WO2007080279A1 - Procédé de détection de défaut de fonctionnement d'un ralentisseur électromagnétique - Google Patents
Procédé de détection de défaut de fonctionnement d'un ralentisseur électromagnétique Download PDFInfo
- Publication number
- WO2007080279A1 WO2007080279A1 PCT/FR2006/002750 FR2006002750W WO2007080279A1 WO 2007080279 A1 WO2007080279 A1 WO 2007080279A1 FR 2006002750 W FR2006002750 W FR 2006002750W WO 2007080279 A1 WO2007080279 A1 WO 2007080279A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- intensity
- current
- primary coils
- coils
- retarder
- 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
- H02H7/085—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 against excessive load
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L7/00—Electrodynamic brake systems for vehicles in general
- B60L7/28—Eddy-current braking
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K11/00—Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection
- H02K11/04—Structural association of dynamo-electric machines with electric components or with devices for shielding, monitoring or protection for rectification
- H02K11/042—Rectifiers associated with rotating parts, e.g. rotor cores or rotary shafts
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K49/00—Dynamo-electric clutches; Dynamo-electric brakes
- H02K49/02—Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type
- H02K49/04—Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type of the eddy-current hysteresis type
- H02K49/043—Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type of the eddy-current hysteresis type with a radial airgap
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/60—Other road transportation technologies with climate change mitigation effect
- Y02T10/64—Electric machine technologies in electromobility
Definitions
- the invention relates to a fault detection method of an electric member carried by a rotary shaft of an electromagnetic retarder.
- the invention also relates to such an electromagnetic retarder.
- the invention applies to a retarder capable of generating a deceleration resistant torque on a main or secondary transmission shaft of a vehicle that it equips, when this retarder is actuated.
- Such an electromagnetic retarder comprises a rotary shaft which is coupled to the main or secondary drive shaft of the vehicle to exert on it the retarding resisting torque to assist in particular the braking of the vehicle.
- the deceleration is generated with inductor coils fed with direct current to produce a magnetic field in a metal part made of ferromagnetic material, in order to reveal eddy currents in this metal part.
- the inductor coils may be fixed to cooperate with at least one metal part of movable ferromagnetic material having a general appearance of disk rigidly secured to the rotary shaft.
- these inductive coils are generally oriented parallel to the axis of rotation and arranged around this axis, vis-à-vis the disc, being secured to a fixed flange. Two successive inductive coils are electrically powered to generate magnetic fields of opposite directions.
- the inductor coils are electrically powered by a current from the electrical network of the vehicle, that is to say for example from a battery of the vehicle. But to increase the performance of the retarder, we use a design in which a current generator is integrated in the retarder.
- the electrical supply of the inductor coils is provided by a current generator comprising primary stator coils supplied by the vehicle network, and rotor secondary coils integral with the rotating shaft, and defining three electrical phases.
- the inductor coils are integral with the rotating shaft being radially protruding, to generate a magnetic field in a fixed cylindrical jacket which surrounds them.
- a rectifier such as a diode bridge rectifier is interposed between the rotor secondary windings and the inductor coils, also being carried by the rotary shaft.
- This rectifier converts the three-phase alternating current delivered by the secondary windings of the generator into DC power supply of the inductor coils.
- Two inductive coils with radial action, consecutive around the axis of rotation generate magnetic fields of opposite directions, one generating a field oriented centrifugally, the other a centripetally oriented field.
- the power supply of the primary coils allows the generator to produce the supply current of the inductor coils, which gives rise to eddy currents in the fixed cylindrical jacket, to generate a resistive torque on the rotating shaft, which slows down the vehicle.
- Such a malfunction of the rectifier may be partial, that is to say only concern one of the electrical phases of the current delivered by the secondary windings, which is then not converted by the rectifier.
- the available deceleration torque decreases by about one third of its nominal value, so that the driver of the vehicle does not necessarily realize this decrease, especially more than such a retarder is usually used in addition to a traditional braking system, which makes the gap even less noticeable.
- Such a retarder can also be controlled via a central processing unit which distributes, from the braking commands exerted by the driver, the power required by the brakes traditional, and that demanded of the retarder. In this case, the driver can not see directly a decrease in the deceleration torque provided by the retarder.
- the detection of a malfunction of the rectifier bridge or of another electrical member carried by the rotary shaft by means of electrical or other sensors mounted on the rotary shaft requires the transmission of data from the rotary shaft. to fixed parts of the retarder, which leads to complex solutions.
- the object of the invention is to provide a low cost detection solution for a malfunction of an electrical member carried by the rotary shaft.
- the subject of the invention is a method for detecting a fault of an electric member carried by a rotary shaft of an electromagnetic retarder, this retarder comprising stator primary coils, a control box for injecting into these primary coils. a current having an intensity corresponding to a theoretical intensity depending on an intensity reference, a sensor delivering a signal representative of an effective intensity value of the current flowing in these primary coils, a rotary shaft carrying secondary coils defining several phase and inductor coils and a current rectifier interposed between the secondary windings and the inductor coils, this method of comparing, in the control box, the theoretical intensity and the effective intensity to identify a defect in case of the difference between the theoretical intensity and the effective intensity greater than a value threshold.
- the invention thus makes it possible to identify the presence of an electrical problem at the level of an electrical member carried by the rotary shaft simply by analyzing the electrical behavior of primary coils when excited. It is thus not necessary to provide a data transmission device between the rotary shaft and a fixed portion of the retarder, which makes it possible to implement a fault detector having a very simple design.
- the invention also relates to a method as defined above, consisting in determining a difference between the theoretical intensity and a minimum or maximum value taken by the effective intensity of the current actually passing through the primary coils during a predetermined time interval.
- the invention also relates to a method as defined above, in which the theoretical intensity is determined in the control box from the intensity setpoint and data representative of a transfer function of the retarder.
- the invention also relates to a method as defined above, consisting in taking into account the intensity setpoint as a value representative of the theoretical intensity.
- the invention also relates to a method as defined above, consisting in slaving, from the control box, the current injected into the primary coils on the signal delivered by the current sensor, and providing primary coils having a constant of time three times greater than the time constant of the secondary windings.
- the invention also relates to a method as defined above, consisting of slaving, from the control box, the current injected into the primary coils on the signal delivered by the sensor, with a servocontrol having a sufficiently long reaction time for be insensitive to a fault of an electrical member carried by the rotary shaft.
- the invention also relates to a method as defined above, consisting in providing a servocontrol having a cut-off frequency Fc satisfying the relation Fc ⁇ 1 / 3.2.pi. T2 in which Fc is expressed in Hertz and in which T2 is the time constant of the secondary windings expressed in seconds.
- the invention also relates to a method as defined above, consisting in implementing inductive measurement turns as an actual current sensor.
- the invention also relates to an electromagnetic retarder comprising stator primary coils, a control box for injecting into these primary coils a current having an intensity corresponding to a theoretical intensity depending on an intensity reference, a sensor delivering a signal representative of an effective current value of the current flowing in these primary coils, a rotating shaft carrying secondary windings defining a plurality of phases and inductive coils and a current rectifier interposed between the secondary windings and the inductor coils, and means for comparing the theoretical intensity with the effective intensity to identify a malfunction of an electric member carried by the rotary shaft in the event of a difference between the theoretical intensity and the effective intensity greater than a threshold value.
- the invention also relates to an electromagnetic retarder as defined above, comprising means for controlling the current injected into the primary coils on the signal delivered by the sensor, and primary coils having a time constant greater than three times the time constant of the secondary windings.
- the invention also relates to an electromagnetic retarder as defined above, comprising means for controlling the current injected into the primary coils on the signal delivered by the sensor, and in which this servocontrol has a cut-off frequency Fc satisfying the relation Fc ⁇ 1 / 3.2.pi. T2 in , which Fc is expressed in Hertz and in which T2 is the time constant of the secondary windings expressed in seconds.
- the invention also relates to an electromagnetic retarder as defined above, wherein the sensor comprises one or more measuring inductive turns coiled with the primary coils.
- FIG. 1 is an overall broken away view of an electromagnetic retarder to which the invention applies;
- FIG. 2 is a schematic representation of the electrical components of the retarder according to the invention
- FIG. 3 is a plot as a function of time of the actual current flowing in the primary coils of a retarder having a malfunction of its rectifier
- FIG. 4 is a schematic representation of a servocontrol of the current of an electromagnetic retarder.
- the electromagnetic retarder 1 comprises a main casing 2 of generally cylindrical shape having a first end closed by a cover 3, and a second end closed by a coupling piece 4 by which retarder 1 is attached to a gearbox case either directly or indirectly, here via a speed multiplier indicated by 6.
- This casing 2 which is fixed, contains a rotary shaft 7 which is coupled to a transmission shaft not visible in the figure, such as a main shaft for transmitting to the wheels of the vehicle, or secondary such as a secondary output shaft. of gearbox via 6.
- a current generator here of the three-phase type, which comprises fixed or statoric primary coils 8 surrounding rotor secondary coils, integral with the shaft. rotating 7.
- These secondary windings are represented symbolically in FIG. 2, being identified by the reference 5.
- These secondary windings 5 here comprise three distinct windings defining three corresponding phases 5A, 5B and 5C for delivering a three-phase alternating current having a frequency conditioned by the speed of rotation. rotating shaft 7.
- An inner liner 9 of generally cylindrical shape is mounted in the main casing 2 while being slightly spaced radially from the outer wall of this main casing 2 to define a substantially cylindrical intermediate space 10 in which a cooling liquid of this liner 9 circulates.
- This main casing which also has a generally cylindrical shape, is provided with a coolant intake duct 11 in the space 10 and a delivery duct 12 of the coolant out of this space 10.
- This jacket 9 surrounds several induction coils 13 which are carried by a rotor 14 rigidly secured to the rotary shaft 7. Each induction coil 13 is oriented to generate a radial magnetic field, while having a generally oblong shape extending parallel to the 7.
- the different inductor coils 13 are interconnected to each other so as to form a dipole.
- the liner 9 and the body of the rotor 14 are made of ferromagnetic material.
- the casing is a moldable aluminum-based part and seals intervene between the casing and the liner 9, the lid 3 and the part 4 are perforated.
- the inductor coils 13 are electrically powered by the rotor secondary coils 5 of the generator via a rectifier bridge carried by the rotary shaft 7.
- This rectifier bridge may be that which is indicated by 15 in FIG. 2, and which comprises six 15A diodes. -15F, for rectifying the three-phase alternating current from the secondary windings 5A-5C in direct current.
- This bridge rectifier can also be of another type, for example being formed from MOSFET type transistors.
- the rectifier bridge 15 is a three-branch circuit each carrying two diodes in series, each phase of the secondary windings is connected to a corresponding branch between the two diodes.
- Each branch has an end connected to a first terminal of the load, which constitute the inductor coils 13, and a second end connected to a second terminal of this load 13.
- the first phase 5A is connected to the two diodes 15A and 15D which are respectively connected to the first and the second terminals of the load 13.
- the second phase 5B is connected to the diodes 15B and 15E which are themselves respectively connected to the first and second terminals of the load 13.
- the third phase is connected to the diodes 15C and 15F which are themselves respectively connected to the first and second terminals of the load 13.
- each branch of the rectifier delivers in the load 13 a current having the shape of the positive sinusoidal parts of the voltage signal of the phase corresponding to this branch, this current being zero when the voltage in question is negative.
- the rotor 14 carrying the induction coils 13 has a general shape of a hollow cylinder connected to the rotary shaft 7 by radial arms 16.
- This rotor 14 thus defines an annular internal space situated around the shaft 7, this internal space being ventilated by an axial fan 17 located substantially in line with the junction of the cover 3 with the casing 2.
- a radial fan 18 is located at the opposite end of the casing 2 to evacuate the air introduced by the fan. axial 17.
- the putting into service of the retarder consists in injecting into the primary coils 8 an excitation current coming from the electrical network of the vehicle and in particular from the battery, so that the current generator delivers an induced current on its secondary coils 5. This current supplies then the inductor coils 13 to produce a resisting torque slowing down of the vehicle.
- the excitation current is injected into the primary coils 8 by means of a control box 19, shown in FIG. 2, which is interposed between a power supply source of the vehicle, and the primary coils 8.
- the control box 19 and the primary coils 8 are connected in series between a mass M of the vehicle and a battery supply Batt of the vehicle battery.
- a diode D is mounted across the primary coils 5 so as to prevent the flow of a reverse current in the primary coils.
- This control unit 19 comprises an input capable of receiving a control signal representative of a level of retarding torque requested from the retarder.
- This input can be connected to a lever or other that is operated directly by a driver of the vehicle.
- This lever can be mobile gradually between two extreme positions, namely a maximum position corresponding to a maximum load torque request, and a minimum position in which the retarder is not requested.
- the retarder is controlled by the housing 19 to exert on 1 rotating shaft 7 a resistive torque proportional to the position of the lever, relative to the maximum available deceleration torque.
- the input of the control box 19 receives a control signal which corresponds to a value between zero and one hundred percent.
- This input can also be connected to a brake control unit which autonomously determines a control signal of the retarder.
- This brake control unit is then connected to one or more braking actuators available to the vehicle.
- the driver does not act directly on the retarder, but it is the brake control unit that controls, from different parameters, the retarder and traditional brakes of the vehicle.
- the control box 19, visible in FIG. 4, is an electronic box comprising, for example, an ASIC-type logic circuit operating at 5V, and / or a power control circuit capable of handling currents of high intensity.
- This housing thus comprises an electronic or PU power module.
- the control unit 19 determines a current setpoint Ci of excitation current to be injected into the primary coils 8, and it applies, via its module PU, to the primary coils 8 a voltage U to inject a current corresponding to this setpoint intensity Ci.
- the current injected into the primary coils 8 has a theoretical intensity It which increases until reaching the set value Ci.
- the value of the theoretical current It is determined in the control box from a transfer function Ft which depends in particular on the inductance and the electrical resistance of the primary coils 8 to be representative of the electrical behavior of the primary coils in transient state.
- the retarder 1 also comprises a sensor 21 which measures the intensity Ie of the current effectively flowing in the primary coils 8 and which delivers a signal representative of this intensity.
- This sensor 21 is connected to the control unit 19 which is programmed to compare the effective intensity Ie measured by the sensor 21 with the theoretical current It.
- a difference between the theoretical current It and the effective current Ie greater than a predetermined value is indicative of a malfunction of an electric member of the rectifier 15, such as in particular the destruction of a diode.
- the mutual currents resulting from this defective diode disturb the current flowing through the primary coils.
- the current Ie effectively flowing in the primary coils 8 has a sinusoidal shape of high amplitude. This sinusoid has a frequency which is related to the speed of the rotary shaft 7.
- the effective current curve Ie is substantially merged with the theoretical current curve It.
- the detection from the control unit 19 of a difference between the effective current Ie and the theoretical current It greater than a predetermined value makes it possible to detect a fault of the rectifier 15 which is mounted on the rotary shaft 7. This detection is made without contact, that is to say without having to transmit data from sensors mounted on the rotary shaft 7 to a fixed portion of the retarder.
- the predetermined value of deviation is advantageously twenty percent of the value of the theoretical current It because, as can be seen in FIG. 3, the amplitude of the mutual currents is relatively high, which facilitates their detection.
- This predetermined value can also be a fixed value.
- the intensity Ie comes from a current sensor which is connected in series with the primary coils 8.
- this current sensor may also be in the form of one or more measuring inductive turns.
- the voltage appearing at the terminals of these measuring inductive turns has the same speed as the current flowing in these inductive turns.
- the effective intensity Ie may consist in determining the maximum or minimum value taken by the effective intensity Ie for a predetermined duration corresponding to several rotation periods of the shaft 7, and comparing this maximum or this minimum with the setpoint value. This .
- the current It which is injected into the primary coils 8 is slaved on the sensor 21, so as to best correspond to the value of the intensity setpoint Ci, this slaving being implemented at the level of the control box 19.
- the control unit comprises, in the aforementioned manner, a power electronics PU which is controlled by a corrector CR for injecting the excitation current Ii into the primary coils 8, which gives rise to the current induced in the secondary windings 5.
- the intensity effective Ie is subtracted at 50 at the intensity setpoint Ci to constitute an input signal of the corrector CR which drives the power electronics PU.
- the corrector When the corrector receives a negative signal input, it drives the power electronics PU to reduce the injected current, and when it receives a positive signal input it drives the power electronics to increase the injected current.
- the effective current Ie flowing in the primary coils 8 corresponds to the current Ii injected by the control box 19 from which the mutual current Im resulting from a malfunction of the rectifier 15 is subtracted.
- the theoretical current It is determined in the control box 15 from the set value Ci, on the basis of the transfer function Ft which is in particular representative of the intensity response of the primary coils 8 to the application of a U voltage. ⁇
- the control of the injected current does not compensate for disturbances due to mutual currents in the event of a faulty diode.
- This can be achieved by sizing the primary coils such that they have a time constant T1 greater than N times the time constant T2 of the secondary coils 5, where N designates a natural integer.
- N is chosen to be greater than or equal to 3 so that this time constant T1 is greater than three times the time constant T2 in order to ensure optimum independence of the detection.
- the servocontrol of the injected current is chosen to have a cut-off frequency Fc satisfying the relation Fc ⁇ l / (2.N.pi.T2), in which Fc is expressed in Hertz, and T2 in seconds, pi representing the number having a value close to 3.14.
- Fc is expressed in Hertz
- T2 in seconds
- pi representing the number having a value close to 3.14.
- N is a natural number which is advantageously chosen as three.
- this component may be a diode or a transistor of the rectifier 15, but this component may also be a secondary winding 15A, 15B or 15C.
- the example described above relates to a retarder in which the generator comprises three-phase secondary windings, but the invention also applies to a retarder comprising secondary windings having a different number of phases, equal to at least two.
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Dynamo-Electric Clutches, Dynamo-Electric Brakes (AREA)
- Synchronous Machinery (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BRPI0618872-9A BRPI0618872A2 (pt) | 2005-12-19 | 2006-12-15 | processo de detecção de defeito de um órgão elétrico levado por uma árvore rotativa de um desacelerador eletromagnético, e, desacelerador eletromagnético |
US12/092,139 US20090219050A1 (en) | 2005-12-19 | 2006-12-15 | Method for detecting a malfunction in an electromagnetic retarder |
MX2008007964A MX2008007964A (es) | 2005-12-19 | 2006-12-15 | Procedimiento de deteccion de falla de funcionamiento de un desacelerador electromagnetico. |
EP06841953A EP1964248A1 (fr) | 2005-12-19 | 2006-12-15 | Procédé de détection de défaut de fonctionnement d'un ralentisseur électromagnétique |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0553939A FR2895166B1 (fr) | 2005-12-19 | 2005-12-19 | Procede de detection de defaut de fobnctionnement d'un ralentisseur electromagnetique |
FR0553939 | 2005-12-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2007080279A1 true WO2007080279A1 (fr) | 2007-07-19 |
Family
ID=36617125
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2006/002750 WO2007080279A1 (fr) | 2005-12-19 | 2006-12-15 | Procédé de détection de défaut de fonctionnement d'un ralentisseur électromagnétique |
Country Status (7)
Country | Link |
---|---|
US (1) | US20090219050A1 (fr) |
EP (1) | EP1964248A1 (fr) |
CN (1) | CN101322302A (fr) |
BR (1) | BRPI0618872A2 (fr) |
FR (1) | FR2895166B1 (fr) |
MX (1) | MX2008007964A (fr) |
WO (1) | WO2007080279A1 (fr) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9067500B2 (en) | 2012-05-21 | 2015-06-30 | Krassimire Mihaylov Penev | Self rechargeable synergy drive for a motor vehicle |
US8646550B2 (en) * | 2012-05-21 | 2014-02-11 | Krassimire Mihaylov Penev | Self rechargeable synergy drive for a motor vehicle |
CN103884953B (zh) * | 2014-03-07 | 2016-08-17 | 中国南方电网有限责任公司超高压输电公司广州局 | 一种电容式电压互感器阻尼回路故障诊断系统 |
CN108152775A (zh) * | 2017-11-21 | 2018-06-12 | 国家电网公司 | 一种阻尼器的检测装置 |
FR3083386B1 (fr) * | 2018-06-28 | 2021-05-14 | Telma | Ensemble ralentisseur electromagnetique et generatrice et vehicule comportant un tel ensemble |
JP7351656B2 (ja) * | 2019-06-28 | 2023-09-27 | 川崎重工業株式会社 | 減速機の故障診断装置及び故障診断方法 |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3534228A (en) * | 1968-05-08 | 1970-10-13 | Westinghouse Electric Corp | Generator and exciter protection circuit |
GB1416910A (en) * | 1972-03-16 | 1975-12-10 | Westinghouse Electric Corp | Ac generator system including differential protection of exciter |
US4164705A (en) * | 1976-04-27 | 1979-08-14 | Westinghouse Electric Corp. | Brushless exciter fault indicator system |
EP0331559A1 (fr) * | 1988-02-25 | 1989-09-06 | Labavia S.G.E. | Ensemble constitué par un ralentisseur électromagnétique et par ses moyens d'alimentation électrique |
FR2842961A1 (fr) * | 2002-07-29 | 2004-01-30 | Telma | Ralentisseur electromagnetique d'un vehicule muni d'un dispositif multiplicateur de vitesse |
Family Cites Families (9)
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---|---|---|---|---|
US5743599A (en) * | 1996-04-08 | 1998-04-28 | K-Tronics, Inc. | Electromagnetic retarder control apparatus and method |
JPH11285233A (ja) * | 1998-03-30 | 1999-10-15 | Isuzu Motors Ltd | 磁石式渦電流減速装置 |
AU2001233133A1 (en) * | 2000-02-02 | 2001-08-14 | Pacific Scientific Electro Kinetics Division | Integrated retarder and accessory device |
FR2853159B1 (fr) * | 2003-03-31 | 2005-06-17 | Telma | Ralentisseur electromagnetique d'un vehicule |
FR2865080B1 (fr) * | 2003-12-19 | 2006-04-28 | Telma | Ralentisseur electromagnetique radial simple comportant des moyens pour assurer une ventilation |
FR2894411B1 (fr) * | 2005-12-07 | 2008-06-13 | Telma Sa | Procede de pilotage d'un ralentisseur electromagnetique |
FR2894734B1 (fr) * | 2005-12-09 | 2008-03-14 | Telma Sa | Procede de mise en service d'un ralentisseur electromagnetique |
FR2895596B1 (fr) * | 2005-12-22 | 2008-03-14 | Telma Sa | Procede de pilotage d'un ralentisseur electromagnetique. |
FR2895595B1 (fr) * | 2005-12-22 | 2008-03-14 | Telma Sa | Procede de pilotage d'un ralentisseur electromagnetique. |
-
2005
- 2005-12-19 FR FR0553939A patent/FR2895166B1/fr not_active Expired - Fee Related
-
2006
- 2006-12-15 WO PCT/FR2006/002750 patent/WO2007080279A1/fr active Application Filing
- 2006-12-15 EP EP06841953A patent/EP1964248A1/fr not_active Withdrawn
- 2006-12-15 BR BRPI0618872-9A patent/BRPI0618872A2/pt not_active IP Right Cessation
- 2006-12-15 CN CNA2006800454972A patent/CN101322302A/zh active Pending
- 2006-12-15 US US12/092,139 patent/US20090219050A1/en not_active Abandoned
- 2006-12-15 MX MX2008007964A patent/MX2008007964A/es unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3534228A (en) * | 1968-05-08 | 1970-10-13 | Westinghouse Electric Corp | Generator and exciter protection circuit |
GB1416910A (en) * | 1972-03-16 | 1975-12-10 | Westinghouse Electric Corp | Ac generator system including differential protection of exciter |
US4164705A (en) * | 1976-04-27 | 1979-08-14 | Westinghouse Electric Corp. | Brushless exciter fault indicator system |
EP0331559A1 (fr) * | 1988-02-25 | 1989-09-06 | Labavia S.G.E. | Ensemble constitué par un ralentisseur électromagnétique et par ses moyens d'alimentation électrique |
FR2842961A1 (fr) * | 2002-07-29 | 2004-01-30 | Telma | Ralentisseur electromagnetique d'un vehicule muni d'un dispositif multiplicateur de vitesse |
Also Published As
Publication number | Publication date |
---|---|
FR2895166B1 (fr) | 2008-06-13 |
BRPI0618872A2 (pt) | 2011-09-13 |
US20090219050A1 (en) | 2009-09-03 |
FR2895166A1 (fr) | 2007-06-22 |
MX2008007964A (es) | 2008-09-26 |
EP1964248A1 (fr) | 2008-09-03 |
CN101322302A (zh) | 2008-12-10 |
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