US20140147306A1 - Structure and method for adjusting balance of turbocharging device incorporating electric motor - Google Patents
Structure and method for adjusting balance of turbocharging device incorporating electric motor Download PDFInfo
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- US20140147306A1 US20140147306A1 US14/117,803 US201214117803A US2014147306A1 US 20140147306 A1 US20140147306 A1 US 20140147306A1 US 201214117803 A US201214117803 A US 201214117803A US 2014147306 A1 US2014147306 A1 US 2014147306A1
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- United States
- Prior art keywords
- rotational balance
- rotor
- balance adjusting
- electromagnetic steel
- rotor core
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D13/00—Pumping installations or systems
- F04D13/02—Units comprising pumps and their driving means
- F04D13/06—Units comprising pumps and their driving means the pump being electrically driven
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/04—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump
- F02B37/10—Engines with exhaust drive and other drive of pumps, e.g. with exhaust-driven pump and mechanically-driven second pump at least one pump being alternatively or simultaneously driven by exhaust and other drive, e.g. by pressurised fluid from a reservoir or an engine-driven pump
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/027—Arrangements for balancing
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B37/00—Engines characterised by provision of pumps driven at least for part of the time by exhaust
- F02B37/005—Exhaust driven pumps being combined with an exhaust driven auxiliary apparatus, e.g. a ventilator
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B39/00—Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
- F02B39/02—Drives of pumps; Varying pump drive gear ratio
- F02B39/08—Non-mechanical drives, e.g. fluid drives having variable gear ratio
- F02B39/10—Non-mechanical drives, e.g. fluid drives having variable gear ratio electric
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/04—Balancing means
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/14—Structural association with mechanical loads, e.g. with hand-held machine tools or fans
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K15/00—Methods or apparatus specially adapted for manufacturing, assembling, maintaining or repairing of dynamo-electric machines
- H02K15/16—Centering rotors within the stator; Balancing rotors
- H02K15/165—Balancing the rotor
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- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the present invention relates to a structure and a method for adjusting rotational balance of a rotor of a turbocharging device incorporating an electric motor turbocharging suction air to an internal combustion.
- the turbocharging device incorporating an electric motor includes a turbo charger incorporating a motor generator, a turbo charger incorporating an electric motor, an electric supercharger, and the like.
- Turbo chargers for compressing and turbocharging suction air by driving with exhaust gas of an internal combustion has been widely used, in order to improve output of the internal combustion.
- turbo charger incorporating a motor generator that improves acceleration responsiveness by incorporating an electric motor in a rotary shaft of the turbocharging device and assisting the acceleration of rotation of a compressor impeller, and collects energy by converting exhaust gas energy into electric energy.
- the turbo charger incorporating a motor generator is an electric supercharger that rotates a compressor impeller by only an electric motor.
- FIG. 6 is a schematic configuration diagram of an engine 01 mounted with a turbo charger 03 incorporating a motor generator disclosed in Japanese Patent Application Laid-open No. H8-182382 (Patent Document 1).
- a turbine wheel 031 of the turbo charger incorporating a motor generator 03 is driven by exhaust gas from an exhaust manifold 011 of the engine 01 .
- a compressor impeller 032 coaxially connected to the turbine wheel 031 is driven, so that suction air from an air cleaner (not shown) is supplied to the engine 01 via a suction manifold 012 .
- a motor rotor 05 for assisting rotation (driving) of the compressor impeller 032 is disposed on the intermediate-portion of a shaft 041 for connecting the turbine wheel 031 and the compressor impeller 032 .
- the motor rotor 05 is axially rotatably supported on a pair of bearing support parts provided in a housing (not shown) of the turbo charger incorporating a motor generator 03 via bearings 049 .
- Reference numeral 06 denotes an engine control unit (ECU), which controls operation of the engine 01 , flows a current to a stator 033 depending on the operation status of the engine 1 , and also controls operation of the turbo charger incorporating a motor generator 03 .
- Reference numeral 07 denotes a battery, which is a power supply of a controller.
- FIG. 7 is a schematic configuration diagram of a conventional motor rotor.
- a motor rotor 05 has a step part 044 that is a narrow shaft part on a side closer to a compressor impeller 043 , on an intermediate part in the thrust direction of a shaft 041 having an end mounted with a turbine wheel 042 .
- a nut 046 which is screwed with a screw part formed on the end of the narrow shaft part, through a thrust bush 056 , a rotor 051 , an oil seal accessory 054 , and the compressor impeller 043 which are fitted with (fitted onto) the narrow shaft part, presses and positions these components with respect to the step part 044 .
- a magnet 052 (permanent magnet) is fitted onto the narrow shaft part of the shaft 041 , a sleeve 057 is further fitted onto the outer peripheral part of the magnet 052 to be fixed to the narrow shaft part of the shaft 041 , thereby forming the rotor 051 .
- the sleeve 057 needs to be fitted onto the outer peripheral part of the magnet arranged on the rotor 051 , in order to prevent breakage and scattering of the magnet.
- a stator 033 for rotating and driving the shaft 041 by utilizing magnetism of the magnet of the rotor 051 is arranged on the housing side of the turbo charger incorporating a motor generator 03 , facing the rotor 051 .
- Patent Document 2 Japanese Patent Application Laid-open No. 2000-145468
- turbo charger incorporating a motor generator is used under a high temperature environment resulting from exhaust gas, performance of a motor that utilizes a magnet significantly deteriorates with rise in temperature, and such a motor is not suitable.
- the magnetic inductor type motor is configured that a rotor made of laminated electromagnetic steel plates and iron, or laminated electromagnetic steel plates are driven by a stator arranged around the rotor.
- the rotor rotates at a high speed in a state of being arranged between a turbine wheel and a compressor impeller, it is important to adjust the rotational balance (dynamic balance) of the rotor made of the laminated electromagnetic steel plates and iron, or the laminated electromagnetic steel plates for balancing. Therefore, the adjustment of the rotational balance on a conventional adjustment part (e.g., a nut part for fastening the compressor impeller to a rotary shaft of the turbo charger) can not cope with increase in an adjustment amount, or fine adjustment.
- a conventional adjustment part e.g., a nut part for fastening the compressor impeller to a rotary shaft of the turbo charger
- the present invention has been conceived in order to solve such problems, and an object thereof is to provide a structure and a method for adjusting balance of a turbo charger incorporating a motor generator capable of achieving increase in adjustment parts (increase in an adjustment amounts and ensuring fine adjustment) for adjusting the rotational balance of a rotary shaft of the turbo charger, and preventing performance deterioration while maintaining sufficient motor driving force even under a high temperature condition.
- a balance adjusting structure for a turbocharging device incorporating an electric motor includes: at least one rotor blade disposed in a housing; a shaft connected to the rotor blade; a bearing formed in the housing, and configured to rotatably axially support the shaft; a rotor core penetrated by the shaft; and a stator disposed at a position facing the rotor core in the housing, and configured to rotate and drive the rotor core together with the shaft by a magnetic field, wherein the rotor core has a sleeve fitted onto the shaft, a plurality of electromagnetic steel plates laminated in an axial direction of the sleeve and fitted onto the sleeve, and a rotational balance adjusting member disposed on a part of the electromagnetic steel plates in a laminating direction, and having a thickness larger than a thickness of each electromagnetic steel plate, and the rotational balance adjusting member is processed to adjust rotational balance.
- the rotational balance adjusting member is made of a magnetic material, for example, iron, and hence magnetic force resulting from magnetic induction is strengthened. This contributes to improvement of performance as a turbo charger with improvement of performance as an electric motor.
- the rotor core is preferably configured such that the rotational balance adjusting member is interposed on an intermediate part in the laminating direction of the laminated electromagnetic steel plates.
- the rotational balance adjusting member is interposed on the intermediate part in the laminating direction of the laminated electromagnetic steel plates, particularly on a central part is referred to as a center ring.
- the rotational balance adjusting member that is interposed on the intermediate part in the laminating direction of the laminated electromagnetic steel plates, particularly on the central part, and hence magnetic induction on the both sides of the rotational balance adjusting member is uniformed, thereby improving output as a motor.
- the rotor core preferably includes the sleeve fitted onto the shaft, the plurality of electromagnetic steel plates fitted onto the sleeve, and arranged as a lamination, and a rotational balance adjusting member fixed to both ends of the sleeve, and configured to fix and sandwich the plurality of electromagnetic steel plates.
- the rotor core preferably includes a rotational balance adjusting member fitted onto the sleeve, and interposed on an intermediate part in the laminating direction of the plurality of electromagnetic steel plates that are arranged as a lamination, and a rotational balance adjusting member configured to fix and sandwich both ends of the laminated electromagnetic steel plates, and fixed to both ends of the sleeve.
- the rotational balance adjustment portions are fixed to the both ends and the intermediate part of the sleeve, and the number of the adjustment portions increases. Therefore, even when rotational balance adjustment singly using the rotor core that requires a large number of steps is omitted, and merged into final rotational balance adjustment after the assembly of the rotor, an adjustment amount can be greatly expanded. Consequently, high accurate rotational balance adjustment is possible.
- At least one balance adjustment member of the balance adjustment members is preferably configured by assembling laminated layers of the same magnetic material as the electromagnetic steel plates of the rotor core.
- the center ring is made of, for example, an electromagnetic steel plate being a magnetic material or iron, and hence magnetic force resulting from magnetic induction is strengthened.
- an electromagnetic steel plate being a magnetic material or iron
- magnetic force resulting from magnetic induction is strengthened.
- the electromagnetic steel plate is used for the center ring, and hence assembly of the center ring is completed in a step of assembling the electromagnetic steel plates of the rotor core. Consequently, the number of assembly steps can be further reduced.
- the turbocharging device incorporating an electric motor is preferably either a turbo charger incorporating a motor generator that is mounted with a turbine wheel, which is a rotor blade for utilizing exhaust gas energy on an end of the shaft penetrated by the rotor core and the bearing, and that is mounted with a compressor impeller, which is a rotor blade for compressing inlet air on other end thereof, or an electric supercharger that does not have the turbine wheel and that is mounted with a compressor impeller for compressing inlet air only on one end of the shaft.
- a rotational balance adjusting method for a rotor of a turbo charger incorporating a motor generator includes the steps of: performing rotational balance adjustment by singly using a rotor blade, for example, such as a turbine wheel, and a compressor impellor; assembling a rotor including the turbine wheel, the compressor impellor, and a rotor core having a rotational balance adjusting member made of a magnetic material; measuring a balance amount by rotating the rotor; and adjusting and processing rotational balance by using an compressor fastening nut, the rotational balance adjusting member of the rotor core, or both of the compressor fastening nut and the rotational balance adjusting member, on the basis of a result of measurement.
- the compressor fastening nut and the rotational balance adjusting member of the rotor core enable the rotational balance adjustment portions, and increase in the number of the adjustment portions and fine adjustment are possible. Consequently, even when rotational balance adjustment singly using the rotor core that requires a large number of steps is omitted, and merged into final rotational balance adjustment after the assembly of the rotor, high accurate rotational balance adjustment is possible.
- a step of adjusting rotational balance by singly using the rotor core before the step of assembling the rotor may be further added.
- the step of adjusting rotational balance by singly using the rotor core is further added, and hence it is possible to obtain the rotor with higher accurate rotational balance.
- rotational balance has been adjusted by cutting a nut for fastening a shaft on a compressor impeller
- the rotational balance adjusting member enabling balance adjustment is added to the rotor core in addition to the nut part, so that the number of portions where the rotational balance is adjusted increases, thereby enabling higher accurate rotational balance adjustment.
- the rotational balance adjusting member is made of a magnetic material, for example, iron, and hence magnetic force resulting from magnetic induction is strengthened. This contributes to improvement of performance as a turbo charger with improvement of performance as an electric motor.
- FIG. 1 is a schematic structure diagram of a turbine rotor according to a first embodiment of the present invention
- FIG. 2 is a schematic structure diagram of a turbine rotor according to a second embodiment of the present invention.
- FIG. 3 is a schematic structure diagram of a turbine rotor according to a third embodiment of the present invention.
- FIG. 4 is a flowchart of processes of rotational balance adjustment work of the turbine rotor according to the first embodiment of the present invention
- FIG. 5 is a flowchart of processes of another rotational balance adjustment work of the turbine rotor according to the first embodiment of the present invention
- FIG. 6 shows a schematic configuration diagram of an engine mounted with a conventional turbo charger incorporating a motor generator
- FIG. 7 shows a schematic explanatory diagram of a conventional turbine rotor.
- a turbine rotor according to a first embodiment of the present invention will be described with reference to FIG. 1 .
- a turbine rotor 1 includes a shaft 4 , a turbine wheel 2 disposed on one end of the shaft 4 , a compressor impeller 3 disposed on the other end thereof, two bearings 7 disposed between the turbine wheel 2 and the compressor impeller 3 at intervals, and a rotor core 5 that serves as an electric rotor, and is disposed between the two bearings 7 , and the rotor core 5 is mounted on the shaft 4 via a sleeve 53 .
- the present invention is applicable to both of a case where the respective bearings 7 are arranged on both outer ends of the rotor core 5 as described above, and a case where the two (pair of) bearings 7 are arranged between the turbine wheel 2 and the rotor core 5 at intervals.
- the shaft 4 is a solid shaft, has a stepped part 44 narrowed from an intermediate part, and is a rotary shaft having a thick portion 41 on one end and a narrow portion 42 on the other end.
- the turbine wheel 2 that is driven by exhaust gas is fixed to the end of the thick portion 41 of the shaft 4 .
- the bearing 7 fixed to a bearing support part formed in a turbine housing (not shown) is disposed on a back surface side of the turbine wheel 2 via a first seal ring 43 formed integrally with the shaft 4 .
- the rotor core 5 that incorporates the sleeve 53 is fitted onto the narrow portion 42 of the shaft 4 by employing, as a stopper, the stepped part 44 being a stopper part.
- the rotor core 5 is configured such that a plurality of electromagnetic steel plates 51 having circular circumference are inserted around the sleeve 53 to be laminated in the plate thickness direction of the electromagnetic steel plates 51 .
- a center ring 52 that is a rotational balance adjusting member, and is made of an electromagnetic steel plate being a magnetic material, or iron is interposed between the electromagnetic steel plates on the intermediate part, particularly the central part, in the laminating direction of the laminated electromagnetic steel plates 51 .
- the rotor core 5 has a structure of regulating relative movement in the rotational direction with the shaft 4 by application of proper pressing by the second seal ring 46 interposed between the nut 31 and the rotor core 5 .
- the bearings 7 disposed between the rotor core 5 and the compressor impeller 3 is fitted onto the sleeve 45 .
- the center ring 52 serves as an adjustment cut part of the rotational balance of the turbine rotor 1 , in addition to the nut 31 , thereby increasing an adjustment range of the rotational balance.
- the center ring 52 has a diameter larger than that of the nut 31 , and hence effects of the balance adjustment of the center ring 52 is larger even if the cutting amount is unchanged, and high accurate adjustment is possible in a wide range. Furthermore, fine adjustment is possible.
- the rotational balance adjusting member made of an electromagnetic steel plate or iron is disposed on the intermediate part, particularly on the central part, of the laminated electromagnetic steel plates 51 , and hence magnetic induction amounts on the both sides of the rotational balance adjusting member are uniformed, thereby exerting an effect of improving output as a motor.
- the center ring 52 that serves as the rotational balance adjusting member is disposed on the intermediate part, particularly on the central part, in the laminating direction of the electromagnetic steel plates 51 .
- an action effect as the rotational balance adjusting member can be obtained.
- the rotational balance adjustment of the turbine wheel 2 and the compressor impeller 3 is performed (cut) on the rear side of the rear side (X part (see FIG. 1 )) of the turbine wheel 2 and on the rear side of the rear side (Y part (see FIG. 1 )) of the compressor impeller 3 .
- Step S 3 of assembling the turbine rotor 1 by mounting the turbine wheel 2 , the compressor impeller 3 , the rotor core 5 , the bearings 7 , the sleeve 45 , and the like on the shaft 4 .
- Step S 5 the cutting work order as to which cutting work is first performed, the cutting work of the nut 31 or the cutting work of the center ring 52 may be determined every time the cutting work is performed.
- Step S 6 the balance adjustment is terminated by Step S 6 of confirming the balance of the turbine rotor 1 .
- Step S 6 In a case where the result of measurement in Step S 6 is not an arbitrary balance amount or less, Step S 5 and Step S 6 are repeatedly performed.
- the adjustment portions for rotational balance of the assembled turbine rotor 1 are the balance adjustment A of the nut 31 , and the balance adjustment B of the center ring 52 , and hence the balance adjustment amount is increases with increase in the balance adjustment portions, and high accurate balance adjustment is possible in a wide range. Furthermore, fine adjustment is also possible.
- the center ring 52 has a diameter lager than that of the nut 31 , and hence the effects of the balance adjustment of the center ring 52 are larger even if the cutting amount is unchanged. Accordingly, the cutting work of the nut 31 can be sometimes omitted by first performing the adjustment cutting of the center ring 52 , and reduction in the number of processes can be expected.
- the rotational balance adjustment of the turbine wheel 2 and the compressor impeller 3 is performed on the rear side (X part) of the turbine wheel 2 and on the rear side (Y part) of the compressor impeller 3 .
- Step S 13 of assembling the turbine rotor 1 by mounting the turbine wheel 2 , the compressor impeller 3 , the rotor core 5 , the bearings 7 , the sleeve 45 , and the like on the shaft 4 .
- Step S 15 the cutting work order as to which cutting work is first performed, the cutting work of the nut 31 or the cutting work of the center ring 52 may be determined every time the cutting work is performed.
- Step S 16 the balance adjustment is performed by Step S 16 of confirming the balance of the turbine rotor 1 .
- Step S 16 In a case where the result of measurement in Step S 16 is an arbitrary balance amount or more, Step S 15 and Step S 16 are repeatedly performed.
- a rotor core 8 is configured such that a plurality of electromagnetic steel plates 51 are disposed on a sleeve 81 fitted onto a narrow portion 42 of a shaft 4 .
- the sleeve 81 is formed with a flange part 82 radially from an open edge on one end side of the sleeve 81 .
- the electromagnetic steel plates 51 are fitted onto the sleeve 81 so as to be laminated in the thrust direction of the sleeve 81 .
- a pressing ring 83 is fitted onto the outer peripheral part of the sleeve 81 to be fixed in caulking to the sleeve 81 in a state of pressing the electromagnetic steel plates 51 in the thrust direction.
- a center target 55 having an outer diameter substantially identical with that of the electromagnetic steel plates 51 , and a thickness larger than that of each electromagnetic steel plate 51 is disposed between the electromagnetic steel plates 51 and the flange part 82 .
- the center target 55 is a part of a revolution speed detection unit used in a case where the revolution speed of the turbine rotor 1 is controlled. In a case where the revolution speed does not need to be detected, the center target 55 is unnecessary.
- the rotor core 8 is pressed against a stepped part 44 via a compressor impeller 3 and a sleeve 45 by a nut 43 , thereby preventing slip in the rotational direction with respect to the shaft 4 .
- the flange part 82 and the pressing ring 83 each have an outer diameter substantially identical with that of each electromagnetic steel plate 51 , and have an action as a rotational balance adjusting member.
- the electromagnetic steel plates 51 are fitted onto the sleeve 81 in a laminated manner, and the both sides of the electromagnetic steel plates 51 are sandwiched between the flange part 82 and the pressing ring 83 , thereby facilitating assembly of the shaft 4 and improving the quality of the assembly.
- a balance adjustment part C of the flange part 82 , and a balance adjustment part D of the pressing ring 83 serve as rotational balance adjustment portions, in addition to a balance adjustment part A of the nut 43 , thereby increasing an adjustment amount of the rotational balance, and enabling fine adjustment.
- a rotor core 9 is configured such that a plurality of electromagnetic steel plates 51 and a center ring 52 being a rotational balance adjusting member are disposed on a sleeve 81 fitted onto a narrow portion 42 of a shaft 4 .
- the sleeve 81 is formed with a flange part 82 radially from an open edge on the one end side of the sleeve 81 .
- the electromagnetic steel plates 51 are fitted onto the sleeve 81 so as to be laminated in the thrust direction of the sleeve 81 .
- the center ring 52 being a rotational balance adjusting member is disposed on the intermediate part of the laminated electromagnetic steel plates 51 in the thrust direction of the sleeve 81 , particularly on the central part.
- a pressing ring 83 is fitted onto the outer peripheral part of the sleeve 81 to be fixed in caulking to the sleeve 81 in a state of pressing the electromagnetic steel plates 51 in the thrust direction.
- the electromagnetic steel plates 51 are fitted onto the sleeve 81 in a laminated manner, and the both sides of the electromagnetic steel plates 51 are sandwiched between the flange part 82 and the pressing ring 83 , thereby forming the rotor core 8 in a cartridge-type, facilitating assembly to the shaft 4 , and improving the quality of the assembly. Additionally, both sides of the electromagnetic steel plates 51 are sandwiched between the flange part 82 and the pressing ring 83 , thereby regulating relative movement of the electromagnetic steel plates 51 and the sleeve 81 during rotation, and easily forming the rotor core 8 in a cartridge type.
- center ring 52 is interposed on the intermediate part (central part) of the laminated electromagnetic steel plates 51 , and hence magnetic induction is uniformed, thereby improving output as a motor.
- a balance adjustment part C of the flange part 82 , a balance adjustment part D of the pressing ring 83 , and a balance adjustment part B of the center ring 52 serve as rotational balance adjustment portions, in addition to a balance adjustment part A of a nut 43 , thereby increasing an adjustment amount of the rotational balance, and enabling fine adjustment.
- a motor generator is incorporated in a rotary shaft of a turbo charger that is driven by exhaust gas of the internal combustion, and compresses and turbocharges supply air, and the rotation of a compressor impeller is assisted for acceleration, thereby improving acceleration responsiveness.
- the turbo charger incorporating a motor generator is suitable for use in an internal combustion that is capable of converting exhaust gas energy into electric energy.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Power Engineering (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
An object is to increase portions (increase the amount of correction), where the rotational balance of a rotary shaft of a turbocharging device incorporating an electric motor is adjusted, and to maintain sufficient motor driving force even under a high temperature condition. In a balance adjusting structure for the turbocharging device incorporating an electric motor, a rotor core 5 formed by laminating electromagnetic steel plates 51 is interposed between rotor blades provided on one end or both ends, a rotational balance adjusting member made of iron (magnetic induction member) having a thickens larger than the thickness of each electromagnetic steel plate 51 is disposed on an end of the laminated electromagnetic steel plates 51, or between the laminated layers.
Description
- The present invention relates to a structure and a method for adjusting rotational balance of a rotor of a turbocharging device incorporating an electric motor turbocharging suction air to an internal combustion. Herein, the turbocharging device incorporating an electric motor includes a turbo charger incorporating a motor generator, a turbo charger incorporating an electric motor, an electric supercharger, and the like.
- Turbo chargers for compressing and turbocharging suction air by driving with exhaust gas of an internal combustion has been widely used, in order to improve output of the internal combustion.
- There has been used a turbo charger incorporating a motor generator that improves acceleration responsiveness by incorporating an electric motor in a rotary shaft of the turbocharging device and assisting the acceleration of rotation of a compressor impeller, and collects energy by converting exhaust gas energy into electric energy. In a case where exhaust gas energy is not utilized and a turbine is omitted, the turbo charger incorporating a motor generator is an electric supercharger that rotates a compressor impeller by only an electric motor.
-
FIG. 6 is a schematic configuration diagram of anengine 01 mounted with aturbo charger 03 incorporating a motor generator disclosed in Japanese Patent Application Laid-open No. H8-182382 (Patent Document 1). Aturbine wheel 031 of the turbo charger incorporating amotor generator 03 is driven by exhaust gas from anexhaust manifold 011 of theengine 01. Acompressor impeller 032 coaxially connected to theturbine wheel 031 is driven, so that suction air from an air cleaner (not shown) is supplied to theengine 01 via asuction manifold 012. - A
motor rotor 05 for assisting rotation (driving) of thecompressor impeller 032 is disposed on the intermediate-portion of ashaft 041 for connecting theturbine wheel 031 and thecompressor impeller 032. - As shown in
FIG. 7 , themotor rotor 05 is axially rotatably supported on a pair of bearing support parts provided in a housing (not shown) of the turbo charger incorporating amotor generator 03 viabearings 049. -
Reference numeral 06 denotes an engine control unit (ECU), which controls operation of theengine 01, flows a current to astator 033 depending on the operation status of theengine 1, and also controls operation of the turbo charger incorporating amotor generator 03.Reference numeral 07 denotes a battery, which is a power supply of a controller. -
FIG. 7 is a schematic configuration diagram of a conventional motor rotor. - A
motor rotor 05 has astep part 044 that is a narrow shaft part on a side closer to acompressor impeller 043, on an intermediate part in the thrust direction of ashaft 041 having an end mounted with aturbine wheel 042. Anut 046, which is screwed with a screw part formed on the end of the narrow shaft part, through athrust bush 056, arotor 051, anoil seal accessory 054, and thecompressor impeller 043 which are fitted with (fitted onto) the narrow shaft part, presses and positions these components with respect to thestep part 044. - A magnet 052 (permanent magnet) is fitted onto the narrow shaft part of the
shaft 041, asleeve 057 is further fitted onto the outer peripheral part of themagnet 052 to be fixed to the narrow shaft part of theshaft 041, thereby forming therotor 051. - In this case, the
sleeve 057 needs to be fitted onto the outer peripheral part of the magnet arranged on therotor 051, in order to prevent breakage and scattering of the magnet. - A
stator 033 for rotating and driving theshaft 041 by utilizing magnetism of the magnet of therotor 051 is arranged on the housing side of the turbo charger incorporating amotor generator 03, facing therotor 051. - As a technology related to such a turbo charger incorporating a motor generator, Japanese Patent Application Laid-open No. 2000-145468 (Patent Document 2) is known.
- Patent Document 1: Japanese Patent Application Laid-open No. H8-182382
- Patent Document 2: Japanese Patent Application Laid-open No. 2000-145468
- However, since the turbo charger incorporating a motor generator is used under a high temperature environment resulting from exhaust gas, performance of a motor that utilizes a magnet significantly deteriorates with rise in temperature, and such a motor is not suitable.
- To cope with this, there is a magnetic inductor type motor as one of motors that do not use a magnet.
- The magnetic inductor type motor is configured that a rotor made of laminated electromagnetic steel plates and iron, or laminated electromagnetic steel plates are driven by a stator arranged around the rotor.
- However, since the rotor rotates at a high speed in a state of being arranged between a turbine wheel and a compressor impeller, it is important to adjust the rotational balance (dynamic balance) of the rotor made of the laminated electromagnetic steel plates and iron, or the laminated electromagnetic steel plates for balancing. Therefore, the adjustment of the rotational balance on a conventional adjustment part (e.g., a nut part for fastening the compressor impeller to a rotary shaft of the turbo charger) can not cope with increase in an adjustment amount, or fine adjustment.
- The present invention has been conceived in order to solve such problems, and an object thereof is to provide a structure and a method for adjusting balance of a turbo charger incorporating a motor generator capable of achieving increase in adjustment parts (increase in an adjustment amounts and ensuring fine adjustment) for adjusting the rotational balance of a rotary shaft of the turbo charger, and preventing performance deterioration while maintaining sufficient motor driving force even under a high temperature condition.
- According to the present invention, in order to attain this object, a balance adjusting structure for a turbocharging device incorporating an electric motor includes: at least one rotor blade disposed in a housing; a shaft connected to the rotor blade; a bearing formed in the housing, and configured to rotatably axially support the shaft; a rotor core penetrated by the shaft; and a stator disposed at a position facing the rotor core in the housing, and configured to rotate and drive the rotor core together with the shaft by a magnetic field, wherein the rotor core has a sleeve fitted onto the shaft, a plurality of electromagnetic steel plates laminated in an axial direction of the sleeve and fitted onto the sleeve, and a rotational balance adjusting member disposed on a part of the electromagnetic steel plates in a laminating direction, and having a thickness larger than a thickness of each electromagnetic steel plate, and the rotational balance adjusting member is processed to adjust rotational balance.
- With such a configuration, although heretofore, rotational balance has been adjusted by cutting a nut for fastening a shaft on a compressor impeller being a rotor blade of the turbocharging device incorporating an electric motor, the rotational balance adjusting member enabling balance adjustment is added in addition to the nut part, so that the number of portions where the rotational balance is adjusted increases, thereby enabling higher accurate rotational balance adjustment.
- Additionally, the rotational balance adjusting member is made of a magnetic material, for example, iron, and hence magnetic force resulting from magnetic induction is strengthened. This contributes to improvement of performance as a turbo charger with improvement of performance as an electric motor.
- In the present invention, the rotor core is preferably configured such that the rotational balance adjusting member is interposed on an intermediate part in the laminating direction of the laminated electromagnetic steel plates.
- The rotational balance adjusting member is interposed on the intermediate part in the laminating direction of the laminated electromagnetic steel plates, particularly on a central part is referred to as a center ring.
- Thus, the rotational balance adjusting member that is interposed on the intermediate part in the laminating direction of the laminated electromagnetic steel plates, particularly on the central part, and hence magnetic induction on the both sides of the rotational balance adjusting member is uniformed, thereby improving output as a motor.
- In the present invention, the rotor core preferably includes the sleeve fitted onto the shaft, the plurality of electromagnetic steel plates fitted onto the sleeve, and arranged as a lamination, and a rotational balance adjusting member fixed to both ends of the sleeve, and configured to fix and sandwich the plurality of electromagnetic steel plates.
- With such a configuration, it is possible to form the rotor core in a cartridge-type, and facilitate assembly to the shaft. Additionally, the rotational balance adjustment portions are fixed to the both ends of the sleeve, and the number of the adjustment portions are increased, and hence an adjustment capacity in final rotational balance adjustment after the assembly to the rotor increases, and fine adjustment is possible. Consequently, high accurate rotational balance adjustment is possible.
- In the present invention, the rotor core preferably includes a rotational balance adjusting member fitted onto the sleeve, and interposed on an intermediate part in the laminating direction of the plurality of electromagnetic steel plates that are arranged as a lamination, and a rotational balance adjusting member configured to fix and sandwich both ends of the laminated electromagnetic steel plates, and fixed to both ends of the sleeve.
- With such a configuration, it is possible to form the rotor core in a cartridge-type, and facilitate assembly to the shaft. Additionally, the rotational balance adjustment portions are fixed to the both ends and the intermediate part of the sleeve, and the number of the adjustment portions increases. Therefore, even when rotational balance adjustment singly using the rotor core that requires a large number of steps is omitted, and merged into final rotational balance adjustment after the assembly of the rotor, an adjustment amount can be greatly expanded. Consequently, high accurate rotational balance adjustment is possible.
- In the present invention, at least one balance adjustment member of the balance adjustment members is preferably configured by assembling laminated layers of the same magnetic material as the electromagnetic steel plates of the rotor core.
- With such a configuration, as the rotational balance adjusting member interposed on the intermediate part in the laminating direction of the laminated electromagnetic steel plates, particularly on the central part, the center ring is made of, for example, an electromagnetic steel plate being a magnetic material or iron, and hence magnetic force resulting from magnetic induction is strengthened. This enables contribution to improvement of performance as a turbocharging device incorporating an electric motor with improvement of performance as an electric motor. Furthermore, the electromagnetic steel plate is used for the center ring, and hence assembly of the center ring is completed in a step of assembling the electromagnetic steel plates of the rotor core. Consequently, the number of assembly steps can be further reduced.
- In the present invention, the turbocharging device incorporating an electric motor is preferably either a turbo charger incorporating a motor generator that is mounted with a turbine wheel, which is a rotor blade for utilizing exhaust gas energy on an end of the shaft penetrated by the rotor core and the bearing, and that is mounted with a compressor impeller, which is a rotor blade for compressing inlet air on other end thereof, or an electric supercharger that does not have the turbine wheel and that is mounted with a compressor impeller for compressing inlet air only on one end of the shaft.
- Furthermore, according to the present invention, a rotational balance adjusting method for a rotor of a turbo charger incorporating a motor generator includes the steps of: performing rotational balance adjustment by singly using a rotor blade, for example, such as a turbine wheel, and a compressor impellor; assembling a rotor including the turbine wheel, the compressor impellor, and a rotor core having a rotational balance adjusting member made of a magnetic material; measuring a balance amount by rotating the rotor; and adjusting and processing rotational balance by using an compressor fastening nut, the rotational balance adjusting member of the rotor core, or both of the compressor fastening nut and the rotational balance adjusting member, on the basis of a result of measurement.
- With such a configuration, the compressor fastening nut and the rotational balance adjusting member of the rotor core enable the rotational balance adjustment portions, and increase in the number of the adjustment portions and fine adjustment are possible. Consequently, even when rotational balance adjustment singly using the rotor core that requires a large number of steps is omitted, and merged into final rotational balance adjustment after the assembly of the rotor, high accurate rotational balance adjustment is possible.
- In the present invention, a step of adjusting rotational balance by singly using the rotor core before the step of assembling the rotor may be further added.
- Thus, the step of adjusting rotational balance by singly using the rotor core is further added, and hence it is possible to obtain the rotor with higher accurate rotational balance.
- According to the present invention, although heretofore, rotational balance has been adjusted by cutting a nut for fastening a shaft on a compressor impeller, the rotational balance adjusting member enabling balance adjustment is added to the rotor core in addition to the nut part, so that the number of portions where the rotational balance is adjusted increases, thereby enabling higher accurate rotational balance adjustment.
- Additionally, the rotational balance adjusting member is made of a magnetic material, for example, iron, and hence magnetic force resulting from magnetic induction is strengthened. This contributes to improvement of performance as a turbo charger with improvement of performance as an electric motor.
-
FIG. 1 is a schematic structure diagram of a turbine rotor according to a first embodiment of the present invention; -
FIG. 2 is a schematic structure diagram of a turbine rotor according to a second embodiment of the present invention; -
FIG. 3 is a schematic structure diagram of a turbine rotor according to a third embodiment of the present invention; -
FIG. 4 is a flowchart of processes of rotational balance adjustment work of the turbine rotor according to the first embodiment of the present invention; -
FIG. 5 is a flowchart of processes of another rotational balance adjustment work of the turbine rotor according to the first embodiment of the present invention; -
FIG. 6 shows a schematic configuration diagram of an engine mounted with a conventional turbo charger incorporating a motor generator; and -
FIG. 7 shows a schematic explanatory diagram of a conventional turbine rotor. - Hereinafter, embodiments of the present invention will be described in detail with reference to the figures.
- As specific names of a rotor blade, a turbine wheel, and a compressor impeller are used in the description of these embodiments. Additionally, as long as not stated specifically in particular, size, quality of materials, shape, relative arrangement of components described in these embodiments are not intended to limit the scope of the invention, but merely exemplary examples.
- A turbine rotor according to a first embodiment of the present invention will be described with reference to
FIG. 1 . - A
turbine rotor 1 includes ashaft 4, aturbine wheel 2 disposed on one end of theshaft 4, acompressor impeller 3 disposed on the other end thereof, twobearings 7 disposed between theturbine wheel 2 and thecompressor impeller 3 at intervals, and arotor core 5 that serves as an electric rotor, and is disposed between the twobearings 7, and therotor core 5 is mounted on theshaft 4 via asleeve 53. - The present invention is applicable to both of a case where the
respective bearings 7 are arranged on both outer ends of therotor core 5 as described above, and a case where the two (pair of)bearings 7 are arranged between theturbine wheel 2 and therotor core 5 at intervals. - The
shaft 4 is a solid shaft, has a steppedpart 44 narrowed from an intermediate part, and is a rotary shaft having athick portion 41 on one end and anarrow portion 42 on the other end. Theturbine wheel 2 that is driven by exhaust gas is fixed to the end of thethick portion 41 of theshaft 4. Thebearing 7 fixed to a bearing support part formed in a turbine housing (not shown) is disposed on a back surface side of theturbine wheel 2 via afirst seal ring 43 formed integrally with theshaft 4. - The
rotor core 5 that incorporates thesleeve 53 is fitted onto thenarrow portion 42 of theshaft 4 by employing, as a stopper, the steppedpart 44 being a stopper part. Therotor core 5 is configured such that a plurality ofelectromagnetic steel plates 51 having circular circumference are inserted around thesleeve 53 to be laminated in the plate thickness direction of theelectromagnetic steel plates 51. Acenter ring 52 that is a rotational balance adjusting member, and is made of an electromagnetic steel plate being a magnetic material, or iron is interposed between the electromagnetic steel plates on the intermediate part, particularly the central part, in the laminating direction of the laminatedelectromagnetic steel plates 51. - On a side closer to the
compressor impeller 3 of therotor core 5,sleeve 45 fitted onto thenarrow portion 42 of theshaft 4 abuts. On the other end of theshaft 4, thecompressor impeller 3 is fixed with anut 31 for fastening via asecond seal ring 46. - Accordingly, the
rotor core 5 has a structure of regulating relative movement in the rotational direction with theshaft 4 by application of proper pressing by thesecond seal ring 46 interposed between thenut 31 and therotor core 5. - The
bearings 7 disposed between therotor core 5 and thecompressor impeller 3 is fitted onto thesleeve 45. - With such a configuration, the
center ring 52 serves as an adjustment cut part of the rotational balance of theturbine rotor 1, in addition to thenut 31, thereby increasing an adjustment range of the rotational balance. - Additionally, the
center ring 52 has a diameter larger than that of thenut 31, and hence effects of the balance adjustment of thecenter ring 52 is larger even if the cutting amount is unchanged, and high accurate adjustment is possible in a wide range. Furthermore, fine adjustment is possible. - Moreover, the rotational balance adjusting member made of an electromagnetic steel plate or iron is disposed on the intermediate part, particularly on the central part, of the laminated
electromagnetic steel plates 51, and hence magnetic induction amounts on the both sides of the rotational balance adjusting member are uniformed, thereby exerting an effect of improving output as a motor. - In this embodiment, the
center ring 52 that serves as the rotational balance adjusting member is disposed on the intermediate part, particularly on the central part, in the laminating direction of theelectromagnetic steel plates 51. However, also in a case where thecenter ring 52 is disposed on any portion in the laminating direction other than the central part, an action effect as the rotational balance adjusting member can be obtained. - The correction portion for adjusting the rotational balance of the
turbine rotor 1 has been described. Now, description will cover a flow of processes of a rotational balance adjusting method of theturbine rotor 1 shown inFIG. 4 . - Step S1 of setting the
turbine wheel 2 in the balance measurement device, measuring a rotational balance amount, and performing balance adjustment of thesingle turbine wheel 2 on the basis of a result of the measurement. - Next, Step S2 of setting the
compressor impeller 3 in the balance measurement device, and performing balance adjustment of thesingle compressor impeller 3 similarly to Step S1. - The rotational balance adjustment of the
turbine wheel 2 and thecompressor impeller 3 is performed (cut) on the rear side of the rear side (X part (seeFIG. 1 )) of theturbine wheel 2 and on the rear side of the rear side (Y part (seeFIG. 1 )) of thecompressor impeller 3. - Step S3 of assembling the
turbine rotor 1 by mounting theturbine wheel 2, thecompressor impeller 3, therotor core 5, thebearings 7, thesleeve 45, and the like on theshaft 4. - Step S4 of setting the assembled
turbine rotor 1 in the balance measurement device, and measuring a balance amount of the whole of theturbine rotor 1. - Step S5 of performing balance adjustment by cutting work of a balance adjustment part A of the
nut 43 for fastening the compressor impeller or cutting work of a balance adjustment part B of the outer peripheral part of thecenter ring 52, on the basis of a result of measurement. - Furthermore, in Step S5, the cutting work order as to which cutting work is first performed, the cutting work of the
nut 31 or the cutting work of thecenter ring 52 may be determined every time the cutting work is performed. - Then, the
turbine rotor 1 is set in the balance measurement, device again, the balance adjustment is terminated by Step S6 of confirming the balance of theturbine rotor 1. - In a case where the result of measurement in Step S6 is not an arbitrary balance amount or less, Step S5 and Step S6 are repeatedly performed.
- Since various balance measurement devices are disclosed in patent documents (e.g., Japanese Patent Application Laid-open Nos. 2008-58008 and 2008-8219) and the like, description of the balance measurement device will be omitted in this embodiment.
- According to the flow of the processes of the rotational balance adjusting method of the
turbine rotor 1 of this embodiment, the adjustment portions for rotational balance of the assembledturbine rotor 1 are the balance adjustment A of thenut 31, and the balance adjustment B of thecenter ring 52, and hence the balance adjustment amount is increases with increase in the balance adjustment portions, and high accurate balance adjustment is possible in a wide range. Furthermore, fine adjustment is also possible. - Moreover, the
center ring 52 has a diameter lager than that of thenut 31, and hence the effects of the balance adjustment of thecenter ring 52 are larger even if the cutting amount is unchanged. Accordingly, the cutting work of thenut 31 can be sometimes omitted by first performing the adjustment cutting of thecenter ring 52, and reduction in the number of processes can be expected. - Now, a flow of processes of another rotational balance adjusting method of the
turbine rotor 1 will be described with reference toFIG. 5 . - Step S10 of setting the
turbine wheel 2 in the balance measurement device, measuring a rotational balance amount, and performing balance adjustment of thesingle turbine wheel 2 on the basis of a result of the measurement. - Next, Step S11 of setting the
compressor impeller 3 in the balance measurement device, and performing balance adjustment of thesingle compressor impeller 3 similarly to Step S10. - Then, Step S12 of setting the
rotor core 5 in the balance measurement device, and performing balance adjustment of thesingle rotor core 5 similarly to Step S10. - The rotational balance adjustment of the
turbine wheel 2 and thecompressor impeller 3 is performed on the rear side (X part) of theturbine wheel 2 and on the rear side (Y part) of thecompressor impeller 3. - Step S13 of assembling the
turbine rotor 1 by mounting theturbine wheel 2, thecompressor impeller 3, therotor core 5, thebearings 7, thesleeve 45, and the like on theshaft 4. - Step S14 of setting the assembled
turbine rotor 1 in the balance measurement device, and measuring a balance amount of the whole of theturbine rotor 1. - Step S15 of performing balance adjustment by cutting work of the balance adjustment part A of the
nut 43 for fastening the compressor impeller or cutting work of the balance adjustment part B of the outer peripheral part of thecenter ring 52, on the basis of a result of measurement. - In Step S15, the cutting work order as to which cutting work is first performed, the cutting work of the
nut 31 or the cutting work of thecenter ring 52 may be determined every time the cutting work is performed. - Then, the
turbine rotor 1 is set in the balance measurement device again, the balance adjustment is performed by Step S16 of confirming the balance of theturbine rotor 1. - In a case where the result of measurement in Step S16 is an arbitrary balance amount or more, Step S15 and Step S16 are repeatedly performed.
- In this embodiment, according to the flow of the processes of the rotational balance adjusting method of the
turbine rotor 1, rotational balance adjustment of thesingle rotor core 5 that is the heaviest among the components is performed, and hence the rotational balance adjustment amount of the assembledturbine rotor 1 is reduced, and balance adjustment performed after theturbine rotor 1 is assembled is facilitated. - In this second embodiment, components that are identical with those of the first embodiment are denoted by the same reference numerals, and description thereof will be omitted.
- As shown in
FIG. 2 , arotor core 8 is configured such that a plurality ofelectromagnetic steel plates 51 are disposed on asleeve 81 fitted onto anarrow portion 42 of ashaft 4. - The
sleeve 81 is formed with aflange part 82 radially from an open edge on one end side of thesleeve 81. - On the outer peripheral part of the
sleeve 81, theelectromagnetic steel plates 51 are fitted onto thesleeve 81 so as to be laminated in the thrust direction of thesleeve 81. - On the other end side of the
sleeve 81, apressing ring 83 is fitted onto the outer peripheral part of thesleeve 81 to be fixed in caulking to thesleeve 81 in a state of pressing theelectromagnetic steel plates 51 in the thrust direction. - Additionally, a
center target 55 having an outer diameter substantially identical with that of theelectromagnetic steel plates 51, and a thickness larger than that of eachelectromagnetic steel plate 51 is disposed between theelectromagnetic steel plates 51 and theflange part 82. Thecenter target 55 is a part of a revolution speed detection unit used in a case where the revolution speed of theturbine rotor 1 is controlled. In a case where the revolution speed does not need to be detected, thecenter target 55 is unnecessary. - The
rotor core 8 is pressed against a steppedpart 44 via acompressor impeller 3 and asleeve 45 by anut 43, thereby preventing slip in the rotational direction with respect to theshaft 4. - The
flange part 82 and thepressing ring 83 each have an outer diameter substantially identical with that of eachelectromagnetic steel plate 51, and have an action as a rotational balance adjusting member. - The processes of a rotational balance adjusting method is similar to those of the first embodiment, and therefore description thereof will be omitted.
- The
electromagnetic steel plates 51 are fitted onto thesleeve 81 in a laminated manner, and the both sides of theelectromagnetic steel plates 51 are sandwiched between theflange part 82 and thepressing ring 83, thereby facilitating assembly of theshaft 4 and improving the quality of the assembly. - Furthermore, a balance adjustment part C of the
flange part 82, and a balance adjustment part D of thepressing ring 83 serve as rotational balance adjustment portions, in addition to a balance adjustment part A of thenut 43, thereby increasing an adjustment amount of the rotational balance, and enabling fine adjustment. - In this third embodiment, components that are identical with those of the first and second embodiments are denoted by the same reference numerals, and description thereof will be omitted.
- As shown in
FIG. 3 , arotor core 9 is configured such that a plurality ofelectromagnetic steel plates 51 and acenter ring 52 being a rotational balance adjusting member are disposed on asleeve 81 fitted onto anarrow portion 42 of ashaft 4. - The
sleeve 81 is formed with aflange part 82 radially from an open edge on the one end side of thesleeve 81. - On the outer peripheral part of the
sleeve 81, theelectromagnetic steel plates 51 are fitted onto thesleeve 81 so as to be laminated in the thrust direction of thesleeve 81. Thecenter ring 52 being a rotational balance adjusting member is disposed on the intermediate part of the laminatedelectromagnetic steel plates 51 in the thrust direction of thesleeve 81, particularly on the central part. On the other end side of thev sleeve 81, apressing ring 83 is fitted onto the outer peripheral part of thesleeve 81 to be fixed in caulking to thesleeve 81 in a state of pressing theelectromagnetic steel plates 51 in the thrust direction. - The processes of a rotational balance adjusting method is similar to those of the first embodiment, and therefore description thereof will be omitted.
- The
electromagnetic steel plates 51 are fitted onto thesleeve 81 in a laminated manner, and the both sides of theelectromagnetic steel plates 51 are sandwiched between theflange part 82 and thepressing ring 83, thereby forming therotor core 8 in a cartridge-type, facilitating assembly to theshaft 4, and improving the quality of the assembly. Additionally, both sides of theelectromagnetic steel plates 51 are sandwiched between theflange part 82 and thepressing ring 83, thereby regulating relative movement of theelectromagnetic steel plates 51 and thesleeve 81 during rotation, and easily forming therotor core 8 in a cartridge type. - Furthermore, the
center ring 52 is interposed on the intermediate part (central part) of the laminatedelectromagnetic steel plates 51, and hence magnetic induction is uniformed, thereby improving output as a motor. - Moreover, a balance adjustment part C of the
flange part 82, a balance adjustment part D of thepressing ring 83, and a balance adjustment part B of thecenter ring 52 serve as rotational balance adjustment portions, in addition to a balance adjustment part A of anut 43, thereby increasing an adjustment amount of the rotational balance, and enabling fine adjustment. - In order to improve the output of an internal combustion, a motor generator is incorporated in a rotary shaft of a turbo charger that is driven by exhaust gas of the internal combustion, and compresses and turbocharges supply air, and the rotation of a compressor impeller is assisted for acceleration, thereby improving acceleration responsiveness. Additionally, the turbo charger incorporating a motor generator is suitable for use in an internal combustion that is capable of converting exhaust gas energy into electric energy.
Claims (8)
1. A balance adjusting structure for turbocharging device incorporating an electric motor, comprising:
at least one rotor blade disposed in a housing;
a shaft connected to the rotor blade;
a bearing formed in the housing, and configured to rotatably axially support the shaft;
a rotor core penetrated by the shaft; and
a stator disposed at a position facing the rotor core in the housing, and configured to rotate and drive the rotor core together with the shaft by a magnetic field, wherein
the rotor core includes:
a sleeve fitted onto the shaft;
a plurality of electromagnetic steel plates laminated in an axial direction of the sleeve and fitted onto the sleeve; and
a rotational balance adjusting member disposed on a part of the electromagnetic steel plates in a laminating direction, and having a thickness larger than a thickness of each electromagnetic steel plate, and
the rotational balance adjusting member is processed to adjust rotational balance.
2. The balance adjusting structure for a turbocharging device incorporating an electric motor according to claim 1 , wherein
the rotor core is configured such that the rotational balance adjusting member is disposed on an intermediate part of the laminated electromagnetic steel plates.
3. The balance adjusting structure for a turbocharging device incorporating an electric motor according to claim 1 , wherein
the rotor core includes:
the sleeve fitted onto the shaft;
the plurality of electromagnetic steel plates fitted onto the sleeve, and arranged as a lamination; and
a rotational balance adjusting member fixed to both ends of the sleeve, and configured to fix and sandwich the plurality of electromagnetic steel plates.
4. The balance adjusting structure for a turbocharging device incorporating an electric motor according to claim 1 , wherein
the rotor core has:
a rotational balance adjusting member fitted onto the sleeve, and interposed on an intermediate part of the plurality of electromagnetic steel plates that are arranged as a lamination; and
a rotational balance adjusting member configured to fix and sandwich both ends of the laminated electromagnetic steel plates, and fixed to both ends of the sleeve.
5. The balance adjusting structure for a turbocharging device incorporating an electric motor according to claim 1 , wherein
at least one rotational balance adjusting member of the rotational balance adjusting members is configured by assembling laminated layers of the same magnetic material as the electromagnetic steel plates of the rotor core.
6. The balance adjusting structure for a turbocharging device incorporating an electric motor according to claim 1 , wherein
the turbocharging device incorporating an electric motor is either a turbo charger incorporating a motor generator that is mounted with a turbine wheel, which is a rotor blade for utilizing exhaust gas energy on an end of the shaft penetrating the rotor core and the bearing, and that is also mounted with a compressor impeller, which is a rotor blade for compressing inlet air on other end thereof, or an electric supercharger that does not have the turbine wheel and that is mounted with a compressor impeller for compressing inlet air only on one end of the shaft.
7. A rotational balance adjusting method for a rotor of the turbocharging device incorporating an electric motor,
the method comprising the steps of:
performing rotational balance adjustment by singly using a rotor blade;
assembling a rotor including the rotor blade, and a rotor core having a rotational balance adjusting member made of a magnetic material;
measuring a balance amount by rotating the rotor; and
adjusting and processing rotational balance by using a rotor blade fastening nut, the rotational balance adjusting member of the rotor core, or both of the rotor blade fastening nut and the rotational balance adjusting member, on the basis of a result of measurement.
8. The balance adjusting method for a turbocharging device incorporating an electric motor according to claim 7 , further comprising
a step of adjusting rotational balance by singly using the rotor core before the step of assembling the rotor.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
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JP2011-127913 | 2011-06-08 | ||
JP2011127913A JP5615231B2 (en) | 2011-06-08 | 2011-06-08 | Balance adjustment structure and method of supercharger with built-in electric motor |
PCT/JP2012/064395 WO2012169463A1 (en) | 2011-06-08 | 2012-06-04 | Structure and method for adjusting balance of supercharger built into electric motor |
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US20140147306A1 true US20140147306A1 (en) | 2014-05-29 |
Family
ID=47296026
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US14/117,803 Abandoned US20140147306A1 (en) | 2011-06-08 | 2012-06-04 | Structure and method for adjusting balance of turbocharging device incorporating electric motor |
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US (1) | US20140147306A1 (en) |
EP (1) | EP2719875B1 (en) |
JP (1) | JP5615231B2 (en) |
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WO (1) | WO2012169463A1 (en) |
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Also Published As
Publication number | Publication date |
---|---|
JP5615231B2 (en) | 2014-10-29 |
EP2719875A1 (en) | 2014-04-16 |
WO2012169463A1 (en) | 2012-12-13 |
CN103620182B (en) | 2018-02-23 |
JP2012255355A (en) | 2012-12-27 |
EP2719875B1 (en) | 2018-04-04 |
CN103620182A (en) | 2014-03-05 |
EP2719875A4 (en) | 2015-12-02 |
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