WO2000051224A1 - Permanent magnet d.c. motor having a radially-disposed working flux gap - Google Patents

Permanent magnet d.c. motor having a radially-disposed working flux gap Download PDF

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Publication number
WO2000051224A1
WO2000051224A1 PCT/US1999/003808 US9903808W WO0051224A1 WO 2000051224 A1 WO2000051224 A1 WO 2000051224A1 US 9903808 W US9903808 W US 9903808W WO 0051224 A1 WO0051224 A1 WO 0051224A1
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WIPO (PCT)
Prior art keywords
motor
rotor
stator
pole
permanent magnet
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PCT/US1999/003808
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English (en)
French (fr)
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Petersen Technology Corporation
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Publication date
Application filed by Petersen Technology Corporation filed Critical Petersen Technology Corporation
Priority to CA002362686A priority Critical patent/CA2362686A1/en
Priority to PCT/US1999/003808 priority patent/WO2000051224A1/en
Priority to EP99973722A priority patent/EP1153472A4/de
Publication of WO2000051224A1 publication Critical patent/WO2000051224A1/en

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Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K21/00Synchronous motors having permanent magnets; Synchronous generators having permanent magnets
    • H02K21/12Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K1/00Details of the magnetic circuit
    • H02K1/06Details of the magnetic circuit characterised by the shape, form or construction
    • H02K1/12Stationary parts of the magnetic circuit
    • H02K1/14Stator cores with salient poles
    • H02K1/146Stator cores with salient poles consisting of a generally annular yoke with salient poles
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K29/00Motors or generators having non-mechanical commutating devices, e.g. discharge tubes or semiconductor devices
    • H02K29/06Motors or generators having non-mechanical commutating devices, e.g. discharge tubes or semiconductor devices with position sensing devices
    • H02K29/08Motors or generators having non-mechanical commutating devices, e.g. discharge tubes or semiconductor devices with position sensing devices using magnetic effect devices, e.g. Hall-plates, magneto-resistors
    • 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
    • H02K2201/12Transversal flux machines

Definitions

  • brush commutation systems are electrically noisy, precluding their use in conjunction with modern electronic equipment such as computers, and further precluding their use for spark free applications as in the marine field.
  • the classic design for brush commutated PM motors does exhibit, however, the salient aspect of providing a relatively high ratio of the radius from their shaft axis with respect to their working gap to their outer radius. That ratio, typically, is about 0.7 or higher.
  • the higher ratio is achieved because of a design wherein the laminar pole components about which windings are provided are mounted upon the rotating shaft of the motor. These rotating pole pieces, then extend radially outwardly to the flux working gap in adjacency with outwardly disposed permanent magnets which are mounted adjacent to the outer housing of the motor.
  • the result is an extended radius to the working gap but with the disadvantage of a substantial inability to transfer heat from heat generating coil components on a practical basis through the shaft and bearings to the outside.
  • Fan components have been attached to the shafts but with no practical improvement in motor performance.
  • the spinning rotor winding requires balancing as part of production.
  • Such typical winding based rotors are characterized by a long average winding turn length that is at least twice as long as the length of the rotor lamination stack.
  • stack length typically is increased rather than diameter.
  • the average turn length increases as the length of the rotor stack is increased to increase motor output power resulting in the requirement to increase the diameter of the wire to maintain the motor impedance.
  • the larger diameter wire often results in less turns per pole which, in turn, works against the desired power improvement which was the reason why the stack length was originally increased.
  • This assembly is seen to occur in the conventional designs of both brush commutated and brushless radial gap motors. Notwithstanding their drawbacks, these brush commutated motors prevail in modern consumer products such as hand tools simply because of lower cost.
  • the permanent magnet assemblage for the motor is mounted on and rotates with the shaft.
  • An immediate advantage of this arrangement resides in good heat dissipation, providing for stable operation over a wide power range. Additionally, a spinning rotor magnet generally does not require balancing.
  • An immediate disadvantage of the motor resides in its poor power production per unit diameter, i.e., the motor exhibits a relatively low ratio of radius to the working gap from the shaft axis with respect to the radius from the shaft axis to the outer surface of the motor. For motors under 3 inches in diameter, that ratio typically will be about 0.5. This means that the motors inherently exhibit lower power production for their weight and bulk. Further, the conventional designs require longer lamination stacks coincident with longer field winding path lengths which results in heavier weight and an elevated cost for the development of equivalent power.
  • the motor is constructed similar to conventional PM D.C. brush type motors with the windings on the inside. They also exhibit similar poor heat dissipation characteristics as PM D.C. brush type motors. Petersen, in U.S. Pat. No. 4,745,345, entitled "D.C. Motor with Axially Disposed
  • Such axial type motors have exhibited excellent dynamic performance and efficiency and, ideally, may be designed to assume very small and desirably variable configurations.
  • the motors are relatively expensive, requiring costly sintered rare earth magnets and the like which, in turn, exhibit a high axial attractive force between the rotor and the stator which is modulated upon the excitation of the field windings creating an undesirable noise level for certain applications such as disk drives.
  • the motor is a specialized device of relatively high cost and intended for the computer industry.
  • the motors not only exhibit the desirable heat dissipation advantages of conventional brushless designs, but also provide improved torque output characteristics.
  • One factor contributing to this improved torque performance resides in a relatively high ratio of the radius from the motor axis to its working gap with respect to the corresponding radius to its outer periphery. For example, that ratio typically is above about 0.7 for motors between about 1 and 3 inches in diameter
  • Fig. 1 is a sectional schematic representation of a conventional d.c. motor having three rotor poles and two stator poles as conventionally commutated utilizing brushes;
  • Fig. 2 is a sectional schematic representation of a conventional brushless d.c. motor
  • Fig. 3 is an electrical schematic diagram of a Y-type excitation winding interconnection
  • Fig. 4 is a perspective view of one motor embodiment according to the invention
  • Fig. 5A is a sectional view taken through the plane 5-5 shown in Fig. 4;
  • Fig. 5B is similar to Fig. 5A but shows an alternate architecture for heat dissipation
  • Fig. 6 is a sectional view taken through the plane 6-6 shown in Fig. 5A;
  • Fig. 7 is a partial perspective view showing a core component and associated field winding assembly employed with the motor of Fig. 4;
  • Fig. 8 is a perspective view of a section of a plastic bonded ring type magnet employed with the motor of Fig. 4;
  • Fig. 9 is a B-H family of curves showing load lines thereon;
  • Fig. 10 is a schematic top view of permanent magnet sectors and pole components of the motor of Fig. 4 showing electromagnetic and permanent magnet flux paths;
  • Fig. 11 is a pictorial view of the stator core assembly employed with the motor of Fig. 4;
  • Figs. 12A-12D are partial plan views of four sheet metal components employed in the formation of the structure of Fig. 11 ;
  • Fig. 13 is a pictorial view of another motor structured in accordance with the invention.
  • Fig. 14 is a sectional view taken through the plane 14-14 in Fig. 13;
  • Fig. 15 is a sectional view taken through the plane 15-15 in Fig. 14;
  • Fig. 16 is a plan view of a sheet metal component utilized in forming a core component for the motor of Fig. 14;
  • Fig. 17 is a partial top view of permanent magnet sectors and pole components for a motor according to the invention with an outwardly disposed radial gap showing a tapered stator pole gap;
  • Fig. 18 is a partial schematic top view of permanent magnet sectors and pole components for an inwardly disposed radial gap motor architecture showing a tapered stator pole gap;
  • Fig. 19 is a partial sectional view of a variation of the architecture of the motor of Fig. 4;
  • Fig. 20 is a sectional view of another motor structured in accordance with the invention
  • Fig. 21 is a top view of another motor structured in accordance with the invention with portions broken away to reveal internal structure
  • Fig. 22 is a sectional view of the motor shown in Fig. 21 taken through the plane 22-22 therein.
  • Brushless D.C. PM motors as now presented, in consequence of their architecture, represent a motor entity which is commercially viable in the consumer products industry. These motors utilize magnets bonded with a plastic or other polymeric material and having an energy product value lower than sintered rare earth magnets, but in a manner which optimizes their capability for magnetic flux generation within a flux working gap. Equivalent or better performance in terms of torque output is achieved through enhanced radial distance from the motor axis to the working gap, particularly as that radius is compared to the overall radius of the motor itself. For motors of what may be considered a larger variety having, for example, diameters of about 4 inches or larger, substantial savings in otherwise expensive magnetically permeable materials employed for stator pole core definition are achieved. In effect, the motors exhibit the motor axis to working gap radial distances made available through conventional brush commutated, PM D.C. motors but with a brushless operation, while enjoying the heat dissipation advantages of conventional brushless motors.
  • FIG. 1 a stylized sectional view of a conventional PM D.C. motor, for example commutated with a brush structuring, is revealed generally at 10.
  • Motor 10 is shown having an outer metal shell 12 which supports and serves as the back iron or magnetically permeable back component for permanent magnets, two of which are shown at 14 and 16.
  • magnets are of a ferrite-type which, compared to rare earth sintered magnets and the like, are relatively inexpensive, thus promoting motors as at 10 to applications in consumer markets.
  • Rotationally mounted upon the motor shaft 18 is a rotor 20, the rotor poles of which at 22-24 are mounted for rotation about the central or motor axis 26.
  • the poles 22-24 generally are formed as a lamination of steel sheets, which structuring facilitates magnetic flux transfer and current flow in consequence of their multiple surfaces.
  • Each of the poles 22-24 is formed having an arcuate or flared outer tip as represented, respectively, at 28-30. Tips 28-30 are structured such that their outward ends are closely proximate each other to permit flux transfer thereacross.
  • each rotor pole rotates in proximity with the inwardly-disposed surfaces of permanent magnets 14 and 16 to define a working air gap which may be referred to as "radial" inasmuch as the polarization of magnets 14 and 16 is along the radius from the motor axis 26.
  • field windings 36-38 are wound about the respective poles 22-24 internally of their outer tip portions 28-30.
  • a field is caused to move about tips 28-30 as the rotor rotates. That field interacts with the magnetic field of permanent magnets 14 and 16 to develop motion.
  • the outermost or maximum outer motor radius, RM is not of substantially greater length than the corresponding radius, RQ, to the center of the working air gaps as at 32 and 34.
  • RG- This quality of torque generating capability may be expressed by the ratio RG/RM-
  • the typically encountered value for the conventional brush PM motor is 0.7 or greater. Because of their lower cost, such motors essentially predominate in the application of motor technology to consumer products.
  • the disadvantages associated with motors as at 10 reside in their poor heat dissipation characteristic. As power is increased, this poor heat dissipation limits the ability to deliver continuous high output power.
  • the heat generating components of the motor 10 are the windings 36-38 which are mounted upon shaft 18.
  • the route for conductive heat transfer out of motor 10 is through the shaft and the bearings, a highly inefficient arrangement.
  • motors such as at 10
  • the presence of windings 36-38 essentially upon the shaft 18 require that the rotor be balanced for most applications.
  • the rotor stack length may be increased which, in turn, increases the average turn length of the rotor windings.
  • Such increase in the average turn length increases the resistance of the windings and thereby ultimately decreases the power out.
  • the wire diameter may be increased such that the resistance of the motor is maintained, there often is insufficient winding area to support the increased wire diameter.
  • a conventional brushless motor is represented in schematic fashion at 40.
  • Motor 40 is formed having an outer shell or stator 42 made up of laminations from which inwardly-depending stator pole pieces 44-52 depend, and terminate in flared tips shown, respectively, at 53-61.
  • Field windings 62-70 are positioned about the respective pole pieces 44-52.
  • a shaft 71, rotating about a motor axis 72 supports a rotor shown generally at 73 which, in turn, supports a sequence of permanent magnets having six magnetic poles thereof which may be alternately polarized in the earlier-noted radial sense, and are represented at 74.
  • a magnetically permeable back component or back iron is shown at 76.
  • a control pick-off assembly for example, magnetically responsive devices located in adjacency with rotor 73 which serve to instantaneously locate the rotational orientation of rotor 73 relative to stator 42. This motor architecture provides for good heat dissipation with stable operation over a wide power range.
  • the heat generating components such as windings 62-70 are coupled in thermal transfer with the outer shell 42.
  • the radius from the motor axis 73 to the working air gap 78 again identified as RG is much smaller than the radius to the outer boundary of the motor RM- Typically, the ratio RG ⁇ RM will De about 0.5 to 0.7. This means that the motor 40 exhibits poorer power production per unit motor diameter.
  • another advantage resides in a spinning rotor 73 which generally does not require balancing.
  • the brushless motor now presented essentially minimizes the amount of lamination or stack material required, particularly for larger motor sizes in the range of 4 inches diameter or more. This lowered material requirement reduces motor cost.
  • the now presented motor uniquely employs an architecture permitting the use of less volume of permanent magnet material to again reduce materials cost while exhibiting good power production per unit diameter, i.e. the ratio RG/RM is at least about 0.7.
  • the rotor of the motor generally does not require balancing and additionally exhibits a short field winding average turn length which is easier to wind and which greatly reduces the costs attending the winding of the motor.
  • the shorter average turn length of each stator turn generally means a smaller required diameter wire and, accordingly, less total copper, again reducing costs.
  • the radius of the motor from its motor axis to its working air gap, RQ is substantially expanded to permit the achievement of high torque outputs from small light motors.
  • the winding excitation approaches for operating brushless motors such as those according to the invention vary somewhat, the windings typically are interconnected in either a "Y" or a "_" configuration for three phase operation.
  • a typical "Y" circuit topology is revealed for nine field windings which may perform, for example, in conjunction with a rotor structure incorporating six polar magnet regions.
  • Each leg of the Y circuit 80 represents a given phase, i.e. phase A, phase B, and phase C.
  • phase A windings 1, 4, and 7 are energized, while in phase B, windings 2, 5, and 8 are energized, and in phase C, windings 3, 6, and 9 are energized.
  • phase B windings 2, 5, and 8 are energized
  • phase C windings 3, 6, and 9 are energized.
  • a "bipolar" form of excitation is employed.
  • positive electrical coupling may be made to one outer terminal of the Y circuit 80, while a negative circuit connection is made to one other terminal.
  • any one given phase is energized in a two-step sequence.
  • phase combination, A-C may be energized by applying a positive source to terminal I, while the corresponding negative connection is applied to terminal III.
  • an energizing sequence may be developed which is repeated in the course of normal motor operation with the objective of creating sequential torque vectors presented as tangent forces to the circular locus of the working air gap driving the rotor structure.
  • design architecture may vary depending upon the diametric size of the motor.
  • motors for example, having outside diameters of about two inches are considered “small” in terms of the present design, while motors of larger diametric extent, for example 4 inches or greater, are considered “larger” to the extent, for example, that cost considerations look more pointedly to the amount of magnetically permeable lamination material which is employed.
  • the highly desirable ratio of the radius to the working gap, RG, to the maximum outer motor radius, R remains greater than about
  • FIG. 4 a perspective representation of a larger motor, having a outer motor diameter of about 4 inches is represented generally at 90.
  • Motor 90 will be seen to have an architecture referred to as "outside radial gap" which maximizes the length of the radius to the working gap, RG.
  • Motor 90 is configured having a cylindrically shaped housing 92. This housing 92 incorporates portions of the stator assembly and extends upwardly in parallel with the motor axis 94 to an annular edge 96. Controlled d.c. input to the motor 90 is through, for example, a cable 98 extending from the side of housing 92.
  • Rotor 100 Above the housing 92 and its edge 96 is a rotor 100 having a top surface 102 which extends to a circumferentially disposed magnet and back iron or back component supporting flange 104.
  • Rotor 100 is driven in rotation about the motor axis 94 and functions to drive a motor shaft as at 106 coaxially disposed with axis 94 and supported at a bearing structure mounted within the housing 92.
  • motor 90 employs a support structure which includes a base 110.
  • Base 110 is circular and formed, for example, of aluminum.
  • a stator pole assembly mounting portion 111 disposed along the outer periphery are a plurality of stator assemblies represented generally at 112 which are arranged in a circular locus.
  • Fig. 6 reveals the presence of 18 such stator pole assemblies which are identified at 114a-114r.
  • Fig. 7 it may be observed that each of the stator poles 114a-114r has a laminar core component 116a-116r which is formed integrally with and extends above a core interconnecting base support portion 118.
  • Core components 116a-116r are relatively lengthy and arranged generally parallel with motor axis 94. Each may be considered to have two portions, one a winding association region as seen at 120a and 120b in Fig. 7, over which is positioned a stator winding assembly 122a-122r, bobbins 124a and 124b being shown in detail in Fig. 7, assemblies 122a and 122b being shown in detail in Fig. 7. Each of the assemblies 122a-122r is formed of a plastic, non-conducting bobbin 124a-124r, about which are provided field windings 126a-126r, windings 126a and 126b of which are revealed in detail in Fig. 7.
  • the field windings 126a-126r when excited, interact to generate electromagnetic flux (an energized field) within the laminar core components 116a-116r and base structure 118.
  • electromagnetic flux an energized field
  • the total radial thickness of the cores is about 0J12 inch.
  • each of the core components 116a-116r continues integrally to establish a pole piece region as seen in Fig. 7 at 128a and 128b.
  • This pole piece region which is referred to generally at 128, typically extends above the windings 126a-126r an amount representing about one-half or less of the height of the windings or their associated winding association region 120. In general, the pole piece region height is not made higher than the height of the windings. It is the flux interaction surface of this pole piece region 128 of relatively large dimension which is employed to confront a relatively thin but axially lengthy magnet across a relatively short working gap. The distance between the pole piece regions 128 is selected such that the electromagnetic flux path is between adjacent stator poles. This is achieved by making that distance a value representing a least impedance to the flow of electromagnetic flux with respect to other paths which might be available.
  • each pole piece is curved or "radiused" as is the outwardly disposed surface of each pole piece.
  • An alternative core structure formed of processed ferromagnetic particles may be employed with the instant motors. Ideally, these powder-based cores should be fashioned such that each particle of ferromagnetic material is electrically insulated from adjacent particles to avoid eddy current circulation.
  • the core structures are formed by powder pressing with a binder and a subsequent heating step or sintering. Alternately, the powdered metal is combined with an adhesive and molded without heating. Core production is both simplified and accelerated with this approach.
  • Such powder-based materials are available, for example, from TDK Corporation of Tokyo, Japan, or Keystone Powdered Metal Co., of St. Marys, PA.
  • the windings for example as shown at 126a and 126b will exhibit a given average turn length about the winding association regions of the core structures. It is interesting to observe that this average turn length remains constant notwithstanding the height selected by the designer for the winding association region or the pole piece region. In all other conventional radial motor structures, average turn length will increase as the height the stator or lamination structure increases.
  • stator pole piece area has two flux interaction surfaces, one facing radially inward and the other facing radially outward.
  • the designer can choose the most advantageous location for the permanent magnet assembly magnet component, utilizing either the inward facing or outward facing surface or in applications requiring maximum power output in a minimum motor envelope two magnet components can be used as shown in Fig. 19.
  • rotor 100 is seen to have the general shape of an inverted cup.
  • it is fashioned of steel, inasmuch as it also serves as back iron to the permanent magnet material which it carries.
  • the permanent magnet assembly shown generally at 130 includes a magnet component containing a sequence of alternating magnetic poles which is generally shaped as a ring. Assembly 130 is fixed to the inward surface of supporting flange 104 of rotor 100. The assembly is seen to have a height in the direction of axis 94 corresponding with the height of pole piece region 128.
  • the flux interaction surface of pole piece region 128 and the corresponding confronting flux interaction surface of permanent magnet assembly 130 define a relatively large area working gap 132 which also is of short radial length, Lg, i.e., the interacting surfaces are close together.
  • Lg long radial length
  • Permanent magnet assembly 130 preferably is formed of a thin magnet material, such as neodymium iron boron bonded in a plastic or polymeric binder.
  • the ring-shaped assembly 130 is formed, for example, in 120 ° sector components seen in Fig.
  • magnet assembly 130 provides a north to south pole component thickness or length, Lm, of relatively small value while the narrow working air gap, Lg, of significantly smaller value promotes highly desirable "load line" values.
  • Lm north to south pole component thickness or length
  • Lg narrow working air gap
  • this favorable L m /L g ratio (load line) makes possible the use of lower energy product magnet materials to achieve equivalent air gap flux values as those present in the axially magnetized motors represented in U.S. Pat. No. 4,949,000.
  • the required magnet material is of a sintered rare earth type with typical energy products of 27 MGO to 37 MGO
  • energy product values of approximately 10 mgo will produce an equivalent air gap flux density.
  • the second quadrant of a conventional B-H curve is revealed for a 10 MGO energy product plastic bonded neodymium-iron-boron permanent magnet.
  • demagnetizing force is shown in progressively negative values from a 0 value, while generated kiloGauss (flux) is shown along the ordinate.
  • Intrinsic demagnetization curves are shown at 150-153 for respective temperatures of 24 ° C (room temperature), 80 ° C, 120°C, and 150 ° C.
  • normal demagnetization curves are represented at 156-159 for the corresponding same sequence of respective temperature values. Load lines having values typical for the motors of the instant invention are represented at 162 and 164.
  • these values can be considered to represent the length of the magnet, Lm divided by the radial width of magnet-to-stator gap, Lg.
  • curves 162 and 164 are empirically adjusted for anticipated flux leakage, for example, to the extent of about 50%.
  • a typical load line value for example falling between lines 162 and 164 at a value of 3.5 will produce an air gap flux density of approximately 5.2 kilogauss at room temperature.
  • Load lines encountered with miniature high performance motors of the type represented in U.S. Pat. No. 4,949,000 (supra) would be represented in the region between load lines 166 and 167.
  • a motor of the type presented in the noted U.S. Pat. No. 4,949,000 with a load line of, for example, 0.85 would require magnet material of approximately 30 MGO energy product.
  • 10 MGO material is of a bonded type (plastic) whereas the 30 MGO material currently is a sintered type and a significant cost differential exists between them.
  • motors of the instant invention would benefit from the use of high energy product materials should those materials become available in cost effective form.
  • the motors of the instant invention benefit from the fact that the magnet pole area can increase significantly without changing the load line by increasing the axial length of the radial magnet coincident with an increase in the height of the pole piece region, thereby effecting a much greater total flux transfer, and therefore, higher motor power production capability.
  • motors of the instant invention have magnet load lines typical of today's high performance radial brushless P.M. D.C. motors and use magnet materials typical for such motors there is a significant difference in how the radial pole surface of the permanent magnet rotor interfaces with the laminations of the stator pole piece regions.
  • working gap lengths, Lg will be in a range of about 0.012 inch to 0.016 inch.
  • the gaps are maintained at a tolerance of ⁇ 0.002 to ⁇ 0.003 inch.
  • Fig. 9 reveals that for the air gap structure at hand with load line values of 3.0 and 4.0, and considering room temperature at curve 156, a flux generation range may be observed to lie between horizontal lines 170 and 172, showing a range from about 4.9 kG to about 5.4 kG. This indicates a highly efficient flux generation utilizing relatively lower energy product magnetic material and attendant lower costs.
  • the standard brushless motors heretofore known in the art for use in hard disk drives employ an outside magnet design with a corresponding spinning outside rotor.
  • These motors have a relatively high RG/RM similar to motors of the instant invention and, in typical form, utilize 10 MGO magnet materials.
  • Such motors also use a large number of laminations relative to the motor of the present invention. Inasmuch as these laminations are disposed within the interior of the motor, relatively poor heat dissipation characteristics are exhibited with this form of brushless motor design.
  • the ring-shaped base support portion 118 of the stator structure 112 is seen to be supported within an annular slot 180 formed within aluminum base 110.
  • the shaft 106 of motor 90 is seen to be aligned along axis 94 and is supported upon the base 110 by a bearing structure represented generally at 182.
  • Structure 182 includes a cylindrically shaped bearing retainer 184, spacer 186, and spaced-apart bearings 188 and 190.
  • Shaft 106 is coupled into and supports rotor 100 at a rotor mount 194 connected to rotor 100 with three machine screws 196-198.
  • a similar three-screw arrangement 200-202 secures bearing retainer 184 and an associated circuit assembly 206 to the base 110.
  • the sequence of operational components of it commencing with axis 94 and shaft 106 include, as a next outwardly component at the drive region, the stator pole piece 116, then next radially outwardly there occurs the working gap 132, and next outwardly from that is the permanent magnet assembly 130, whereupon, the final component is back iron 104, the outer surface of which also is the outward radial extent, RM, of motor 90.
  • FIG. 10 the flux paths generated in connection with motors as at 90 are schematically revealed.
  • the numeration employed in conjunction with Figs. 5A-5B is repeated to identify corresponding components.
  • core component 116a of stator structure 112 is shown to be energized in a north polar sense, while adjacent stator cores 116r and 116b are energized in a south polar sense.
  • the flux path from core 116a will be, as represented at arrows 214 and 216, across the gaps between the stator structures and into the adjacent stator cores. The paths then return, for example, through base structure 118.
  • Flux interaction of the permanent magnet sectors, as at 136-138, is, as represented by arrows 218 and 220, into the adjacent stator core as at 116a.
  • the orientation of permanent magnet and stator core is that at which a maximum torque is developed for that pole, the south permanent magnet tending to be attracted to the north stator core and the north permanent magnet flux tending to be repulsed thereby to develop a vector which is tangent to the circular locus of the permanent magnets and stator cores.
  • FIG. 5A a substantial amount of interior space is made available as represented by the interior chamber 204 (Fig. 5A) defined between the base 110 and rotor 100 of motor 90.
  • FIG. 5B another utilization of that interior space, shown at 204', is depicted.
  • the general motor architecture remains identical with that shown in conjunction with motor 90 of Fig. 5A. Accordingly, components of commonality between the figures are shown in primed fashion in connection with Fig. 5B.
  • the motor shown in Fig. 5B incorporates a base structure represented generally at 141 which is of enhanced volume by virtue of the utilization of an array of concentric cooling fins or rings, certain of which are represented at 143.
  • the stator assembly mounting portion is reconfigured as represented at 142 to accommodate for the height of the base structure 141.
  • the inward bearing support is integrally formed as represented at cylindrical bearing support portion 144.
  • Base support structure 141 thus provides a circular upper base platform 145 which may be employed to support a circuit board 146.
  • Circuit board 146 is seen to extend at extension 147 outwardly of motor 140 so as to provide lead inputs to the circuit.
  • Circuit board 146 additionally supports Hall effect devices, one of which is shown at 148, each fitting within a gap intermediate two stator pole pieces.
  • circuit board 146 An interesting aspect of the embodiment of Fig. 5B resides in the advantageous assembly procedure for circuit board 146 and stator structure.
  • the laminar core components 116' are mounted within the base annular slot 180'.
  • Circuit board 146 is configured having a locus of openings therein corresponding in position with the locations of the core components 116'.
  • the field winding assemblies with bobbins are electrically connected by appropriate leads with the circuit located and supported by circuit board 146.
  • the circuit board assembly is positioned over the core components 116' and down essentially against the base platform 145. Close adjacency with the platform 145, however, is not required. With this arrangement, the assembly of the stator components and associated circuitry is completed.
  • circuit board 146 now supports each pole piece region of the core components 116' just below the working gap 132'. This arrangement aids in overcoming the attraction between the permanent magnets of the rotor and the adjacent pole pieces.
  • Hall effect sensing devices as at 148 inasmuch as they are pre-positioned on the circuit board 146.
  • FIG. 17 an alternate embodiment for the laminar pole structuring employed with motor 90 is revealed.
  • Two laminar poles, 352a and 352b are shown in an architecture wherein the gap between the pole regions at the outermost laminations adjacent outer radial gap 132 are more closely spaced together than the inwardly disposed laminations. This then defines a tapered gap 354 which serves to concentrate the flux density in the course of transfer as represented at arrow 355 in a manner enhancing flux flow in adjacency to the gap 132 and permanent magnet segments as at 136 and 137.
  • Fig. 18 the same arrangement is illustrated in connection with a motor as at 270 in Fig. 14 or as at 500 in Fig. 22 wherein the radial gap is inwardly disposed from the stator structure.
  • that lamination of the core structures herein shown at 356a and 356b which is closest to the permanent magnets 340 is configured having the narrowest pole-to-pole gap width.
  • the gap between pole pieces increases to achieve the tapered configuration represented in general at 357. This serves to enhance the transfer of flux or flux flow at a location in adjacency with the gap 344 and magnets 340. This flux transfer is represented by the arrow 358.
  • stator core structure 112 for motor 90 is revealed in perspective fashion.
  • This 18-pole or 18 core (116a-116r) stator structure 112 is formed with 8 laminations, each having a thickness of about 0.014 inch.
  • These laminations are formed of 8 sheet members of varying dimensions selected to form the stator core structure. Utilizing the laminations as a strip metal stamping eliminates a substantial amount of the waste otherwise encountered in forming the core structure.
  • the outermost one of the laminations is shown as a metal sheet member 230 formed as a sheet metal stamping of magnetically permeable material which is configured having 18 integrally formed upstanding core elements, certain of which are revealed from the sequence 230a-230r.
  • These elements 230a-230r are configured having a first predetermined widthwise extent representing the widthwise extent of the core structure outer periphery.
  • the sheet 230 includes two upstanding half core elements 230r and 230r'. These latter elements have a widthwise extent amounting to almost half that of elements 230a-230q. Further, the elements 230a-230r are seen to be spaced apart by slots of predetermined width as represented by select components of a sequence 236a-236r.
  • the member 230 is formed having a core base 238 and extends from an end 240a formed in half core component 230r to an end 240b.
  • an outer core ring is developed as represented and identified in Fig. 11.
  • Fig. 12B reveals the pattern for a next internally disposed core ring formed of metal sheet member 231.
  • sheet member 231 includes a core base 242 and 18 upstanding core elements 231a-231r, only certain of which are revealed in view of the relatively larger number involved.
  • the upstanding core components 231a-231r are of a next predetermined widthwise extent slightly less than the corresponding core elements 230a-230r.
  • two half core elements 231 r and 231 r' are formed in member 231 exhibiting edges 244a and 244b.
  • the end-to-end lengthwise extent of member 231 is selected such that when the latter edges 244a, 244b are brought together to form a next interior core ring, that ring, as seen in Fig. 11 will nest within the core ring corresponding to sheet member 230.
  • the abutting edges 244a and 244b will be positioned away from adjacent edges 240a and 240b.
  • the spacing between core elements 231a-231r are represented as a sequence of slots 246a-246r. These slots are configured having a widthwise extent equal to those described at 236a-236r in Fig. 12A.
  • the slots are dimensioned equally from lamination to lamination. This provides a final gap which exhibits a constant width. By varying the slot width, a variable or tapered gap geometry can be achieved as discussed herein in connection with Fig. 17.
  • metal sheet member 232 is seen to be configured in similar fashion, having a core base 248 from which are integrally formed 18 upstanding core elements 232a-232r, only certain of which are revealed and the end elements 232r and 232r' being of half width.
  • the latter elements define edges 250a and 250b which are drawn together to form a core ring of a third diametric extent configured to nest within the ring formed of metal sheet 231 as seen in Fig. 11. Additionally, it is preferred that edges 250a and 250b be positioned in abutment at a location spaced from the corresponding edge abutments 244a, b and 240a, b.
  • the core components 232a-232r are shown spaced by slots 252a-252r, only certain of which are pictured. Such slots are of a widthwise extent equal to corresponding slots 246a-246r of member 231 as discussed above. Thus, the arcuate segment structuring represented in Fig. 11 is further defined.
  • Fig. 12D shows the next inwardly disposed metal sheet member 233 is comprised of a core base 254 from which are provided upstanding integrally formed core elements 233a-233r. As before, only certain of these elements are shown in view of the larger number of core elements at hand.
  • Core elements 233a-233r are provided having a widthwise extent slightly less than those shown at 232a-232r.
  • Half element components 233r and 233r' are shown having upstanding outer edges 256a- 256b which are brought together in abutting adjacency to form the next inwardly disposed core ring and are located away from the abutting edges of the other components 230-232.
  • the spacing between upstanding core elements 233a-233r is such as to define slots 258a-258r having a widthwise dimension equal to the corresponding widthwise dimensions of slots 252a-252r of member 232 as discussed above.
  • the above sequence of sheet metal members continues through the 8 iterations required for a 8-piece laminar core structure.
  • the above-discussed brushless PM d.c. motor architecture is one achieving desirable cost attributes for larger diameter devices. As the motors become smaller, for example, at diameters of 2 inches and below, then their topology may change while maintaining the important cost considerations permitting their use in the consumer oriented fields. Referring to Fig. 13, a smaller motor is shown in perspective fashion in general at 270.
  • the base or support structure 272 of motor 270 is configured about a motor axis 274. Projecting outwardly from the base 272 is a motor shaft 276. A cylindrical side or housing 278 extends from the base 272 to a cylindrically-shaped polymeric cap 280 to complete the assembly. It may be noted that no exposed rotating rotor is in evidence at motor 270 as compared with motor 90. Looking to Figs. 14 and 15, motor 270 is seen to have a stator assembly represented generally at 282 which provides nine upstanding stator components 284a-284i.
  • Components 284a-284i are formed having laminar core components shown, respectively, at 286a, 286i, which are bent upwardly from a diameter base portion 288 further including a centrally disposed opening 290 which is centered about axis 274 and supported upon base 272.
  • a plurality, for example seven laminations are combined to form the core components 286a-i, and associated base 288.
  • one of the seven lamination blanks making up the core structure is revealed showing the circular opening 290, the periphery of the ring-shaped base 292, and the legs 294a-294i, for this laminar sheet prior to their being bent perpendicularly upwardly from the periphery 292.
  • Fig. 14 Seven of the lamination blanks, which are formed of a magnetically permeable material, typically covered with an insulative coating, are placed in a forming tool to achieve the structure required. Following such forming, the laminar sheets are assembled together to requisite dimensions and tolerances. It may be observed in Fig. 14 that variations in the length of the legs as at 294a-294i, need not be provided. In this regard, the core component 286c is seen to have a "stairstep" form at its tip. This serves to lower manufacturing costs. Fig. 16 additionally shows the presence of three holes 296-298. These holes are aligned upon the formation of the core structure and are used in conjunction with bolts or rivets to attach the structure to the base 272. Three such bolts are shown in Fig.
  • a bearing support represented generally at 308 is seen to be connected to base 272.
  • the support 308 includes a downwardly depending first cylindrical portion 310 which nests within a corresponding opening 312 formed within base 272.
  • a second cylindrical portion 314 of support 308 extends through the opening 316 of the assembled core components, and is retained against the bottom thereof as a sub- assembly by bent-up circular engaging tab 318.
  • the upward portion of bearing support 308 is formed as a flange 320 having an annular receiving opening 322 which supports a bearing 324.
  • Bearing 324 supports shaft 276 and is retained in position by adhesive attachment to the bearing support 308.
  • a retainer ring 326 and spacer 328 locate the rotor shaft assembly between bearings 324 and 330.
  • shaft 276 is supported by a bearing 330 positioned within a bearing receiving opening 332 formed within polymeric cap 280.
  • Bearing 330 is retained in position by adhesive attachment to cap 280.
  • Spacers 336 are positioned intermediate the bearing 330 and rotor 334.
  • Rotor 334 is formed having a central portion of steel as at 338 which serves as the back iron for a ring-shaped permanent magnet component 340.
  • Magnet 340 is formed, as before, of a relatively inexpensive and lower energy plastic bonded rare earth magnet material of, for example, about 10,000,000 Gauss Oersteds. Such a material typically is provided, for example as a neodymium iron boron material.
  • the magnet preferably is magnetized in six equal sectors with alternating polarities.
  • the outwardly disposed flux interaction surface of magnet 340 confronts the upwardly extending flux interaction surface of the pole piece regions of core components 286a-286i, two such flux interaction regions being seen in Fig. 14 at 342c and 342h.
  • stator pole pieces define a working air gap 344 with the outer flux interaction surface of magnet 340.
  • the mid-point of this gap 344 is seen to be at a radius, RG, from axis 274, while the corresponding outermost radius of motor 270 is shown at radius, RM- AS before, the field winding and bobbin assemblies extend upwardly along each core component a distance or stator winding height of about twice the corresponding pole height distance established at working air gap 344.
  • the polymeric, electrically insulative bobbins upon which the field windings are wound each incorporate a thickened region as seen, for example, at 346c and 346h, which provides a starting and ending for the winding procedure through the utilization of slots (not shown).
  • the sequence of components commencing with shaft 274 include, in order, rotor back iron; rotor magnet; working air gap; the stator pole piece flux interaction surface of the pole piece region; the pole piece, and the polymeric cap.
  • the motor 270 exhibits an unusually high torque output notwithstanding the internal disposition of the radial gap 344.
  • motor 270 maintains a relatively high value for the ratio, RG/RM, for example having values of about 0.7 and above. Additionally, the design permits the development of a relatively small working gap 344 to provide a ratio, Lm/Lg, of value greater than about 3 with allowances made for flux leakage.
  • the motor 270 is particularly characterized in providing a working gap which is considered radial in that the sectors of ring magnet 344 are magnetized in the radial sense of the motor. However, the gap is disposed inwardly of the flux interaction surface of the core components. This facilitates the positioning of Hall effect position sensors. In this regard, the sensors may be positioned between the stator pole components to respond to the passage of the poles of the permanent magnet ring 340. Such sensors may be supported from the polymeric cap 280 and are seen in Fig. 14 as well as in Fig. 15 at 348-350.
  • a partial sectional view of a variation of motor 90 described above in connection with Figs. 4-8 is represented in general at 360.
  • the motor variation 360 includes a base member 362 having an annular slot 364 within which is supportably inserted the multiple laminate ring type core assembly described in connection with Figs. 11 and 12, and represented here generally at 366.
  • a bobbin and field winding assembly as represented generally at 368 is positioned over the lower approximate two thirds of the upstanding core components.
  • the pole piece region 370 provides two, oppositely disposed, flux interaction surfaces 372 and 374.
  • Rotor 380 may, for example, be formed of steel so as to provide necessary back iron to the ring magnets 376 and 378. Alternately, separate steel rings can be carried by the rotor 380 behind each of the permanent magnet assemblies 376 and 378.
  • the magnetic sectors in permanent magnets 376 and 378 are magnetized or formed in a polar sense which is radial with respect to the axis of the motor 360.
  • rotor 380 not only includes an outer supporting flange 386 similar to that shown at 104 in the case of motor 90, but also includes an inner supporting flange 388 depending downwardly from the interior surface of rotor 380.
  • the two magnet ring, double radial gap, design has other salient advantages besides significantly increasing torque generating capability with only a minor increase in the motor dimensions.
  • One of those advantages relates to the forces that are present in the working gap of an energized pole in a motor.
  • All motor designs generate force vectors in the working gap of the motor as a result of energized fields or a combination of energized and permanent magnet stored fields.
  • the force vectors are three dimensional and can be represented by a rotating vector centered in the working gap of an energized pole of a motor.
  • One component of the force vector is torque, and by use of sequential switching of the energized field elements, that component is controlled as the major component of the force vector.
  • the other two components are an unbalance force acting to pull the rotor in a radial direction (inward or outward) and an axial component pulling the rotor in one direction or the other along its axis.
  • This third component can be minimized by careful placement of the rotor within the stator's unwanted force vector. All standard motors normally cancel that component by providing a series of energized pole fields around the motor in sequential uniformly dispersed locations such that when summing all the energized poles, the torque vectors add and the element motor that would mean the phases are wound A, B, C, A, B, C, A, B, C in a progression around the motor such as that described in Fig. 3. Since the motor of the instant invention has the provision for two working gaps at each stator pole, the use of a double radial magnet design produces two force vectors, one at each working gap, at each energized pole.
  • Another feature of the two magnet ring, double radial magnet design lies in the ability to place the pole components of one magnet ring slightly out of angular alignment with the corresponding pole components of the magnet ring located on the opposite side of the stator pole piece area. This feature is used to reduce or eliminate the traditional detent or cogging torque present in single annular working gap designs used in most all traditional brush and brushless motors and in single annular working gap designs of the present invention.
  • the rotor has preferred circumferential rest positions when the motor is not energized which result from preferred magnetic alignment of the permanent magnet poles to the ferromagnetic pole components. Therefore, there is a force or torque required to rotate the shaft of a de-energized motor.
  • That torque is defined as the detent or cogging torque and if measured versus angular rotation, would inscribe a nearly sinusoidal torque waveform with both positive and negative torque values which could be described as clockwise and counterclockwise torque values.
  • the average value is zero which occurs at the rest positions and at positions intermediate the rest positions.
  • detent torque is added to or subtracted from the energized torque values which likely will create higher energized torque ripple, that is the peak value of torque to the minimum value, which usually occurs at the point of commutation.
  • the magnitude of torque ripple can be detrimental to motor performance in many applications, especially at low load values and low speeds.
  • the motor could be considered to be two motors in one and by using that criteria, the detent torque characteristic of each motor element, meaning the motor characteristic due to each radial gap, can be analyzed individually, although there is interaction between the two magnet rings. Normally each magnet ring would be aligned angularly with the north magnetized pole element of the other magnet ring and conversely the south magnetized pole element of one ring would face the south magnetized pole element of the other ring.
  • the detent torque characteristic curve values of one more element would be in angular phase with the detent torque characteristic curve values of the other motor element, meaning due to the inner of the two radial gaps, and therefore, the torque values would directly add giving a combined motor with approximately twice the magnitude of detent torque as was present in each of the individual detent torque characteristic curves due to each of the two radial air gaps. The same would be true of the energized torque characteristic curves due to each radial gap.
  • the two magnet rings are trying to knock each other down or demagnetize each other and, therefore, the combined magnet load line will be slightly lower than what would be the magnet operating load line of each magnet ring individually. This means the resultant detent an energized torque values will not be exactly twice what the values would be if each motor were measured alone, meaning with only the inside or outside permanent magnet ring present. If the inner permanent magnet ring was angularly misaligned from the outer permanent magnet ring by an amount that would create a 180 degree phase shift in the detent torque characteristic curve from one motor element to the other, then the sum of the two curves would approximate zero.
  • the motor would have 24 cycles of detent torque in one revolution and four cycles of energized torque in one revolution. Since there are six cycles of detent torque for one cycle of energized torque, the amount of offset that would be necessary to almost eliminate detent torque would be small, in this case only a 7.5 degree angular shift. The effect on the energized torque would only be to reduce it by about 4% and with almost a 100% reduction in detent torque, the result can be a motor characteristic that is very advantageous for many applications.
  • a rotor/stator pair combination which would give this characteristic is an eight pole element rotor with a nine pole component stator.
  • This also results in a decrease in the value of energized torque and because the distribution of individual phase stator pole components is not uniformly dispersed around the motor the unbalance force vector component defined earlier is not cancelled when summed around the motor as would be with conventional rotor/stator pole element pairs.
  • this three-phase nine stator pole element motor that would mean the phases are would A, A, A, B, B, B, C, C, C in a progression around the motor which will not result in the desired cancellation of the radial unbalance force vector components when energizing any two phases.
  • FIG. 20 an alternative embodiment of an inner radial gap motor according to the present invention is shown in cross-section generally at 400.
  • the base or supporting structure 402 of motor 400 is configured about a motor axis 404, with a motor shaft 406 projecting outwardly from base 402.
  • a separate, generally cylindrical side housing 408 is provided to extend from base 402 about a flanged portion, 410, thereof, to a generally annular clamp, 412.
  • clamp 412 is formed of a plastic or other polymeric material or the like.
  • Side housing 408 is received about a corresponding flanged portion, 414, of clamp 412 to form an inherently rigid arrangement with clamp 412 and base 402.
  • stator assembly 420 which includes a centrally disposed opening, represented at 422, is coaxially aligned with shaft 406 about motor axis 404.
  • Stator assembly 420 is supported upon base 402, and may be removably attached thereto with a number of fasteners or the like, one of which is shown at 424.
  • stator assembly 420 is constructed as having a plurality of upstanding stator components, one of which is shown at 426.
  • Each of stator components 426 is formed as having a laminar core component, one of which is shown at 428, which is bent upwardly from a diameter base portion 430.
  • a plurality of, for example, five laminations are combined to form the core components 428 and associated base 430.
  • stator assembly 420 may be provided as having the generally annular configuration described in connection with Figs. 11 and 12.
  • the five lamination blanks making up the core structure of stator assembly 420 are placed in a forming tool to achieve the structure required. Following such forming, the laminar sheets are assembled together to requisite dimensions and tolerances. Again, and as was observed in Fig. 14, variations in the length of the legs forming the core components need not be provided as each such components may be utilized with the "stairstep" profile shown at tip 432 of core component 428.
  • field windings are positioned upon insulated bobbins, 436, which, in turn, are placed over each core component 426, a pole piece region 438 thereof extending to tip 432.
  • a rotor mounted onto an end 439 of shaft 406 is a rotor, shown generally at 440 to include a central portion of steel as at 442 which serves as the back iron for a ring- shaped permanent magnet component 444.
  • Magnet 444 is formed, as before, of a relatively inexpensive and lower energy plastic bonded rare earth magnet material of, for example, about 10,000,000 Gauss Oersteds. Such a material typically may be provided as a neodymium iron boron material.
  • the magnet preferably is magnetized in six equal sectors with alternating polarities.
  • the outwardly disposed flux interaction surface 446 of magnet 444 confronts a corresponding, upwardly extending stator pole flux interaction surface, one such surface being shown at 448 for stator pole piece region 438, to define a generally radial working air gap as is represented at 450.
  • the mid-point of this gap 450 is seen to be at radius RQ from axis 404, while the corresponding outermost radius of motor 400 is shown at radius RM- AS before, the field winding 434 and bobbin 436 assemblies extend upwardly along each core component 428 at a distance or stator winding height of about twice the corresponding height of pole piece region 438 established at working air gap 450.
  • base 402 may be integrally-formed with an upstanding, generally annular region, 452, which is received by opening 422 of stator base 430.
  • Annular region 452 extends coaxially with motor axis 406 toward rotor 440 to define a generally cylindrical cavity, represented at 454, receiving shaft 404 and its associated bearings, 456a and 456b, which may be of a sleeve-type. Annular region 452 additionally defines at its terminal end an upstanding shoulder portion, 458, which is spaced-apart from rotor 440. Shoulder portion 458 is configured to receive a generally annular stator support, 460, which extends radially outwardly therefrom to an abutting adjacency with each of stator core components 428 generally at pole pieces 438 thereof.
  • Motor 400 also includes a circuit board, 470, which is mounted to base 402 via clamp 412 and a number of fasteners, one of which is shown at 472.
  • Circuit board 470 defines with base 402 and side housing 408 an internal chamber, shown at 474, receiving stator assembly 420 and rotor 440.
  • the location of circuit board 470 in the arrangement shown covers the rotating rotor 440 such that no portion thereof is exposed, and facilitates the disposition in adjacency with rotor 440 of any number of board-mounted sensors, one of which is shown at 476.
  • Sensor 476 may be provided as a Hall-effect type to be magnetically responsive to the rotation of rotor 440 and magnet 444 to provide output signals corresponding to the instantaneous rotational position of rotor 440. Also, as was previously demonstrated, with motor 270 of Fig. 14, it is apparent that the Hall effect sensor location in motor 270 is consistent with a board-mounted sensor for motor 400. These output signals may be supplied to associated control circuitry (not shown) additionally carried in an integrated fashion by board 470 for effecting the selective excitation of stator windings 434 in correspondence therewith.
  • sensors 476 may be provided as of a type which is optically responsive to a reflective indexing indicia, 478, disposed on rotor 440 at a spaced-apart distance from motor axis 404.
  • motor 400 With the geometry of motor 400 as thus described, it may be observed that the sequence of components commencing with shaft 406 include, in order: rotor back iron 442; rotor magnet 444; magnet flux interaction surface 446 thereof; working air gap 450; pole piece flux interaction surface 448; pole piece 438; and clamp 412.
  • motor 400 has been observed to exhibit an unusually high torque output notwithstanding the internal, radial disposition of work air gap 450. That is, motor 400 nevertheless maintains a relatively high value of, for example, at least about 0.7 for the ratio RG/RM-
  • the described design additionally leads to the development of a relatively small working gap 450 providing a ratio L m /Lg of value greater than about 3 with allowances made for flux leakage.
  • a motor structured according to the invention is revealed.
  • This motor is of a "larger" variety, typically being implemented, for example, with a topology creating a diameter of between about 4 and 5 inches, and a thickness of between 1 and 2 inches.
  • the principal components of base and rotor preferably are injection molded or die cast to reduce costs, such molding being carried out with materials such as a rigid plastic or aluminum. Where plastic materials are employed, such materials should be structurally rigid.
  • a thermoplastic polyester resin marketed under the trademark RYNITE by DuPont de Nemours Corporation may be employed. This resin is available in unreinforced and reinforced versions, the latter containing uniformly dispersed short glass fibers.
  • Fig. 21 shows the motor 500 in general as including a base 502 having heat dissipating fins, certain of which are identified at 504.
  • Fig. 22 also shows that these fins are integrally molded with and extend outwardly from an outer integral wall
  • FIG. 22 also shows that the inner wall 512 is integrally formed in conjunction with the base portion 506 and emanates from an inner reinforcing ring represented generally at 527.
  • the wall 505 at mounting portion 508 forms the outward component of mounting cavity 510 with wall 512 forming the inner component, these components being seen more clearly in Fig. 22.
  • Cavity 510 extends in a circular locus positioned radially outwardly from the motor axis 514 (Fig. 22) and is configured having an upstanding annular mounting ridge 516 which receives a circular stator assembly represented generally at 518.
  • Stator assembly 518 is configured in the manner described in connection with Figs.
  • Ribs as 524 extend from inner wall 512 to a bearing support region 526 within which bearings 528 and 530 are mounted to support rotating shaft or axle 532. It may be observed in Fig. 21 that the rib structures 524 also define a sequence of open cavities, two of which are seen at 534 which extend to the bottom portion 506. Wth the present embodiment, 27 upstanding, spaced apart core components, some of which are represented generally at 536 are provided. The 27 core components of the instant embodiment are arranged in conjunction with the noted circular locus of mounting cavity 510. As before, each has a winding association region as seen in Fig.
  • Each core component 536 also, as before, includes a bobbin, one of which is identified at 544 in Fig. 22. These bobbins as at 544 may be formed of the earlier-described thermoplastic polyester resin. The bobbins 544 are wound with a field winding as seen in Fig. 22 at 546. Of particular note in connection with the present embodiment, the core components and stator windings with bobbins are stabilized with an electrically insulative, thermally conductive potting material seen in Fig.
  • This potting material may be provided, for example, as a low viscosity, two-component epoxy potting and encapsulating system marketed under the trade designation "EPOCAP 19284" by Harcros Chemicals, Inc. of Belleville, New Jersey 07109.
  • EPOCAP 19284" a low viscosity, two-component epoxy potting and encapsulating system marketed under the trade designation "EPOCAP 19284" by Harcros Chemicals, Inc. of Belleville, New Jersey 07109.
  • the rotor of motor 500 as represented generally at 600 is of generally thin, cylindrical configuration, as before, being formed preferably via molding techniques.
  • Rotor 600 is mounted upon axle 532 for rotation about axis 514, such mounting including a spacer present as a wavy washer 602 as seen in Fig. 22 and an upper mounting region 604.
  • the rotor is formed incorporating stiffening or reinforcing ribs, certain of which are revealed at 610 in Fig. 21. That figure also shows that the ribs extend to a ring-shaped peripheral support region represented at 612. This region 612 extends to an outer cylindrical magnet support portion represented generally at 614 which includes an outwardly-disposed cylindrically shaped surface 616.
  • the outward surface of back iron 618 functions to support a permanent magnet assembly incorporating alternating polarity segments as represented at 620.
  • the outwardly disposed cylindrical face 622 of permanent magnet structure or assembly 620 provides a flux interaction surface generally parallel with the motor axis 514 which is coextensive and in adjacency with the corresponding flux interaction surface of the stator assembly to define a gap as seen at 630 in Fig. 22.
  • Such acoustic noise diminution is developed with the instant embodiment by an arrangement isolating the axial strain imposed upon rotor 600 by axially directed magnetic force vectors to a region adjacent the mounting portion 614.
  • the rotor magnet support portion 614 is configured to exhibit a stiffness to forces imposed radially with respect to axis 514 and a flexibility to those lesser vector forces which may be generated vertically or in parallel relationship with axis 514. This restricts noise inducing vibrations to the very outward portion of the rotor 600. In effect, the rotor flexes at its tip very slightly with the imposition of vertical force magnetically induced vectors.
  • the rotor magnet support portion 614 is configured having an annular cavity seen in Fig. 22 at 640.
  • This cavity 640 extends to an annular bridge portion 642 having a thickness which permits a very slight flexure along directions parallel to axis 514 but exhibiting high stiffness radially from that axis.
  • the tendency for the outer wall 644 of cavity 640 to bend inwardly or outwardly is offset by the rigid support to its outer surface supplied by the ring-shaped back iron 618 which is a continuous component.
  • Fig. 21 further reveals that the annular bridge 642 at outer portion 650 of rotor 600 is formed having a sequence of openings as at 652 which extend along a generally circular locus and between which are located radiation reflection surfaces, certain of which are represented at 654. These openings 652 and intermediately disposed reflective surfaces 654 function as part of an arrangement developing rotor position signals for carrying out appropriately synchronized commutation.
  • the motor 500 is enclosed at its top portion by a top support which, advantageously, may serve as a printed circuit support for motor control purposes.
  • the arrangement of this embodiment incorporates reflective switches or optical sensors (such as in motor 400 at 476 and shown here) as at 662-664 which are located over the locus of opening 652 and reflective surfaces 654.
  • the reflective switches may be provided, for example, as a type MTRS9080 infrared LED and phototransistor marketed by Marktech, Inc. of Menand, New York 12204.
  • All motors of the current featured invention can have their torque generating capabilities increased by increasing the surface area of the pole piece region that confronts the permanent magnet pole elements of the rotor permanent magnet assembly. For a given number of stator pole components, this would normally be accomplished by making the stator pole piece component as angularly wide as possible to confront as much of the rotor magnet pole elements as possible and still leave room for the field winding supported on a bobbin to be inserted over each stator pole core component and not interfere with the adjacent field winding. Further increases in stator pole surface area would then normally be accomplished by increasing the height of the pole piece region along with a corresponding increase in the height of the rotor permanent magnet pole elements.
  • Another method to gain stator pole piece region surface area without increasing the height of the pole piece region and therefore increase the torque generating capabilities of the motor without increasing overall package size is to extend the angular width of the stator pole piece region without a corresponding increase in the angular width in the winding association region.
  • This flared pole piece region gives greater stator pole piece area and increased interaction with the rotor permanent magnet pole elements and also reduces the gap between adjacent stator poles which further enhances the energized field flux flow in the desired area between adjacent stator poles.
  • the result is enhanced torque production capability with the same number of stator pole elements and without increasing the overall height of the motor or increasing the height of the rotor permanent magnet pole elements.

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  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Iron Core Of Rotating Electric Machines (AREA)
  • Permanent Field Magnets Of Synchronous Machinery (AREA)
  • Permanent Magnet Type Synchronous Machine (AREA)
  • Brushless Motors (AREA)
PCT/US1999/003808 1999-02-22 1999-02-22 Permanent magnet d.c. motor having a radially-disposed working flux gap WO2000051224A1 (en)

Priority Applications (3)

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CA002362686A CA2362686A1 (en) 1999-02-22 1999-02-22 Permanent magnet d.c. motor having a radially-disposed working flux gap
PCT/US1999/003808 WO2000051224A1 (en) 1999-02-22 1999-02-22 Permanent magnet d.c. motor having a radially-disposed working flux gap
EP99973722A EP1153472A4 (de) 1999-02-22 1999-02-22 Davermagnet-gleichstrommotor mit radialem luftspalt.

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EP1547229A2 (de) * 2002-07-02 2005-06-29 Petersen Technology Corporation Pm-motor und generator mit aus druckgeformten verarbeiteten ferromagnetischen partikeln gebildeter vertikal-statorkernbaugruppe
DE102005011196A1 (de) * 2005-03-09 2006-09-14 Robert Bosch Gmbh Sensoranordnung zur Erfassung eines Differenzwinkels
DE102019216803A1 (de) * 2019-10-30 2021-05-06 Robert Bosch Gmbh Elektromotor für einen Getriebeaktuator

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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1547229A2 (de) * 2002-07-02 2005-06-29 Petersen Technology Corporation Pm-motor und generator mit aus druckgeformten verarbeiteten ferromagnetischen partikeln gebildeter vertikal-statorkernbaugruppe
EP1547229A4 (de) * 2002-07-02 2006-04-12 Petersen Technology Corp Pm-motor und generator mit aus druckgeformten verarbeiteten ferromagnetischen partikeln gebildeter vertikal-statorkernbaugruppe
DE102005011196A1 (de) * 2005-03-09 2006-09-14 Robert Bosch Gmbh Sensoranordnung zur Erfassung eines Differenzwinkels
DE102005011196B4 (de) 2005-03-09 2024-05-08 Robert Bosch Gmbh Sensoranordnung zur Erfassung eines Differenzwinkels
DE102019216803A1 (de) * 2019-10-30 2021-05-06 Robert Bosch Gmbh Elektromotor für einen Getriebeaktuator

Also Published As

Publication number Publication date
EP1153472A4 (de) 2002-11-27
CA2362686A1 (en) 2000-08-31
EP1153472A1 (de) 2001-11-14

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