Patent Document

CROSS-REFERENCE TO RELATED APPLICATIONS 
   This application is a divisional of application Ser. No. 10/440,935 filed May 19, 2003, which issued as U.S. Pat. No. 6,848,495 on Feb. 1, 2005. 

   BACKGROUND OF THE INVENTION 
   The present invention relates generally to a method of manufacturing a laminated rotor for a motor. More specifically, the present invention is related to methods of manufacturing a laminated rotor with laminations having a desired rotor bridge thickness prior to the assembly of the laminated rotor core. 
   A squirrel cage rotor for use in an induction motor has a rotor core and a rotor cage that extends through the rotor core and is connected together at each end of the rotor core by end rings. The rotor core is typically made of a magnetic material such as iron or steel and the rotor cage is typically made of an electrically conductive material such as copper, aluminum or an aluminum alloy. The rotor core has a substantially cylindrical shape with a longitudinally extending central bore to receive the shaft of the motor and a plurality of longitudinally extending rotor slots or apertures, which rotor slots may be slightly skewed, to receive corresponding rotor bars of the rotor cage. A laminated rotor core is commonly manufactured or formed by stacking or assembling a plurality of discs or laminations of the magnetic material on top of each other until the desired substantially cylindrical shape is obtained. During the stacking or assembling process, the laminations are also aligned or oriented into their proper position. Alternatively, the rotor core can be manufactured from a single piece of the magnetic material, but this technique is less common. 
   Each lamination in the rotor core is formed or extruded to a pre-selected thickness, shape and configuration. The pre-selected configuration of the laminations includes an aperture for the central bore, a plurality of apertures for the rotor slots positioned equidistantly about the central bore and a predetermined bridge thickness, which bridge thickness is defined as the radial distance between the outer circumference of the lamination and the aperture for the rotor slot. The dimensioning of the bridge thickness is important because the bridge thickness of the rotor is related to the motor&#39;s performance, wherein a thinner bridge thickness provides better performance. The pre-selected configuration of the lamination can also include other features as needed. As the laminations are stacked to form the rotor core, they are aligned and/or oriented into an appropriate position to form substantially continuous apertures in the rotor core and, if necessary, other desired features of the rotor core. 
   Next, the rotor cage is manufactured or formed by positioning or disposing a rotor bar into each of the plurality of rotor slots in the rotor core, which rotor bars extend to at least the ends of the rotor slots, and connecting the adjacent ends of the rotor bars to each other with an end ring. In one technique, the stacked laminations forming the rotor core can be welded together and/or axially compressed to fix their position and can then be placed in a mold. Once in the mold, the rotor bars, and possibly the rings, can then be formed by die casting or injection molding molten aluminum (or other suitable material), under high pressure, directly into the rotor slots and possibly into molds for the end rings. Alternatively, the rotor bars can be placed or positioned in the rotor slots using any suitable technique and can then be connected together by attaching or connecting a ring to each end of the rotor bars using any suitable technique such as brazing. It should be noted that if the end rings are not cast during the casting process, the end rings can be connected or attached using the brazing technique described above. 
   One potential problem with casting the rotor bars into the laminated rotor core is that additional steps have to be taken to prevent the molten casting material, e.g. molten aluminum, from leaking or seeping between the laminations. To prevent the molten casting material from leaking or seeping between the laminations, the laminations are typically formed or extruded with a greater than desired outer diameter or bridge thickness and are welded together or compressed axially as discussed above. When these additional steps are performed, both the inner diameter and outer diameter of the laminated rotor have to be subsequently machined or processed after the casting process to obtain the desired inner diameter, outer diameter and bridge thickness for the laminated rotor. 
   Therefore, what is needed are techniques for manufacturing a laminated rotor with laminations having an outer diameter and/or bridge thickness that restricts the molten material cast into the rotor core from leaking or seeping out between the laminations during the casting process. 
   SUMMARY OF THE INVENTION 
   One embodiment of the present invention is directed to a method of manufacturing a laminated rotor for a motor. The method of manufacturing including the step of providing a plurality of laminations. Each lamination of the plurality of laminations having a plurality of rotor slots and a preselected bridge thickness. The preselected bridge thickness is selected to provide optimal motor performance. Next, the plurality of laminations are assembled into a laminated rotor core and both axial and radial forces are applied to the laminated rotor core to secure the laminated rotor core in a fixed position. Finally, a molten material is introduced into each of the plurality of rotor slots to form a plurality of rotor bars, wherein the axial and radial forces applied to the laminated rotor core prevent the molten material from leaking between assembled laminations. 
   Another embodiment of the present invention is directed to a method of manufacturing a laminated rotor for a motor. The method of manufacturing includes the step of providing a plurality of laminations. Each lamination of the plurality of laminations having a first planar surface, a second planar surface opposite the first planar surface and a bridge thickness providing optimal motor performance. Each lamination of the plurality of laminations including a plurality of rotor slots, a plurality of countersink portions disposed in the first planar surface, and a plurality of collar portions disposed on the second planar surface. Each rotor slot of the plurality of rotor slots has a corresponding countersink portion and a corresponding collar portion. The next step is assembling the plurality of laminations into a laminated rotor core, wherein the plurality of collar portions of one lamination fit in the plurality of countersink portions of an adjacent lamination. A force is applied to the laminated rotor core to secure the laminated rotor core in a fixed position. Finally, a molten material is cast into each of the plurality of rotor slots to form a plurality of rotor bars, wherein the countersink portion and the collar portion of adjacent laminations prevent the molten material from leaking between assembled laminations. 
   A further embodiment of the present invention is directed to a rotor core lamination for a laminated rotor. The lamination includes a substantially cylindrical body having a central axis and an outer circumference. The substantially cylindrical body also has a first planar surface and a second planar surface opposite the first planar surface. The lamination also includes a plurality of apertures disposed between the central axis and the outer circumference of the substantially cylindrical body. The plurality of apertures extend from the first planar surface to the second planar surface. The lamination further includes a plurality of channels disposed in the first planar surface of the substantially cylindrical body and a plurality of collar portions extending away from the second planar surface of the substantially cylindrical body. Each channel of the plurality of channels being disposed adjacent to a corresponding aperture and each collar portion of the plurality of collar portions being disposed adjacent to a corresponding aperture. Finally, each collar portion of the plurality of collar portions is configured and disposed to fit within a corresponding channel of the plurality of channels of another lamination upon assembly of the lamination in the laminated rotor. 
   One advantage of the present invention is that a laminated rotor can be manufactured with laminations having the desired outer diameter and/or bridge thickness without the need for a subsequent machining operation. 
   Another advantage of the present invention is that the rotor manufacturing process is more economical and efficient because expensive and laborious machining processes are eliminated. 
   Other features and advantages of the present invention will be apparent from the following more detailed description of the preferred embodiment, taken in conjunction with the accompanying drawings which illustrate, by way of example, the principles of the invention. 

   
     BRIEF DESCRIPTION OF THE DRAWINGS 
       FIG. 1  illustrates a perspective view of a laminated rotor core for use with the present invention. 
       FIG. 2  illustrates a top view of a lamination from the laminated rotor core of FIG.  1 . 
       FIG. 3  illustrates schematically the force applying members in one embodiment of the present invention. 
       FIG. 4  illustrates schematically the force applying members in another embodiment of the present invention. 
       FIG. 5  illustrates a top view of a lamination in another embodiment of the present invention. 
       FIG. 6  illustrates a cross-sectional view of the lamination of  FIG. 5  taken along line VI—VI in FIG.  5 . 
       FIG. 7  illustrates a cross sectional view of several laminations of  FIGS. 5 and 6  assembled together. 
   

   Wherever possible, the same reference numbers will be used throughout the drawings to refer to the same or like parts. 
   DETAILED DESCRIPTION OF THE INVENTION 
     FIG. 1  illustrates a laminated rotor core  100  for use with the present invention. The laminated rotor core  100  is preferably used in a squirrel cage rotor of an induction motor for a compressor. The laminated rotor core  100  is formed or assembled by stacking a plurality of laminations  102 . The number of laminations required to assemble the laminated rotor core  100  is dependent upon the thickness of the laminations  102  and the desired height of the laminated rotor core  100 . In one embodiment of the present invention, the thickness of the laminations can range from about 0.015 inches to about 0.025 inches and is preferably 0.022 inches thick for a standard application and 0.018 inches thick for a “low loss” application. 
     FIG. 2  illustrates a top view of a lamination  102 . Each lamination  102  that is assembled into the laminated rotor core  100  preferably has a central aperture or bore  104 . The central bore  104  of the laminated rotor core  100  is configured to receive the shaft of the motor upon complete assembly of the motor. In addition, each lamination  102  preferably has a plurality of rotor slots or apertures  106 . The rotor slots  106  are preferably completely enclosed by the outer circumference of the laminated rotor core  100 , i.e., they are closed rotor slots. It is to be understood that apertures  106 , while being referred to as rotor slots and shown as circular apertures in the Figures can have any desired shape including oval, circular, rectangular, irregular or any other suitable shape. The plurality of rotor slots  106  are positioned circumferentially about the center axis A of the lamination  102 . The plurality of rotor slots  106  are preferably positioned equidistant and/or equiangular to one another about the axis A. The shape, number and size of the rotor slots  106  are dependent on the particular configuration of the motor and rotor cage used. In one embodiment of the present invention, the number of rotor slots (and bars) can range from about 20 to about 40 and is preferably 34 bars for a high torque application and 28 bars for a high performance application. 
   Furthermore, each rotor slot  106  is positioned a distance “d” from the outer circumference of the lamination  102 . The distance “d” corresponds directly to the bridge thickness of the lamination  102  and laminated rotor core  100 . To obtain optimal motor performance, the bridge thickness “d” should be as small or thin as possible while still maintaining the structural integrity of the rotor during operation of the motor. For example, for a laminated rotor core  100  having an outer diameter of 2.6 inches, the bridge thickness is preferably between about 0.01 inches and about 0.02 inches wide. The preferred bridge thickness “d” can vary depending on the configuration and size of the motor. Finally, it is to be understood that the lamination  102  can include additional features which are not shown for simplicity. 
   The laminations  102  are preferably formed from a magnetic material such as iron or steel by an extrusion or pressing operation of one or more steps. Once the extrusion operation is complete, the laminations  102  will preferably have a top view similar to the top view of FIG.  2 . After the laminations  102  are extruded, they are stacked or assembled to obtain the laminated rotor core  100 . During the assembly operation, the laminations  102  are preferably aligned and/or oriented to obtain a central bore  104  which extends substantially longitudinally and coaxially through the laminated rotor core  100  and to obtain rotor slots  106  which extend substantially longitudinally and coaxially through the laminated rotor core  100 , i.e., the rotor slots  106  have a skew of 0 degrees. In another preferred embodiment, the laminations  102  can be oriented to obtain rotor slots  106  that extend longitudinally through the laminated rotor core  100  with a skew of 2-15 degrees and preferably between about 4-12 degrees. The embodiment of the laminated rotor core  100  that does not have a skew of the rotor slots  106  can be used for a three phase application and the embodiment of the laminated rotor core  100  that has a skew of the rotor slots  106  can be used for a single phase application. 
   In a preferred embodiment of one process of the present invention, laminations  102  are formed or extruded with a bridge thickness “d” that provides for optimal performance of the motor, and are then assembled together to form the laminated rotor core  100 . The laminated rotor core  100  is placed in a mold of a casting or injection molding apparatus (not shown). Once the laminated rotor core  100  is placed in the mold, both radial forces and pressure and axial forces and pressure are applied to the laminated rotor core  100  by the mold and/or casting or injection molding apparatus to hold or secure the laminated rotor core  100  in position for the casting or injection molding operation and to prevent the molten material used in the casting or injection molding process, preferably aluminum or aluminum alloy, from leaking or seeping between the stacked laminations  102  of the laminated rotor core  100 . Upon being secured in the mold of the casting or injection molding apparatus, the laminated rotor core  100  is now ready for the commencement of the casting or injection molding operation to manufacture some or all of the rotor cage. The casting or injection molding apparatus includes a system or device for casting, injecting or introducing the rotor bars into the rotor slots  106  of the laminated rotor core  100  and preferably a mold or cast for casting, injecting or introducing end rings to connect the ends of the rotor bars. The application of both the radial and axial forces to the laminated rotor core  100  during the casting or injection molding operation prevents the leaking or seeping of the molten material between the stacked laminations  102  even though the laminations  102  and laminated rotor core  100  have a “thin” bridge thickness “d” for optimal performance of the motor. 
     FIGS. 3 and 4  illustrate schematically two embodiments for applying the axial and radial forces to the laminated rotor core  100 . In  FIG. 3 , the laminated rotor core  100  is held in position by one or more axial force members  302  and one or more radial force members  304 . The axial force members  302  are configured and disposed to apply an axial force F A , as shown in  FIG. 3 , to the top and bottom of the laminated rotor core  100  to axially compress the laminated rotor core  100  and laminations  102  without interfering with the casting operation. In addition, the axial force members  302  are configured and disposed to preferably apply the axial force F A  about substantially the entire circumference of the laminated rotor core  100 , although the axial force F A  can be applied to selected segments of the laminated rotor core  100 . Similarly, the radial force members  304  are configured and disposed to apply a radial force F R , as shown in  FIG. 3 , to the sides or outer perimeter of the laminated rotor core  100  to radially compress the laminated rotor core  100  and laminations  102  without interfering with the casting operation. In addition, the radial force members  304  are configured and disposed to preferably apply the radial force F R  about substantially the entire outer perimeter of the laminated rotor core  100 , although the radial force F R  can be applied to selected segments of the laminated rotor core  100 . 
   In  FIG. 4 , the laminated rotor core  100  is held in position by two or more “L”-shaped force members  402 . The “L”-shaped force members  402  are configured and disposed to apply both an axial force F A , as shown in  FIG. 4 , to the top and bottom of the laminated rotor core  100  to axially compress the laminated rotor core  100  and laminations  102  without interfering with the casting operation and to apply a radial force F R , as shown in  FIG. 4 , to the sides or outer perimeter of the laminated rotor core  100  to radially compress the laminated rotor core  100  and laminations  102  without interfering with the casting operation. In addition, the “L”-shaped force members  402  are configured and disposed to preferably apply the axial force F A  and the radial force F R  about substantially the entire circumference and outer perimeter of the laminated rotor core  100 , although the axial force F A  and the radial force F R  can be applied to selected segments of the laminated rotor core  100 . 
   In this embodiment of the present invention, any suitable type of casting or injection molding apparatus and/or mold can be used for the casting or injection molding of the rotor cage so long as the casting or injection molding apparatus and/or mold can apply both an axial force or pressure and a radial force or pressure to the laminated rotor core at the same time during the casting operation. Finally, while not described herein, the remaining process steps for the manufacture of the rotor and motor would be completed as is well known in the art. 
   In another preferred embodiment of the present invention, the laminated rotor core  100  is assembled using the laminations shown in  FIGS. 5-7 .  FIG. 5  illustrates a top view of the lamination  500  of this embodiment of the present invention. As shown in  FIG. 5 , lamination  500  has a central bore  502  and a plurality of rotor slots  504 , similar to the lamination  102  described above. However, in contrast to the lamination  102  of  FIG. 2 , the lamination  500 , as shown in greater detail in  FIG. 6 , has a countersink or groove portion  506  and a collar or lip portion  508  adjacent to each rotor slot  504 . The countersink portion  506  is preferably disposed on one planar side of the lamination  500  and is preferably a channel or groove in the side of the lamination  500  that is open to the rotor slot  504  and substantially circumferentially encloses or surrounds the rotor slot  504 . The collar portion  508  is disposed opposite the countersink portion  506  on the other planar side of the lamination  500  and is preferably an extension or projection extending from the other planar side and circumferentially enclosing or surrounding the rotor slot  504 . Preferably, the countersink portion  506  and the collar portion  508  are substantially coaxial to the center axis of the rotor slot  504 . 
   As shown in  FIG. 7 , when assembling the laminated rotor core  100  with laminations  500 , the collar portions  508  of each lamination  500  are preferably configured to mate with or fit in the countersink portions  506  of adjacent laminations  500 , such that an interference fit or connection is formed between the two. The countersink portions  506  and the collar portions  508  are preferably configured and disposed on the lamination  500  such that a substantially cylindrical rotor slot  504  is produced as shown in  FIG. 7 , which rotor slot  504  is similar to the rotor slot  106  of lamination  102 . When assembled, the countersink portion  506  and the collar portion  508  form a liquid barrier between a spacing  510  between the laminations  500  and the rotor slots  504 . The liquid barrier formed by the countersink portion  506  and the collar portion  508  is used to prevent the molten material used to cast the rotor bars from leaking or seeping between the laminations  500  during the casting operation. 
   While the countersink portion  506  and the collar portion  508  are shown with surfaces that are substantially parallel or perpendicular to the central axis of the rotor slot  504 , the surfaces of the countersink portion  506  and the collar portion  508  can have any type of surface including angled or curved surfaces so long as the countersink portion  506  and the collar portion  508  can be fit together to form an interference fit and the rotor slot  504  is not altered. Furthermore, the depth of the countersink portion  506  is substantially equal to the height of the collar portion  508 . However, it should be noted that slight differences in the depth and height of the countersink portion  506  and the collar portion  508  may be accommodated for in the casting operation when the laminated rotor core  100  is axially compressed. In a preferred embodiment of the present invention, the height of the collar portion  508  (or the depth of the countersink portion  506 ) is between about 10% and about 30% of the thickness of the lamination. 
   The process of manufacturing a laminated rotor core  100  with laminations  500  will now be described. To begin, laminations  500  are produced by an extrusion or stamping process with a bridge thickness “d” that provides for optimal performance of the motor, and then the laminations  500  are assembled together to form a laminated rotor core  100 . The laminated rotor core  100  is positioned in a mold of a casting or injection molding apparatus (not shown) and secured or held in place. The securing and holding of the laminated rotor core  100  can be accomplished using techniques that are known in the art or by the technique described above that applies both radial forces and pressure and axial forces and pressure are applied to the laminated rotor core  100 . Upon being secured in the mold of the casting or injection molding apparatus, the laminated rotor core  100  is now ready for the commencement of the casting or injection molding operation to manufacture some or all of the rotor cage. The casting or injection molding apparatus includes a system or device for casting, injecting or introducing the rotor bars into the rotor slots  504  of the laminated rotor core  100  and preferably a mold or cast for casting or injection molding end rings to connect the ends of the rotor bars. The presence of the countersink portions  506  and the collar portions  508  form a barrier in the rotor slots  504  to prevent the leaking or seeping of the molten material from between the stacked laminations  502  even though the laminations  502  and laminated rotor core  100  have a “thin” bridge thickness for optimal performance of the motor. 
   While the invention has been described with reference to a preferred embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this invention, but that the invention will include all embodiments falling within the scope of the appended claims.

Technology Category: 4