Abstract:
Method and apparatus for forming an electrodynamic device such as a motor or generator. The device is formed with an encapsulation structure which is developed by insert molding. A rigid pressed powder stator core and stator backiron subassembly with associated stator core windings is formed. This subassembly is the insert for an insert molding procedure developing an encapsulation structure which mechanically supports the stator structure; provides mechanical support and improved heat dissipation and incorporates integrally formed bearing mounts. With the procedure, substantially lower device costs are realized.

Description:
CROSS-REFERENCE TO RELATED APPLICATIONS 
     STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH 
     Not applicable. 
     BACKGROUND OF THE INVENTION 
     Investigators in the electric motor arts have been called upon to significantly expand motor technology from its somewhat static status of many decades. Improved motor performance particularly has been called for in such technical venues as computer design and secondary motorized systems carried by vehicles, for example, in the automotive and aircraft fields. With progress in these fields, classically designed electric motors, for example, utilizing brush-based commutation, have been found to be unacceptable or, at best, marginal performers. 
     From the time of its early formation, the computer industry has employed brushless d.c. motors for its magnetic memory systems. The electric motors initially utilized for these drives were relatively expensive and incorporated a variety of refinements particularly necessitated with the introduction of rotating disc memory. Over the recent past, the computer industry has called for very low profile motors capable of performing in conjunction with very small disc systems and at substantially elevated speeds. 
     Petersen, in U.S. Pat. No. 4,745,345, entitled “D.C. Motor with Axially Disposed Working Flux Gap”, issued May 17, 1988, describes a PM d.c. motor of a brushless variety employing a rotor-stator pole architecture wherein the working flux gap is disposed “axially” with the transfer of flux being in parallel with the axis of rotation of the motor. This “axial” architecture further employs the use of field windings which are simply structured, being supported from stator pole core members, which, in turn, are mounted upon a magnetically permeable base. The windings positioned over the stator pole core members advantageously may be developed upon simple bobbins insertable over the upstanding pole core members. Such axial type motors have exhibited excellent dynamic performance and, ideally, may be designed to assume very small and desirably variable configurations. 
     Petersen in U.S. Pat. No. 4,949,000, entitled “D.C. Motor”, issued Aug. 14, 1990 describes a d.c. motor for computer applications with an axial magnetic architecture wherein the axial forces which are induced by the permanent magnet based rotor are substantially eliminated through the employment of axially polarized rotor magnets in a shear form of flux transfer relationship with the steel core components of the stator poles. The dynamic tangentially directed vector force output (torque) of the resultant motor is highly regular or smooth lending such motor designs to numerous high level technological applications such as computer disc drives which require both design flexibility, volumetric efficiency, low audible noise, and a very smooth torque output. 
     Petersen et al, in U.S. Pat. No. 4,837,474 entitled “D.C. Motor”, issued Jun. 6, 1989, describes a brushless PM d.c. motor in which the permanent magnets thereof are provided as arcuate rings which rotate about a circular locus of core component defining pole assemblies. The paired permanent magnet rings are magnetized in a radial polar sense and interact without back iron in radial fashion with three core components of each pole assembly which include a centrally disposed core component extending within a channel between the magnet pairs and to adjacently inwardly and outwardly disposed core components also interacting with the permanent magnet radially disposed surface. With the arrangement, localized rotor balancing is achieved and, additionally, discrete or localized magnetic circuits are developed with respect to the association of each permanent magnet pair with the pole assembly. 
     Petersen in U.S. Pat. No. 5,659,217, issued Aug. 19, 1997 and entitled “Permanent Magnet D.C. Motor Having Radially-Disposed Working Flux-Gap” describes a PM d.c. brushless motor which is producible at practical cost levels commensurate with the incorporation of the motors into products intended for the consumer marketplace. These motors exhibit a highly desirable heat dissipation characteristic and provide improved torque output in consequence of a relatively high ratio of the radius from the motor axis to its working gap with respect to the corresponding radius to the motors&#39; outer periphery. The torque performance is achieved with the design even though lower cost or, lower energy product permanent magnets may be employed with the motors. See also: Petersen, U.S. Pat. No. 5,874,796, issued Feb. 23, 1999. 
     Over the years of development of what may be referred to as the Petersen motor technology, greatly improved motor design flexibility has been realized. Designers of a broad variety of motor driven products including household implements and appliances, tools, pumps, fans and the like as well as more complex systems such as disc drives now are afforded an expanded configuration flexibility utilizing the new brushless motor systems. No longer are such designers limited to the essentially “off-the-shelf” motor varieties as listed in the catalogues of motor manufacturers. Now, motor designs may become integral components of and compliment the product itself in an expanded system design approach. 
     During the recent past, considerable interest has been manifested by motor designers in the utilization of magnetically “soft” processed ferromagnetic particles in conjunction with pressed powder technology as a substitute for the conventional laminar steel core components of motors. So structured, when utilized as a motor stator core component, the product can exhibit very low eddy current loss which represents a highly desirable feature, particularly as higher motor speeds and resultant core switching speeds are called for. As a further advantage, for example, in the control of cost, the pressed powder assemblies may be net shaped wherein many intermediate manufacturing steps and quality considerations are avoided. Also, tooling costs associated with this pressed powder fabrication are substantially lower as compared with the corresponding tooling required for typical laminated steel fabrication. The desirable net shaping pressing approach provides a resultant structurally rigid magnetic particle structure that is 3-dimensional magnetically (isotropic) and avoids the difficulties encountered in the somewhat two-dimensional magnetic structure world of laminations. See generally U.S. Pat. No. 5,874,796 (supra) and U.S. Pat. No. 6,441,530. 
     The above-discussed PM D.C. motors achieve their quite efficient and desirable performance in conjunction with a multiphase-based rotational control. This term “multiphase” is intended to mean at least a three step commutation sequence in conjunction with either a unipolar or bipolar stator coil excitation. Identification of these phases in conjunction with rotor position to derive a necessary controlling sequence of phase transitions traditionally has been carried out with two or more rotor position sensors. By contrast, simple, time domain-based multiphase switching has been considered to be unreliable and impractical since the rotation of the rotor varies in terms of speed under load as well as in consequence of a variety of environmental conditions. 
     The multiphase motors may be described, for instance, by arbitrarily designating the commutation phase sequence of a three-phase motor as: A, B, and C. During those phases, a three-phase unipolar motor control must determine rotor position information for establishing the transitions from phase A to phase B to phase C to phase A as the sequence continues. Such control has been considered to require three rotor position sensors. The most typical of the position sensors are Hall devices and optical sensors. Somewhat costlier control also can be achieved with a back EMF circuit monitoring approach which eliminates all physical position sensors. 
     Still higher efficiencies are achieved with a three-phase bipolar motor wherein such commutation phase sequencing arbitrarily may be designated as calling for transitions from phase AB to phase AC, to phase BC to phase BA, to phase CA, to phase CB, to phase AB as the sequence continues. Here again, a practical control for such motor architecture has been considered to require three rotor position sensors. Four-phase motors with an arbitrarily designated commutation sequence of A, B, C and D are considered to require two rotor position sensors. 
     While the stator architecture and pressed powder implementation of the above-discussed motors has not only substantially enhanced their practically and has lowered their structural cost, further, quite substantial cost improvements can be realized by limiting the number of bi-state rotor position sensors required for multiphase motors to only one such sensor. In this regard, currently, the multiple sensors must be positioned in substantially spaced apart locations with respect to the rotor or some slave form of sensing structuring. Thus, the significant cost advantages associated with the integration of the positional sensor and the control circuit in a single chip is lost. The resultant cost factor generally precludes the use of efficient multiphase motors with very low cost applications such as electrical circuit cooling fans. However, as the era of electronic-based systems expands, battery-based power limitations are setting the stage for much higher motor efficiency requirements. Those higher efficiencies only are available with multiphase motors. Higher efficiencies for fan motors may be required, for example, for utilization with a rapidly expanding development of laptop computers. The technology long associated with electronic circuit, low load cooling fans has been somewhat static. Usually implemented as D.C. PM devices, the motors have been structured with a single phase or “two-pulse” architecture in order to retain a capability for operation with a single sensor. Such phasing is highly inefficient, the motors necessarily experiencing zero torque based commutation switching. 
     In co-pending application for United States patent, Ser. No. 10/706,412 entitled “Multiphase Motors With Single Point Sensing Based Commutation” by Peterson, filed Nov. 12, 2003, a simplified control for multiphase electrically commutated motors is described. The control approach utilizes a single sensor in association with a sensible system to establish reliable phase commutation sequencing. An important result is a significant lowering of the cost of the commutation function of the motors. 
     Still other motor and generator (collectively referred to as electrodynamic devices) cost considerations are associated with the housings carrying electrical and mechanical components of these devices. These costs are concerned with the precise centering of bearings with respect to stator components. For instance, for some devices, the base metal plates supporting the motor or generator components can represent a predominating cost component of the completed device. Further, where adjunct modalities such as gear trains and the like are incorporated with or within the motors, their assembly in conjunction with motor construction has been observed to dramatically increase overall costs. 
     BRIEF SUMMARY OF THE INVENTION 
     The present invention is addressed to electrodynamic apparatus and method of their assembly wherein a completed stator subassembly is employed as the insert in an insert molding-based assembly procedure. With this subassembly approach, a plastic encapsulation structure is developed which provides a mechanically strengthened device, while the procedures for necessary alignment of components is both simplified and improved. The stator subassembly is formed utilizing stator core members and an associated stator backiron which are integrally formed of magnetically soft pressure shaped processed ferromagnetic particles which are generally mutually insulatively associated. Over these stator cores there are positioned bobbin wound stator core windings. These windings may be interconnected in the desired winding scheme with their exit leads or lead extensions (termini) emerging from the encapsulation structure following insert molding, or as shown in the embodiment drawings, each core winding may have it&#39;s start and finish leads (exit leads) or extensions which are supported by the bobbins emerge from the encapsulation following insert molding. The thermoplastic encapsulation structure completely surrounds these stator coils and extends radially outwardly from and within the interstices between all of the stator core components. Thus, the plastic itself enhances the dissipation of heat necessarily generated in the stator coil assemblies. Encapsulation further may additionally form the case of the motor or generator. That case, in and of itself may form the outer wall of a utilitarian device such as a power tool or the like. A particular advantage of the encapsulation approach resides in the utilization of pressed powder stator core members and backiron components in a “vertical” format. Because of their cylindrical structural form the insert molding process can create a feature such as gear teeth within the core structure itself yielding a very compact and much lower cost assembly than would otherwise be available with conventional assembly. 
     Looking at the encapsulation arrangement, bearing mounts are integrally molded with the encapsulation structure and thus, metal bearings may be press fitted within these plastic motor mounts simplifying the assembly process over mounting such devices within metal base or housing components and then assembling those components and the stator component. In the latter regard, metal base components may be eliminated to, in effect, remove what is considered one of the more expensive components of the electrodynamic devices. 
     In one embodiment, the plastic encapsulation structure also forms the ring gear of a planetary gear head. In this regard, the ring gear is automatically centered with respect to the bearings and the sun gear since the bearing mounts which center the bearings and the sun gear are integral to the molding tool. The result of the above features is an electrodynamic device such as a motor or generator which exhibits improved quality and importantly lower cost. 
     Other objects of the invention will, in part, be obvious and will, in part, appear here and after. The invention, accordingly, comprises the method and apparatus possessing the construction, combination of elements, arrangement of parts, and steps which are exemplified in the following detailed description. 
     For a fuller understanding of the nature and objects of the invention, reference should be made to the following detailed description taken in conjunction with the accompanying drawings. 
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS 
     FIG. 1 is a perspective view of a motor embodiment of the invention; 
     FIG. 2 is a sectional view taken through the plane  2 — 2  shown in FIG. 1; 
     FIG. 3 is a perspective view of a mold insert subassembly for fabricating the motor of FIG. 1; 
     FIG. 4 is a sectional view of an encapsulated stator structure; 
     FIG. 5 is a sectional view taken through the plane  5 — 5  shown in FIG. 2; 
     FIG. 6 is a bottom view of the structure of FIG. 4; 
     FIG. 7 is a top view of the structure of FIG. 4; 
     FIG. 8 is a sectional view taken through the plane  8 — 8  shown in FIG. 2; 
     FIG. 9 is a top view of the motor shown in FIG. 2; and 
     FIG. 10 is a sectional view similar to FIG. 2 but showing an implementation employing a self-aligning sleeve bearing. 
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     In the discourse to follow, the electrodynamic apparatus according to the invention initially is described as a motor embodiment, whereupon the techniques of its insertion mold based formation are discussed. The resultant product is a motor which is fabricated at significant cost reduction and which enjoys enhanced mechanical strength in consequence of the union of a rigid pressed powdered metal stator with a thermoplastic encapsulation structure. That structure which includes the stator winding assembly, provides improved heat dissipation at the region of the stator windings. 
     Looking to FIG. 1, a d.c. PM motor configured according to the precepts of the invention is represented generally at  10 . Motor  10  is formed with an outer cylindrical case  12  formed in the course of encapsulation or insert molding which will be seen to evolve an encapsulation structure. Adhered to the cylindrical case  12  is a polymeric cap  14  having a bushing form of bearing  16  supported therein which, in turn, supports a motor output shaft  18  here seen to be axially aligned with the axis  20  of the motor  10 . 
     Looking to FIG. 2, the motor  10  is seen in section as being configured with a mold insert or subassembly represented generally at  22 . Looking additionally to FIG. 3, the subassembly  22  includes six spaced apart stator poles or core members identified generally in FIG. 3 at  24   a - 24   f . Stator cores  24   a - 24   f  are formed of a material composed of magnetically soft pressure shaped processed ferromagnetic particles which are generally mutually insulatively associated. These materials such as Somaloy  550  are sometimes referred to as involving soft magnetic composite technology and are marketed, inter alia, by North American Hoganas, Inc., of Hollsopple, Pa. Cores  24   a - 24   f  are formed integrally with a ring-shaped backiron shown at  26 . Slidably positioned over the winding core portions  28   a - 28   f  of respective stator cores  24   a - 24   f  are polymeric, electrically insulative bobbins  30   a - 30   f.    
     Each bobbin  30   a - 30   f  supports a stator coil winding generally adjacent the winding core portions  28   a - 28   f  as revealed respectively at  32   a - 32   f . Above these windings the bobbins are configured with an integrally formed radially outwardly disposed lead supporting shoulder as shown at  34   a - 34   f . Supported axially upwardly from these shoulders  34   a - 34   f  are integrally formed electrically insulative lead shields  36   a - 36   f . Shields  36   a - 36   f  electrically isolate paired start and finish leads represented generally at  38   a - 38   f . Leads  38   a - 38   f  are seen in the subassembly of FIG. 3 as extending axially on the outward side of the stator core members from the lead supporting shoulders  34   a - 34   g  to lead termini represented generally at  42   a - 42   f . As seen in FIG. 2, as the motor  10  is assembled, the lead termini  42   a - 42   f  are bent over to contact a circular control platform  50 . At the platform  50 , the termini  42   a - 42   f  are coupled with a control circuit. While dual leads are shown extending from each coil, these windings may be mutually interconnected such that only two, three or four leads or lead extensions (depending on motor winding scheme) are coupled to the circuit at platform  50 . Additionally shown supported from the underside of platform  50  is a sensing circuit or device  52  employed for multiphase commutation of the motor  10 . Such circuits are described, for example, in the above-identified application for United States patent Ser. No. 10/706,412. 
     FIG. 2 further reveals that motor  10  includes a shaft or drive shaft  54  disposed about axis  20  and supported by ball bearings  56  and  58 . Bearing  56  is pressed upon a shoulder-configured bearing mount  62  and a loading force is applied by a wavy washer  64 . Bearing  58  is positioned against a shoulder-configured bearing mount  66 . The loading and retention of both bearings is completed by the combination of a washer  68  and E-ring  70 . 
     Shaft  54  extends upwardly into a rotor operational region represented generally at  72  and is connected to a rotor represented generally at  74  configured with a rotor backiron  76  and a radial magnet  78  with a sequence of four magnetic regions of alternating polarity. The outwardly disposed surface of rotor magnet  78  is spaced from the radially inwardly facing surfaces of stator core flux interaction regions  40   a - 40   f  to define a working gap  80 . 
     Shaft  54  extends along axis  20  in the opposite direction to a stepped down shaft portion  82  which extends into a gearhead operational region represented generally at  84  which is configured as a gearhead mount within which a planetary gearhead represented generally at  86  is mounted. In this regard, shaft portion  82  is coupled in driving relationship with a sun gear  88 . Looking additionally to FIG. 5, gear  88  is seen to be coupled in driving relationship with three planet gears  90 - 92  which, in turn, are engaged with a ring gear  94 . Planet gears  90 - 92  are mounted upon respective short metal shafts  96 - 98  which, in turn, are mounted within a rotatable platform  100  connected with or formed integrally with output shaft  18 . As noted above, shaft  18  is rotatably mounted within bushing  16  of motor cap  14 . Bushing  16  may be formed, for example of bronze and alternately may be provided as a ball bearing. Typically, the sun gear  88  will be formed of a metal, while the planet and ring gears will be fashioned of a plastic material. Such gearheads may be located within the encircled region of the wound stator assembly as shown in FIG.  2 . 
     An alternate form of a planetary gearhead may also be incorporated. In that form the planet gears are fixed in position riding on fixed shafts that are mounted in the encapsulated structure at the gearhead mount region and the ring gear rotates being coupled directly to the output shaft. Also, it is obvious that multi-stage planetary gearheads may be incorporated within the encapsulation structure. 
     Motor  10  is formed or assembled employing an insert molding technique utilizing insert mold tools which pull apart and join together along the axis  20 . When the mold tools are joined together for molding, a molten thermoplastic material is injected or “shot” into the tool die cavity containing the wound stator assembly to create a plastic encapsulation structure. The insert for this procedure is the subassembly represented generally at  22  in FIG. 3 also possibly along with a removable insert that locates and seals the exit wires. In keeping with conventional insert molding techniques, the insert  22  must be properly radially “located” within the die as well as properly axially “located”. These procedures are facilitated by the utilization of a quite rigid pressed powder stator core and backiron component. While a variety of plastics may be employed for this molding procedure, in general, a member of the nylon family may be employed. The selection of a particular plastic will be determined with regard to whether a gearhead is employed and, in turn, whether a component of the gearhead such as ring gear  94  is to be incorporated with the process. Additionally, the heat dissipation characteristics of the plastic should be considered. In general, nylon is the generic term for any long-chain synthetic polymeric amide which has recurring amide groups as an integral part of the main polymer chain. The material is characterized by high strength, elasticity, and resistance to water and chemicals. Such plastics are marketed, for instance, by DuPont Co., DuPont Engineering Polymers, of Wilmington, Del., 19880-0713. 
     Following curing of the thermoplastic, an encapsulated stator structure will have been formed. Looking to FIG. 4, this encapsulated stator structure is represented generally at  110 . Structure  110 , in addition to incorporating the upstanding stator insert  22  (FIG. 3) will contain the plastic encapsulation structure represented generally at  112 . FIG. 6 is a bottom view of component  110  and looking to FIGS. 4 and 5, it may be observed that structure  112  includes an integrally formed lower ring-shaped portion  114  which surrounds the backiron region  26  of the stator core assembly and further defines generally cylindrically shaped gearhead operational region or gearhead mount  84 . For the instant embodiment, ring gear  94  is integrally formed within plastic lower region  114 . Region  114  extends upwardly to define an annular shoulder  116  which functions to abut against the upwardly depending edge of cap  14 . From lower region  114 , the encapsulation structure extends about the spaced apart bobbins  30   a - 30   f  and their associated coil windings  32   a - 32   f  as well as the spaces between them. This intermediate region is represented at  118  in FIGS. 4 and 7. Note that region  118  extends initially to level  120  (FIG. 4) which is generally coplanar with the radially inwardly depending flanged components  122   a - 122   f  (FIG. 7) of respective bobbins  30   a - 30   f . Region  118  also defines a central opening region represented generally at  124  which is symmetrically disposed about axis  20  and extends to communication with lower gearhead mount region  84 . From level  120  region  118  extends to upper annulus-shaped level  126  where it defines an upper bearing mount represented generally at  128  and configured with an annular bearing support shoulder or ridge  130 . Central opening  124  further is configured to define a lower bearing mount represented generally at  132  and configured with an upwardly disposed annular shaped shoulder or ridge  134  (see additionally FIG.  6 ). FIGS. 4 and 7 further reveal that the encapsulation structure extends outwardly from the stator windings to define case portion  12  as seen additionally in FIGS. 1,  6  and  7 . 
     FIGS. 4 and 8 reveal that the encapsulation structure extends upwardly to define the case  12  radially outwardly from the stator structure. Note in these figures that the start and finish leads  38   a - 38   f  are fully encapsulated radially outwardly from the stator structure. FIG. 8 further reveals that the upwardly disposed core flux interaction regions  40   a - 40   f  are laterally supported by the radially inwardly depending stator core interstitial regions  140   a - 140   f . FIG. 4 illustrates that the encapsulation structure extends as a wall structure or case upwardly above the core interactions portions  40   a - 40   f  to define an annular ledge or control platform support  142 . As described in connection with FIG. 2, the support  142  functions to support control platform  50 . 
     The general procedure for assembling motor  10  commences with the formation of the insert  22  as described in connection with FIG.  3 . Insert  22  is located within an insertion die or tool. Its radial alignment may be referenced, for example, by the radially inwardly depending surfaces of core flux interaction portions  40   a - 40   f . Axial locating may, for example, be carried out with tool mounted pins or the like. The insertion tool provides for shutting off against the radially inwardly facing surfaces of the core flux interaction portions to define the noted rotor operational region. Similarly, the central opening region  124  and gear mount region  84  are shut off as the oppositely disposed tool components are closed. Depending on tool design, an additional removable insert which locates the coil winding termini and shuts off plastic leakage around those exit wires could be included with the stator insert  22 . Plastic then is shot into the die. Upon curing the oppositely disposed tool components are parted and the removable insert, if included, is removed from the top portion of the encapsulated stator. The result is the formation of the encapsulated stator structure represented in general at  110  in FIG.  4 . Bearing  56  is then press fitted into bearing mount  62  and bearing  58  is press fitted into bearing mount  66 . Rotor assembly  74  containing shaft  54  is installed within bearings  56  and  58  and wavy washer  64  is installed as well as washer  68  and E-ring  70 . Sun gear  88  is affixed to stepped down shaft portion  82 . Planet gears  90 - 92  are installed upon the platform  100  incorporating output shaft  18 . Cap  14  then is installed with output shaft  18  extending through bushing or bearing  16 . In general, the cap  14  is adhesively attached to the encapsulation structure. 
     Looking to FIGS. 2 and 9, support platform  50  and its associated circuit with sensor component  52  then is installed. FIG. 9 reveals that the platform is configured having radially outwardly disposed openings or notches  150   a - 150   f  which receive respective start and finish lead termini  42   a - 42   f . Termini  42   a - 42   f  are then electrically coupled to respective flat surface terminals represented generally at  152   a - 152   f.    
     Referring to FIG. 10 a modification of motor  10  is revealed in general at  160 . This modification provides for the implementation of a self-aligning sleeve bearing in support of the drive shaft. Accordingly, where components are common with those identified in FIGS. 1-9 they are again identified with that numeration but in primed form. In this regard, stator backiron  26 ′ is seen extending to upstanding stator cores as at  24   a ′ and  24   d ′ over which bobbins as at  30   a ′ and  30   d ′ are inserted in conjunction with core windings  32   a ′ and  32   d ′. Shaft  54 ′ is seen disposed about axis  20 ′ and is mounted within upwardly disposed ball bearing  56 ′ which is press fit into bearing mount  62 ′. Shaft  54 ′ supports a rotor  74 ′ having a rotor magnet  78 ′, the outward face of which is spaced from the inwardly disposed face of core flux interaction regions, as at  40   a ′ and  40   d ′ to establish a working gap  80 ′. Shaft  54  extends to a necked down portion  82 ′ which, in turn, is engaged with planetary gearhead  86 ′. Control platform  50 ′ extends over the rotor region and carries flat terminals which electrically communicates with start and finish lead termini as at  42   a ′ and  42   d ′. A commutational sensing device  52 ′ is mounted on the underside of platform  50 ′. The plastic encapsulation structure now is represented in general at  162 . While defining the same form of wall structure or case  12 ′ and lower region  114 ′, structure  162  exhibits a modified profile at its central opening region represented generally at  164  which defines a radially inwardly tapering bearing mount surface  166 . Surface  166  has a curvature for supporting a self-aligning sleeve bearing. That self-aligning sleeve bearing is shown at  168  slidably mounted over drive shaft  54 ′. Bearing  168  is permitted to initially slightly rotate to effect its appropriate alignment with shaft  54 ′. 
     In the above-description the term “top” and “bottom” have been utilized, as well as the terms “upper” and “lower”. These terms are arbitrary in the sense that they are utilized in the sense of the orientation of components in the figures. The terms should not be interpreted in a limiting sense. Similarly, the terms “locate”, “shoot” and “shutting off” are terms commonly employed in the insertion molding or encapsulation arts and are not intended to be interpreted in a limiting sense. 
     Since certain changes may be made in the above-described apparatus and method without departing from the scope of the invention herein involved, it is intended that all matter contained in the above-description or shown in the accompanying drawings shall be interpreted as illustrative and not in a limiting sense.