turbine assembly 26 .
  • the turbine is initially started with the valves 48 in the draft tubes 44 , 46 closed so that no air enters the housing 12 through the inlet 14 .
  • the pressure at its outlet 16 causes the pressure at its outlet 16 to be lower than the pressure at its inlet 14 , and also below ambient pressure.
  • the valves 48 are opened this negative pressure pulls air through the draft tubes. This causes the air to spiral up and out of the first section 52 a of the rotor array and into the first section 30 a of the stator array, and down and out of the second section 52 b of the rotor array and into the second section 30 b of the stator array. It also causes air to be pulled into the inlet at a velocity above the ambient wind velocity.
  • One function of the draft tubes is to convert into useable power the energy tied up in its high velocity as it leaves the rotors. This is done by gradually reducing the high air velocity at the inlet end of the draft tubes to a lower velocity at the discharge end of the draft tubes.
  • the turbine is shut down by gradually closing the valves 48 in the draft tubes.
  • the turbine and/or a device driven by it would rotate at a rate that is above their design limits.
  • one of the valves 48 can be closed and air will only enter the turbine through one of the draft tubes 44 , 46 .
  • the air will impact only one of the turbine sections. This will cause the turbine to operate at a lower speed than it would if air were admitted to both turbine sections and the turbine will provide roughly one-half of the energy. While the same result could be obtained by partially closing both valves 48 , placing a partial restriction in the draft tubes would result in an unacceptable level of noise being generated.
  • the large cross-section area at the housing outlet 16 causes the turntable 18 to rotate such that the inlet 14 always faces into the wind. If the rotational force caused by the turbine assembly 26 causes misalignment of the housing relative to the direction of the wind, there are several ways of compensating for this. Due to the large cross-sectional area at the outlet end 22 of the housing 12 , the housing will not pinwheel.
  • the outlet end 22 of the housing 12 extends rearwardly a short distance past where the upper and lower draft tubes 44 , 46 come together.
  • the outlet end 22 of the housing 12 is closed with an end plate 84 , and the outlet is a series of slots 86 located in the lower wall 88 of the housing 12 .
  • the total cross sectional area of the slots 86 needs to be at least as equal as the total cross sectional area of the inlet 14 , and preferably is considerably larger.
  • This configuration provides a greater pressure differential between the inlet and outlet than the embodiment illustrated in FIGS. 1-3 . As a result, the air enters the stator array 30 more uniformly around its periphery, which creates a higher turbine efficiency.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Wind Motors (AREA)

Abstract

A wind-powered turbine has a housing with an inlet and an outlet. Located in the housing is a cylindrical stator array having a plurality of spaced-apart stators located in it. An annular cylindrical rotor array having a plurality of cups rotates about a central axis, fits inside of the stator array. The stators are positioned to cause air which flows around the outer periphery of the stator array to impinge on the rotors and an air handling system causes air entering the housing to be distributed substantially around the periphery of the stator array.

Description

    RELATED APPLICATIONS
  • This application is a Continuation of application Ser. No. 13/588,359 filed Aug. 17, 2012, which is a Continuation of application Ser. No. 12/284,970 filed Sep. 25, 2008, which is a Continuation-In-Part of application Ser. No. 12/214,273 filed Jun. 16, 2008, which in turn is a Continuation-In-Part of application Ser. No. 11/652,429 filed Jan. 11, 2007.
  • BACKGROUND OF THE INVENTION
  • The subject invention relates to wind-powered turbines. Wind has been used as a source of power for many years. Windmills historically have been used to grind grain, pump water and provide other forms of mechanical energy. In recent times they have been used to generate electric power. However, windmills typically utilize a blade or air foil which the wind passes over without significantly changing directions.
  • Water-powered turbines, on the other hand, are often impulse turbines where the direction of the water is significantly changed as it interacts with the turbine blade. A typical example of this is the pelton turbine. However, impulse turbines have not been used to convert wind energy to electric power.
  • BRIEF SUMMARY OF THE INVENTION
  • In the subject invention, a wind-powered turbine has a housing with an inlet and an outlet. Mounted in the housing is a plurality of spaced-apart stators that are arranged in a fixed annular cylindrical stator array. A plurality of cupped rotors are arranged in an annular cylindrical rotor array which is rotatable about a central axis and fits inside of the stator array. The stators are positioned to cause air which flows around the outer periphery of the stator array to impinge on the rotors. An air handling system causes air entering the housing to flow around the outer periphery of the stator array.
  • The foregoing and other objectives, features, and advantages of the invention will be more readily understood upon consideration of the following detailed description of the invention, taken in conjunction with the accompanying drawings.
  • BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
  • FIG. 1 is a perspective view of a wind turbine embodying the subject invention.
  • FIG. 2 is a perspective view of the wind turbine of FIG. 1 with the housing in a different orientation.
  • FIG. 3 is a cross-sectional view, at an enlarged scale, taken along the lines 3-3 in FIG. 2.
  • FIG. 4 is a cross-sectional view, at an enlarged scale, taken along the lines 4-4 in FIG. 3.
  • FIG. 5 is an exploded fragmentary view showing how a rotor is attached to a rotor ring.
  • FIG. 6 is a cross-sectional view, at an enlarged scale, taken along the lines 6-6 in FIG. 3.
  • FIG. 7 is an exploded fragmentary view showing how a stator is attached to a stator ring.
  • FIG. 8 is an exploded view showing portions of the turbine.
  • FIG. 9 is a cross-sectional view taken on the line 9-9 in FIG. 8.
  • FIG. 10 is a cross-sectional view taken on the line 10-10 in FIG. 8.
  • FIG. 11 is a cross-sectional view taken on the line 11-11 in FIG. 2.
  • FIG. 12 is a perspective view, similar to FIG. 2 of an alternate embodiment of the invention.
  • FIG. 13 is a cross-sectional view, at an enlarged scale, taken along the lines 13-13 in FIG. 12.
  • DETAILED DESCRIPTION OF PREFERRED EMBODIMENT
  • Referring now to FIGS. 1 and 2, a wind-powered turbine 10 comprises a housing 12 with an inlet end 24 containing an inlet 14 and an outlet end 22 containing an outlet 16. In the embodiment illustrated in FIGS. 1-3, the entire inlet end 12 a is open to provide the inlet 14, and the entire outlet end 12 b is open to provide the outlet 16. The housing 12 is mounted on a turntable 18 which in turn is mounted on top of a tower 20. Referring now also to FIG. 11, the turntable 18 has an outer ring 19 which is attached to the tower 20. The outer ring 20 has a slot 21 formed in its inner periphery. The outer periphery 23 of a cylindrical plate 25 extends into the slot 21. Roller bearings 27 are located between the top, bottom and edge of the plate 25 and the ring 19. Thus, the plate 25 rotates freely and supports the housing against vertical and radial loads. The housing 12 is attached to the plate through struts 29. The struts support the housing 10 sufficiently above the turntable 18 that the turntable has no effect on wind entering the housing. In the embodiment illustrated the struts separate the housing from the turntable by an amount equal to 50% of the height of the inlet 14. The turntable allows complete rotation of the housing 12 so that the inlet can face into the wind. The housing 12 has a larger cross-sectional shape at its outlet end 22 than at its inlet end 24. This causes wind-driven air passing over the housing to accelerate as it moves from the inlet end 24 to the outlet end 22, thereby causing the pressure at the housing outlet 16 to be lower than the pressure at the housing inlet 14. The advantage of this will be more fully explained later. In the embodiment illustrated, the housing is square in cross-section but it could have many other cross-sectional shapes. Preferably the entire housing is symmetrical so that the distance from the inlet end to the outlet end is equal around its entire extent.
  • Referring now to FIG. 3, a cylindrical turbine assembly 26 is mounted in the housing between the inlet end and the outlet end. The turbine assembly 26, best seen in FIGS. 4, 6 and 8 includes a plurality of stators 28 which are arranged in an annular cylindrical stator array 30. The stator array is divided into a first section 30 a and a second section 30 b which are separated from one another. The first stator section is located between an annular upper stator ring 32 and an annular middle stator ring 34 and the second stator section is located between the middle stator ring 34 and an annular lower stator ring 36. The outer periphery of the middle stator ring contains a rounded bull nose 37 which projects outwardly from the stators to assist in splitting air entering the turbine assembly 26 between the first and second Sections 30 a, 30 b. Each stator 28 has a hole 38 extending centrally through it, and a rod 40, which passes through the hole 38, is attached to the upper, middle and lower stator rings. Thus, the rod joins the stators and stator rings into an integral unit. The stators are tear-drop shaped and are symmetrical side to side. They are angled to direct air entering the turbine in the desired manner, as will be explained later. Pins 42 extend between the tops and bottoms of the stators into the stator rings to prevent the stators from rotating on the rods 40, FIG. 7. The number of stators, and thus the spacing between them, is set to cause the air entering the turbine assembly 26 to be distributed relatively equally around the entire outer periphery of the stator array 30.
  • The turbine assembly 26 also includes a plurality of cupped rotors 50 which are arranged in an annular rotor array 52 which fits immediately inside of the stator array 30. The rotors have an entry end and an opposed exit end such that air passing over each stator impinges on the entry end of an associated rotor, passes along the entire cupped face of the rotor and exits the exit end of this rotor. The cupped shape of the rotors causes air striking them to change direction much as the rotors do in a pelton hydraulic turbine. In the embodiment illustrated, the air exits the rotors at approximately 164 degrees relative where it enters them, but increasing or decreasing this angle may increase the efficiency of the turbine. There is one rotor for each stator and the stators and rotors are positioned such that air directed by each stator impinges substantially on the cupped side of an associated rotor. In the embodiment illustrated the rotors are oriented such that a line A, which connects their tips, extends through the center of the rotor array, FIG. 4. The rotor array also is divided into a first section 52 a and a second section 52 b, which are separated from one another.
  • The turbine assembly 26 also includes a plurality of cupped rotors 50 which are arranged in an annular rotor array 52 which fits immediately inside of the stator array 30. The rotor array also is divided into a first section 52 a and a second section 52 b, which are separated from one another. The cupped shape of the rotors causes air striking them to change direction much as the rotors do in an pelton hydraulic turbine. In the embodiment illustrated, the air exits the rotors at approximately 164 degrees relative to where it enters them, but increasing or decreasing this angle may increase the efficiency of the turbine. In the embodiment illustrated the rotors are oriented such that a line A which connects their tips extends through the center of the rotor array, FIG. 4.
  • The first rotor section 52 a is located between an annular upper rotor ring 54 and a cylindrical cross-sectioned rotor plate 56, and the second rotor section 52 b is located between the rotor plate 56 and an annular lower rotor ring 58. In the embodiment illustrated, the rotor plate is wider proximate its center than at its periphery to assist in dividing air between the first and second sections 52 a, 52 b. Each rotor 50 has a hole 60 extending centrally through it, and a rod 62, which passes through the hole 60, is attached to the upper and lower rotor rings and the rotor plate. Thus, the rod joins the rotors, rotor rings and rotor plate into an integral unit. Pins 63 extend between the tops and bottoms of the rotors into the rotor rings and rotor plate to prevent the rotors from rotating on the rods 62, FIG. 5. In the embodiment illustrated there are the same number of rotors as there are stators. An axle 66, which is attached to the center plate 56, extends downwardly out of the housing to a driven device such as a generator, compressor, flywheel, etc. (not shown). The axle 66 is journaled in stabilizer bearings 68 which are mounted in the housing 12. A thrust bearing 70 located on the ground at the bottom of the axle supports it. A pulley 74 located on the axle 66 is connected through a belt 78 to a small alternator 76, which is mounted on the housing. The alternator keeps a battery 80 located in an isolation space 81 between the isolation walls 47 charged. The battery powers a small computer 82 which monitors environmental conditions and shuts the turbine down when conditions, such as high wind or ice, dictate.
  • A rectangular nozzle 72 located in the inlet end 22 of the housing directs wind-driven air entering the housing onto the turbine assembly 26.
  • The turbine is initially started with the valves 48 in the draft tubes 44, 46 closed so that no air enters the housing 12 through the inlet 14. As mentioned above, because of the shape of the housing air flowing over it causes the pressure at its outlet 16 to be lower than the pressure at its inlet 14, and also below ambient pressure. When the valves 48 are opened this negative pressure pulls air through the draft tubes. This causes the air to spiral up and out of the first section 52 a of the rotor array and into the first section 30 a of the stator array, and down and out of the second section 52 b of the rotor array and into the second section 30 b of the stator array. It also causes air to be pulled into the inlet at a velocity above the ambient wind velocity. Providing the proper number of stators limits the amount of air that can pass between each adjacent pair of stators. This limitation and the alignment of the stators causes the air to enter the stator array 30 around substantially its entire peripheral extent. One function of the draft tubes is to convert into useable power the energy tied up in its high velocity as it leaves the rotors. This is done by gradually reducing the high air velocity at the inlet end of the draft tubes to a lower velocity at the discharge end of the draft tubes. The turbine is shut down by gradually closing the valves 48 in the draft tubes.
  • When the velocity of the wind entering the housing 12 reaches a certain level, the turbine and/or a device driven by it would rotate at a rate that is above their design limits. When this occurs one of the valves 48 can be closed and air will only enter the turbine through one of the draft tubes 44, 46. Thus the air will impact only one of the turbine sections. This will cause the turbine to operate at a lower speed than it would if air were admitted to both turbine sections and the turbine will provide roughly one-half of the energy. While the same result could be obtained by partially closing both valves 48, placing a partial restriction in the draft tubes would result in an unacceptable level of noise being generated.
  • The large cross-section area at the housing outlet 16 causes the turntable 18 to rotate such that the inlet 14 always faces into the wind. If the rotational force caused by the turbine assembly 26 causes misalignment of the housing relative to the direction of the wind, there are several ways of compensating for this. Due to the large cross-sectional area at the outlet end 22 of the housing 12, the housing will not pinwheel.
  • In another embodiment of the invention, shown in FIGS. 12 and 13, the outlet end 22 of the housing 12 extends rearwardly a short distance past where the upper and lower draft tubes 44, 46 come together. In this embodiment the outlet end 22 of the housing 12 is closed with an end plate 84, and the outlet is a series of slots 86 located in the lower wall 88 of the housing 12. The total cross sectional area of the slots 86 needs to be at least as equal as the total cross sectional area of the inlet 14, and preferably is considerably larger. This configuration provides a greater pressure differential between the inlet and outlet than the embodiment illustrated in FIGS. 1-3. As a result, the air enters the stator array 30 more uniformly around its periphery, which creates a higher turbine efficiency.
  • The terms and expressions which have been employed in the foregoing specification are used therein as terms of description and not of limitation, and there is no intention, in the use of such terms and expressions, of excluding equivalents of the features shown and described or portions thereof, it being recognized that the scope of the invention is defined and limited only by the claims which follow.

Claims (5)

What is claimed is:
1. A wind powered turbine comprising:
(a) a housing having an inlet end with an inlet defined therein and an outlet end with an outlet defined therein;
(b) a plurality of spaced-apart stators arranged in a fixed annular cylindrical stator array;
(c) a plurality of cupped rotors arranged in an annular cylindrical rotor array which is rotatable about a central axis and fits within said stator array;
(d) said stators being positioned to cause air which flows around an outer periphery of said stator array to impinge on said cupped rotors; and
(e) an air handling system which causes air entering said housing to flow around substantially the entire outer periphery of said stator array.
2. The turbine of claim 1 wherein said housing has a cross-sectional shape which is symmetrical along an elongate axis which extends between said inlet end and said outlet end and said outlet is oriented substantially perpendicular to said elongate axis.
3. The turbine of claim 1 wherein said housing has a cross-sectional shape which is symmetrical along an elongate axis which extends between said inlet end and said outlet end and said outlet is oriented substantially parallel to said elongate axis.
4. The turbine of claim 1 wherein said outlet is located in at least one of said sidewalls of said housing.
5. The turbine of claim 1 wherein said outlet is located in a downwardly facing sidewall of said housing.
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US13/588,359 US8556571B2 (en) 2007-01-11 2012-08-17 Vertical axis dual vortex downwind inward flow impulse wind turbine
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CN111120223A (en) * 2019-12-16 2020-05-08 大连赛听科技有限公司 Blade fault monitoring method and device based on double arrays

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