WO2007104285A2 - Transversalflussmaschine und turbomaschine mit derartiger transversalflussmaschine - Google Patents
Transversalflussmaschine und turbomaschine mit derartiger transversalflussmaschine Download PDFInfo
- Publication number
- WO2007104285A2 WO2007104285A2 PCT/DE2007/000435 DE2007000435W WO2007104285A2 WO 2007104285 A2 WO2007104285 A2 WO 2007104285A2 DE 2007000435 W DE2007000435 W DE 2007000435W WO 2007104285 A2 WO2007104285 A2 WO 2007104285A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- stator
- stator coil
- flux machine
- transverse flux
- rotor
- Prior art date
Links
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
- H02H7/00—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions
- H02H7/08—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for dynamo-electric motors
- H02H7/0833—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for dynamo-electric motors for electric motors with control arrangements
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K21/00—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets
- H02K21/12—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets
- H02K21/24—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets axially facing the armatures, e.g. hub-type cycle dynamos
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P29/00—Arrangements for regulating or controlling electric motors, appropriate for both AC and DC motors
- H02P29/02—Providing protection against overload without automatic interruption of supply
- H02P29/032—Preventing damage to the motor, e.g. setting individual current limits for different drive conditions
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P9/00—Arrangements for controlling electric generators for the purpose of obtaining a desired output
- H02P9/006—Means for protecting the generator by using control
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K2201/00—Specific aspects not provided for in the other groups of this subclass relating to the magnetic circuits
- H02K2201/12—Transversal flux machines
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P2101/00—Special adaptation of control arrangements for generators
- H02P2101/30—Special adaptation of control arrangements for generators for aircraft
Definitions
- stator winding As generators for electrical power synchronous generators are often used. Such machines have in the embodiment as an inner rotor an outer winding (stator winding), which generates a magnetic rotating field. A pole wheel (rotor) contributes to field generation either permanent magnets or a field winding. In these induction machines, the rotor speed is equal to the number of revolutions.
- the stator is formed to reduce the eddy current losses of layered, electrically insulated from each other iron magnetic sheets.
- the stator winding is inserted in axially parallel grooves, between the radially inwardly facing poles of the stator and interconnected. The moving magnetic fields circulating through the rotor overcome the air gap between rotor and stator poles and intersect the stator windings.
- an AC voltage is generated due to the changing with each rotor circulation magnetic fields in each of the windings, whose frequency is synchronous to the rotor speed.
- the synchronous machine can generate single-phase or multi-phase AC voltage.
- the active power is determined in the generator mode by the Polradwinkel, which results in a twist angle between the rotor of the loaded machine and the unloaded machine. If the twist angle becomes too large, the engine speed increases greatly and the machine can be destroyed by the centrifugal force of its own components. It must be switched off as quickly as possible in this operating state and resynchronized. In particular, when used in the aviation sector, the electrical / mechanical access to the generator for obvious reasons is not possible.
- Machines related to their basic structure with permanent-magnet synchronous machines are transversal flux machines which have a circumferential winding in contrast to the normal machines with a diameter winding.
- the magnetic flux is transverse (perpendicular) to the plane of rotation.
- a rotor has a plurality of axially adjacent to each other arranged permanent magnet rings, consisting of individual magnets. These are oriented in the radial direction with alternating magnetic direction.
- the stator has one or more circumferential windings comprised of intermeshing soft magnetic poles. As the rotor moves relative to the stator, a magnetic alternating flux is passed through each stator coil which induces a generator voltage.
- transverse flux machines facilitates their respective dimensioning. Furthermore, the usual in synchronous machines so-called. Winding heads, which do not contribute to torque generation omitted. According to the design principle, machines operating according to the transverse flux principle can have considerably less ohmic losses than a longitudinal flux motor comparable to the magnetic thrust forces. As a result, a much finer pole pitch is possible, resulting in a large torque and higher efficiency even at low speed.
- transverse flux machines have a more complex mechanical structure. With permanently excited machines, high efficiencies can be achieved; However, the permanent magnets to be used are costly.
- the invention teaches a
- Transverse flux machine in which a rotor has a plurality of axially adjacent to each other arranged permanent magnet rings, which are formed of individual magnets with alternating magnetic direction in the radial direction, the stator surrounds the rotor concentrically to form an air gap at least partially and has one or more stator coils, coaxial with are oriented to the permanent magnet rings, a stator coil has two terminals and at its the air gap to the rotor toward side facing out of interlocking poles facing the permanent magnet rings of the rotor and each aligned with individual of the individual magnets, one to controlling active reactive power source having two terminals for each stator coil, with which the respective stator coil is connected, at least one monitoring arrangement which in case of failure in one or more stator coils drive signals for the ak tive reactive power source, so that the two terminals of the respective stator coil are connected to each other with low resistance.
- the stator coil is enclosed between two soft-magnetic stator disks, which have alternately intermeshing poles at their edge facing the air gap to the rotor.
- a continuous edge of one or both stator disks surrounds the stator coil.
- the monitoring arrangement can be of very simple construction and is set up to detect one or more of the following conditions in the transversal flux machine as an accident:
- the monitoring arrangement may be configured to detect and compare currents flowing in the stator coils of the transverse flux machine and / or voltages dropping across the stator coils in order to detect a fault in one or more stator coils.
- the monitoring arrangement may be adapted to detect by means arranged on one or more stator coils of the transverse flux machine temperature sensors heating of the affected stator coil to overloads, short circuits or the like. to detect the affected stator coil.
- the monitoring arrangement can be configured to detect ground faults of one or more stator coils of the transverse flux machine by means of a potential monitoring circuit for insulation monitoring.
- the active reactive power source may comprise two half-bridges for switching electrical power.
- the two half bridges are connected for the respective stator coil to the full bridge. It should be noted that for converting the output power provided by the transverse flux machine during operation, a converter is usually used anyway. This converter usually contains such half bridges for switching electrical powers and therefore assumes in the present inventive configuration of the turbine jet engine generator a dual function: inverter and active reactive power source.
- the two half-bridges of the active reactive power source have at least two semiconductor switches connected in series. It is also possible, depending on the (reactive) power to be switched, to connect several such series-connected semiconductor switches in parallel.
- Each of the semiconductor switches has a control input.
- the first semiconductor switch has a first power terminal which is connected to a high voltage potential connect is.
- the second semiconductor switch has a second power terminal to be connected to a low voltage potential.
- a second power terminal of each first semiconductor switch is connected to a first power terminal of the respective second semiconductor switch to form a terminal for the stator coil.
- each of the semiconductor switches may have a freewheeling diode which is parallel to the two power terminals of the respective semiconductor switch.
- the monitoring device controls the active reactive power source in case of failure of the turbine air jet engine generator so that remain in the two half bridges either the second semiconductor switches turned on and the first semiconductor switch unchecked, or the first semiconductor switches remain turned on and the second semiconductor switches remain unchecked. In both cases, a short-circuit current takes a controlled path over the respectively switched semiconductor switches.
- the invention further provides that in the
- the one for the full power delivery 00435 The one for the full power delivery 00435
- required rated current can only build up by interaction of the stator coil with a reactive power generator. Without active reactive power generator, i. In an accident, according to the invention, even in the event of a short circuit, never a magnetic flux builds up, which approximately reaches the nominal flux. Thus, even with a short circuit of the entire stator coil only a current below the nominal value. However, in the case of a short circuit of only a part of the stator coil or even only one turn, the locally flowing current can reach or even exceed the nominal value.
- a further hazard could arise at shutdown of the inverter or the associated H-bridge at high generator speeds, because then without induced field-weakening current component, the induced voltage across the freewheeling diodes could charge a downstream DC voltage intermediate circuit to impermissibly high voltages.
- the invention also protects against this by the controlled short-circuiting of the respective stator coil.
- Another significant advantage of the inventive concept is that virtually only the magnetically active components (the permanent magnets) contribute to the inertial mass of the rotor, while all other parts of the motor (coils, magnetic return, etc.) are associated with the stator. In this way, a particularly high ratio of force exerted by the electric machine to inert mass can be achieved.
- stator coil Due to the very simple design annular disc-shaped arrangement of the stator coil (s) of the electric machine, it is possible to keep the force acting on the coil shaking forces low, so that vibrations of the coil or friction of the coil on the wall of the stator coil chamber are low. This makes it possible to make do with minimal insulating material or lining material of the stator coil chamber. This also contributes to the compactness and reliability of the overall arrangement. In addition, this causes a high power density even with small inventive concepts, since the fill factor of the stator coil chamber (coil volume in the stator coil chamber based on the total volume of the stator coil chamber) is high.
- the stand can be constructed in known manner from electrical sheet metal parts. However, it is also possible to simplify the production, at least partially as a soft magnetic molded body, for example, pressed and / or sintered metal powder shape.
- the stator is made of solid iron because even with the increased dynamic requirements, the eddy current properties of solid iron are sufficient.
- transversal flux machine in the form of a generator, it is understood that hereby both a generator operation and a motor (ie driving) operation is possible.
- the term "transverse flux machine” according to the invention thus understood both generators and engines.
- the invention it is possible by the invention on the one hand to use a generator for converting the available torque in electrical power.
- the electric machine in engine operation can also put parts in rotation.
- the invention is to be realized both in the form of internal rotor machines and external rotor machines.
- the invention provides to transfer a short-circuit current between individual winding sections of the stator coil by controlled short-circuiting of the overall stator coil in a safe area.
- a short-circuit current can be performed in a danger minimized manner to the outside. This is at least E2007 / 000435
- one of the stator coils is formed from a plurality of annular sections, wherein in each case a plurality of the ring sections form a ring which is arranged concentrically to adjacent rings substantially, each ring section is connected at least one of its two ends with a radially outer or further inside ring portion, and radially completely outside or radially inwardly located ring sections are connected at one of its two ends with radially inwardly or radially outmost located annular portions.
- This aspect of the invention how to make the stator coil advantageous, can also be used independently of the reactive power source to be controlled by the monitoring arrangement with a considerable increase in intrinsic safety of the transverse flux machine according to the invention.
- the combined application offers a particularly high level of protection against accidents.
- the invention may be used to advantage in automotive or stationary applications.
- the invention is used in connection with a turbomachine, in particular a gas turbine, in particular an aircraft gas turbine, because in this context the specific advantages of the invention come into their own.
- the transverse flux machine is in particular rotatably coupled to a rotating shaft of the turbomachine.
- the transverse flux machine is advantageously coupled in the region of the low-pressure turbine to the low-pressure shaft, which is easily accessible in the rear region of the aircraft gas turbine.
- the transversal flux machine can be used as a generator or as a motor / starter.
- the transversal flux machine preferably combines both functions as a so-called starter generator in one.
- the invention may be used to advantage in automotive or stationary applications.
- Fig. 1 shows a schematic partial longitudinal sectional view of a transverse machine according to the invention as a starter generator of a gas turbine, in particular aircraft gas turbine
- Fig. 2 shows a schematic, enlarged partial view in an exploded perspective view of the electrical machine, which is shown in Fig. 1 as a starter generator.
- FIG. 3 shows a schematic representation of an active reactive power source according to the invention to be controlled, which is to be connected to the stator coil of the transverse flux machine.
- FIG. 4 shows a schematic representation of a stator coil of the transverse flux machine according to the invention in a plan view.
- a transverse flux machine is illustrated as a starter generator in partial longitudinal section.
- a rotor 52 of the generator 50 rotatably coupled on the rotating shaft 18 of the low-pressure turbine 18 (as well as the entire gas turbine not shown for the sake of clarity) is a rotor 52 of the generator 50 rotatably coupled.
- the starter generator can be flanged in particular to the shaft.
- the rotor 52 has a hollow cylindrical carrier 54, on the outer surface of which a plurality of coaxially to the central longitudinal axis A adjacent to each other arranged permanent magnet rings 56 are attached.
- the permanent magnet rings 56 are formed from individual magnets 56a, 56b,... With radial direction alternating magnetic orientation N, S, N, S (see also FIG. 2).
- the starter generator 50 has a stator 58 which is constructed of a soft magnetic material, for example of electric sheet metal parts. It is also possible to use it as a soft-magnetic shaped body, for example of pressed and / or sintered Shape metal powder.
- the stator 58 concentrically surrounds the rotor 52 to form an air gap 60 and has a plurality of stator coils 62 coaxial with and aligned with the permanent magnet rings 56.
- a stator coil 62 has two terminals 62a, 62b each and is projected on its side facing the air gap 60 to the rotor 52 toward side of soft magnetic, interlocking poles 64.
- poles 64 are each disposed on a soft iron annular disc 66a, 66b at their respective inner edge along the entire inner circumference.
- the poles 64 are interleaved in the manner of claw poles facing the permanent magnet rings 56 of the rotor 52 and each aligned with individual ones of the individual magnets 56a, 56b. This is illustrated in detail in FIG. 2.
- One or both of the soft iron ring discs 66a, 66b have at their outer edge a ring land 66c, which is dimensioned so that in the assembled state of the two soft iron ring discs 66a, 66b, the corresponding stator coil 62 is included.
- the poles 64 of the two soft iron ring discs 66a, 66b are mutually insulated by a distance. According to the number of stator coils or magnetic rings in the generator (see FIG. 1), the configurations shown in FIG. 2 are assembled.
- an active reactive power source 70 to be electronically controlled which is connected to the respective stator coil 62, is provided. Furthermore, at least one monitoring arrangement 68 is provided, which is connected to the reactive power source 70 and provides control signals for the active reactive power source 70 in the event of a fault in one or more stator coils 62, so that the two terminals 62a, 62b of the respective stator coil 62 are connected to each other in a low-impedance manner shorted a word - are. It has been found that, especially in the case of the application described here in the aviation sector, a large number of different Stor fallen with this configuration to detect and bring to a safe operating condition.
- These include short circuits of one, several, or all windings of one or more stationary coil 62, a single or multiple ground fault of one or more stationary coils 62, a low-resistance connection between two stationary coils 62, or a high-resistance connection within a stationary coil 62, and a high-resistance connection between two Stand coils 62.
- the monitoring arrangement 68 is adapted to detect currents flowing in the stationary coils 62 and voltages dropping across the stationary coils 62 and to compare them with one another in order to detect a fault in one or more stationary coils 62. Furthermore, the monitoring arrangement 68 is set up to detect heating of the stationary coils 62 by means of temperature sensors 74 arranged in the form of stationary coils 62, in order to detect overloads, short circuits or the like of the relevant stationary coils 62.
- the monitoring arrangement 68 is set up to detect ground faults of one or more stationary coils 62 by means of a potential monitoring circuit 76 for insulation monitoring.
- a potential monitoring circuit 76 for insulation monitoring.
- the exact positioning of the provided temperature sensors and current / voltage detectors on the stationary coils is not illustrated in detail for the sake of clarity.
- the active reactive power source 70 has two half bridges 80, 82 for switching electrical power.
- Each of the two half-bridges 80, 82 has at least two power MOSFET semiconductor switches 84, 86; 84 ', 86' are connected in the m series.
- Each of the semiconductor switches 84, 86; 84 ', 86' has an intrinsic freewheeling diode Di, which is parallel to the two power terminals of the respective semiconductor switch and which has silicon junction diode characteristics.
- a backup capacitor 88 is provided between the high and the low voltage potential V ss and V DD .
- the control of the MOSFETs takes place at their control inputs G via (not further illustrated) gate resistors by a drive circuit ECU.
- the drive circuit comprises the monitoring arrangement 68 with the potential monitoring circuit 76 and the temperature sensors 74. It is able to detect a fault immediately by detecting the currents flowing in the stator coils 62 and the stator coils 62 in the position and temperatures
- the active reactive power source 70 is controlled via its control inputs G so that either the second semiconductor switches 86, 86 'remain turned on in the two half bridges 80, 82 and the first semiconductor switches 84, 84' remain uncontrolled, or the first semiconductor switches 84, 84 'remain turned on and the second semiconductor switches 86, 86' remain uncontrolled. In both cases, the respective stator coil 62 is short-circuited.
- the affected stator coil supplies only a very small part of the possible proportional rated power, while the inverter continues to feed the (reactive) current initially regulated also in the affected stator coil, as in the other stator coil.
- the maximum absorbed torque in the affected disc is reduced compared to their share of the rated torque. This reduces the maximum absorbable torque of the entire generator.
- stator coil with its associated reactive power source / converter is shown, to which the monitoring arrangement 68 is assigned.
- all stator coils are equipped so that the respective reactive power sources / inverters are fed by a common monitoring arrangement 68 with drive signals, which receives information from sensors, which are distributed to all stator coils of the generator stand.
- the converter is to be controlled for generator operation by means of an electronic control in such a way that pulsating current flowing in the stator coils is converted into corresponding useful current
- this electronic controller can be connected to the corresponding sensors and current / Provided voltage sensors and programmed / configured accordingly, also take over the function of the monitoring device 68.
- stator coils 62 and their current balance are dimensioned so that in case of failure never a magnetic flux occurs, which reaches the nominal flux of the stator coils 62. This can be achieved, in particular in the controlled induced short circuit, that in a preferred embodiment of the invention, a continuous current through the short-circuited stator coils is less than half of the rated current. Such a structurally related low short-circuit current means a considerable security.
- the stator coils 62 are each formed from a plurality of ring sections 1a ... 4d (see FIG. 4).
- the ring portions are approximately quarter-circle rings, four of which together with the same radius of curvature together form a ring with interruptions.
- a plurality of rings (four in the example) are arranged substantially concentrically to their adjacent rings.
- the individual ring sections 1a ... 4d each have two ends. With one of the two ends of each ring portion is connected to an adjacent radially further outward or adjacent further inside ring portion.
- the ring portion 2b is connected at one end to the ring portion 1a and at the other end to the ring portion 3c.
- the ring sections 1a, 2a, 3a, 4a or Id, 2d, 3d, 4d, which are located radially on the very outside or radially inward, are connected at one of their two ends to ring sections located radially on the inside or radially outwards.
- the ring portion Id is connected at one end to the ring portion 2a.
- Fig. 3a shows an embodiment of how the connecting pieces 90 are to be provided with corresponding mating, open at the edge recesses 92.
- stator coils 62 can be achieved by the configuration of the stator coils described above.
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- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Control Of Eletrric Generators (AREA)
- Permanent Magnet Type Synchronous Machine (AREA)
- Windings For Motors And Generators (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2007800092571A CN101405922B (zh) | 2006-03-16 | 2007-03-09 | 横向磁场电机和具有这种横向磁场电机的涡轮机械 |
EP07722010A EP1994631A2 (de) | 2006-03-16 | 2007-03-09 | Transversalflussmaschine und turbomaschine mit derartiger transversalflussmaschine |
JP2008558631A JP2009529851A (ja) | 2006-03-16 | 2007-03-09 | 横方向磁束機およびこのような横方向磁束機を有するタービン型機械 |
CA002644023A CA2644023A1 (en) | 2006-03-16 | 2007-03-09 | Transverse flux machine and turbine-type machine having such a transverse flux machine |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102006012215.1 | 2006-03-16 | ||
DE102006012215A DE102006012215A1 (de) | 2006-03-16 | 2006-03-16 | Transversalflussmaschine und Turbomaschine mit derartiger Transversalflussmaschie |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2007104285A2 true WO2007104285A2 (de) | 2007-09-20 |
WO2007104285A3 WO2007104285A3 (de) | 2007-12-27 |
Family
ID=38374872
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DE2007/000435 WO2007104285A2 (de) | 2006-03-16 | 2007-03-09 | Transversalflussmaschine und turbomaschine mit derartiger transversalflussmaschine |
Country Status (8)
Country | Link |
---|---|
US (1) | US7629718B2 (de) |
EP (1) | EP1994631A2 (de) |
JP (1) | JP2009529851A (de) |
CN (1) | CN101405922B (de) |
CA (1) | CA2644023A1 (de) |
DE (1) | DE102006012215A1 (de) |
RU (1) | RU2410823C2 (de) |
WO (1) | WO2007104285A2 (de) |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7774148B2 (en) * | 2007-01-30 | 2010-08-10 | Gm Global Technology Operations, Inc. | Torque estimator for IPM motors |
TWI446689B (zh) | 2007-07-09 | 2014-07-21 | Clearwater Holdings Ltd | 具有獨立可移除線圈、模組部分與自持被動磁性軸承的電磁機 |
US7830057B2 (en) * | 2008-08-29 | 2010-11-09 | Hamilton Sundstrand Corporation | Transverse flux machine |
EP2340602B1 (de) | 2008-09-26 | 2019-01-02 | Clearwater Holdings, Ltd. | Permanentmagnetisch operierende maschine |
TW201020161A (en) * | 2008-11-20 | 2010-06-01 | Shutter Prec Co Ltd | Generator structure for a bicycle hub |
US8310118B2 (en) * | 2010-03-17 | 2012-11-13 | Hamilton Sundstrand Corporation | Packaging improvement for converter-fed transverse flux machine |
JP5534338B2 (ja) | 2010-09-30 | 2014-06-25 | 日立工機株式会社 | ディスクモータ及び電動作業機 |
JP5534337B2 (ja) * | 2010-09-30 | 2014-06-25 | 日立工機株式会社 | ディスクモータ及び電動作業機 |
CN104865528A (zh) * | 2010-11-12 | 2015-08-26 | 庄景阳 | 一种充放电系统的检测方法 |
DE102011076516A1 (de) * | 2011-05-26 | 2012-11-29 | Robert Bosch Gmbh | Verfahren und Vorrichtung zum Betreiben einer Leistungsendstufe |
AT511440B1 (de) * | 2011-08-12 | 2012-12-15 | Traktionssysteme Austria Gmbh | Verfahren zur regelung einer antriebseinheit für schienenfahrzeuge und antriebseinheit für schienenfahrzeuge |
DE102011084580A1 (de) * | 2011-10-14 | 2013-04-18 | Universität Bremen | Windkraftmaschine |
JP5557971B2 (ja) * | 2012-04-10 | 2014-07-23 | 三菱電機株式会社 | 電動機 |
DE102012022495A1 (de) | 2012-11-19 | 2014-05-22 | Micronas Gmbh | Brückenschaltung mit einer erhöhten Ausfallssicherheit |
US10505412B2 (en) | 2013-01-24 | 2019-12-10 | Clearwater Holdings, Ltd. | Flux machine |
US10205358B2 (en) * | 2014-04-12 | 2019-02-12 | GM Global Technology Operations LLC | Electric machine for a vehicle powertrain and the electric machine includes a permanent magnet |
US9925889B2 (en) | 2015-08-24 | 2018-03-27 | GM Global Technology Operations LLC | Electric machine for hybrid powertrain with dual voltage power system |
US10284036B2 (en) | 2015-08-24 | 2019-05-07 | GM Global Technology Operations LLC | Electric machine for hybrid powertrain with engine belt drive |
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CN111344933B (zh) | 2017-10-29 | 2023-04-07 | 清水控股有限公司 | 模块化电磁机器及其使用和制造方法 |
US20200063595A1 (en) * | 2018-08-27 | 2020-02-27 | Michael Newgent | Compressed gas and recycled liquid turbine power system |
US10666099B1 (en) | 2018-11-26 | 2020-05-26 | GM Global Technology Operations LLC | Slotted permanent magnets for electric machines |
US11323001B2 (en) * | 2019-07-02 | 2022-05-03 | GM Global Technology Operations LLC | Segmented bar conductors for electric machines |
US10780849B1 (en) | 2019-08-07 | 2020-09-22 | GM Global Technology Operations LLC | Electric drive units with integrated power electronics for vehicle powertrains |
GB201913015D0 (en) * | 2019-09-10 | 2019-10-23 | Rolls Royce Plc | electrical systems |
US11147193B2 (en) | 2020-02-25 | 2021-10-12 | GM Global Technology Operations LLC | Vascular cooling system for electrical conductors |
CN113394922B (zh) * | 2020-03-13 | 2022-06-14 | 中车永济电机有限公司 | 永磁电机调整方法、装置、设备以及存储介质 |
US11128251B1 (en) * | 2020-04-29 | 2021-09-21 | The Boeing Company | Fault-tolerant power system architecture for aircraft electric propulsion |
US11230288B1 (en) | 2020-09-28 | 2022-01-25 | GM Global Technology Operations LLC | Optimized regenerative braking for hybrid electric vehicle (HEV) powertrain configurations |
US11710993B2 (en) | 2020-10-28 | 2023-07-25 | GM Global Technology Operations LLC | Electric machines with features for enhancing load transfer performance of stacked-laminate rotors |
US11682535B2 (en) | 2021-03-12 | 2023-06-20 | Essex Industries, Inc. | Rocker switch |
US11688568B2 (en) | 2021-03-15 | 2023-06-27 | Essex Industries, Inc. | Five-position switch |
US11942822B2 (en) | 2021-12-23 | 2024-03-26 | GM Global Technology Operations LLC | Stator tooth and winding conductor designs for electric machines |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3218494A (en) * | 1963-01-03 | 1965-11-16 | Gen Electric | Alternating current generator |
GB1401245A (en) * | 1972-09-04 | 1975-07-16 | Texas Instruments Ltd | Over-voltage protection for electrical generators |
US20040150376A1 (en) * | 2003-02-03 | 2004-08-05 | Peter David Allan | System and method for controlling load dump voltage of a synchronous machine |
US20050012427A1 (en) * | 2003-06-04 | 2005-01-20 | Masahiro Seki | Claw pole motor stator |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2797346A (en) * | 1954-07-16 | 1957-06-25 | Agnes Jones Ranseen | Electric motors |
US5731645A (en) * | 1996-02-05 | 1998-03-24 | Magnetic Bearing Technologies, Inc. | Integrated motor/generator/flywheel utilizing a solid steel rotor |
DE19818035A1 (de) * | 1998-04-22 | 1999-10-28 | Bayerische Motoren Werke Ag | Transversalflußmaschine |
US6566775B1 (en) * | 2000-01-10 | 2003-05-20 | Richard Benito Fradella | Minimal-loss flywheel battery and related elements |
CA2482125C (fr) * | 2002-04-11 | 2013-05-21 | Eocycle Technologies Inc. | Machine electrique a flux transverse a rotor dente |
US6750588B1 (en) * | 2002-06-03 | 2004-06-15 | Christopher W. Gabrys | High performance axial gap alternator motor |
CN1241309C (zh) * | 2002-06-25 | 2006-02-08 | 江建中 | 聚磁式横向磁场电机 |
DE10325085B3 (de) * | 2003-06-03 | 2004-12-09 | Compact Dynamics Gmbh | Transversalflussmaschine |
CN2689571Y (zh) * | 2004-03-22 | 2005-03-30 | 华中科技大学 | 一种横向磁场永磁电机 |
-
2006
- 2006-03-16 DE DE102006012215A patent/DE102006012215A1/de not_active Withdrawn
- 2006-04-28 US US11/413,875 patent/US7629718B2/en not_active Expired - Fee Related
-
2007
- 2007-03-09 CN CN2007800092571A patent/CN101405922B/zh not_active Expired - Fee Related
- 2007-03-09 EP EP07722010A patent/EP1994631A2/de not_active Withdrawn
- 2007-03-09 CA CA002644023A patent/CA2644023A1/en not_active Abandoned
- 2007-03-09 RU RU2008140384/07A patent/RU2410823C2/ru not_active IP Right Cessation
- 2007-03-09 JP JP2008558631A patent/JP2009529851A/ja active Pending
- 2007-03-09 WO PCT/DE2007/000435 patent/WO2007104285A2/de active Application Filing
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3218494A (en) * | 1963-01-03 | 1965-11-16 | Gen Electric | Alternating current generator |
GB1401245A (en) * | 1972-09-04 | 1975-07-16 | Texas Instruments Ltd | Over-voltage protection for electrical generators |
US20040150376A1 (en) * | 2003-02-03 | 2004-08-05 | Peter David Allan | System and method for controlling load dump voltage of a synchronous machine |
US20050012427A1 (en) * | 2003-06-04 | 2005-01-20 | Masahiro Seki | Claw pole motor stator |
Also Published As
Publication number | Publication date |
---|---|
CN101405922B (zh) | 2011-09-07 |
DE102006012215A1 (de) | 2007-09-20 |
CN101405922A (zh) | 2009-04-08 |
RU2008140384A (ru) | 2010-04-27 |
RU2410823C2 (ru) | 2011-01-27 |
WO2007104285A3 (de) | 2007-12-27 |
US20070216249A1 (en) | 2007-09-20 |
JP2009529851A (ja) | 2009-08-20 |
EP1994631A2 (de) | 2008-11-26 |
US7629718B2 (en) | 2009-12-08 |
CA2644023A1 (en) | 2007-09-20 |
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