US20110241473A1 - Electric Motor Rotor - Google Patents
Electric Motor Rotor Download PDFInfo
- Publication number
- US20110241473A1 US20110241473A1 US13/153,642 US201113153642A US2011241473A1 US 20110241473 A1 US20110241473 A1 US 20110241473A1 US 201113153642 A US201113153642 A US 201113153642A US 2011241473 A1 US2011241473 A1 US 2011241473A1
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- United States
- Prior art keywords
- rotor
- laminations
- slots
- bars
- support disk
- Prior art date
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- Abandoned
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- 238000003475 lamination Methods 0.000 claims abstract description 69
- 239000003351 stiffener Substances 0.000 claims abstract description 31
- 238000000034 method Methods 0.000 claims description 29
- 238000003466 welding Methods 0.000 claims description 8
- 229910045601 alloy Inorganic materials 0.000 claims description 5
- 239000000956 alloy Substances 0.000 claims description 5
- 238000001746 injection moulding Methods 0.000 claims description 4
- 238000002347 injection Methods 0.000 claims description 3
- 239000007924 injection Substances 0.000 claims description 3
- 238000003754 machining Methods 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 238000005452 bending Methods 0.000 abstract 1
- 229910000831 Steel Inorganic materials 0.000 description 5
- 230000006698 induction Effects 0.000 description 5
- 239000010959 steel Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000009826 distribution Methods 0.000 description 2
- 238000010894 electron beam technology Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910000976 Electrical steel Inorganic materials 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
Images
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K17/00—Asynchronous induction motors; Asynchronous induction generators
- H02K17/02—Asynchronous induction motors
- H02K17/16—Asynchronous induction motors having rotors with internally short-circuited windings, e.g. cage rotors
- H02K17/20—Asynchronous induction motors having rotors with internally short-circuited windings, e.g. cage rotors having deep-bar rotors
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/46—Fastening of windings on the stator or rotor structure
- H02K3/48—Fastening of windings on the stator or rotor structure in slots
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49002—Electrical device making
- Y10T29/49009—Dynamoelectric machine
- Y10T29/49012—Rotor
Definitions
- This disclosure relates to the field of electric motors and more specifically to rotors of such motors that contain magnetic field reactive elements suitable for high speed operations.
- Electric motor rotors disclosed herein are suitable for use in turbochargers and other environments where motors may be required to operate at significantly high speeds exceeding 100,000 rpm.
- electrically controlled turbochargers employ a high speed electrical motor to rotate the turbo shaft which exists between the oppositely mounted compressor and turbine.
- the embodiments disclosed herein provide a center supporting disk on the rotor to provide additional support to the rotor bars to minimize their outward deformation during high speed operation.
- FIGS. 1A and 1B are exploded views of components included in a rotor of an electric induction motor.
- FIG. 2 is a cross-sectional plan view along the axis of an induction motor rotor assembly comprising the components shown in FIGS. 1A and 1B .
- FIG. 3 is a plan view of a lamination taken along section line III-III in FIG. 2 .
- FIG. 4 is an enlarged view of a lamination aperture from FIG. 3 , containing a rotor bar.
- FIG. 5 is a plan view of a center support ring taken along section line V-V in FIG. 2 .
- FIG. 6 is an enlarged view of a portion of FIG. 5 of a center support ring aperture containing a rotor bar.
- FIG. 7 is a cross-sectional plan view along the axis of an induction motor rotor assembly mounted directly on a shaft.
- FIGS. 8 and 9 illustrate embodiments by which a rotor may be assembled.
- the major components of a rotor 200 of an electric induction motor include an assembled rotor element 210 , containment rings 204 and 206 and stiffener sleeve component 202 for mounting on a rotor shaft 240 ( FIG. 2 ).
- rotor element 210 is shown to include two end rings 212 and 214 (sometimes referred to as “balance” rings) having a plurality of apertures 112 and 114 , a plurality of (19) rotor bars 218 , and a plurality of (65) steel laminations in sets 216 a and 216 b arranged in axially aligned stacks.
- a central supporting disk (also referred to herein as an anti-expansion disk) 226 is centrally located between laminations sets 216 a and 216 b .
- Rotor bars 218 slide through apertures in steel lamination sets 216 a and 216 b , through apertures in supporting disk 226 , and through apertures in end rings 212 and 214 .
- the purpose of central supporting disk 226 is to minimize the effects of centrifugal forces from distorting the rotor bars 218 during high speed operations.
- Steel laminations 216 can be formed of high-strength electrical steel, such as Hyperco 50TM heat treated to provide maximum strength, and oxide coated to prevent electrical current losses between laminations.
- Rotor bars 218 can be made from a high strength-to-density ratio (specific modulus) and high electrical conductivity alloy, such as 2219 A1.
- Rotor lamination sets 216 a and 216 b are coaxially arranged in stacks on either side of lamination supporting disk 226 .
- Rotor bars 218 are inserted into (or molded in) slots 217 ( 217 a - 217 s ) and 227 ( 227 a - 227 s ).
- End rings 212 and 214 are installed on each end and the ends of rotor bars are received into apertures 112 and 114 of the balance rings 212 and 214 , respectively.
- the assembly is then clamped together axially to compress the laminations together.
- Rotor bars 218 are then welded to end rings 212 and 214 .
- Such welding may employ an electron beam process or any other process that provides effective high strength welding for such metals.
- Heat sinks are attached to the rotor during this process to minimize the distortional effects of welding.
- rotor 210 is machined on all outside surfaces and the ID to improve concentricity of the inside diameter, ID, and outside diameter, OD, as well as balance.
- the rotor assembly 210 is slid onto the stiffener sleeve 202 .
- the assembly is then balanced and the stiffener sleeve 202 is press fitted onto shaft 240 .
- the end rings 212 and 214 and central support disk 226 are press fitted onto the sleeve 202 to secure the rotor assembly 210 to shaft 240 under extremes in operational circumstances.
- Rotor 210 can alternatively be injection molded in a high-pressure injection molding process where the rotor laminations 216 a and 216 b are placed in a mold and molten aluminum is injected into slots 217 and 227 to form the rotor bars 218 .
- end rings 212 and 214 and central support disk 226 are also formed.
- End rings 212 and 214 are preferably fabricated from the same or similar alloy used to fabricate the rotor bars 218 and serve to minimize expansion of the rotor ends during high speed operations. Furthermore, central support disk 226 may be fabricated from the same or similar alloy as used for end rings 212 and 214 and rotor bars 218 .
- the end rings 212 and 214 can include axial extensions 213 and 215 .
- Extensions 213 and 215 are smaller in diameter than the main body of the end rings 212 and 214 . By making end-ring extensions 213 and 215 smaller in diameter, the extensions experience much less centrifugal force and therefore retain their press fit onto the stiffener 202 and shaft 240 throughout the broad range of operating speed.
- containment rings 204 and 206 are clamped around the end rings 212 and 214 to further ensure the integrity of the press fit between end rings, stiffener sleeve 202 and shaft 240 .
- containment rings 204 and 206 are located on end ring extensions 213 and 215 .
- motor rotors When employed in an electrically-controlled turbocharger design, motor rotors are typically elongated. There is a concern that longer rotor bars, such as 218 in FIGS. 1B and 2 may be subjected to large centrifugal forces at high rotational speeds that act on the central portions of the rotor bars forcing them outwardly in a radial direction sufficient to affect the motor-to-stator air gap. If distortion of the rotor bars is too great, the rotor contacts the stator.
- the individual laminations are provided with an oxide coating to prevent shorting between adjacent laminations and to prevent shorting between the surfaces of the slots formed in the laminations to the rotor bars.
- end rings 212 and 214 as well as central support disk 226 restrain expansion of the rotor rods 218 .
- central support disk 226 is shown between lamination stacks 216 a and 216 b .
- at least one additional support disk is provided between additional sets of lamination stacks.
- a first protuberance 222 and a second axial protuberance 223 extend outwardly in a radial direction from stiffener sleeve 202 .
- the space between the two protuberances 222 and 223 is of a smaller diameter. This smaller diameter portion provides a shoulder for a tool to grab onto the stiffener sleeve 202 for disassembly.
- FIG. 3 a cross-sectional view of lamination 216 a taken along section line III-III in FIG. 2 , shows the distribution of the 19 slots 217 a - 217 s .
- the stiffener 202 is shown surrounding the rotor shaft 240 .
- Rotor bars 218 a - 218 s are inserted into the corresponding slots 217 a - 217 s.
- slot 217 a in lamination 216 a is radially oriented.
- Rotor bar 218 a is inserted into the slot 217 a .
- slot 217 a is slightly larger than rotor bar 218 a .
- An air gap 219 exists between slot 217 a and rotor bar 218 a .
- rotor bar 218 a expands more than lamination set 216 a and thus more than slot 217 a . Therefore, at high speed, air gap 219 is taken up by the expanded rotor bar 218 a .
- FIG. 5 a cross-sectional view through central support disk 226 taken along section line V-V in FIG. 2 shows the distribution of the 19 slots 227 a - 227 s .
- Central support disk 226 surrounds stiffener 202 which is press fitted to the rotor shaft 240 .
- Rotor bars 218 a - 218 s are inserted into the corresponding slots 217 a - 217 s .
- There is no air gap between slot 227 a of central support disk 226 and rotor bar 218 a as can be seen in detail in the embodiment shown in FIG. 6 because rotor bar 218 a and central support disk 226 are made of materials with similar expansion characteristics. Further, by avoiding an air space, support disk restrains rotor bar 218 a from outward movement.
- FIG. 7 illustrates a rotor assembly 300 that is mounted directly on rotor shaft 340 that can be used in environments where a stiffening component is not included.
- Rotor assembly 300 includes two end rings 312 and 314 , a plurality of rotor bars 318 (only one of which is shown in this cross section) and steel lamination sets 316 a and 316 b that are axially aligned stacks.
- a central support disk 326 is centrally located and has slots through which rotor bars 318 are inserted. Central disk 326 provides stiffening to minimize the distortion of the rotor bars at high rotational speeds.
- Extensions 313 and 315 extending axially from end rings 312 and 314 are smaller in diameter than the main body of the end rings 312 and 314 to reduce the mass surrounding the press fit to shaft 340 .
- FIG. 8 The procedure to assemble the rotor assembly onto the shaft, according to one embodiment, is illustrated in FIG. 8 .
- laminations stacks 216 a and 216 b are arranged on either side of supporting disk 226 .
- the slots are aligned so that in 802 the rotor bars 218 a - s can be inserted in the slots through 216 a , 216 b , and 226 .
- end rings 212 and 214 are slid onto rotor bars 218 a - s with apertures in the end rings engaging with the rotor bars.
- rotor assembly 210 is formed, designated as 810 in FIG. 8 . After rotor assembly 210 is welded, it is machined to improve its concentricity and balance. In embodiments that include containment rings 204 and 206 , they are fit onto extensions 213 and 215 , respectively, in 814 . Rotor assembly 210 is press fit onto stiffener sleeve 202 in block 816 .
- stiffener sleeve 202 is press fit onto rotor shaft 240 .
- the end rings, the central support disk, and the rotor bars are made of the same material, e.g., an aluminum alloy, and these are produced by injection molding.
- the manufacture begins with stacking laminations sets 216 a and 216 b , as illustrated in FIG. 9 , starting at 900 .
- Lamination sets 216 a and 216 b are placed in an injection mold and secured in place during molding, at 902 .
- a die is centrally located within the laminations so that aluminum is not injected into the space reserved for rotor shaft 240 and stiffener sleeve 202 .
- the molten aluminum alloy is injected into the mold, in 904 .
- the end rings, central support disk, and rotor bars are one integral part, which, of course, cannot be disassembled from the laminations.
- the combination of parts forms the rotor assembly.
- the rotor assembly is cooled, 906 , before being ejected from the mold, 908 .
- the die is removed from the rotor assembly.
- Group 910 designates the processes to form the rotor assembly.
- the rotor assembly is machined to remove artifacts from the mold process. Additionally, the machining may improve the dimensional accuracy and hence balance and fit of the rotor assembly. In embodiments that include containment rings 204 and 206 , they are fit onto extensions of the end rings, respectively, in 914 .
- Rotor assembly is press fit onto stiffener sleeve 202 in block 916 .
- stiffener sleeve 202 is press fit onto rotor shaft 240 .
- the rotor assembly is press fit directly onto rotor shaft 240 .
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- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Manufacture Of Motors, Generators (AREA)
- Iron Core Of Rotating Electric Machines (AREA)
Abstract
A rotor of an electric machine is disclosed that resists expansion of the rotor components even at high rotational speed. The rotor includes first and second pluralities of laminations having slots to accept rotor bars. A support disk, also having slots, is placed between the laminations. The support disk, into which the rotor bars are slid, restrains the rotor bars from bending outwardly at high rotational speeds of the rotor. The rotor bars are further restrained at the ends by end rings, which have apertures into which ends of the rotor bars are placed. In some embodiments, containment rings are placed over axial extension of the end rings to prevent outward bowing at high speeds. In some embodiments, the rotor includes a stiffener sleeve to provide additional resistance to expansion during high rotational speeds.
Description
- This application is a continuation in part of U.S. application Ser. No. 12/791,832, filed 1 Jun. 2010, and which is incorporated herein. This application claims benefit of U.S. provisional application Ser. No. 61/217,674 filed 3 Jun. 2009.
- This disclosure relates to the field of electric motors and more specifically to rotors of such motors that contain magnetic field reactive elements suitable for high speed operations.
- Particularly challenging aspects in the design of the rotor of an electric motor that has the capability to be driven at speeds exceeding 100,000 rpm concern the prevention of centrifugal forces from expanding the rotor elements such that they become separated from the shaft to which they are attached. In the case of an induction motor, it is important to prevent expansion of the rotor elements to avoid coming into contact with the stator element.
- Electric motor rotors disclosed herein are suitable for use in turbochargers and other environments where motors may be required to operate at significantly high speeds exceeding 100,000 rpm. Typically, electrically controlled turbochargers employ a high speed electrical motor to rotate the turbo shaft which exists between the oppositely mounted compressor and turbine. The embodiments disclosed herein provide a center supporting disk on the rotor to provide additional support to the rotor bars to minimize their outward deformation during high speed operation.
-
FIGS. 1A and 1B are exploded views of components included in a rotor of an electric induction motor. -
FIG. 2 is a cross-sectional plan view along the axis of an induction motor rotor assembly comprising the components shown inFIGS. 1A and 1B . -
FIG. 3 is a plan view of a lamination taken along section line III-III inFIG. 2 . -
FIG. 4 is an enlarged view of a lamination aperture fromFIG. 3 , containing a rotor bar. -
FIG. 5 is a plan view of a center support ring taken along section line V-V inFIG. 2 . -
FIG. 6 is an enlarged view of a portion ofFIG. 5 of a center support ring aperture containing a rotor bar. -
FIG. 7 is a cross-sectional plan view along the axis of an induction motor rotor assembly mounted directly on a shaft. -
FIGS. 8 and 9 illustrate embodiments by which a rotor may be assembled. - In
FIG. 1A the major components of arotor 200 of an electric induction motor include an assembledrotor element 210,containment rings stiffener sleeve component 202 for mounting on a rotor shaft 240 (FIG. 2 ). - In
FIGS. 1B and 2 ,rotor element 210 is shown to include twoend rings 212 and 214 (sometimes referred to as “balance” rings) having a plurality ofapertures rotor bars 218, and a plurality of (65) steel laminations insets laminations sets Rotor bars 218 slide through apertures insteel lamination sets disk 226, and through apertures inend rings disk 226 is to minimize the effects of centrifugal forces from distorting therotor bars 218 during high speed operations. -
Steel laminations 216 can be formed of high-strength electrical steel, such as Hyperco 50™ heat treated to provide maximum strength, and oxide coated to prevent electrical current losses between laminations.Rotor bars 218 can be made from a high strength-to-density ratio (specific modulus) and high electrical conductivity alloy, such as 2219 A1. - During assembly,
rotor lamination sets lamination supporting disk 226.Rotor bars 218 are inserted into (or molded in) slots 217 (217 a-217 s) and 227 (227 a-227 s).End rings apertures balance rings Rotor bars 218 are then welded toend rings rotor 210 is machined on all outside surfaces and the ID to improve concentricity of the inside diameter, ID, and outside diameter, OD, as well as balance. - Following machining, the
rotor assembly 210 is slid onto thestiffener sleeve 202. The assembly is then balanced and thestiffener sleeve 202 is press fitted ontoshaft 240. While there may be some tolerance between thestiffener sleeve 202 and the ID of the laminations to prevent pre-stress in the laminations, theend rings central support disk 226 are press fitted onto thesleeve 202 to secure therotor assembly 210 toshaft 240 under extremes in operational circumstances. -
Rotor 210 can alternatively be injection molded in a high-pressure injection molding process where therotor laminations slots rotor bars 218. In the same process,end rings central support disk 226 are also formed. -
End rings rotor bars 218 and serve to minimize expansion of the rotor ends during high speed operations. Furthermore,central support disk 226 may be fabricated from the same or similar alloy as used forend rings rotor bars 218. - To further mitigate the effects of centrifugal forces generated at high rotational speeds, the
end rings axial extensions Extensions end rings ring extensions stiffener 202 andshaft 240 throughout the broad range of operating speed. - In some embodiments,
containment rings end rings stiffener sleeve 202 andshaft 240. InFIGS. 1A and 2 ,containment rings end ring extensions - When employed in an electrically-controlled turbocharger design, motor rotors are typically elongated. There is a concern that longer rotor bars, such as 218 in
FIGS. 1B and 2 may be subjected to large centrifugal forces at high rotational speeds that act on the central portions of the rotor bars forcing them outwardly in a radial direction sufficient to affect the motor-to-stator air gap. If distortion of the rotor bars is too great, the rotor contacts the stator. In some embodiments, the individual laminations are provided with an oxide coating to prevent shorting between adjacent laminations and to prevent shorting between the surfaces of the slots formed in the laminations to the rotor bars. If large outward forces act upon the laminations the oxide coating on the surfaces ofslots 217 could wear and eventually lead to shorting between laminations and the rotor bars.End rings central support disk 226 restrain expansion of therotor rods 218. In the embodiment shown inFIG. 2 ,central support disk 226 is shown betweenlamination stacks - In
FIG. 2 , afirst protuberance 222 and a secondaxial protuberance 223 extend outwardly in a radial direction fromstiffener sleeve 202. The space between the twoprotuberances stiffener sleeve 202 for disassembly. -
FIG. 3 , a cross-sectional view oflamination 216 a taken along section line III-III inFIG. 2 , shows the distribution of the 19slots 217 a-217 s. In this view, thestiffener 202 is shown surrounding therotor shaft 240.Rotor bars 218 a-218 s are inserted into the correspondingslots 217 a-217 s. - As can be seen in
FIG. 4 , the enlarged view ofslot 217 a inlamination 216 a is radially oriented.Rotor bar 218 a is inserted into theslot 217 a. When stationary, as shown inFIG. 4 , slot 217 a is slightly larger thanrotor bar 218 a. Anair gap 219 exists betweenslot 217 a and rotor bar 218 a. At high rotational speeds,rotor bar 218 a expands more than lamination set 216 a and thus more thanslot 217 a. Therefore, at high speed,air gap 219 is taken up by the expandedrotor bar 218 a. Anair gap opening 220 provides a separation so that poles are formed in the adjacent teeth (the radial portions of the laminations between the adjacent slots). InFIG. 5 , a cross-sectional view throughcentral support disk 226 taken along section line V-V inFIG. 2 shows the distribution of the 19slots 227 a-227 s.Central support disk 226 surroundsstiffener 202 which is press fitted to therotor shaft 240.Rotor bars 218 a-218 s are inserted into the correspondingslots 217 a-217 s. There is no air gap betweenslot 227 a ofcentral support disk 226 and rotor bar 218 a as can be seen in detail in the embodiment shown inFIG. 6 becauserotor bar 218 a andcentral support disk 226 are made of materials with similar expansion characteristics. Further, by avoiding an air space, support disk restrainsrotor bar 218 a from outward movement. -
FIG. 7 illustrates arotor assembly 300 that is mounted directly onrotor shaft 340 that can be used in environments where a stiffening component is not included.Rotor assembly 300 includes two end rings 312 and 314, a plurality of rotor bars 318 (only one of which is shown in this cross section) and steel lamination sets 316 a and 316 b that are axially aligned stacks. Acentral support disk 326 is centrally located and has slots through which rotor bars 318 are inserted.Central disk 326 provides stiffening to minimize the distortion of the rotor bars at high rotational speeds.Extensions shaft 340. - The procedure to assemble the rotor assembly onto the shaft, according to one embodiment, is illustrated in
FIG. 8 . In 800, laminations stacks 216 a and 216 b are arranged on either side of supportingdisk 226. The slots are aligned so that in 802 therotor bars 218 a-s can be inserted in the slots through 216 a, 216 b, and 226. In 804, end rings 212 and 214 are slid ontorotor bars 218 a-s with apertures in the end rings engaging with the rotor bars. In 806, the assembly is clamped together to compress the laminations axially and a heat sink is attached prior to welding the end rings 212 and 214 to the rotor bars 218. The welding process may be an electron beam process. In blocks 800 through 808,rotor assembly 210 is formed, designated as 810 inFIG. 8 . Afterrotor assembly 210 is welded, it is machined to improve its concentricity and balance. In embodiments that include containment rings 204 and 206, they are fit ontoextensions Rotor assembly 210 is press fit ontostiffener sleeve 202 inblock 816. In one embodiment, only the end rings 212 and 214 andcentral support disk 226 are press fit on the stiffener sleeve. Lamination sets 216 a and 216 b are slightly oversize, with respect to the inner diameter, to avoid cracking the laminations during assembly. Inblock 818,stiffener sleeve 202 is press fit ontorotor shaft 240. - In one embodiment, the end rings, the central support disk, and the rotor bars are made of the same material, e.g., an aluminum alloy, and these are produced by injection molding. In such embodiment, the manufacture begins with stacking laminations sets 216 a and 216 b, as illustrated in
FIG. 9 , starting at 900. Lamination sets 216 a and 216 b are placed in an injection mold and secured in place during molding, at 902. Also in 902, a die is centrally located within the laminations so that aluminum is not injected into the space reserved forrotor shaft 240 andstiffener sleeve 202. The molten aluminum alloy is injected into the mold, in 904. The end rings, central support disk, and rotor bars are one integral part, which, of course, cannot be disassembled from the laminations. The combination of parts forms the rotor assembly. The rotor assembly is cooled, 906, before being ejected from the mold, 908. In 908, the die is removed from the rotor assembly.Group 910 designates the processes to form the rotor assembly. In 912, the rotor assembly is machined to remove artifacts from the mold process. Additionally, the machining may improve the dimensional accuracy and hence balance and fit of the rotor assembly. In embodiments that include containment rings 204 and 206, they are fit onto extensions of the end rings, respectively, in 914. Rotor assembly is press fit ontostiffener sleeve 202 inblock 916. In one embodiment, only the end rings andcentral support disk 226 are press fit on the stiffener sleeve. Lamination sets 216 a and 216 b may be slightly oversize, with respect to the inner diameter, to avoid cracking the laminations during assembly. Inblock 818,stiffener sleeve 202 is press fit ontorotor shaft 240. In embodiments in which astiffener sleeve 202 is not used, the rotor assembly is press fit directly ontorotor shaft 240. - The embodiments shown here are exemplary in nature and shall not be considered to be a restriction on the scope of the claims set forth herein.
Claims (25)
1. A method to manufacture a rotor of an electric machine, the method comprising:
arranging two sets of rotor laminations on either side of a support disk;
inserting rotor bars into slots defined in the rotor laminations and the support disk; and
installing end rings at ends of the rotor bars with apertures defined in the end rings engaging with ends of the rotor bars.
2. The method of claim 1 wherein:
the inserting rotor bars comprises injection molding the rotor bars into the slots; and
the slots in the rotor laminations and the central support disk are aligned prior to the injection molding.
3. The method of claim 1 , further comprising:
clamping the end rings axially with the rotor laminations and the support disk clamped therebetween; and
welding tips of the rotor bars to the end rings.
4. The method of claim 1 wherein the rotor laminations, the rotor bars, the end rings, and the support disk comprise a rotor assembly, the method further comprising:
providing a heat sink in contact with the rotor assembly during the welding.
5. The method of claim 3 wherein the rotor laminations, the rotor bars, the end rings, and the support disk comprise a rotor assembly, the method further comprising:
machining outer surfaces of the rotor assembly to improve the balance of the rotor assembly during rotation of the rotor assembly.
6. The method of claim 3 wherein the rotor laminations, the rotor bars, the end rings, and the support disk comprise a rotor assembly, the method further comprising: press fitting the rotor assembly onto a stiffener sleeve.
7. The method of claim 6 further comprising: press fitting the stiffener sleeve on a rotor shaft.
8. The method of claim 3 wherein the rotor laminations, the rotor bars, the end rings, and the support disk comprise a rotor assembly, the method further comprising: press fitting the rotor assembly onto a rotor shaft.
9. A rotor of an electric machine, comprising:
a first plurality of laminations arranged axially, the first plurality of laminations defining a plurality of slots;
a second plurality of laminations arranged axially, the second plurality of laminations defining a plurality of slots; and
a support disk defining a plurality of slots wherein the support disk is located between the first and second plurality of lamination with slots of the first and second pluralities of lamination and slots of the support disk being aligned.
10. The rotor of claim 9 , further comprising: rotor bars slid into the aligned slots.
11. The rotor of claim 10 , further comprising: first and second end rings defining apertures with first ends of the rotor bars engaging with the apertures of the first end ring and second ends of the rotor bars engaging with the apertures of the second end ring.
12. The rotor of claim 11 wherein the first ends of the rotor bars are welded to the first end disk and the second ends of the rotor bars are welded to the second end disk.
13. The rotor of claim 12 , further comprising:
a stiffener sleeve wherein the welded assembly is fit onto the stiffener sleeve; and
a rotor shaft wherein the stiffener sleeve is fit onto the rotor shaft.
14. The rotor of claim 13 wherein the stiffener sleeve comprises a protuberance extending radially outwardly from the stiffener sleeve wherein the protuberance provides a shoulder for a removal tool.
15. The rotor of claim 12 , further comprising: a rotor shaft wherein the welded assembly is fit onto the rotor shaft.
16. A rotor of an electric machine, comprising:
a first plurality of laminations arranged axially, the first plurality of laminations defining a plurality of slots;
rotor bars provided within the slots;
first and second end rings defining apertures with first ends of the rotor bars engaging with the apertures of the first end ring and second ends of the rotor bars engaging with the apertures of the second end ring wherein the first ends of the rotor bars are welded to the first end ring and the second ends of the rotor bars are welded to the second end ring.
17. The rotor of claim 16 , further comprising:
a second plurality of laminations arranged axially, the second plurality of laminations defining a plurality of slots; and
a support disk defining a plurality of slots wherein the support disk is located between the first and second plurality of laminations with slots of the first and second pluralities of laminations and slots of the support disk being aligned; and the rotor bars extend through the slots in the support disk and the slots in the second plurality of laminations.
18. The rotor of claim 16 , further comprising:
a stiffener sleeve wherein the welded assembly is fit onto the stiffener sleeve; and
a rotor shaft wherein the stiffener sleeve is fit onto the rotor shaft.
19. The rotor of claim 16 wherein the first end ring has a first extension extending axially; the first extension extends away from the first plurality of laminations; the second end ring has a second extension extending axially; and the second extension extends away from the first plurality of laminations, the rotor further comprising:
a first containment ring placed over the first extension; and
a second containment ring placed over the second extension.
20. The rotor of claim 17 wherein the rotor bars, the support disk, and the first and second end disks are injection molded onto the first and second pluralities of laminations.
21. A method to manufacture a rotor of an electric machine, the method comprising:
arranging two sets of rotor laminations with slots defined in the laminations aligned;
placing the rotor laminations into a mold surrounding a die;
securing the laminations in place; and
injecting molten alloy into the die.
22. The method of claim 21 wherein the alloy and the rotor laminations form a rotor assembly, the method further comprising:
ejecting the rotor assembly from the mold; and
removing the die from the rotor assembly.
23. The method of claim 22 , further comprising: fitting first and second containment rings over extensions that extend axially from ends of the rotor assembly.
24. The method of claim 22 , further comprising: press fitting the rotor assembly onto a sleeve stiffener.
25. The method of claim 24 , further comprising: press fitting the sleeve stiffener onto a rotor shaft.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/153,642 US20110241473A1 (en) | 2009-06-03 | 2011-06-06 | Electric Motor Rotor |
GB1113970.6A GB2492422B (en) | 2011-06-06 | 2011-08-15 | Electric motor rotor |
DE102011053632A DE102011053632A1 (en) | 2011-06-06 | 2011-09-15 | Rotor for an electric motor |
JP2011203630A JP2012253998A (en) | 2011-06-06 | 2011-09-16 | Electric motor rotor |
CN2012101842417A CN102820742A (en) | 2011-06-06 | 2012-06-06 | Electric motor rotor |
US14/686,446 US9729035B2 (en) | 2009-06-03 | 2015-04-14 | Electric motor rotor |
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US12/791,832 US8344576B2 (en) | 2009-06-03 | 2010-06-01 | Electric motor rotor |
US13/153,642 US20110241473A1 (en) | 2009-06-03 | 2011-06-06 | Electric Motor Rotor |
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US20120267978A1 (en) * | 2009-09-09 | 2012-10-25 | Ansaldobreda S.P.A. | Squirrel-cage rotor for asynchronous motors |
US20130113331A1 (en) * | 2011-11-09 | 2013-05-09 | Volker Dölz | Rotor of an asynchronous machine with retaining element |
US8443769B1 (en) | 2012-05-18 | 2013-05-21 | Raymond F. Lippitt | Internal combustion engines |
US20140125208A1 (en) * | 2011-06-08 | 2014-05-08 | Mitsubishi Heavy Industries, Ltd. | Motor rotor structure for electric turbo charger and method of assembling same |
US20150123511A1 (en) * | 2013-11-01 | 2015-05-07 | Tesla Motors, Inc. | Flux Shield for Electric Motor |
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US8643242B2 (en) * | 2009-09-09 | 2014-02-04 | Ansaldobreda S.P.A. | Squirrel-cage rotor for asynchronous motors |
US20120267978A1 (en) * | 2009-09-09 | 2012-10-25 | Ansaldobreda S.P.A. | Squirrel-cage rotor for asynchronous motors |
US20140125208A1 (en) * | 2011-06-08 | 2014-05-08 | Mitsubishi Heavy Industries, Ltd. | Motor rotor structure for electric turbo charger and method of assembling same |
US10148141B2 (en) * | 2011-06-08 | 2018-12-04 | Mitsubishi Heavy Industries Engine & Turbocharger, Ltd. | Motor rotor structure for electric turbo charger and method of assembling same |
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US8443769B1 (en) | 2012-05-18 | 2013-05-21 | Raymond F. Lippitt | Internal combustion engines |
US9599016B2 (en) | 2012-05-18 | 2017-03-21 | Raymond F. Lippitt | Internal combustion engines |
US9303559B2 (en) | 2012-10-16 | 2016-04-05 | Raymond F. Lippitt | Internal combustion engines |
EP2804297A3 (en) * | 2013-05-18 | 2016-01-06 | Tesla Motors, Inc. | Squirrel-cage rotor assembly with electron beam welded end caps |
US20150123511A1 (en) * | 2013-11-01 | 2015-05-07 | Tesla Motors, Inc. | Flux Shield for Electric Motor |
US10938280B2 (en) * | 2013-11-01 | 2021-03-02 | Tesla, Inc. | Flux shield for electric motor |
US9719444B2 (en) | 2013-11-05 | 2017-08-01 | Raymond F. Lippitt | Engine with central gear train |
US9217365B2 (en) | 2013-11-15 | 2015-12-22 | Raymond F. Lippitt | Inverted V-8 internal combustion engine and method of operating the same modes |
US9664044B2 (en) | 2013-11-15 | 2017-05-30 | Raymond F. Lippitt | Inverted V-8 I-C engine and method of operating same in a vehicle |
WO2016154111A1 (en) * | 2015-03-23 | 2016-09-29 | Franklin Electric Co., Inc. | Electric motor and method of assembling an electric motor |
US10587174B2 (en) * | 2015-03-23 | 2020-03-10 | Franklin Electric Co., Inc. | Electric motor and method of assembling an electric motor |
US11108290B2 (en) * | 2016-02-15 | 2021-08-31 | Mitsubishi Electric Corporation | Three-phase induction motor and secondary conductor thereof |
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US9729035B2 (en) | 2017-08-08 |
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