WO2015137814A1 - Ensemble de couplage magnétique - Google Patents

Ensemble de couplage magnétique Download PDF

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Publication number
WO2015137814A1
WO2015137814A1 PCT/NL2015/050164 NL2015050164W WO2015137814A1 WO 2015137814 A1 WO2015137814 A1 WO 2015137814A1 NL 2015050164 W NL2015050164 W NL 2015050164W WO 2015137814 A1 WO2015137814 A1 WO 2015137814A1
Authority
WO
WIPO (PCT)
Prior art keywords
hub
inductor
magnetic coupling
coupling assembly
rotor
Prior art date
Application number
PCT/NL2015/050164
Other languages
English (en)
Inventor
Dirk Geert VAN DER BIJL
Robert Lalesse
Original Assignee
Zytec International B.V.
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
Priority claimed from NL2013219A external-priority patent/NL2013219B1/en
Application filed by Zytec International B.V. filed Critical Zytec International B.V.
Priority to US15/125,677 priority Critical patent/US10211716B2/en
Priority to EP15719517.3A priority patent/EP3117509B1/fr
Publication of WO2015137814A1 publication Critical patent/WO2015137814A1/fr

Links

Classifications

    • 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
    • H02K49/046—Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type of the eddy-current hysteresis type with an axial airgap
    • 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
    • H02K2201/03—Machines characterised by aspects of the air-gap between rotor and stator
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K2213/00—Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
    • H02K2213/09—Machines characterised by the presence of elements which are subject to variation, e.g. adjustable bearings, reconfigurable windings, variable pitch ventilators
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/06—Means for converting reciprocating motion into rotary motion or vice versa

Definitions

  • the present invention relates to a magnetic coupling assembly for coupling a first rotary shaft and a second rotary shaft.
  • the invention also relates to a method of adjusting at least one air gap in a magnetic coupling assembly.
  • Magnetic coupling assemblies for coupling a first shaft, for instance a drive or motor shaft, to a second shaft, for instance a load or machine shaft, are known as such.
  • a magnetic coupling assembly may comprise one or more magnet rotors, with each magnet rotor having a respective set of permanent magnets.
  • Each magnet rotor of the known magnetic coupling assembly is associated with at least one electromagnetic inductor rotor spaced apart from the magnet rotor. Torque may be transferred from the first shaft to the second shaft, with the speed of the load shaft reduced with respect to the speed of the drive shaft, without the drive shaft being in contact with the load shaft.
  • the assembly comprises one rotatable central magnetic rotor and a pair of conductors, the conductors being made of electro-conductive material, arranged at either side of the central magnetic rotor and mounted on a rotatable conductor housing (herein also referred to as "conductor cage” or simply "cage").
  • An advantage of magnetic coupling assemblies relative to the more traditional couplings is the contactless torque/speed transmission, which provides the coupling assemblies with a large lifespan, low maintenance costs and high energy efficiency.
  • the known magnetic coupling assemblies have installation issues since the magnetic rotor and conductors need to be spaced apart in a defined position. Furthermore installation may be difficult as a result of the large magnetic forces that occur in the assembly.
  • the axial alignment is typically accomplished by moving the machinery at the driver and/or the load side of the coupling, for instance by moving the drive motor and/or the pump.
  • the axial alignment of a magnetic coupling in the installation phase is a difficult task and is labor intensive, for instance because of the magnetic attraction between the elements of the coupling.
  • the motor and load extend in a vertical direction and need to be installed using shims and the like, it is difficult to achieve the required effective distances of the air gaps.
  • Magnetic couplings with positioning mechanisms for positioning the central rotor and the conductor rotors relative to each other during operation of the coupling are known as such. These mechanisms are intended to synchronously adapt the air gaps between the central rotor and each of the conductors in order to vary the transmission ratio of the coupling. As mentioned above, the variation of the transmission ration is typically performed when the coupling is in operation, for instance when the rotors of the coupling are rotated.
  • An example of such positioning mechanism is disclosed in CN 103107675 A. If the left air gap between the left conductor disk and the left magnetic disk is increased, the right air gap between the right conductor disk and the right magnetic disk is increased to the same extent.
  • the known positioning mechanism is unsuitable for proper alignment of the rotors of the coupling at the installation phase. For instance, if one of the air gaps is larger than the other air gap, a repositioning of the rotors to provide air gaps of equal widths is not possible.
  • a magnetic coupling assembly for associating a first rotatable shaft to a second rotatable shaft, the magnetic coupling assembly comprising:
  • a rotatable first hub to be connected to the first rotatable shaft, the first hub comprising a magnet rotor comprising a plurality of permanent magnets;
  • the second hub comprising a conductor housing comprising a first inductor rotor connected to the second hub and arranged at a distance on one side of the magnet rotor facing the second rotatable shaft and a second inductor rotor arranged at the opposite side of the magnet rotor;
  • At least one of the second hub and first hub comprises an inner hub part and an outer hub part, wherein the hub parts are configured to allow the outer hub part to be axially movable over the inner hub part to adjust the axial position of the inductor rotors relative to the magnet rotor;
  • the conductor housing also comprises at least one connector unit for connecting the first inductor rotor to the second inductor rotor, the at least one connector unit being configured to control the axial distance between the first and second inductor rotor.
  • the mounting of the drive and load (for instance, a drive motor and a pump) can be facilitated.
  • the construction allows for the precise axial alignment and control as necessary for a magnetic coupling.
  • the outer hub may be fixated on the inner hub.
  • the inner hub may be fixated on either of the sides of the coupling assembly.
  • the precise axial alignment of the first and second hubs and therefore of the elements connected to the first and second hubs, such as the at least one magnet rotor and the at least one inductor rotor, allows an air gap adjustment (more or less) without moving motor or load shaft enabling field adjustment to suit or adjust to actual load conditions, for instance in case of balancing a multi-drive installation (conveyor, crane), decreasing the speed of the load (pump, fan, etc.) for energy saving purposes, increasing the speed of the load (pump, fan, etc.) for more output, and adjusting the coupling peak torque to prevent motor or transmission overload.
  • the coupling assembly may save re -installation effort and labor after repair of pump and motor.
  • the air gaps are equalized at the installation phase, i.e. before the coupling is actually in operational condition.
  • the air gaps may also be equalized in a later stage, for instance after prolonged operation of the coupling, for instance when the coupling is first operated at relative low temperature conditions and then at higher temperature conditions.
  • he (independent) movability of the first and second hubs may improve the coupling performance in the sense that it allows easy compensation of unequal air gap in operating conditions.
  • the installed air gaps may be equal in cold conditions, but after start thermal expansion, vibrations, load bending, pump piping under pressure pushing the pump away may cause the air gaps to become different. The balancing can be more easily accomplished in the coupling assembly defined herein.
  • a fine adjustment of the magnet rotor axial position may be accomplished, for example in order to equalize slip heat load between the inductor rotors (for instance, between the inductor plates). More generally, the coupling assembly makes it possible to equalize in a simple manner the effective coupling load on the rotors.
  • the connector unit comprises a spacer configured connected to both the inner surface of the first inductor rotor and the inner surface of the second inductor rotor, the spacer preferably being configured to position the first and second inductor rotors relative to each other at a selected axial distance from a plurality of axial distances.
  • the spacer can be embodied to have an adjustable length. In other embodiments the spacer may be movable in associated openings in the inductor rotors. The inductor rotors are moved in axial direction, for instance by rotating the spacer that is threadingly engaged in openings in the inductor rotors, until they are spaced apart at a suitable distance.
  • the outer hub and inner hub comprise respective threads to threadingly engage on each other, the threads configured to move the outer and inner hub relative to one another by rotating the outer hub part relative to the inner hub part.
  • the conductor housing comprises at least one inductor rotor (conductor) positioned at a first distance from a side of the magnet rotor facing the second rotatable shaft and at least one inductor rotor positioned at a second distance from a side of the magnet rotor facing the first rotatable shaft so as to define respective air gaps between the inductor rotors and the magnet rotor.
  • the magnetic coupling assembly is configured to independently control the width of the first and second air gap by a combination of adapting the position of the inductor rotors relative to the magnet rotor by moving the outer hub relative to the inner hub and adapting the axial distance between the first and second inductor rotors by changing the length of the connector unit. Because the air gaps my be independently (and individually) controlled, the correct distances between the inductor rotors and magnet rotors (for instance in the installation phase) can be easily set and a correct alignment may be achieved.
  • the inner hub part may be fixated relative to the outer hub part by at least one fixation element.
  • the fixation element may be configured to resist rotation of the outer hub part relative to the inner hub part and thereby avoid the inadvertent axial movement of the hub parts.
  • fixation element comprises a clamping device configured to clampingly attach the outer hub part to the inner hub part.
  • fixation element may comprise:
  • a conical element preferably a conical ring, ring positioned between the outer and inner hub part and at least partly surrounding the inner hub part;
  • a pressing element configured to be inserted between the conical element and at least one of the outer and inner hub part.
  • the magnet rotor extends in radial direction relative to the axial direction defined by the concentric first and second hub.
  • the conductor housing may be configured to at least partly surround this magnet rotor. More specifically, in further embodiments of the invention, the conductor housing comprises a first inductor rotor connected to the second hub and arranged at one side of the magnet rotor, a second inductor rotor arranged at the opposite side of the magnet rotor, and at least one connector unit for connecting the first inductor rotor to the second inductor rotor.
  • a first electro-conductive conductor may be arranged between the first inductor rotor and magnet rotor.
  • first inductor rotor also referred to as the conductor rotor
  • second inductor rotor The distance between the first inductor rotor and magnet rotor and similarly defines a second air gap.
  • the axial position of the first and second conductor relative the magnet rotor and/or relative to the first and second inductor rotor may be varied by the connection unit. More specifically, the connector unit controls the axial distance between the conductors while the axially movable outer hub part and inner hub part control the axial position of the first and second conductor relative to the magnet rotor (or vice versa).
  • the combination of the two control mechanisms enables selective and individual variation of the first and second air gaps.
  • connection unit i.e. the distance between the inductor/conductor rotors to which the conductors are mounted.
  • connection unit i.e. the distance between the inductor/conductor rotors to which the conductors are mounted.
  • the first and second air gaps may have an equal effective distance (so that the magnet rotor is effectively centred between the inductor rotors), but in other embodiments the distances are not equal, at least not equal at each radial position (magnet rotor off centre)
  • the at least one connector unit comprises a spacer bolt assembly comprising a spacer bolt threadinlgy engaged by a spacer sleeve and configured to control the axial distance between the inductor rotors by rotation of the spacer bolt relative to the spacer sleeve.
  • a method is provided of associating a first rotatable shaft to a second rotatable shaft in a magnetic coupling assembly as defined herein, the method comprising:
  • the method comprises changing the distance between the first and second conductor by increasing or decreasing the length of the connection units and changing the position of the first and second conductor relative to the magnet rotor by moving the outer hub in axial direction relative to the inner hub.
  • the length of the connection units is changed first and only after the length has been properly set, the positioning of the magnet rotor with respect to the one or more conductors is performed.
  • performing the method in the reverse order is conceivable as well.
  • the method may comprise controlling the width of the first air gap independently from the width of the second air gap.
  • the controlling of the width of the first (or second) air gap may comprise a combination of adapting the position of the inductor rotors relative to the magnet rotor by moving the outer hub relative to the inner hub and adapting the axial distance between the first and second inductor rotors by changing the length of the connector unit.
  • Figure 1 is a partly taken away schematic view in cross-section of an embodiment of the coupling assembly according to the invention, connected between a drive motor and a load;
  • Figure 2 is a cross-section of the embodiment of the inner hub part and outer hub part of the magnetic coupling assembly
  • Figure 3 is a front view of the embodiment of figure 2;
  • Figure 4 is a view in perspective of a further embodiment of the invention.
  • Figure 5 is a cross-section of a detail of the embodiment of figure 4.
  • Figure 6A-6C are detailed cross-sections of the outer end of the magnet rotor and induction rotors, wherein the induction rotors are coupled with at least one adjustable connection unit, in case of small air gaps, intermediate air gaps and large air gaps, respectively;
  • Figures 7-9 are views of embodiments of the connection unit
  • Figures 10 and 11 are a view in perspective and in cross-section of a further embodiment of the invention.
  • Figures 12A-12C show the schematic view of figure 1, in various states.
  • FIGS 1-4 show an embodiment of a magnetic coupling assembly 1 according to an embodiment of the present invention wherein the axial positioning can be accomplished in an easier and more reliable manner.
  • the magnetic coupling assembly may be connected to a first rotatable shaft (Si) (herein also referred to as a drive shaft or motor shaft) of a driving motor, for instance an electric engine, and to a second rotatable shaft (S 2 ) (herein also referred to as a load shaft or machine shaft) of a load, for instance a pump or similar device.
  • the first and second shafts are releasably connected to, for instance assembled on, respectively a motor side hub 2 and a load side hub 3 of the magnetic coupling assembly 1 , for instance through means of respective clamping sleeves or similar coupling devices.
  • the magnetic coupling assembly is configured to control the rotational speed of the load shaft, at a speed equal or reduced from the rotational speed of the drive shaft in an essentially contactless manner.
  • the clearance allows the two shafts to rotate and transmit power while being slightly out of alignment without the vibration that would occur if they were connected by mechanical couplings.
  • the magnetic coupling assembly 1 comprises an inductor assembly 20 having two inductor rotors 21, 22 (herein also referred to as conductor rotors 21,22) (connected to a common central hub part 4 of the hub 2 to rotate synchronously. More specifically, the inductor rotor 21 is directly connected to the outer hub part 4 via a radial flange 14 using a number of bolts 19. The other inductor rotor 22 is not connected to the outer hub part 4, but is connected to the inductor rotor 21 through a number of connection units 53 at positions close to the circumference of the inductor rotors 21,22.
  • the magnetic coupling assembly 1 also comprises a magnet rotor assembly 30.
  • the magnet rotor assembly 30 is coupled to the load side hub 3 which is connected to the load shaft (alternatively, to the motor drive shaft), while the two inductor rotors 21,22 are attached to the drive side hub 2, more specifically tot the outer hub part 4 thereof.
  • the magnet rotor assembly 30 has a single magnet rotor 31 arranged centrally between the two inductor rotors 21,22.
  • the magnet rotor 31 contains a number of permanent magnets 32, loaded in alternating north/south pattern and positioned near the outer circumference of the rotor 31.
  • the permanent magnets are spaced by air gaps from the respective inductor rotors 21,22.
  • Rotation of the first or second hub 2,3 results in rotation of the other shaft by magnetic action without there being any direct mechanical connection between the first and seconds shafts. More specifically, torque may be transferred between the magnet rotor and the inductor rotors and thereby between the first and second shaft via Lenz's law.
  • FIGS 2 and 3 show the first and second hubs 2,3 in more detail.
  • the first hub 2 comprises an outer hub part 4 and an inner hub part 5.
  • the inner hub part 5 is fastened to the input shaft Si.
  • the inner hub part 5 may for instance be connected to the input shaft by a clamping set 15.
  • the set may comprise of a clamping device including fastening bolts or of one or more sets of conical rings 16 around the shaft and pressed together with a pressing element 17 and fastened with bolts 18 in the inner hub part 5.
  • the inner hub part 5 bears a bushing 10, for instance made of bronze, a synthetic material or a similar material.
  • the bushing 10 supports the outer hub part 4 and allows the outer hub part 4 to be rotatable with respect to the inner hub part 5, as will be described hereafter.
  • a thread 11 is provided on the inner hub part 5 and a thread 12 is provided on the outer hub part 4.
  • the hub parts may be rotated relative to each other. Rotation of one of the hub parts relative to the other causes an axial displacement (P a ) of the hubs relative to each other and thereby enables an precise axial positioning of the hub parts 4,5.
  • the axial movement of the outer hub part 4 relative to the inner hub part 5 enables the axial displacement of the inductor assembly 20 relative to the magnet rotor assembly 30 connected to the shaft S 2 .
  • the relative axial displacement of the hub parts 4,5 (by rotation of a hub part relative to the other hub part) enables the axial displacement of the hub parts including the magnet rotor and inductor rotors connected thereto and therefore the setting of the air gap(s).
  • the outer hub part 4 is screwed on the inner hub part 5.
  • the coupling can be rotated in place axially.
  • the outer hub part 4 slides over the bushing 10.
  • the outer hub part 4 is fixated on the inner hub part 5, for instance by a locking set or a clamping set 8.
  • the clamping set 8 may comprise of a clamping device including fastening bolts or of one or more sets of conical rings 9 around the inner hub part 4 and pressed together with a pressing element 7 and fastened with bolts 6 screwed in the inner hub part 5.
  • Figures 4-8 show a further embodiment of the present invention.
  • Figure 4 shows a portion of a magnetic coupling assembly 41.
  • the assembly 41 comprises a first inductor rotor 42 and a second induction rotor 43.
  • the magnet rotor 46 including a number of permanent magnets 50 is arranged.
  • electro-conductive material 51 is arranged, while at the inner side of the second inductor rotor 43 similar electro-conductive material 52 is mounted.
  • the first and second inductor rotors 42,43 are connected to each other at a number of connection points close to the outer circumference of the rotors using respective connection units 53.
  • the figures show that the first inductor rotor 42 is connected to a first hub part 44.
  • the second inductor rotor 43 is connected only to the first inductor rotor 42 by means of the connection units.
  • the magnet rotor 46 is connected to a second hub (not shown in the figures).
  • the first (outer) hub part 44 is connected to a second (inner) hub part 49.
  • the hub parts 44,49 may be displaced in axial direction by turning the one hub part relative to the other. The axial displacement of the hub parts control the position of the inductor rotors relative to the magnet rotor.
  • connector unit comprises a spacer configured to be connected to both the inner surface of the first inductor rotor and the inner surface of the second inductor rotor.
  • the spacer is configured to position the first and second inductor rotors relative to each other at a selected axial distance from a plurality of axial distances (i.e. a discrete number of distances or a continuum of distances).
  • connection unit 53 comprises a spacer, more specifically a spacer bolt, (assembly) configured to connect the inductor rotors with a fixed but adjustable space between them.
  • Figure 6 A shows a situation wherein the induction rotors are arranged relatively close to each other and the air gaps are relatively small.
  • Figures 6B and 6C represent situations wherein the induction rotors are displaced in an axial direction 64 to form larger air gaps G ! ,G 2.
  • the figures show a spacer bolt 56 including two locknuts 57,59 at both ends.
  • the locknuts and spacer bolt are threaded to allow the locknuts to be attached to the spacer bolt.
  • the spacer bolt 56 is also externally threaded at a central area (cf. threaded portion 58) .
  • the figures also show a spacer sleeve 60.
  • the spacer sleeve 60 is internally threaded (cf. threaded portion 61) to fit around the spacer bolt 56. Loosening the locknut 57 allows the spacer bolt 56 to be rotated in the spacer sleeve 60 to increase or decrease the distance between the conductors 51,52 (see direction of movement 64 in figure 5).
  • the adjustable connection units allow easy and accurate centering of the rotor between the inductor rotors, without having to reposition the complete motor or pump. For instance, the application (pump or other machine) may require another speed after installing the coupling as installed. Adjusting the air gap allows a lower or higher output speed.
  • the connection units enable setting the inductor distance, moving one inductor rotor towards or away from the other inductor rotor. After this the magnet rotor may be at an off center position between the inductor rotors. The magnet rotor may then be centered again with the earlier described axial displacement mechanism of the inner and outer hub parts. This repositions the coupling assembly in axial direction.
  • FIGS 10 and 11 show another embodiment of a magnetic coupling assembly 70.
  • the assembly 70 comprises an inner hub part 71 and an outer hub part 72.
  • the outer hub part 72 is provided with thread 73 and the inner hub part 71 with thread 74, so that the outer hub part and inner hub part may be moved in axial direction 75 by rotating the outer hub part relative to the inner hub part.
  • the inner hub part 71 includes a radial flange 76 that may be mounted to an inductor cage (not shown) using a number of bolts 77.
  • Figure 12A shows the situation wherein the air gap (GO between the inductor rotor 21 and the side face of the magnet rotor 30 and the air gap (G 2 ) between the inductor rotor 22 and the side face of the magnet rotor 30 is the same.
  • Figure 12B shows the situation wherein the outer hub part 4 has been moved outward in axial direction (by rotation of the outer hub part 4 relative to the inner hub part 5) and has been fixed to the inner hub part 5 in the outwardly moved position.
  • Figure 12C shows the situation wherein the distance between the left inductor rotor 21 and the right inductor rotor 22 has been increased by operation of the connection units 52.
  • the axial displacement of the conductor cage may be accomplished at the same time as the axial displacement of the inductor rotors.
  • the axially movable hub parts according to embodiments of the invention may be arranged at the drive side, the load side or both at the load and drive sides of the coupling.

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Dynamo-Electric Clutches, Dynamo-Electric Brakes (AREA)

Abstract

L'invention se rapporte à un ensemble de couplage magnétique permettant d'associer un premier arbre rotatif à un second arbre rotatif, l'ensemble de couplage magnétique comprenant : un premier moyeu rotatif destiné à être raccordé au premier arbre rotatif, le premier moyeu comprenant un rotor à aimants comprenant une pluralité d'aimants permanents ; un second moyeu rotatif destiné à être raccordé au second arbre rotatif, le second moyeu comprenant un logement de conducteur comprenant au moins un conducteur positionné à une certaine distance d'un côté du rotor à aimants faisant face au second arbre rotatif ; le second moyeu et/ou le premier moyeu comprenant une partie de moyeu interne et une partie de moyeu externe, les parties de moyeu étant configurées de sorte à permettre à la partie du moyeu externe d'être mobile axialement sur la partie de moyeu interne pour ajuster la position axiale d'un ou plusieurs conducteurs par rapport au rotor à aimants.
PCT/NL2015/050164 2014-03-13 2015-03-13 Ensemble de couplage magnétique WO2015137814A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US15/125,677 US10211716B2 (en) 2014-03-13 2015-03-13 Magnetic coupling assembly
EP15719517.3A EP3117509B1 (fr) 2014-03-13 2015-03-13 Ensemble de couplage magnétique

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
NL2012431 2014-03-13
NL2012431 2014-03-13
NL2013219A NL2013219B1 (en) 2014-03-13 2014-07-18 Magnetic coupling assembly.
NL2013219 2014-07-18

Publications (1)

Publication Number Publication Date
WO2015137814A1 true WO2015137814A1 (fr) 2015-09-17

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015011960A1 (de) * 2015-09-18 2017-03-23 INGENIEURBüRO CAT M. ZIPPERER GMBH Starter-Anordnung
NL2016163B1 (en) * 2016-01-27 2017-08-04 Zytec Tech B V Magnetic coupling assembly
CN110472329A (zh) * 2019-08-14 2019-11-19 中国电建集团河南工程有限公司 中间加长轴联轴器的找正方法
CN113098229A (zh) * 2021-04-04 2021-07-09 合肥工业大学 一种筒式聚磁盘式涡流传动装置
CN114915135A (zh) * 2022-06-20 2022-08-16 青岛海润隆泰动力科技有限公司 一种磁力耦合器及其使用方法

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05252728A (ja) * 1992-12-07 1993-09-28 Ogura Clutch Co Ltd 磁気継手
US5668424A (en) * 1993-05-21 1997-09-16 Magna Force, Inc. Permanent magnet coupling and transmission
CN101814820A (zh) * 2010-02-26 2010-08-25 王荣松 一种永磁驱动调速器
CN201629653U (zh) * 2010-01-15 2010-11-10 南京艾凌节能技术有限公司 一种永磁调速器
WO2011018015A1 (fr) * 2009-08-11 2011-02-17 Lin Guisheng Dispositif de régulation de vitesse et de transmission par accouplement par aimant permanent et arbre de transmission réglable à couple magnétique
US20120019087A1 (en) * 2010-07-20 2012-01-26 Jones Johnnie L Magnetic Electron Exciter and Methods
WO2013009903A2 (fr) * 2011-07-12 2013-01-17 MaxForce Energy Technologies Co., Ltd. Coupleur magnétique
CN103107675A (zh) 2013-01-14 2013-05-15 浙江大学 可调速磁涡流联轴器

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH05252728A (ja) * 1992-12-07 1993-09-28 Ogura Clutch Co Ltd 磁気継手
US5668424A (en) * 1993-05-21 1997-09-16 Magna Force, Inc. Permanent magnet coupling and transmission
WO2011018015A1 (fr) * 2009-08-11 2011-02-17 Lin Guisheng Dispositif de régulation de vitesse et de transmission par accouplement par aimant permanent et arbre de transmission réglable à couple magnétique
CN201629653U (zh) * 2010-01-15 2010-11-10 南京艾凌节能技术有限公司 一种永磁调速器
CN101814820A (zh) * 2010-02-26 2010-08-25 王荣松 一种永磁驱动调速器
US20120019087A1 (en) * 2010-07-20 2012-01-26 Jones Johnnie L Magnetic Electron Exciter and Methods
WO2013009903A2 (fr) * 2011-07-12 2013-01-17 MaxForce Energy Technologies Co., Ltd. Coupleur magnétique
CN103107675A (zh) 2013-01-14 2013-05-15 浙江大学 可调速磁涡流联轴器

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015011960A1 (de) * 2015-09-18 2017-03-23 INGENIEURBüRO CAT M. ZIPPERER GMBH Starter-Anordnung
DE102015011960B4 (de) 2015-09-18 2023-02-09 INGENIEURBüRO CAT M. ZIPPERER GMBH Gasturbine, insbesondere Strahltriebwerk
NL2016163B1 (en) * 2016-01-27 2017-08-04 Zytec Tech B V Magnetic coupling assembly
US11356009B2 (en) 2016-01-27 2022-06-07 Zytec Technologies B.V. Magnetic coupling assembly
CN110472329A (zh) * 2019-08-14 2019-11-19 中国电建集团河南工程有限公司 中间加长轴联轴器的找正方法
CN110472329B (zh) * 2019-08-14 2022-10-04 中国电建集团河南工程有限公司 中间加长轴联轴器的找正方法
CN113098229A (zh) * 2021-04-04 2021-07-09 合肥工业大学 一种筒式聚磁盘式涡流传动装置
CN114915135A (zh) * 2022-06-20 2022-08-16 青岛海润隆泰动力科技有限公司 一种磁力耦合器及其使用方法

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