WO2023113590A1 - Magnetically levitated horizontal axis rotor, axial flux wind turbine - Google Patents

Magnetically levitated horizontal axis rotor, axial flux wind turbine Download PDF

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Publication number
WO2023113590A1
WO2023113590A1 PCT/MY2022/050103 MY2022050103W WO2023113590A1 WO 2023113590 A1 WO2023113590 A1 WO 2023113590A1 MY 2022050103 W MY2022050103 W MY 2022050103W WO 2023113590 A1 WO2023113590 A1 WO 2023113590A1
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WO
WIPO (PCT)
Prior art keywords
rotor
electrically
conductive
permanent magnet
support frame
Prior art date
Application number
PCT/MY2022/050103
Other languages
French (fr)
Inventor
Boon Peng SIM
Zong Xern SIM
Original Assignee
Bamboo Turbo Technology Sdn Bhd
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 Bamboo Turbo Technology Sdn Bhd filed Critical Bamboo Turbo Technology Sdn Bhd
Publication of WO2023113590A1 publication Critical patent/WO2023113590A1/en

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Classifications

    • 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
    • F03D80/70Bearing or lubricating arrangements
    • 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
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C32/00Bearings not otherwise provided for
    • F16C32/04Bearings not otherwise provided for using magnetic or electric supporting means
    • F16C32/0406Magnetic bearings
    • F16C32/0408Passive magnetic bearings
    • F16C32/041Passive magnetic bearings with permanent magnets on one part attracting the other part
    • F16C32/0421Passive magnetic bearings with permanent magnets on one part attracting the other part for both radial and axial load
    • 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
    • F05B2240/50Bearings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2240/00Specified values or numerical ranges of parameters; Relations between them
    • F16C2240/26Speed, e.g. rotational speed
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2240/00Specified values or numerical ranges of parameters; Relations between them
    • F16C2240/40Linear dimensions, e.g. length, radius, thickness, gap
    • F16C2240/46Gap sizes or clearances
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2300/00Application independent of particular apparatuses
    • F16C2300/30Application independent of particular apparatuses related to direction with respect to gravity
    • F16C2300/32Horizontal, e.g. bearings for supporting a horizontal shaft
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2360/00Engines or pumps
    • F16C2360/31Wind motors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2380/00Electrical apparatus
    • F16C2380/26Dynamo-electric machines or combinations therewith, e.g. electro-motors and generators
    • 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

Definitions

  • the present invention related to horizontal axis rotor axial flux miniature wind turbine, in particular axial flux miniature wind turbine with magnetically levitated horizontal axis rotor.
  • Axial flux means the lines of magnetic flux that pass through the coils of wire, travel along the "axis" of the rotating motion.
  • Rotor is a rotating component coupled to the rotor of axial flux wind turbine.
  • “Stator” is a stationary component coupled to the support frame assembly of axial flux wind turbine. “Permanent magnet”: is a magnet that retains its magnetic properties in the absence of an inducing field or current.
  • Air core coil is a type of insulated wire winding coil that has no ferrite core inside the coil.
  • Permanent magnet stator is a stator comprising a plate substrate and a plurality of permanent magnets mounted therein.
  • Air core coils rotor is a rotor comprising a plate substrate with a plurality of air core coil mounted therein.
  • Blade solidity is the ratio of total blade area to total swept area.
  • SUBSTITUTE SHEET (RULE 26) It is the primary object of the present invention to provide horizontal axis rotor wind turbine that start to generate electrical power at minimum operating wind speed of at least 1.2m/s.
  • the present invention propose a novel design of magnetic levitation to the rotor, without the use of bearings to support the rotor as seen in prior arts which has significant bearing contact friction while operating at a very low wind speed.
  • the magnetic levitation to the rotor is achieved by having ferromagnetic tapered tip members on both end portions of the rotor shaft, which attracted to the permanent magnets that are mounted on both windward side and leeward side of the support frame assembly.
  • the magnetic levitation to the rotor shaft minimizes the rotating mechanical frictions to a near zero value.
  • a very low starting torque generated by a very low wind speed such as 1.2m/s that passing through the rotor blades is sufficient to rotate the rotor and electrical power is then generated.
  • the rotor structure needs to have a higher aerodynamic lift force and a lower moment of inertia.
  • One way to reduce moment inertia is to use rotor components which have a lower density and weight.
  • the selection of lower density rotor components need to have a high modulus of elasticity MOE and thus high stiffness.
  • the present invention disposed the novel use of bamboo skin as rotor blades.
  • the bamboo skin blades are characterized in high aerodynamic lift force, high stiffness and low material density.
  • the preferred embodiment of the present invention comprising two permanent magnet stators, an air core coils rotor coupled with a plurality of blades, a support frame assembly and two wires for external electrical output connection, wherein the rotor comprising electrically-conductive and ferromagnetic tapered tip members on both end portions, wherein the plurality of blades are made from bamboo skin, wherein the alternating current circuit generated out from the air core coils rotor is electrically connected to both electrically-conductive and ferromagnetic tapered tip member at the end portions of the rotor to the electrically-conductive permanent magnets that are mounted on the support frame assembly, and then connected to external circuit for direct current rectification and/or load via two wires.
  • FIG. 1 is a perspective view of an axial flux wind turbine 100 according to the preferred embodiment of the present invention.
  • FIG. 2 is an exploded view of an axial flux wind turbine 100 according to the preferred embodiment of the present invention.
  • FIG. 3 is a cross-sectional view taken along line S-S in FIG 1, of an axial flux wind turbine 100 according to the preferred embodiment of the present invention
  • FIG. 4 is a perspective view of the rotor with the electrically-conductive and ferromagnetic tapered tip members mounted on both end portions of the rotor, of an axial flux wind turbine 100 according to the preferred embodiment of the present invention
  • FIG. 5 is a perspective view of the air core coils rotor of an axial flux wind turbine 100 according to the preferred embodiment of the present invention
  • FIG. 6 is a circuit diagram view of connection of conductive path from the coils in series to the electrically-conductive and ferromagnetic tapered tip members of the rotor, of an axial flux wind turbine 100 according to the preferred embodiment of the present invention.
  • FIG. 7 is a partial perspective view of the rotor shaft magnetically levitated by the two electrically-conductive permanent magnets mounted on the support frame assembly. As for illustration purpose, views of rotor plate substrate, air core coils, blades and support frame assembly are not shown
  • FIG. 1 , FIG. 2 and FIG. 3 show a perspective view, an exploded view and a cross-sectional view respectively of a horizontal axis rotor axial flux wind turbine 100 according to the preferred embodiment of the present invention.
  • the horizontal axis rotor axial flux wind turbine 100 comprising a rotor shaft 110, two permanent magnet stators 120, an air core coils rotor 140 with a plurality of blades 145 coupled with, a support frame assembly 150 and two wires 155.
  • Fig. 4 shows a rotor shaft 110 according to the preferred embodiment 100 of the present invention.
  • the rotor shaft 110 comprising an electrically-non-conductive rotor shaft body 111 and electrically-conductive and ferromagnetic tapered tip member 112 on both end portions.
  • the shape of the electrically-conductive and ferromagnetic tapered tip member 112 on both end portions of the rotor shaft 110 may be cone, multi-angular pyramid, sphere, hemisphere or combinations thereof without limitation herein.
  • Fig. 5 shows an air core coils rotor 140 according to the preferred embodiment 100 of the present invention.
  • the air core coils rotor 140 comprising a rotor shaft 110, a rotor plate substrate 141, a plurality of air core coil 142 circumferentially mounted on the rotor plate substrate 141, and a plurality of blades 145 coupled to the outer rim of rotor plate substrate 141.
  • blades rotor diameter is 100mm.
  • the plurality of air core coil 142 are connected in series.
  • One end of the air core coil 142 lead of the series connected air core coils is coupled on the electrically-conductive and ferromagnetic tapered tip member 112, wherein the other end of the air core coil 142 lead of the series connected air core coil 142 is coupled on the other electrically-conductive and ferromagnetic tapered tip member 112 (not shown in Fig 5).
  • the series connection of air core coil 142 to both electrically-conductive and ferromagnetic tapered tip member 112 can be understood by viewing on circuit diagram Fig. 6.
  • SUBSTITUTE SHEET (RULE 26) conductive permanent magnet 153 on both side of the support frame assembly 150, as can be seen in FIG. 3.
  • the electrical connections from the said electrically-conductive permanent magnets 153 is then further electrically connected to external circuit for direct current rectification and/or load via both wires 155.
  • the air core coils rotor 140 is disposed in the air gap between the two permanent magnet stators 120.
  • the rotor plate substrate 141 is made from non-magnetic and electrically-non-conductive material and has a thickness of 3mm, wherein each annular shape air core coil 142 having insulated copper wire diameter of 0.12mm, an outer annular diameter of 12mm, an inner annular diameter of 6mm and a thickness of 3mm.
  • the plurality of air core coil 142 is two, correspond to eight permanent magnets 122 on the stator to generate same phase alternating current.
  • the plurality of air core coil 142 may vary as long as the plurality of air core coil 142 are in same phase with relation to the plurality of permanent magnets 122.
  • each of the two permanent magnet stators 120 comprising a stator plate substrate 121 and a plurality of permanent magnets 122 circumferentially mounted thereon and also disposed in N-S-N arrangement.
  • One of the permanent magnet stators 120 is coupled on the windward side support frame member 151, the other permanent magnet stator 120 is coupled on the leeward side support frame member 152.
  • the two permanent magnet stators 120 are spaced apart from one another by an air gap, wherein the north pole of a permanent magnet 122 on one of the permanent magnet stator 120 is facing a south pole of a permanent magnet 122 on the other permanent magnet stator 120 and vice versa.
  • the stator plate substrate 121 is made from an electrically-non-conductive, non-ferromagnetic material which is light in weight.
  • the stator plate substrate 121 has a diameter of 32mm and a thickness of 3mm
  • the permanent magnet 122 is neodymium type, disc-shape and has a diameter of 6mm and a thickness of 3mm
  • the air gap between two permanent magnet stators 120 is 5mm.
  • the number of permanent magnets 122 mounted on each stator plate substrate 121 is eight, correspond to two air core coil 142 on air core coils rotor 140 for generating alternating current of same phase by each air core coil 142, upon rotating and cutting through magnetic field.
  • the plurality of permanent magnet 122 may vary as long as the plurality of permanent magnet 122 are in same phase correspond to the plurality of air core coil 142.
  • Fig. 1 and Fig. 3 show a support frame assembly 150 that providing magnetic levitation to the rotor shaft 110 and also fixing two permanent magnet stators 120, according to the preferred embodiment 100 of the present invention.
  • the support frame assembly 150 comprising a windward side support frame member 151 with an electrically-conductive permanent magnet 153 mounted and a leeward side support frame member 152 with an electrically-conductive permanent magnet 153 mounted.
  • a windward side support frame member 151 with an electrically-conductive permanent magnet 153 mounted mounted and a leeward side support frame member 152 with an electrically-conductive permanent magnet 153 mounted.
  • a leeward side support frame member 152 with an electrically-conductive permanent magnet 153 mounted.
  • SUBSTITUTE SHEET (RULE 26) plurality of fasteners 154 may be used for fastening both windward side and leeward side support frame member 151, 152 together as a support frame assembly 150.
  • the fixing of the support frame assembly 150 from both windward side support frame member 151 and leeward side support frame member 152 can be also other methods of fixing, instead of fastening with a plurality of fasteners as given as example in the prototype of the preferred embodiments 100 of the present invention.
  • the electrically-conductive and ferromagnetic tapered tip members 112 on both end portions of the rotor shaft 110 are attracted to the electrically-conductive permanent magnets 153 mounted on both windward side and leeward side support frame member 151, 152 as illustrated in Fig. 3 and Fig. 7, with a single point of contact.
  • the electrically-conductive and ferromagnetic tapered tip member 112 must coincide with the axis of the two electrically-conductive permanent magnets 153 mounted on windward side and leeward side support frame members 151, 152, in order to achieve magnetic levitation to the rotor shaft 110 with a near zero rotational friction value.
  • a very low starting torque produced by a very low wind speed is sufficient to rotate the rotor shaft 110 that coupled with an air core coils rotor 140 and a plurality of blades 145 and start to generate electrical power.
  • disc-shape permanent magnets 122 are shown in the preferred embodiment 100 of the present invention as example, shape of permanent magnet 122 may be also in arc, trapezoidal, rectangular or any other suitable shape, though not shown in the drawing.
  • Fig. 1, 2, 3 show a nose cone 160 may be coupled on the windward side support frame member 151, providing a streamline wind directly flow through blades, instead of hitting on stator plate substrate 121 area which may cause turbulent and affecting performance of the present invention, if without nose cone in used.
  • annular shape air core coil 142 which are easy to be manufactured and winding are shown in the prototype of the preferred embodiment 100 of the present invention, for example, shape of air core coil 142 may be also in arc, trapezoidal, rectangular or any other suitable shape, though not shown in the drawing.
  • the prototype of the present invention generates electrical power from wind speed as low as 1.2m/s.
  • human walking speed is 1.4m/s.

Abstract

The present invention related to horizontal axis rotor axial flux miniature wind turbine that comprising rotor shaft, permanent magnets coupled on stators, air core coils coupled on rotor shaft, blades and support frame assembly. It uses magnetic levitation to the rotor, in order to eliminate rotor rotational contact friction. It uses bamboo skin airfoil blades that have high aerodynamic lift, high stiffness and low density as compare to glass fiber. The present invention is generating electrical power from very low wind speed upward.

Description

MAGNETICALLY LEVITATED HORIZONTAL AXIS ROTOR, AXIAL FLUX WIND TURBINE
FIELD OF INVENTION
The present invention related to horizontal axis rotor axial flux miniature wind turbine, in particular axial flux miniature wind turbine with magnetically levitated horizontal axis rotor.
BACKGROUND ARTS
Current horizontal axis rotor, axial flux wind turbine typically uses bearings to support rotor. Drawback of current design is that it has bearing rotor contact friction, preventing wind turbine from generating power at very low wind speed. Therefore, problem to be solved is to eliminate rotor contact friction, so that invented wind turbine can generate power at very low wind speed with high efficiency.
DEFINITION OF TERMS
“Axial flux”: means the lines of magnetic flux that pass through the coils of wire, travel along the "axis" of the rotating motion.
“Rotor”: is a rotating component coupled to the rotor of axial flux wind turbine.
“Stator”: is a stationary component coupled to the support frame assembly of axial flux wind turbine. “Permanent magnet”: is a magnet that retains its magnetic properties in the absence of an inducing field or current.
“Air core coil”: is a type of insulated wire winding coil that has no ferrite core inside the coil. “Permanent magnet stator”: is a stator comprising a plate substrate and a plurality of permanent magnets mounted therein.
“Air core coils rotor”: is a rotor comprising a plate substrate with a plurality of air core coil mounted therein.
“Rotor solidity” is the ratio of total blade area to total swept area.
SUMMARY OF THE INVENTION
The following summary is provided to facilitate an understanding of some of the innovative features unique to the embodiments present and is not intended to be a full description. A full appreciation of the various aspects of the embodiments can be gained by taking the entire specifications, claims, drawings, and abstract as a whole.
SUBSTITUTE SHEET (RULE 26) It is the primary object of the present invention to provide horizontal axis rotor wind turbine that start to generate electrical power at minimum operating wind speed of at least 1.2m/s.
In order to achieve this primary object of having minimum operating wind speed of at least 1.2m/s, the present invention propose a novel design of magnetic levitation to the rotor, without the use of bearings to support the rotor as seen in prior arts which has significant bearing contact friction while operating at a very low wind speed. The magnetic levitation to the rotor is achieved by having ferromagnetic tapered tip members on both end portions of the rotor shaft, which attracted to the permanent magnets that are mounted on both windward side and leeward side of the support frame assembly. The magnetic levitation to the rotor shaft minimizes the rotating mechanical frictions to a near zero value. As such, a very low starting torque generated by a very low wind speed such as 1.2m/s that passing through the rotor blades is sufficient to rotate the rotor and electrical power is then generated.
It is another object of the present invention to increase the rotor rotational speed at very low wind speed, because the fact that generated electric power is proportional to the square of the rotor rotational speed. In order to increase the rotor rotational speed, the rotor structure needs to have a higher aerodynamic lift force and a lower moment of inertia. One way to reduce moment inertia is to use rotor components which have a lower density and weight. However, on the other hand, in order to ensure that the rotor structure can withstand strong wind without getting any damage, the selection of lower density rotor components need to have a high modulus of elasticity MOE and thus high stiffness.
It is another object of the present invention to increase the rotor solidity up to an optimum condition whereby the starting torque generated by wind speed of at least 1.2m/s enable rotor rotating that start producing electric power.
In order to achieve the objects just described, the present invention disposed the novel use of bamboo skin as rotor blades. The bamboo skin blades are characterized in high aerodynamic lift force, high stiffness and low material density.
The preferred embodiment of the present invention comprising two permanent magnet stators, an air core coils rotor coupled with a plurality of blades, a support frame assembly and two wires for external electrical output connection, wherein the rotor comprising electrically-conductive and ferromagnetic tapered tip members on both end portions, wherein the plurality of blades are made from bamboo skin, wherein the alternating current circuit generated out from the air core coils rotor is electrically connected to both electrically-conductive and ferromagnetic tapered tip member at the end portions of the rotor to the electrically-conductive permanent magnets that are mounted on the support frame assembly, and then connected to external circuit for direct current rectification and/or load via two wires.
These and other objectives of the present invention will become readily apparent upon further review of the following specifications and drawings.
SUBSTITUTE SHEET (RULE 26) BRIEF DESCRIPTION OF THE DRAWINGS
The present invention will become more fully understood from the subsequent detailed descriptions and accompanying drawings, which are given by way of illustration only, and thus are not limitative of the present invention, and wherein;
FIG. 1 is a perspective view of an axial flux wind turbine 100 according to the preferred embodiment of the present invention;
FIG. 2 is an exploded view of an axial flux wind turbine 100 according to the preferred embodiment of the present invention;
FIG. 3 is a cross-sectional view taken along line S-S in FIG 1, of an axial flux wind turbine 100 according to the preferred embodiment of the present invention;
FIG. 4 is a perspective view of the rotor with the electrically-conductive and ferromagnetic tapered tip members mounted on both end portions of the rotor, of an axial flux wind turbine 100 according to the preferred embodiment of the present invention;
FIG. 5 is a perspective view of the air core coils rotor of an axial flux wind turbine 100 according to the preferred embodiment of the present invention;
FIG. 6 is a circuit diagram view of connection of conductive path from the coils in series to the electrically-conductive and ferromagnetic tapered tip members of the rotor, of an axial flux wind turbine 100 according to the preferred embodiment of the present invention.
FIG. 7 is a partial perspective view of the rotor shaft magnetically levitated by the two electrically-conductive permanent magnets mounted on the support frame assembly. As for illustration purpose, views of rotor plate substrate, air core coils, blades and support frame assembly are not shown
SUBSTITUTE SHEET (RULE 26) DETAILED DESCRIPTION OF THE INVENTION
The present invention now will be described more fully hereinafter with reference to the accompanying drawings, in which preferred embodiments of the invention are shown. The invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided, so that this disclosure will be thorough and complete, and will fully convey the scope of the present invention to those skilled in the art.
Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which the present invention belongs. The methods and examples provided herein are illustrative only, and not intended to be limiting.
FIG. 1 , FIG. 2 and FIG. 3 show a perspective view, an exploded view and a cross-sectional view respectively of a horizontal axis rotor axial flux wind turbine 100 according to the preferred embodiment of the present invention.
The horizontal axis rotor axial flux wind turbine 100 comprising a rotor shaft 110, two permanent magnet stators 120, an air core coils rotor 140 with a plurality of blades 145 coupled with, a support frame assembly 150 and two wires 155.
Fig. 4 shows a rotor shaft 110 according to the preferred embodiment 100 of the present invention. The rotor shaft 110 comprising an electrically-non-conductive rotor shaft body 111 and electrically-conductive and ferromagnetic tapered tip member 112 on both end portions. The shape of the electrically-conductive and ferromagnetic tapered tip member 112 on both end portions of the rotor shaft 110 may be cone, multi-angular pyramid, sphere, hemisphere or combinations thereof without limitation herein.
Fig. 5 shows an air core coils rotor 140 according to the preferred embodiment 100 of the present invention. The air core coils rotor 140 comprising a rotor shaft 110, a rotor plate substrate 141, a plurality of air core coil 142 circumferentially mounted on the rotor plate substrate 141, and a plurality of blades 145 coupled to the outer rim of rotor plate substrate 141. In the prototype of the preferred embodiment 100 of the present invention, for example, blades rotor diameter is 100mm. The plurality of air core coil 142 are connected in series. One end of the air core coil 142 lead of the series connected air core coils is coupled on the electrically-conductive and ferromagnetic tapered tip member 112, wherein the other end of the air core coil 142 lead of the series connected air core coil 142 is coupled on the other electrically-conductive and ferromagnetic tapered tip member 112 (not shown in Fig 5). The series connection of air core coil 142 to both electrically-conductive and ferromagnetic tapered tip member 112 can be understood by viewing on circuit diagram Fig. 6.
The electrical connections from the said electrically-conductive and ferromagnetic tapered tip members 112 of rotor shaft 110 is then further electrically connected to both of the electrically-
SUBSTITUTE SHEET (RULE 26) conductive permanent magnet 153 on both side of the support frame assembly 150, as can be seen in FIG. 3. The electrical connections from the said electrically-conductive permanent magnets 153 is then further electrically connected to external circuit for direct current rectification and/or load via both wires 155.
The air core coils rotor 140 is disposed in the air gap between the two permanent magnet stators 120. In the prototype of the preferred embodiment 100 of the present invention, for example, the rotor plate substrate 141 is made from non-magnetic and electrically-non-conductive material and has a thickness of 3mm, wherein each annular shape air core coil 142 having insulated copper wire diameter of 0.12mm, an outer annular diameter of 12mm, an inner annular diameter of 6mm and a thickness of 3mm. The plurality of air core coil 142 is two, correspond to eight permanent magnets 122 on the stator to generate same phase alternating current. However, the plurality of air core coil 142 may vary as long as the plurality of air core coil 142 are in same phase with relation to the plurality of permanent magnets 122.
In the preferred embodiment 100 of the present invention, for example, each of the two permanent magnet stators 120 comprising a stator plate substrate 121 and a plurality of permanent magnets 122 circumferentially mounted thereon and also disposed in N-S-N arrangement. One of the permanent magnet stators 120 is coupled on the windward side support frame member 151, the other permanent magnet stator 120 is coupled on the leeward side support frame member 152. The two permanent magnet stators 120 are spaced apart from one another by an air gap, wherein the north pole of a permanent magnet 122 on one of the permanent magnet stator 120 is facing a south pole of a permanent magnet 122 on the other permanent magnet stator 120 and vice versa.
In the prototype of the preferred embodiment 100 of the present invention, for example, the stator plate substrate 121 is made from an electrically-non-conductive, non-ferromagnetic material which is light in weight. The stator plate substrate 121 has a diameter of 32mm and a thickness of 3mm, the permanent magnet 122 is neodymium type, disc-shape and has a diameter of 6mm and a thickness of 3mm, and the air gap between two permanent magnet stators 120 is 5mm.
The number of permanent magnets 122 mounted on each stator plate substrate 121 is eight, correspond to two air core coil 142 on air core coils rotor 140 for generating alternating current of same phase by each air core coil 142, upon rotating and cutting through magnetic field. However, the plurality of permanent magnet 122 may vary as long as the plurality of permanent magnet 122 are in same phase correspond to the plurality of air core coil 142.
Fig. 1 and Fig. 3 show a support frame assembly 150 that providing magnetic levitation to the rotor shaft 110 and also fixing two permanent magnet stators 120, according to the preferred embodiment 100 of the present invention. The support frame assembly 150 comprising a windward side support frame member 151 with an electrically-conductive permanent magnet 153 mounted and a leeward side support frame member 152 with an electrically-conductive permanent magnet 153 mounted. In the prototype of the preferred embodiment 100 of the present invention, for example, a
SUBSTITUTE SHEET (RULE 26) plurality of fasteners 154 may be used for fastening both windward side and leeward side support frame member 151, 152 together as a support frame assembly 150. However, the fixing of the support frame assembly 150 from both windward side support frame member 151 and leeward side support frame member 152 can be also other methods of fixing, instead of fastening with a plurality of fasteners as given as example in the prototype of the preferred embodiments 100 of the present invention.
The electrically-conductive and ferromagnetic tapered tip members 112 on both end portions of the rotor shaft 110 are attracted to the electrically-conductive permanent magnets 153 mounted on both windward side and leeward side support frame member 151, 152 as illustrated in Fig. 3 and Fig. 7, with a single point of contact. The electrically-conductive and ferromagnetic tapered tip member 112 must coincide with the axis of the two electrically-conductive permanent magnets 153 mounted on windward side and leeward side support frame members 151, 152, in order to achieve magnetic levitation to the rotor shaft 110 with a near zero rotational friction value. With a near zero rotational friction value, a very low starting torque produced by a very low wind speed, such as 1.2m/s, is sufficient to rotate the rotor shaft 110 that coupled with an air core coils rotor 140 and a plurality of blades 145 and start to generate electrical power.
Although disc-shape permanent magnets 122 are shown in the preferred embodiment 100 of the present invention as example, shape of permanent magnet 122 may be also in arc, trapezoidal, rectangular or any other suitable shape, though not shown in the drawing.
Fig. 1, 2, 3 show a nose cone 160 may be coupled on the windward side support frame member 151, providing a streamline wind directly flow through blades, instead of hitting on stator plate substrate 121 area which may cause turbulent and affecting performance of the present invention, if without nose cone in used.
Although annular shape air core coil 142 which are easy to be manufactured and winding are shown in the prototype of the preferred embodiment 100 of the present invention, for example, shape of air core coil 142 may be also in arc, trapezoidal, rectangular or any other suitable shape, though not shown in the drawing.
In the preferred embodiment 100 of the present invention and according to the dimensions and specifications provided in the example, the prototype of the present invention generates electrical power from wind speed as low as 1.2m/s. Typically, human walking speed is 1.4m/s. By holding the present invention during walking and without any ambient wind, the walking induced wind is sufficient for the present invention to generate power.
Finally, the forgoing examples are not intended to limit the scope of the invention disclosed herein, which is set forth in the following claims. In particular, various equivalents and substitutions will be recognized by those of ordinary skill in the art in view of the foregoing disclosure, and these are contemplated to be within the scope of the invention disclosed herein.
SUBSTITUTE SHEET (RULE 26)

Claims

7 What is claim is:
1. An axial flux wind turbine (100) comprising: a rotor shaft (110) comprising an electrically-non-conductive rotor shaft body (111) and two electrically-conductive and ferromagnetic tapered tip members (112) on both end portions of the rotor shaft body (111); two permanent magnet stators (120), wherein each permanent magnet stator (120) comprising a stator plate substrate (121) with a plurality of permanent magnets (122) circumferentially mounted, wherein one permanent magnet stator (120) is coupled on the windward side support frame member (151), wherein the other permanent magnet stator (120) is coupled on the leeward side support frame member (152), wherein the two permanent magnet stators (120) are spaced apart from one another by an air gap; an air core coils rotor (140) comprising a rotor plate substrate (141), a plurality of air core coil (142) circumferentially mounted and series connected on rotor plate substrate (141), wherein one end of series connected air core coil (142) lead is connected to one of the electrically- conductive and ferromagnetic tapered tip member (112) at one end portion of the rotor shaft (110), wherein the other end of series connected air core coil (142) lead is connected to the other electrically-conductive and ferromagnetic tapered tip member (112) on the other end portion of the rotor shaft (110), wherein the air core coils rotor (140) is coupled to the rotor shaft (110), wherein the air core coils rotor (140) is disposed in the air gap between the two permanent magnet stators (120); a plurality of blades (145) coupled to the outer edge of the rotor plate substrate (141); and a support frame assembly (150) comprising a windward side support frame member (151) with an electrically-conductive permanent magnet (153) mounted therein and a leeward side support frame member (152) with an electrically-conductive permanent magnet (153) mounted therein, wherein the electrically-conductive permanent magnets (153) mounted on both windward side and leeward side support frame member (151, 152) are aligned on the same axis, providing magnetic levitation to the rotor shaft (110) by mean of ferromagnetic attraction formed by the electrically-conductive permanent magnets (153) to the electrically- conductive and ferromagnetic tapered tip member (112) on both end portions of the rotor shaft (HO).
SUBSTITUTE SHEET (RULE 26) 8 The axial flux wind turbine according to claim 1, wherein the plurality of blades (145) is made from bamboo skin. The axial flux wind turbine according to claim 1, wherein one end of the first wire (155) is coupled to the electrically-conductive permanent magnet (153) on the windward side support frame member (151), while the other end of the first wire (155) is disposed for connecting to external circuit and/or load, wherein one end of the second wire (155) is coupled to the electrically-conductive permanent magnet (153) on the leeward side support frame member (152), while the other end of the second wire (155) is disposed for connecting to external circuit and/or load.
SUBSTITUTE SHEET (RULE 26)
PCT/MY2022/050103 2021-12-16 2022-11-04 Magnetically levitated horizontal axis rotor, axial flux wind turbine WO2023113590A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
MYPI2021007520 2021-12-16
MYPI2021007520 2021-12-16

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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6710489B1 (en) * 2001-08-30 2004-03-23 Indigo Energy, Inc. Axially free flywheel system
WO2009100443A2 (en) * 2008-02-10 2009-08-13 Empire Magnetics Inc. Axial gap electric dynamo machine with magnetic bearing
EP2536009A1 (en) * 2010-02-08 2012-12-19 National Wind Energy Co. Ltd. Magnetic levitation supporting structure for vertical shaft disc-type motor
KR20130050299A (en) * 2010-04-09 2013-05-15 스웨이 터빈 에이에스 Wind turbine rotor and wind turbine
US20150028590A1 (en) * 2006-12-20 2015-01-29 Unimodal Systems Llc Modular electric generator for variable speed turbines

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6710489B1 (en) * 2001-08-30 2004-03-23 Indigo Energy, Inc. Axially free flywheel system
US20150028590A1 (en) * 2006-12-20 2015-01-29 Unimodal Systems Llc Modular electric generator for variable speed turbines
WO2009100443A2 (en) * 2008-02-10 2009-08-13 Empire Magnetics Inc. Axial gap electric dynamo machine with magnetic bearing
EP2536009A1 (en) * 2010-02-08 2012-12-19 National Wind Energy Co. Ltd. Magnetic levitation supporting structure for vertical shaft disc-type motor
KR20130050299A (en) * 2010-04-09 2013-05-15 스웨이 터빈 에이에스 Wind turbine rotor and wind turbine

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