WO2004107549A1 - Homopolar electro-mechanical rotary power converter - Google Patents

Homopolar electro-mechanical rotary power converter Download PDF

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Publication number
WO2004107549A1
WO2004107549A1 PCT/GB2004/001501 GB2004001501W WO2004107549A1 WO 2004107549 A1 WO2004107549 A1 WO 2004107549A1 GB 2004001501 W GB2004001501 W GB 2004001501W WO 2004107549 A1 WO2004107549 A1 WO 2004107549A1
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WO
WIPO (PCT)
Prior art keywords
rotor
stator
winding
windings
phase
Prior art date
Application number
PCT/GB2004/001501
Other languages
French (fr)
Inventor
Michael Owen
Original Assignee
Michael Owen
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 Michael Owen filed Critical Michael Owen
Priority to EP04726562A priority Critical patent/EP1629592A1/en
Publication of WO2004107549A1 publication Critical patent/WO2004107549A1/en

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Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K47/00Dynamo-electric converters
    • H02K47/02AC/DC converters or vice versa
    • H02K47/08Single-armature converters
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02MAPPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M7/00Conversion of ac power input into dc power output; Conversion of dc power input into ac power output
    • H02M7/003Constructional details, e.g. physical layout, assembly, wiring or busbar connections
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02MAPPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M7/00Conversion of ac power input into dc power output; Conversion of dc power input into ac power output
    • H02M7/42Conversion of dc power input into ac power output without possibility of reversal
    • H02M7/54Conversion of dc power input into ac power output without possibility of reversal by dynamic converters

Definitions

  • Electro-mechanical Rotary Power Converters are used for converting incoming electrical energy into outgoing electrical energy.
  • the energy transformation may be either an incoming Direct Current (DC) to outgoing single or polyphase Alternating Current (AC); or an incoming single or polyphase AC to outgoing DC; or an incoming single or polyphase AC to outgoing polyphase or single phase AC.
  • the ERPC rotor is driven by a motor to facilitate the electromagnetic phenomena, however in an ideal converter, the energy supplied by the motor, apart from accelerating the inertia! mass to its steady state speed, only feeds mechanical losses within the converter.
  • HVDC Power Electronic Converter In the rectifier mode, breaks up the AC waveform and reconstructs it into DC. It does the same in the inverter mode from DC to AC.
  • the disarrangement - rearrangement however is not a straight process reversal between the rectifier and inverter.
  • the resulting pieced together waveforms are imperfect and contain harmonics. Energy losses occur due to conduction and switching in the semiconductor devices. Reduction of the harmonics is possible by filtering, however energy losses are then also incurred in the filters. The overall amount of equipment required is substantial and costly. Because of their complexity and size, HVDC PECs are generally air insulated. The converter chambers contain exposed live parts and staff must follow special procedures when working within their vicinity.
  • ERPC namely the (Homopolar) HERPC
  • the HERPC would be substantially safer by not having exposed live parts; be relatively small and compact consisting only of a small number of assembled parts; be easy to manufacture due to its rotating homopolar machine construction; be extremely reliable, similar to that of an AC motor; have a high efficiency; retain the very stable output voltage level characteristic of the ERPC; and as with the transformer, the terminal output voltage would be determined in part by the number of turns on the respective windings. As an inverter it would develop near perfect AC waveforms.
  • Fig. 1 shows the basic arrangement for the Rotary Power Converter.
  • the upper part represents a cross section along axis of rotation.
  • Three other cross sections, perpendicular to the axis of rotation, at defining locations, are also depicted.
  • Fig. 2 shows the electrical interconnections between the coils, the source of DC excitation and load burdens connected to the three phase AC output coils.
  • Fig. 3 shows the mathematical function used for a particular shape of the stator AC winding limb face.
  • Fig. 4 shows the progression of the magnetically conductive portion of the rotor (rectangular section) across the stator limb faces at intervals of 30° degrees.
  • Magnetically conductive rotor parts 4.
  • Non-magnetically conductive rotor parts 5.
  • Each AC phase winding has coils 6, that encircle each stator limb that bears a pole 11 , in the respective phase set.
  • a principal winding 2 has coils that encircle all the stator limbs that bear poles 11 , on all the phase sets.
  • the principal winding is wound such that with a constant DC source, the flux always flows either radially inwards or radially outwards in all pole bearing stator limbs 11.
  • Energy conversion is performed by varying the reluctance of the three-phase sections of the magnetic circuit through turning the rotor.
  • the rotor 4 & 5 has no windings. Its function is to divert the magnetic flux on a time varying basis through each of the three-phase windings 6, on the stator pole limbs 11. It consists of some magnetically conducting portions 4, and some non-magnetically conducting portions 5. The non-magnetic portions 5, are required to channel the flux and prevent magnetic short circuits.
  • the output AC waveforms are determined by the shape of the AC winding limb faces.
  • the induced AC voltage is proportional to the rate of change of flux passing through the winding.
  • the flux however is distributed in proportion to the reluctance of the magnetic circuits - which is in turn proportional to the overlapping areas between the passing rotor and stator faces.
  • Fig. 3 The mathematical function used for a particular shape of the stator AC winding limb face is shown in Fig. 3. It shows an area that changes in the form of a sinusoid. It is created from a function that is itself the combination of a positive and negative sinusoid.
  • the sum of all the three-phase AC fluxes is equal to the flux flowing through the stator body 3.
  • the sum of all the three-phase AC fluxes also equates to the total flux generated by the principal winding 2.
  • the reluctance of the stator body, and all magnetic circuit paths in parallel with it remain constant.
  • Fig. 4 the overlapping area between all facing rotor and stator parts 14, is shown at intervals of 30 degrees. In particular it shows how the area corresponding to each phase, changes in a sinusoidal pattern 15, as a result of the shape of the AC winding limb faces.
  • An auxiliary motor 1 drives the rotor 4 & 5, at the appropriate speed to generate the desired output AC frequency. Unlike an alternator, no electromagnetic restraining force acts. The driving torque is required for inertial accelerations and to counter friction and windage losses.
  • the magnetic circuits are arranged such that flux links through windings rather than cutting across conductors.
  • a non-magnetically conductive spacer 8 is incorporated in the stator body 3.
  • the spacer is secured by means of a non-magnetically conductive locating pin 9.
  • Fig. 1 show two AC winding coils 6, per phase. As the rotor turns through one complete rotation, one frequency cycle of flux passes through each of the coils.
  • Fig. 2 therefore shows two series connected coils per phase, resulting in two cycles of output current per revolution of the rotor.
  • Frequency conversion also occurs between the input and output currents.
  • the frequency transformation is determined by the speed of the driven rotor.
  • the HERPC may be used to power installations from land based Combined Cycle Gas Turbine onshore power plants.
  • HVDC cables By interconnecting using HVDC cables, and replacing offshore Gas Turbines with electric motors, more reliable and near maintenance free offshore facilities with overall reductions in C0 2 emissions would be possible.
  • the HERPC could replace the PEC inverter, especially for the power conditioning of fuel cell output.
  • the HERPC may alternatively be applied as a brushless Synchro, generally used for position sensing applications, in which case the principal winding would be excited from an AC source.

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Inverter Devices (AREA)

Abstract

The Homopolar Electro-mechanical Rotary Power Converter, converts electrical, but not mechanical energy. It may act as: an inverter of DC to polyphase AC; a converter of single phase AC to polyphase AC; or a converter of polyphase AC to single phase AC. The output waveform(s) shape(s) are governed by the shapes of the stator and rotor pole faces. The rotor (4) and (5), which is driven by a motor (1), has magnetically conductive segments (4) and carries no windings. The torque supplied to the rotor is only necessary for inertial accelerations and to counter mechanical energy losses. The reluctance of the main magnetic circuit remains constant. The subsections vary their reluctance with the position of the rotor. The device is homopolar because, when excited by DC, all flux paths are unidirectional and are channelled through the stator body (3) to the rotor pole. The speed of the rotor determines the output frequency.

Description

Homopolar Electro-mechanical Rotary Power Converter.
Technical Field.
Electro-mechanical Rotary Power Converters (ERPCs) are used for converting incoming electrical energy into outgoing electrical energy. The energy transformation may be either an incoming Direct Current (DC) to outgoing single or polyphase Alternating Current (AC); or an incoming single or polyphase AC to outgoing DC; or an incoming single or polyphase AC to outgoing polyphase or single phase AC. The ERPC rotor is driven by a motor to facilitate the electromagnetic phenomena, however in an ideal converter, the energy supplied by the motor, apart from accelerating the inertia! mass to its steady state speed, only feeds mechanical losses within the converter.
Background Art.
Edison in the late 1870s first established the electric power business. Power was generated and distributed as DC, because then only DC motors existed. Very soon however, Westinghouse employed Stanley, who in 1886 developed an effective transformer. Later, in 1888 Westinghouse purchased the patents for Tesla's AC induction motor. By 1890 the Westinghouse Company was installing substantial high voltage AC transmission systems feeding lower voltage distribution systems. Until 1920, the AC and DC systems were largely competitive due to the AC to DC rotary converter, which could supply power to the commonplace DC motors. Demands for higher power levels and longer circuits however required higher voltages. Eventually DC power systems were constrained by the voltage factor. The AC systems due to the transformer, could apply the higher voltages with ease. This led to the dominance of AC over DC. DC however is now emerging as an effective and sometimes superior power transmission alternative. The resurgence of HVDC started in the 1930s and 40s when during World War II the Germans developed plans to implement an HVDC link using electronic mercury arc valves. These were to be configured as AC to DC and DC to AC power converters. The war however prevented its implementation. After the war in 1950, the Russians adopted the plans and built a successful 120kV, 65 mile long line from Moscow. From that initial scheme, HVDC power transmission has developed via power electronics through mercury arc valves, to semiconductor thyristors and latterly transistors. Now many of the world's largest power transmission schemes apply HVDC. As power and distance limits have increased over the years, it is the turn of AC transmission schemes to be constrained. Excessive currents due to line charging and line voltage instability set power transfer limits, especially in cable systems. Power companies have consequently been turning to HVDC transmission.
To operate, a modern HVDC Power Electronic Converter (PEC), in the rectifier mode, breaks up the AC waveform and reconstructs it into DC. It does the same in the inverter mode from DC to AC. The disarrangement - rearrangement however is not a straight process reversal between the rectifier and inverter. The resulting pieced together waveforms are imperfect and contain harmonics. Energy losses occur due to conduction and switching in the semiconductor devices. Reduction of the harmonics is possible by filtering, however energy losses are then also incurred in the filters. The overall amount of equipment required is substantial and costly. Because of their complexity and size, HVDC PECs are generally air insulated. The converter chambers contain exposed live parts and staff must follow special procedures when working within their vicinity.
In the aircraft industry multi-polar ERPCs (Moffit, G.R. "Variable reluctance device". US patent, 3041486, 6/1962) have been used for DC to polyphase AC conversion at 400Hz. A particular feature of the ERPC is its ability to maintain a very stable output voltage level when its input DC is controlled to a constant level. The number of poles and winding arrangement that these devices employ however restrict their suitability for 'utility' sized machines.
In the field of energy production, some devices such as fuel cells inherently produce DC at a relatively low voltage. Most power systems however utilise AC at a substantially higher voltage. To be useful for the bulk supply of electrical energy, the output of a fuel cell would typically be converted to AC using a PEC, and then the PEC output voltage boosted to utility levels by a conventional transformer. An ERPC that combines both of these operations could replace both the PEC and transformer.
Disclosure of Invention.
A new form of ERPC, namely the (Homopolar) HERPC is disclosed. It has many advantages over the multi-polar ERPC, the PEC, and the PEC-transformer combination.
The HERPC would be substantially safer by not having exposed live parts; be relatively small and compact consisting only of a small number of assembled parts; be easy to manufacture due to its rotating homopolar machine construction; be extremely reliable, similar to that of an AC motor; have a high efficiency; retain the very stable output voltage level characteristic of the ERPC; and as with the transformer, the terminal output voltage would be determined in part by the number of turns on the respective windings. As an inverter it would develop near perfect AC waveforms.
Brief Description of Drawings.
The following figures illustrate an example of the device construction and the principle of operation. Other alternative arrangements are possible.
Fig. 1 shows the basic arrangement for the Rotary Power Converter. The upper part represents a cross section along axis of rotation. Three other cross sections, perpendicular to the axis of rotation, at defining locations, are also depicted.
Fig. 2 shows the electrical interconnections between the coils, the source of DC excitation and load burdens connected to the three phase AC output coils.
Fig. 3 shows the mathematical function used for a particular shape of the stator AC winding limb face. Fig. 4 shows the progression of the magnetically conductive portion of the rotor (rectangular section) across the stator limb faces at intervals of 30° degrees.
In Fig. 1 the following components and features are identified:
1. Driving motor.
2. Principal winding coil.
3. Stator body.
4. Magnetically conductive rotor parts. 5. Non-magnetically conductive rotor parts.
6. AC phase winding coil.
7. Rotor and stator surfaces meet.
8. Non-magnetically conducting spacer in stator body.
9. Non-magnetically conducting locating pin to assist assembly of stator parts. 10. Cross section through rotor and stator, perpendicular to axis of rotation.
11. Pole bearing stator limbs.
In Fig. 2 the following components and features are identified:
2. Principal winding coils. 6. AC phase winding coils.
12. Typical source of DC for the device.
13. Typical load burden for the device.
Best Mode for Carrying Out the Invention.
The description is written to describe a three-phase device, however the general principles extend to a polyphase machine.
Each AC phase winding has coils 6, that encircle each stator limb that bears a pole 11 , in the respective phase set. A principal winding 2, has coils that encircle all the stator limbs that bear poles 11 , on all the phase sets. The principal winding is wound such that with a constant DC source, the flux always flows either radially inwards or radially outwards in all pole bearing stator limbs 11.
Energy conversion is performed by varying the reluctance of the three-phase sections of the magnetic circuit through turning the rotor.
The rotor 4 & 5, has no windings. Its function is to divert the magnetic flux on a time varying basis through each of the three-phase windings 6, on the stator pole limbs 11. It consists of some magnetically conducting portions 4, and some non-magnetically conducting portions 5. The non-magnetic portions 5, are required to channel the flux and prevent magnetic short circuits. The output AC waveforms are determined by the shape of the AC winding limb faces. The induced AC voltage is proportional to the rate of change of flux passing through the winding. The flux however is distributed in proportion to the reluctance of the magnetic circuits - which is in turn proportional to the overlapping areas between the passing rotor and stator faces.
The mathematical function used for a particular shape of the stator AC winding limb face is shown in Fig. 3. It shows an area that changes in the form of a sinusoid. It is created from a function that is itself the combination of a positive and negative sinusoid.
At any one time, the sum of all the three-phase AC fluxes is equal to the flux flowing through the stator body 3. The sum of all the three-phase AC fluxes also equates to the total flux generated by the principal winding 2. The reluctance of the stator body, and all magnetic circuit paths in parallel with it remain constant.
In Fig. 4 the overlapping area between all facing rotor and stator parts 14, is shown at intervals of 30 degrees. In particular it shows how the area corresponding to each phase, changes in a sinusoidal pattern 15, as a result of the shape of the AC winding limb faces.
An auxiliary motor 1 drives the rotor 4 & 5, at the appropriate speed to generate the desired output AC frequency. Unlike an alternator, no electromagnetic restraining force acts. The driving torque is required for inertial accelerations and to counter friction and windage losses.
The magnetic circuits are arranged such that flux links through windings rather than cutting across conductors. The Lorentz force law (F=B.I.L) that applies to generators is therefore minimal. Restraining forces on the rotor are those due to friction and windage.
A non-magnetically conductive spacer 8, is incorporated in the stator body 3. The spacer is secured by means of a non-magnetically conductive locating pin 9. By adjusting the spacer thickness, the relationships between the input and output currents and voltages may be altered.
The cross sections 10, in Fig. 1 show two AC winding coils 6, per phase. As the rotor turns through one complete rotation, one frequency cycle of flux passes through each of the coils. Fig. 2 therefore shows two series connected coils per phase, resulting in two cycles of output current per revolution of the rotor.
Frequency conversion also occurs between the input and output currents. The frequency transformation is determined by the speed of the driven rotor.
Industrial Applicability. In offshore oil and gas production facilities, the HERPC may be used to power installations from land based Combined Cycle Gas Turbine onshore power plants. By interconnecting using HVDC cables, and replacing offshore Gas Turbines with electric motors, more reliable and near maintenance free offshore facilities with overall reductions in C02 emissions would be possible.
In the energy utility business the HERPC could replace the PEC inverter, especially for the power conditioning of fuel cell output.
On land based power grid systems, the likely reduction in costs and increased reliability of the HERPC plant over PECs would encourage underground cable installations in place of overhead power lines. Acquisition of the resulting narrower and un-intrusive wayleaves by energy utilities would be far easier. The elimination of overhead power lines is commonly seen as a major benefit to the environment.
The HERPC may alternatively be applied as a brushless Synchro, generally used for position sensing applications, in which case the principal winding would be excited from an AC source.

Claims

Claim.
An Electro-mechanical Rotary Power Converter that converts the form of incoming electrical energy into outgoing electrical energy without conversion of mechanical energy into electrical energy, by driving a rotor not carrying windings to divert magnetic flux into ordered paths through the stator, the stator carrying both input field excitation and output induction windings, one winding being designated the principal winding, either it being wound such that it consists of serially connected coils corresponding in number to the number of pole bearing stator limbs, with each coil arranged to encircle just one pole bearing stator limb, or it being wound as one coil encircling the stator body; the other windings being designated the Alternating Current (AC) phase windings, each phase being wound such that it consists of a coil or serially connected coils corresponding in number to the number of pole bearing stator limbs on that particular phase, with each coil arranged to encircle just one pole bearing stator limb; and the magnetic circuit being formed from a number of parallel limbs comprising both stator and rotor, into which is incorporated a non-magnetically conductive spacer that permits alteration of the relationships between the input and output currents and voltages through adjustment of its thickness; and when the principal winding is excited by Direct Current (DC), outgoing polyphase AC is produced by the AC phase windings which operate as induction windings, with output electrical frequency being controlled by manipulation of the rotor speed; and when the principal winding is excited by single phase AC, outgoing polyphase AC is produced by the AC phase windings which operate as induction windings, with output electrical frequency being controlled by manipulation of the rotor speed; and when the AC phase windings are excited by polyphase AC, outgoing single phase AC is produced by the principal winding which operates as an induction winding, with output electrical frequency being controlled by manipulation of the rotor speed; and in every case of input excitation involving rotation of the rotor, the outgoing electrical waveform shapes are determined by the time varying magnetically conducting facing rotor and stator areas on each of the limbs that supports an output induction winding; and the device is constructed such that the stator body carries the sum of the magnetic fluxes which flow into it from all the limbs that are two or more in number, with the parallel combination of all the limbs taken together having a constant reluctance that is independent of rotor and stator relative position; the Electro-mechanical Rotary Power Converter being characterised by the stator body interfacing with the rotor via magnetic circuit surfaces that have a constant overlapping area independent of the rotor's angular position, and when the principal winding is excited by a DC source, all the flux produced by the DC flows unidirectionally through the stator body, the direction being dependent upon the polarity of the DC source terminals and their interconnection with the terminals of the principal winding.
PCT/GB2004/001501 2003-05-30 2004-04-08 Homopolar electro-mechanical rotary power converter WO2004107549A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP04726562A EP1629592A1 (en) 2003-05-30 2004-04-08 Homopolar electro-mechanical rotary power converter

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0312378A GB0312378D0 (en) 2003-05-30 2003-05-30 Electro-mechanical rotary power converter
GB0312378.3 2003-05-30

Publications (1)

Publication Number Publication Date
WO2004107549A1 true WO2004107549A1 (en) 2004-12-09

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GB (1) GB0312378D0 (en)
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Cited By (16)

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Publication number Priority date Publication date Assignee Title
EP2302755A1 (en) * 2009-09-29 2011-03-30 OpenHydro IP Limited An electrical power conversion system and method
US8308422B2 (en) 2006-07-14 2012-11-13 Openhydro Group Limited Submerged hydroelectric turbines having buoyancy chambers
US8466595B2 (en) 2006-07-14 2013-06-18 Openhydro Group Limited Hydroelectric turbine
US8596964B2 (en) 2006-07-14 2013-12-03 Openhydro Group Limited Turbines having a debris release chute
US8690526B2 (en) 2008-12-18 2014-04-08 Openhydro Ip Limited Hydroelectric turbine with passive braking
US8754540B2 (en) 2008-02-05 2014-06-17 James Ives Hydroelectric turbine with floating rotor
US8784005B2 (en) 2008-04-17 2014-07-22 Openhydro Group Limited Turbine installation method
US8864439B2 (en) 2006-07-14 2014-10-21 Openhydro Ip Limited Tidal flow hydroelectric turbine
US8872371B2 (en) 2009-04-17 2014-10-28 OpenHydro IP Liminted Enhanced method of controlling the output of a hydroelectric turbine generator
US8933598B2 (en) 2009-09-29 2015-01-13 Openhydro Ip Limited Hydroelectric turbine with coil cooling
US20150073610A1 (en) * 2013-09-11 2015-03-12 General Electric Company Auxiliary electric power system and method of regulating voltages of the same
US9054512B2 (en) 2008-12-19 2015-06-09 Openhydro Ip Limited Method of installing a hydroelectric turbine generator
US9236725B2 (en) 2009-09-29 2016-01-12 Openhydro Ip Limited Hydroelectric turbine cabling system
US9234492B2 (en) 2010-12-23 2016-01-12 Openhydro Ip Limited Hydroelectric turbine testing method
US9284709B2 (en) 2007-04-11 2016-03-15 Openhydro Group Limited Method of installing a hydroelectric turbine
US9765647B2 (en) 2010-11-09 2017-09-19 Openhydro Ip Limited Hydroelectric turbine recovery system and a method therefor

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US2769106A (en) * 1953-02-06 1956-10-30 United Aircraft Corp Reaction inductor alternator
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Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8864439B2 (en) 2006-07-14 2014-10-21 Openhydro Ip Limited Tidal flow hydroelectric turbine
US8308422B2 (en) 2006-07-14 2012-11-13 Openhydro Group Limited Submerged hydroelectric turbines having buoyancy chambers
US8466595B2 (en) 2006-07-14 2013-06-18 Openhydro Group Limited Hydroelectric turbine
US8596964B2 (en) 2006-07-14 2013-12-03 Openhydro Group Limited Turbines having a debris release chute
US9284709B2 (en) 2007-04-11 2016-03-15 Openhydro Group Limited Method of installing a hydroelectric turbine
US8754540B2 (en) 2008-02-05 2014-06-17 James Ives Hydroelectric turbine with floating rotor
US8784005B2 (en) 2008-04-17 2014-07-22 Openhydro Group Limited Turbine installation method
US8690526B2 (en) 2008-12-18 2014-04-08 Openhydro Ip Limited Hydroelectric turbine with passive braking
US9054512B2 (en) 2008-12-19 2015-06-09 Openhydro Ip Limited Method of installing a hydroelectric turbine generator
US8872371B2 (en) 2009-04-17 2014-10-28 OpenHydro IP Liminted Enhanced method of controlling the output of a hydroelectric turbine generator
CN102577007A (en) * 2009-09-29 2012-07-11 开放水知识产权有限公司 An electrical power conversion system and method
WO2011039249A1 (en) * 2009-09-29 2011-04-07 Openhydro Ip Limited An electrical power conversion system and method
US8933598B2 (en) 2009-09-29 2015-01-13 Openhydro Ip Limited Hydroelectric turbine with coil cooling
US9236725B2 (en) 2009-09-29 2016-01-12 Openhydro Ip Limited Hydroelectric turbine cabling system
KR20120081170A (en) * 2009-09-29 2012-07-18 오픈하이드로 아이피 리미티드 An electrial power conversion system and method
US9473046B2 (en) 2009-09-29 2016-10-18 Openhydro Ip Limited Electrical power conversion system and method
KR101686902B1 (en) 2009-09-29 2016-12-15 오픈하이드로 아이피 리미티드 AN ELECTRIAL POWER CONVERSION SYSTEM and METHOD
EP2302755A1 (en) * 2009-09-29 2011-03-30 OpenHydro IP Limited An electrical power conversion system and method
US9765647B2 (en) 2010-11-09 2017-09-19 Openhydro Ip Limited Hydroelectric turbine recovery system and a method therefor
US9234492B2 (en) 2010-12-23 2016-01-12 Openhydro Ip Limited Hydroelectric turbine testing method
US20150073610A1 (en) * 2013-09-11 2015-03-12 General Electric Company Auxiliary electric power system and method of regulating voltages of the same
US9513614B2 (en) * 2013-09-11 2016-12-06 General Electric Company Auxiliary electric power system and method of regulating voltages of the same

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EP1629592A1 (en) 2006-03-01

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