GB2089583A - Induction Motors - Google Patents

Induction Motors Download PDF

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Publication number
GB2089583A
GB2089583A GB8134993A GB8134993A GB2089583A GB 2089583 A GB2089583 A GB 2089583A GB 8134993 A GB8134993 A GB 8134993A GB 8134993 A GB8134993 A GB 8134993A GB 2089583 A GB2089583 A GB 2089583A
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United Kingdom
Prior art keywords
rotor
conductors
formations
stator
induction motor
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Granted
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GB8134993A
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GB2089583B (en
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Rolls Royce Power Engineering PLC
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Northern Engineering Industries PLC
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Application filed by Northern Engineering Industries PLC filed Critical Northern Engineering Industries PLC
Priority to GB8134993A priority Critical patent/GB2089583B/en
Publication of GB2089583A publication Critical patent/GB2089583A/en
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Publication of GB2089583B publication Critical patent/GB2089583B/en
Expired legal-status Critical Current

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Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K17/00Asynchronous induction motors; Asynchronous induction generators
    • H02K17/02Asynchronous induction motors
    • H02K17/16Asynchronous induction motors having rotors with internally short-circuited windings, e.g. cage rotors
    • H02K17/168Asynchronous induction motors having rotors with internally short-circuited windings, e.g. cage rotors having single-cage rotors
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K2201/00Specific aspects not provided for in the other groups of this subclass relating to the magnetic circuits
    • H02K2201/06Magnetic cores, or permanent magnets characterised by their skew

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Induction Machinery (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)

Abstract

An induction motor with an improved torque/slip characteristic has a solid rotor 12 having longitudinal grooves 10 running parallel to the axis of rotation which connect with circumferential grooves 14 at each end of the rotor. The rotor is plated with copper so that the grooves are filled with copper. The rotor is then machined over the cylindrical outer surface to produce a solid, non- laminated rotor having high- conductivity paths 16 in the longitudinal grooves connected by high-conductivity short-circuiting rings 18 in the circumferential grooves. In a modification the longitudinal grooves may be skewed. Other high conductivity material may replace copper, for example aluminium. <IMAGE>

Description

SPECIFICATION induction Motors The invention relates to induction motors.
The rotors of known induction motors are required to have high permeability magnetic flux paths and high conductivity electric current paths.
Accordingly it is usual to construct the rotor from thin steel laminations threaded with copper or aluminium bars. One important reason for laminating the rotor steel is to avoid the high frequency loss caused by pulsation of the air gap flux due to the stator slots.
A necessary design feature of laminated rotor induction motors is that the circular depth of the rotor laminations be of the same order as that of the stator (in order to carry the flux) (Figure 1).
In certain special applications, where the overall machine diameter is limited, it is not possible to provide the necessary annular depth for the rotor laminations, while providing a shaft of sufficient cross-section for torque transmission, without a substantial derating of the power output of the machine.
Non-laminated rotors have been proposed for highly specialised relatively long machines of relatively small transverse dimensions. Such machines are in a class of low power machines.
The rotor then comprises a homogeneous steel cylinder, or tube, and the rotor material is chosen for its ability to carry magnetic flux and electric current and to transmit torque.
The material usually chosen is a low carbon steel which often gives an acceptable compromise of magnetic and electric properties (Figure 2). However, known motors having solid steel rotors suffer from two major disadvantages: high slip speed (and hence low efficiency) and poor power factor.
To reduce slip speed the rotor surface of known motors is sometimes covered with a high conductivity sleeve of copper. In such motors the steel carries the flux and the copper carries most of the current. However a major limitation to this type of rotor is the presence of high frequencyrotor losses which can only be avoided by restrictive stator design. Also, because the high conductivity sleeve is in the airgap of the machine, the magnetic airgap ("entrefer") is increased over that for a homogeneous rotor and the power factor is considerably worsened (Figure 3). Such rotors are therefore proposed only in small induction motors of low output power or in current-driven machines, such as eddy-current couplings.
The present invention has the following objectives for an electric motor such as a submersible induction motor driving a pump, for example: (1) most robust construction possible (2) high ratio of starting torque/starting current (3) minimum axial length (to minimise flexible shaft problems) (4) best efficiency and power factor compatible with (1), (2) and (3).
Most known submersible pump motors have outside casing diameters in the range 100 to 350 mm. (3.94 inches to 13.78 inches). Axial lengths range from a few metres to 25 m. (984 inches).
Conventional known rotor constructions, involving laminations built up on a shaft, suffer from disadvantages in respect of the objectives: (a) the laminations do not contribute to the strength of the rotor: this is provided by the shaft; (b) starting torque/starting current ratios are of the order of 0.5:1 to 0.3:1 due to the natural characteristics of a laminated cage rotor.
Increasing the rotor resistance to improve this ratio causes a reduction in full load efficiency and the need to dissipate excess heat from the rotor; (c) because of (a), the laminations do not contribute to shaft rigidity. The shaft diameter must therefore be chosen to ensure an acceptable maximum bending deflection under excited conditions. This means that the radial depth available for the passage of rotor flux is severly limited. (This effect is compounded if there is an additional requirement for the shaft to be hollow).
Consequently, in machines of same diameter, the ratio radial depth becomes the limiting factor in achieving an adequate flux/pole and hence limits output per unit axial length.
The present invention combines three aspects of construction: to a solid ferromagnetic rotor; a conducting material; and disposition of conducting material in grooves. These aspects are discussed separately below: A. Solid Ferromagnetic Rotor The flux-carrying sections and stress-carrying sections in a non-laminated rotor are not distinct and separate but are common and the rotor throughout its full diametral dimension contributes to rigidity and is available for carrying flux. For a given saturation flux density the fluxper-pole, mean air-gap flux-density, and, hence, torque-per-unit-axial=length is relatively increased.
The air-gap flux-density is relatively increased some 20 to 35%, depending on gap/diameter.
Because of the inherent high resistance of homogeneous ferromagnetic material excited with alternating current, an excellent starting torque/starting current ratio can be achieved (typical values in the range 1:1 to 0.7:1).
However a relatively high slip of around 6% is required to produce full load torque under full speed running conditions which causes inefficiency and rotor heating.
The solid ferromagnetic rotor provides rigidity, robustness and a good starting torque/current characteristic but at the low slip end of the torque/speed curve the curve is the wrong shape.
B. Conducting Material The shape of the torque/speed curve of a solid rotor machine is dictated by a dimensionless parameter, the so-called Gamma factor (F), derived in the analysis by Davis et al. (See Proceedings of the Institution of Electrical and Electronic Engineers Volume 124, No. 12, pages 1187-1196, 1977). Page 1190 of that paper gives generalised torque/speed curves for solidrotor, eddy-current couplings and illustrates that a homogeneous ferromagnetic rotor has a r factor in excess of 2 for most of the torque/speed curve.
An ideal r factor which provides good starting characteristics is in the range 0.1 to 0.3, depending on specific requirements. The paper describes how a copper can be used to achieve these values.
C. Conducting Material in Grooves The techniques described in that paper give excellent results in couplings but induction motors in the size range applicable to pump drives for oil-wells, for example, very significant highfrequency losses are caused by negativesequence fields arising from the interaction of the main air-gap field and the stator slotting pattern at normal running speeds.
In a motor according to the invention these losses are minimised and, at the same time, a r a factor of 0.1 to 0.3 is achieved. The conducting material is disposed in axial grooves. The number of grooves can thus be chosen to give the minimum high-frequency loss compatible with the avoidance of parasitic reluctance torques.
It should be noted that the invention is applicable also to inverted machines, in which the wound stator is mounted concentrically inside the rotor. In this case the plated grooves would be angularly spaced about the rotor within the bore of the rotor.
In this specification the term "unitary" means "non-laminated" and the term "plating" means electro-plating or spray plating or a process of deposition of material by which the deposited material is bonded to the substrate onto which it is deposited.
An induction motor according to the invention comprises a stator and a rotor and the rotor is a unitary member of ferromagnetic material having formations extending lengthwise of the rotor and angularly spaced about the rotor and conductors located by said formations and extending lengthwise of the rotor, said conductors being composed of conductive material applied to said member by plating, and said member and said conductors presenting to said stator surfaces forming part of a common cylindrical shape.
Preferably, the rotor has first formations extending around the ferromagnetic member and second formations extending lengthwise of the rotor between the first formations and angularly spaced about the rotor, the rotor having ring conductors located by the first formations and extending about the rotor and the rotor having second conductors contiguous with the ring conductors and located by the second formations and extending lengthwise of the rotor.
Motors having the improved rotor are described herein by way of example to illustrate the invention with reference to the accompanying drawings in which: Fig. 1 is a diagrammatic end view of a known type of motor showing a known rotor in a known stator; Figures 2 and 3 are graphs illustrating characteristics of known motors having known rotors; Figure 4A is a diagrammatic end view of an improved rotor embodying the invention, the upper half showing the rotor before the application of copper by plating, the lower half showing the finished rotor; Figure 4B is a diagrammatic side view of the rotor shown in Figure 4A, the upper half corresponding to the upper half of Figure 4A and the lower half corresponding to the lower half of Figure 4A but also being shown partly in vertical section;; Figure 5 is a graph illustrating characteristics of a known motor and of a motor embodying the invention; Figure 6 is a diagrammatic end view of a modified rotor embodying the invention; Figures 7A, 7B and 11 are diagrammatic longitudinal diametral sections through parts of downhole pumping equipment for use in an oilwell installation including, and primarily showing, the electric pump motor thereof; Figure 9 is a diagrammatic end elevation with parts removed, of the motor shown in Figures 7A and 7B showing a stator end ring thereof; and Figures 8, 10 and 12 are diagrammatic transverse sections on the lines VIll-VIll, X--X and XIl-Xll, respectively, in Figures 7A and 11.
The rotor shown in Figures 4A and 4B consists of a solid cylindrical member 12 of steel, for example a low-carbon steel (or other ferromagnetic material) which is machined (or forged or cast) to an overall size slightly greater than the final reference size referred to below.
As shown on the upper halves of Figures 4A and 48, rotor member 12 has eight equiangularly spaced straight grooves 10 extending parallel to the rotational axis of the member 12. Each groove is machined in the member 12 and is of rectangular cross-section. Typically the radial depth of such grooves 10 lies in the range 3 mm to 1 5 mm (0.12 to 0.60 inch), for example.
Deeper grooves may be used for certain applications.
At each end, the member 12 is machined to provide an annular spigot relief 14, the radial depth of which equals the radial depth of the grooves 10 and the width of which equals the width of the grooves. (Figures 4A and 48, upper halves).
After the grooves 10 and spigot reliefs 14 have been machined, the member 12 is prepared for overall electroplating with high conductivity copper. The preparation follows known practice in electroplating technology to ensure very good bonding between the plated copper and the steel and includes sandblasting; polishing; pickling if necessary; washing in solvent such as trichloroethylene, for example; cleaning in an electrolytic cleaner; and final rinsing and drying.
The member 12 is then immersed in an electro-plating bath using a suitable cyanide copper solution and electrical conditions are arranged to deposit high conductivity copper on the member 12 overall. Sufficient copper is applied to ensure that the grooves and reliefs are completely filled with copper. This requires that the thickness of copper in the grooves 10 and spigot reliefs 14 is not less than the original depth of those formations and in the spigot reliefs, not less than the original width.
The plated member 12 is then machined over the outer surface and the ends to remove surplus copper and a very small amount of steel to bring the finished surfaces to reference dimensions. The resulting rotor (Figures 4A and 4B lower halves) has external, longitudinaily-extending, copper conductors 16, which are located in, and bound to the surfaces of, the grooves 10 and has copper end-rings 18, which are located in and bound to the surfaces of, the spigot reliefs 14.
The conductors 1 6 interconnect the endrings 18 and the radially outer surfaces of the conductors 1 6 and the end-rings 1 8 are flush with the cylindrical surface of the steel member 12. The end surfaces of the end-rings 18 are flush with the steel end surfaces of the member 12.
The end rings 1 8 and conductors 1 6 and the steel member 12 present to the stator surfaces which are parts of a common external cylindrical shape of the rotor 1 2.
The improvement in torque-slip performance provided by the new design of rotor is shown in Figure 5.
In a modification (not shown) the grooves may be skewed with respect to the rotational axis instead of being parallel to the rotational axis.
In a modification (Figure 6) the rotor may have cooling holes 20, shown in transverse crosssection through the rotor.
Such a motor is of particular advantage where the power output is required to be relatively high and the motor dimensions include relatively great length and relatively small diameter. For example, a motor for use in driving a down-hole pump for use in a drilled borehole of an oil-well may be 1400 millimetres (mm) (55 inches) long and some 200 mm (7.9 inches) in diameter. The rotor in such a machine would be some 1400 mm (55 inches) long and slightly less than 100 mm (3.9 inches) in diameter. Such a motor embodying the invention can be rated at 75 kilowatts (kW), equivalent to 50 kW per metre length of the machine. An example of such a motor is described below with reference to Figures 7 to 12.
The invention is also applicable to other types of induction motor having unitary rotors.
The following modifications may be adopted: Instead of electroplating the conductive material may be applied to the rotor by sprayplating.
Instead of copper, alloys of copper or aluminium may be used as the high-conductivity material applied to the rotor.
Instead of spigot reliefs, the end-rings 1 8 may be formed in circumferential grooves in the member 12 adjacent its ends, for example as described below in relation to Figures 7 to 1 2.
Instead of rectangular-section slots, trapezoidal, part-circular or other cross-sectional shapes may be used. A trapezoidal section, for example, can be machined as an undercut groove to provide a dovetail shape which mechanically interlocks the finished conductor of copper (or other material) to the member 12. Similar undercutting and interlocking can be provided at the end grooves or spigot reliefs to secure the end-rings 1 8.
After the plated rotor has been machined as described above, a very thin layer of material such as nickel, molybdenum zinc or chromium or material containing such elements may be applied by electro-plating or spray-plating. Such material is chosen to give protection against corrosion and erosion and the layer would usually be less than 10 micrometres (394 micro-inch) thick.
The member 12 may be a hollow cylinder instead of solid, for example as described below.
A different number of grooves may be used.
The motor shown in Figures 7 to 12 consists of the following main parts: an outer stator 22; stator windings 24; an inner rotor 26; and the rotor conductive cage 28.
The stator 22 includes an outermost stator tube 30 and the motor is shown in the drawings positioned within a cylindrical lining of a borehole of an oil-well in strata 31, the lining being the socalled production tube 32. Of course, the orientation of the tube 32 and the rotational axis of the motor would in practice be vertical or inclined to the vertical rather than horizontal as shown in the drawings. The left-hand end of the motor as shown in the drawings would be the upper end in practice.
The stator includes two similar packs of annular steel laminations 34 mounted in the tube 30 between end rings 36. The end rings 36 (Figure 9) each have 24 equiangularly spaced open-ended slots 38 in the inner face thereof. The stacks of laminations 34 (Figure 10) each have corresponding inner close-ended slots 39. The two stacks are separated by an annular bearing 40 at the centre of the motor supporting the rotor 26. The bearing 40 has corresponding closedended slots 41 and an innermost bearing ring 43 (Figure 12), which is a shrink fit in the bearing 40.
The stacks of laminations 34 have three sets each of three outer grooves 40 to receive insulated bus bars 42, which extend right through the stator 22 and to which electrical connections such as 44 are made. Such connections 44 connect the stator windings 24 to switchgear (not shown) contained in a housing (not shown) connected to the remote end of a pressure equalising apparatus, which has a housing 46 secured to the stator tube 30. The pressure equalising apparatus is preferably of the kind described in the co-pending application of D.S.M.
Gould filed.
An annular bearing 48 is secured between the stator tube 30 and the housing 46. A similar bearing 50 is provided at the left-hand end of the motor (Figure 7B). The stator tube 30 is secured at that end to an annular connector piece 52 within which thrust bearing pads 54 are mounted which slidingly engage a thrust ring 56 mounted on a shaft extension 58 integral with the rotor 26.
The bearing 50 is secured between the piece 52 and a cylindrical extension 60, which carries a seal assembly (not shown) running against the shaft 58.
The rotor 26 as shown is a hollow cylindrical steel (for example, low-carbon steel) member having at the lefthand end the integral shaft extension 58 and a similar integral extension 62 at the right-hand end. The bearings 48, 50 are engaged by the shaft extensions 58, 62, respectively.
The rotor conductive cage 28 consists of two end-rings 70 each 30 millimetres (1.15 inch) wide and 3 mm (0.115 inch) radially deep in respective annular grooves in the rotor 26. The rings 70 are interconnected by eighteen equiangularly spaced straight conductors 72 making up the remainder of the cage 28. Each conductor 72 is 7.5 mm (0.29 inch) wide and 3 mm (0.115 inch) radially deep and is in a corresponding straight groove in the rotor 26.
The conductors 72 are circumferentiallyspaced by an amount equal to their widths but other numbers, widths and spacings may be used.
The outer cylindrical surface of the cage 28 is flush with the adjacent cylindrical steel surface of the rotor 26 and the common diameter is 83 mm (3.26 inches). The length of the cage 28 is 1734 mm (68.26 inches).
The cage 28 is formed by electroplating copper onto the rotor 28 (which has already had the grooves machined in its surface) so as to fill the grooves completely. After plating the rotor 26 was machined to remove excess copper and a skin thickness of steel to bring the rotor outer diameter to the required finished dimension. The rotor surface was of course carefully prepared as explained above in relation to Figures 1 to 5 to ensure excellent bonding of the copper to the steel substrate surface beneath.
The air-gap at 80 between the rotor 26 and the innermost surfaces of the stator laminations 34 is 1.5 mm (0.057 inch).
The motor proper has a length over the ends of the stator windings 24 measured to the ends of the stator tube 30 of approximately 2180 mm (85.82 inches). The outer diameter of the stator tube is 178 mm (7 inches).
The motor is typically rated for example at 85 kilowatts, 3,300 volts, 23 amperes for a 3phase supply at 100 hertz.
The motor is filled with mineral oil under pressure before it is passed into the production tube 32. During installation the pressure is maintained above ambient. Upon first running up to speed the pressure is equalised to ambient.
These functions are performed by the pressure equalising apparatus as explained in the copending application of the applicants entitled "Pressurising Apparatus".
If preferred, the rotor just described may be given a protective finish, after it has been machined to size, by a second plating technique as already described above.
Although in the preferred embodiments of the invention described above by way of example the rotor has end-rings which short-circuit the lengthwise conductors, it may be possible to dispense with end-rings in some constructions.
For example the rotor may have conductive members other than rings which short-circuit the lengthwise conductors or the lengthwise conductors may be interconnected electrically in some other way, for example, by conductors of copper or other material not applied to the rotor by plating. In all such modifications the rotor presents a cylindrical surface to the stator and the construction of the rotor is such as to give the motor the torque/slip characteristic described above, the lengthwise conductors in all cases being in the form of material applied by plating as described above.

Claims (9)

Claims
1. An induction motor comprising a stator and a rotor in which the rotor is a unitary cylindrical member of ferromagnetic material having formations extending lengthwise of the rotor an angularly spaced about the rotor and conductors located by said formations and extending lengthwise of the rotor, said conductors being composed of conductive material applied to said member by plating, and said member and said conductors presenting to said stator surfaces forming part of a common cylindrical shape.
2. An induction motor comprising a stator and a rotor in which the rotor is a unitary member of ferromagnetic material having first formations extending around the member and second formations extending lengthwise of the rotor between said first formations and angularly spaced about the rotor, the rotor having ring conductors located by said first formations and extending about said rotor and the rotor having second conductors contiguous with said ring conductors and located by said second formations and extending lengthwise of said rotor, said ring conductors and said second conductors being composed of conductive material applied to said member by plating, and said member said ring conductors and said second conductors presenting to said stator surfaces forming part of a common cylinder shape.
3. A motor according to claim 1 or claim 2, in which said conductive material is applied overall to a cylindrical surface of said member including said formations, material subsequently being removed to leave said common cylindrical shape.
4. A motor according to claim 1 or claim 2, in which said conductive material is applied overall to a cylindrical surface of said member, including said formations, said member subsequently being machined to remove conductive material and ferromagnetic material from said cylindrical surface and to leave said common cylindrical shape.
5. An induction motor comprising a stator and a rotor in which the rotor is a unitary cylindrical output shaft of ferromagnetic material having formations locating an array of conductors composed of conductive material applied to said shaft by plating as a contiguous layer, said array and said shaft presenting to said stator, surfaces forming part of a common cylindrical shape, said shaft throughout its full diametral dimension contributing both mechanial rigidity and electromagnetic flux-carrying capability.
6. An induction motor according to claim 5, in which the overall diameter of the motor is such as to enable the motor to be installed in oil-well production tube with said rotor extending lengthwise of said production tube and in which said array of conductors is of copper comprises two conductor rings and equiangularly distributed straight conductors contiguous with said conductor rings, said conductor rings being located in annular grooves in said shaft and said conductors being located in straight grooves in said shaft, the radial depth of said conductor rings and conductors being in the range 3 to 1 5 millimetres.
7. An induction motor according to claim 5, substantially as herein described with reference to Figures 4A, 4B and 5 of the accompanying drawings.
8. An induction motor according to claim 7, modified substantially as herein described with reference to Figure 6 of the accompanying drawings.
9. An induction motor according to claim 5, substantially as herein described with reference to Figures 7A to 12 of the accompanying drawings.
GB8134993A 1980-12-11 1981-11-20 Induction motors Expired GB2089583B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8134993A GB2089583B (en) 1980-12-11 1981-11-20 Induction motors

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8039707 1980-12-11
GB8134993A GB2089583B (en) 1980-12-11 1981-11-20 Induction motors

Publications (2)

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GB2089583A true GB2089583A (en) 1982-06-23
GB2089583B GB2089583B (en) 1985-02-06

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0067704A2 (en) * 1981-06-17 1982-12-22 MATHER &amp; PLATT LIMITED Electric motors
FR2525830A1 (en) * 1982-04-23 1983-10-28 Renault ELECTRODYNAMIC MACHINE COOLED BY A LIQUID
EP0583994A1 (en) * 1992-07-07 1994-02-23 High Speed Tech Oy Ltd. Asynchronous electric machine and rotor and stator for use in association therewith
EP0637867A1 (en) * 1993-02-24 1995-02-08 Fanuc Ltd. Cage rotor of induction motor
NL1026424C2 (en) * 2004-06-15 2005-12-19 Siemens Ind Turbomachinery B V Rotor for electric motor, compressor unit provided with rotor, method for manufacturing a rotor for an electric motor.
DE102017206567A1 (en) * 2017-04-19 2018-10-25 Robert Bosch Gmbh Stator core and electric machine with the stator core

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0067704A2 (en) * 1981-06-17 1982-12-22 MATHER &amp; PLATT LIMITED Electric motors
EP0067704A3 (en) * 1981-06-17 1983-03-09 MATHER &amp; PLATT LIMITED Electric motors
FR2525830A1 (en) * 1982-04-23 1983-10-28 Renault ELECTRODYNAMIC MACHINE COOLED BY A LIQUID
US5473211A (en) * 1992-07-07 1995-12-05 High Speed Tech Oy Ltd. Asynchronous electric machine and rotor and stator for use in association therewith
EP0583994A1 (en) * 1992-07-07 1994-02-23 High Speed Tech Oy Ltd. Asynchronous electric machine and rotor and stator for use in association therewith
EP0637867A1 (en) * 1993-02-24 1995-02-08 Fanuc Ltd. Cage rotor of induction motor
EP0637867A4 (en) * 1993-02-24 1995-09-27 Fanuc Ltd Cage rotor of induction motor.
US5572080A (en) * 1993-02-24 1996-11-05 Fanuc Ltd. Squirrel-cage rotor for induction motor
NL1026424C2 (en) * 2004-06-15 2005-12-19 Siemens Ind Turbomachinery B V Rotor for electric motor, compressor unit provided with rotor, method for manufacturing a rotor for an electric motor.
WO2005124973A1 (en) * 2004-06-15 2005-12-29 Siemens Industrial Turbomachinery B.V. Rotor for electric motor, compressor unit provided with rotor, method for producing a rotor for an electric motor
US7646128B2 (en) 2004-06-15 2010-01-12 Siemens Aktiengesellschaft Rotor for electric motor, compressor unit provided with rotor, method for producing a rotor for an electric motor
EP2403116A1 (en) * 2004-06-15 2012-01-04 Siemens Aktiengesellschaft Rotor for electric motor, compressor unit provided with rotor, method for producing a rotor for an electric motor
DE102017206567A1 (en) * 2017-04-19 2018-10-25 Robert Bosch Gmbh Stator core and electric machine with the stator core

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PCNP Patent ceased through non-payment of renewal fee

Effective date: 19931120