doe nasafractional slot winding, that is, an odd number of coils, was used. fifteen slots were used...

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.-W//z.¢ F2x- 7/d-_-y DOE/NASA/51044-14 NASA-TM-81654 19810006949 NASA TM-81654 Edward A. Maslowski National Aeronautics and Space Administration Lewis Research Center Work performed for U.S. DEPARTMENT OF ENERGY Consewation and Solar Energy Office of Transportation Programs [i_Illii]'fI_t]PY AUG1 los< 3 t,J_. ',J "" Prepared for L.;,.o-_ ,. _,, s_-.,_.c_ c_<,r,, uc_Ar_Y, ,',, _sA Society of Automotive Engineers ,,_To,_.v,_c-.,.,^. International Congress and Exposition Detroit, Michigan, February 23-27, 1981 https://ntrs.nasa.gov/search.jsp?R=19810006949 2020-04-01T02:59:46+00:00Z

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Page 1: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

.- W//z.¢F2x-7/d-_-y

DOE/NASA/51044-14 NASA-TM-81654 19810006949NASA TM-81654

Edward A. MaslowskiNational Aeronautics and Space AdministrationLewis Research Center

Work performed forU.S. DEPARTMENT OF ENERGYConsewation and Solar EnergyOffice of Transportation Programs

[i_Illii]'fI_t]PY

AUG1 los<3 t,J_. ',J ""

Prepared for L.;,.o-_,._,,s_-.,_.c_c_<,r,,uc_Ar_Y,,',,_sASociety of Automotive Engineers ,,_To,_.v,_c-.,.,^.International Congress and ExpositionDetroit, Michigan, February 23-27, 1981

https://ntrs.nasa.gov/search.jsp?R=19810006949 2020-04-01T02:59:46+00:00Z

Page 2: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

r

NOTICE

This report was prepared to document work sponsored by the United StatesGovernment•Ne=therthe United Statesnor its agent, the UnitedStates Department ofEnergy,nor any Federalemployees,nor anyof theircontractors,subcontractorsor theiremployees, makes any warranty, express or implied, or assumes any legal liability orresponsieility fo? the accuracy, completeness, or usefulness of any information,apparatus, product or process disclosed, or represents that its use would not infringe

• privately owned rights.

Page 3: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

• DOE/NASA/51044-14NASA TM-81654

ElectronicallyCommutateddc Motors,• for Electric Vehicles

EdwardA. MaslowskiNationalAeronauticsand SpaceAdministrationLewis ResearchCenterCleveland,Ohio 44135

Work performed forU.S. DEPARTMENTOF ENERGYConservation and Solar EnergyOffice of Transportation ProgramsWashington, D.C. 20545Under Interagency Agreement DE-AI01-77CS51044

g

Prepared forSociety of Automotive EngineersInternational Congress and ExpositionDetroit, Michigan, February 23-27, 1981

Page 4: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the
Page 5: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

ELECTRONICALLY COMMUTATED dc MOTORS FOR ELECTRIC VEHICLES

Edward A. Maslowski

National Aeronautics and Space AdministrationLewis Research Center

ABSTRACT samarium-cobaltpermanent magnet material. Basedon these test results, each contractor is

A motor development program to explore the presently fabricating a refined version of itsfeasibility of electronically commutated dc motors samarium-cobaltdesign suitable for installation(also known as brushless) for electric cars is in an electric vehicle. In addition, both VPI anddescribed. Two different design concepts and a Garrett have completedstudiesto identifynumber of design variations based on these magnetic materials which may be used in place ofconcepts are discussed. One design concept is samarium-cobalt. As a result of these studies,based on a permanent magnet, medium-speed, machine ferrite materials have been identified asrated at 7000-9000 rpm and powered via a presently available magnetic materials suitabletransistor-inverter power conditioner. The other for application in these motors. A medium-speedconcept is based on a permanent magnet, version of a ferrite magnet motor is beinghigh-speed,machine rated at 22,000-26,000 rpm and fabricated and will be tested for performance. Apowered via a thyristor-inverter power preliminary design of a high-speed ferrite motorconditioner. Test results are presented for a has been completed.medium-speed motor and for a high-speed motor eachof which have been fabricated using PROGRAM GUIDELINESsamarium-cobalt permanent magnet material.

The following general guidelines were adoptedfor the motor designs: 1) the performance of avehicle using the electronicallycommutated (e.c.)motor should match that of the best currentlyavailable electric vehicles, 2) the efficiencyshould exceed the efficiency of presentlyavailable dc motors and controllers, 3) the

projected manufacturing cost in productionELECTRIC CARS AS PRESENTLY MANUFACTURED use brush quantities should make the e.c. motors competitivetype, wound field dc traction motors for with dc systems, and 4) the motor, includingpropulsion. The choice is a practical one based electronics,must be compatible with present dayon the commercial availability of motors having electric vehicles and components.the horsepower required and the capability of Based on these guidelines, the motors wereoperating over a wide speed range. The designed to supply the propulsion needed for aapplication of power electronics makes possible 1360 kg (3,000-pound) vehicle. This included thethe alternative of using a smaller, lighter, less following requirements: i) operation over thecostly ac machine. The system comprising a Schedule D driving cycle of the SAE J227a testsynchronous ac machine operated from adc source standards (1),* 2) acceleration from zero to 72.5by using electronic switching is commonly referred km/h (45 mph) in 28 seconds, 3) continuousto as an electronically commutated dc motor or a operation at 89 km/h (55 mph) for two hours, andbrushless dc motor. 4) the ability to climb a 10% grade while

As part of the DOE Electric and Hybrid maintaining 48 km/h (30 mph). In addition, twoVehicle Program, a motor development project is important assumptions were made: first, the inputbeing carried out to explore in detail the voltage would be 120 volts with 0.05 ohms internalfeasibilityof an electronically commutated dc resistance, approximating a lead-acid batterymotor attractive in performance and price to pack; and, second, that 100,000 units per year

• electric vehicle manufacturers. As part of this would constitute a viable production quantity toproject, 1) the Garrett-AiResearch Company (under be used in cost projections. Achievement of theDOE/NASA Contract DEN3-64) and 2) Virginia performance goals requires a motor rated at 11 kWPolytechnic Institute and State University in (15 hp) continuous and 26 kW (35 hp) peak (2).conjunction with Inland Motor Company (underDOE/NASA Contract DEN3-65) have each been GENERAL DESCRIPTION OF MOTORSdeveloping electronically commutated motors forelectric vehicle use. Each contractor has The essential features of the electronically

completed testing of a motor designed to use commutated motor are shown in figure i.(3) Aninverter is gated by a shaft position sensor

* Numbers in parentheses designate References atend of paper.

Maslowski

Page 6: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

cooplpd to the shaft of a synchronous machine.1Ill' ITlVl,,'t('I' pl'ovirles the power' switching functionand its operation is analogous to brushconmutation in a conventional dc motor. Theconverter (chopper) controls the voltage orcurrent to the motor.

Two different design concepts have resulted,differing in the rated speed of the motor and inthe approach to the design of the powerconditioner electronics. A medium-speed machinerated in the range from 7,000 rpm to g,OOO rpm andpowered via a transistor inverter is the systemdeveloped by Virginia Polytechnic Institute andState University in conjunction with Inland MotorCompany. This machine is designed and rated fornatural convective cooling in a moving vehicle. Ahigh-speed machine rated for operation between~2,uOU rpm and 26,UOO rpm and using thyristors(also known as silicon-controlled-rectifiers, orSCR's) for the inverter switches is the designcOncept for the system designed byGarrett-AiResearch. This machine is designed forforced air cooling by an externally mounted fan.

The design variations to be discussed in thispaper, as well as some important characteristics,are summarized in table 1. The medium speed andhigh-speed motors which have already been builtand tested are designated as VPI/RECO-I andAR/RECO, respectively. (The acronym "RECO"indicates rare-earth cobalt permanent magnets).V?1/RECO-2 is presently being built as a modifiedversion of VPI/RECO-1 having lighter magnets andtwo additional poles. A modified version of theAR/RECO motor is also being built but incorporatesonly minor changes in the stator windings.VPl/FERRlTE is a medium speed ferrite magnet motornow being fabricated. AR/FERRITE is a preliminarydesign of a high speed ferrite magnet motor.Power ratings shown are the minimum designratings. AR/FERRITE has been designed to matchthe actually tested performance of the AR/RECOmotor for purposes of comparison.

MACHINE DESCRIPTION

Each of the machines designed in this motordevelopment program are of the permanent magnetsynchronous type. The inherent simplicity of thistype of construction is illustrated by figure 2which shows the component parts (except for theconventional-appearing stator) of one of the e.c.machines discussed here. The major componentswhich will be discussed in more detail are thepermanent magnet rotor, the stator armature, andthe rotor-position sensors. Costs are alsoaddressed.

PERrlANENT r1AGNET ROTOR- Interes tin permanentmagnet motors increased with the development ofhigh energy permanent magnet material, especially,samarium-coDa1t, which became available in thelate 195U's. The attractiveness ofsamarium-CObalt can be seen by comparing itsmagnetic properties with three of the bestavailable magnetic materials, Ferrite, Alnico 5,and Alnico 8, as shown in figure 3.(4) Themaximum value of the product of Band H, (BH)max.is commonly used as a figure of merit and

represents the maximum energy per unit volume ofthe magnetic material. Also of importance is theshape of the curve with increasiny demagnetizingforce. A linear characteristic as exhibited bythe samarium-cobalt indicates excellent resistanceto demagnetization, both self-demagnetization (5)which can occur during the assembly or disassemblyof the machine and demagnetization due to highcurrents flowing in a heavily loaded motor.

Both samarium-cobalt (SmC05 alloy) machinesVPI/RECO-1 and AR/RECO, the first machinesdeveloped and tested in this motor developmentproject, have four pole rotors. Samarium-CObaltmagnets are bonded to a steel shaft, as shown infigure 4, and held in place by a nonmagneticsleeve as shown in figure 5. The use of highenergy permanent magnets leads to a rotorstructure that is smaller and lighter than theconventional dc motor armature rotor. The resultis lower rotor inertia and a smaller mechanicaltime constant. The smoother surface configurationpossible results in lower windage loss.

The medium-speed samarium-cobalt machine hasbeen redesigned with a six-pole rotor(VPI/RECO-2). The use of a greater number ofpoles allows the amount of magnet material to bereduced for the same power output. However, thefrequency of switching required in the inverter isincreased. Consequently, this design change iseasier to effect in the lower speed machine.

Uncertainties about the future availabilityof samarium-cobalt and continually rising cobaltprices prompted an investigation into thepossibilities of substituting another material forsamarium-cobalt used in the rotors of thesemachines. The most promising readily availablematerial appears to be strontium-ferrite 8.Designs based On this material were made for botha medium-speed and high-speed motor, VP1/FERRITEand AR/FERRITE shown on table 1. The resultingferrite machines are 50-60% larger than theirsamarium-cobalt magnet counterparts. TheVPI/FERRITE was selected for further evaluation.This machine is presently being fabricated andwill undergo testing to establish the performancecharacteristic of this type of maChine, andthereby, it is hoped, establish the feasibility offerrite magnet material in these applications.

STATOR-ARMATURE-Compared to the conventionaltype de machine in which the armature must rotateto effect commutation, the e.c. machine is an"inside-out" construction in which the armature isstationary and commutation is achievedelectronically. A number of important advantagesresult from having the winding stationary. Theteeth and slots of the magnetic steel laminationsbecome larger than in the conventionalconstruction. The teeth can carry more magneticflux and the slots can carry more copper. The neteffect is that the resistance of the winding canbe decreased, lowering the Joule loss (I2R) in thewinding and improving the efficiency. At the sametime, the heat dissipation area of the winding isincreased. A higher power output, thus, can beachieved for the same temperature rise. Noodleman(6) has estimated that this type of inside-outconstruction can dissipate twice the losses of the

Maslowski

2

Page 7: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

cunvvntiunal ::Jact!ine construction. Uasin'1 hiscalculations on this factor, Nagarkatti (7) hasfurther sho~n that this inside-out design canprovide as high as l.b times the continuous torqueof a conventional de machine of the same volume.Figure b shows the armature lamination stack ofone of the machines and figure 7 shows thelaninations with the coils installed.

Two different techniques have been used toMinimize variations in torque at low speeds causedby alignJlent of teeth and poles, i.e., cogging.In the first design of the medium-speed motor afractional slot winding, that is, an odd number ofcoils, was used. Fifteen slots were used in afour-pole, three-phase design giVing 1.25 slotsper-pole-per-phase. In the final design of this~achine (VPI/~ECO-2), for purposes ofmanufacturing econo~~, an integral slot windingwas adopted, i.e., IH slots for a 6-pole field or1 slot per pole per phase. In this latter design,the laminations were skewed to minimize cogging.In the high-speed motor designs, the skewedlamination technique was used. In the AR/RECO-1:nachine ,4 slots were used with a four-pole field.No cogging was apparent in any of the macinestes ted.

An additional feature of the medium-speedmachine is the use of a tapped armature windingcapaDle of Deing changed to " 3, or 4 turns percoil. The tap changing scheme was adopted,primarily, to avoid excessively hiqh currents at1011 speedS. This was modified in the VPI/RECO-2and VfJI/Ferrite to a t~lo-step change :Jy allOllin~

eitller parall el or series connections of sets ofcoils to be selected.

ROTOR POSITIOtJ SEUSmS-In the high-speedmachine in normal operation, the shaft positioninformcltion is derived fror:l the machine's back8W. Hence, the position sensors are in effectttle arnldture windings of the machine itself,activateo Dy the rotatinfl field poles. At 101-1

speeds villen the back EllF is too 10Vi for reliableoperation, an optical sensor coupled with ashutter asse~oly mounted on the Shaft is used.Tili s optical system is used whenever the Plotor isoperating at less than luh ot the rated speed.

In the medium-speed machine, four smallmagnets, one for each pole, are attached to theshaft of the nachine and three Hall effectdevices, one for each phase, are attached to thehousing. As the magnets move past the Hall effectdevices, a pulse is generated which indicates theprecise position of the rotor. This positioninformation is processed by the electronics toachieve switching of the transistors in the propersequence. This is shown schematically in figured. The position sensor assembly can be seen'nounted in the machine in figure 9.

COSTS-The cost of cobalt has increased by afactor of 4 to 7 since 1977. The best qualitymagnets consist of five parts CObalt to one partrare earth. Consequently, their cost hasincreased proportionately to a present day cost ofS~~ to Sou per pound of 14U kj/~3 (3H)max. magnetsin quantity. HO>lever, hecause of the simplerstructure, the per~anent magnet synchronousi1actJine can be manufactured in quantity at less

than half the cost of a comparable, conventional,dc machine, even with the present cost ofrare-earth material s. The (l.LII. cost of thepermanent magnet machine has been estimated atbetween 5250 and 5300 in quantities of lUU,OUOunits per year. If the cost of samarium-cobaltwere to stabilize at the present levels, the useof territe magnet material May not result in asignificantly lower cost due to the cost of theaddtional materials, particularly copper, requiredfor the bulkier machine. This is especially truefor the high speed Machine. However, the ferritematerial has the advantage of assured availabil ityand a relatively stable cost.

POUER CONDITIONING ELECTRONICS

Two differently designed power conditionersto effect electronic control and motor co~utation

have been built. Functionally, these twoconditioners are very similar, but they differsubstantially in the impleplentation of thesefunctions. High power transistors are used asswitches in the inverter for the meaium-speedmotor, whereas SCR's are used in the inverter forthe high-speed motor. Each of these two designswill be described separately. Costs are addressedalso.

TRA~SISTOR INVERTER POUER CONOITIONER-A blockdiagra"7l of the cO'llplete syste:n is shown in figurelu. The major power components are shown infigure 11. Transistors, ();I and UfJ comprise ablo-quadrant converter (chopper) ana control pallerflow in either direction. During the motoring~ode (positive enerqy flow), the current isreflulated to provide the torClue cOlnllanded Jy thevehicle operator. Average current is controlledby means of a closed loop system which conparesthe output of an in-line current shunt to acommand signal and uses the output of a comparatorto control the duty cycle of the chopper. Thechoke, L, is included to provirle additionalinductance to reduce current ripple. This type ofreflulation was selecteo rather than an op!n looptechnique such as pulse Hidth fTIodulation (f''''') ofthe inverter tran sis tors fa r the fa 11 Old ngadvantaqes: inherent stability, controllable deripple, and simplification of the protectionschemes. A description of this type ofcontroller, as well as additional details of thetransistor inverter pOHer conditioner discussedhere, can be found in reference (H). Theregulated current is switched by the three-phasetransistor inverter bridge prOViding the power tothe machine armature windings in the propersequence for motor operation. The broken line infigure 11 sholls the current path for phase A-lJ inthe motoring mode. In this case, transistors Urand U6 are turned on. Transistor selection iscontrolleo by the position sensors mounted on themachine shaft.

In the regenerative mode, diodes 01-06 act asa three-phase, full Ilave, bridge recti fierallowing power to floll frorn the ~otor to t~e

battery. The qenerated 81F of the Motor isDoosted by the action of the chopper transistor,Qa, and the choke, L, to overcone the battery

Maslowski

3

Page 8: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

voltage. Inertial energy of the electric vehicle increasing interest by transistor manufacturers incan, in this manner, be returned to the battery. Io_ cost high Dower transistors. If Dower

Tlle weight of tile completed breadboard transistors with good heat transferversion of the controller is about 41 kg (90 characteristics were to become available at apounds}. Ho;_ever, with the use of custom designed price of $0.15 per ampere, a figure considered toheJt sinks and attention to packaging details, be realistically achievable, transistor powerthis _leiqht could be reduced to about 27 kg (6U conditioninq as described here could De producedpounusl, at an O.E.I¿.cost of about $6uo per unit. The

SCR INVERTER PU$1ERCO_DITIONER-The power total cost of the electronicallycommutated motorconditioner using SCR's as inverter switches is would then be under SIuuu.sho_m schematically in figure 12. SCR's have anadvantage over po_vertransistors in that SCR's are TEST RESULTSreadily availa_le in any current and voltage rangeof interest for electric vehicle applications, are Both the medium-speed and the high-speedvery rugged, and are presently much less electronically commutated motors, comprising theexpensive. The major problem is that the SCRcan permanent magnet machine and power conditioningDe difficult to turn off. Turn-off, or electronics, have been dynamometer tested forcommutation, requires that the current throuqh the performance. The completed high-speed machine isdevice be reduced to zero by removing the EIIF shown in figure 15. Fiqure 16 shows the method of(natural commutation) or reversing the E_IF (forced testing used for the high-speed machine. Theco,_m_utation). The latter technique is used to medium-speed machine was tested independently in adecrease the time required to turn off the SCR. similar set UP.

In the motoring mode, the SCR's are turned on Test results are shown in figures 17 throughin the proper sequence using rotor position 2U. Curves of efficiency as a function of torqueinformation determined from the near-sinusoidally for various speeds are shown. These curves arevarying back EIIF of the machine. The back E!IF of shown for both the motoring and the regenerationthe machine is also used to commutate the SCR's by (brake) modes.a technique described in reference (9). This Figures 17 and 18 show the efficiency of thetechnique is based on the fact that a reverse EIIF high-speed motor system including both the powerwill appear across the SCRto be commutated if the conditioner and permanent magnet machine. Thenext SCR in the sequence is turned on at an curves for the motor in the motorinq mode ofappropriately advanced angle. At low speeds, the operation indicates a peak of about 9U% at fullPack EilF is too low to properly turn off the speed, and fairly constant efficiency over most ofSCR's. Therefore, the optical rotor position the torque range. In the brake, or regenerativesensor is used in conjunction with logic circuitry mode, the efficiencies fall off much more rapidlyto turn off the current control chopper, _II, for a with speed. This is due to the higher lossesperiou of time sufficient to allow the incurred by the electronics in boosting thecorresponding SCR to turn oft by natural voltage output of the machine.commutation. Transistor chopper UL may be Figures 19 and 2U show the efficiency ot theincluded, as an option, to achieve forced medium-speed machine but do not include the powercoa_mutation. It has been found that elimination conditioner losses. Losses higher than normalof this transistor results in only a slight power occurred in the power conditioner due to theloss at very low speeds. In _otoring mode of unavoidable substitution of an underdesiqned chokeoperation switch S;JI is closed. Power is supplied for the proper choke in order to complete testingvia the choke L1 to the inverter bridge Ql-k)O. on schedule. Resistive losses were also hiqherThe current level is controlled by the switching than necessary because of the breadboard nature ofacIlon of UIi. In the regenerative mode, switch the power conditioner. The power conditionerS_II is open, and the SCR'S are operated as a three efficiencies are, therefore, not included in thesep_lase bridge rectifier. The voltage is boosted to fiqures for the medium-speed machine because thean appropriately high level by QII, DI, and LI. test data is not believed to be representative ofThe SCR inverter power conditioner in breadboard the potential performance of this powerform is shown in figure 13. The weight of this conditioner. This power conditioner has beenpower conditioner is 36 kq (8'apounds) in this upgraded for future testing of the VPI/RECD-2forn. In a production prototype, its weight version of the motor and the above problems havesilouldbe abOUt 27 kg (6U pounds), been eliminated. The machine efficiencies as

COSTS-The electronics are, without question, shown on these curves are in excess of 93% overthe most expensive part of the electronically most of the torque range. The machinecom,nutatedmotor. However, it must be kept in efficiencies are not strongly dependent on speedminu that the power conditioners as described in in either the motoring mode or the brake mode.this paper contain virtually all the control Based on the test data, efficiencies were •functions that are likely to be required for calculated for operation over the SAE JZZ7a,operation in an electric vehicle. The O.E.H. cost Schedule D, driving cycle and are sho_n in tableof the power conditioner has been esti_ated at 2. Efficiency over this cycle is defined as total$1_Ou to $165u for the SCR version. The output energy of the motor required to propel thetransistor inverter cost is considerably higher vehicle over the cycle ciivided oy the total energynow, but is potentially less expensive due to the input to the motor over the cycle. Energy due toless complex circuitry required. There is an

Maslowski

Page 9: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

regeneratlon is represented as negative and is, 3. J. M. D. Murphy, "Thyristor Control ofthus, Subtracted from the input energy. A.C. Motors," Pergamon Press, New York, 1973.

4. D. Weinmann, "Recoma-NewStandards inCONCLUDING REMARKS Permanent Magnet Applications" Brown Boveri

Review, volume 66, p. 21, January 1979.Permanent magnet, electronically commutated 5. R. J. Parker and R. J. Studders,

motors have been shown to be capable of very high "Permanent Magnets and Their Application," Johnperformance. The weights of the resulting Wiley and Sons, Inc., New York, 1962.machine-controller systems can be significantly 6. S. Noodleman, "Rare-Earth Cobalt Magnetslower than those of comparable dc motor-controller and Their Use in D.C. Machines," Paper presentedcombinations. The most significant problem is at Int. Conf. Elect. Machines, Brussels, Septemberthat of cost. The motor development program is ll-13, 1978.

continuing at present with emphasison reducing 7. A. K. Nagarkatti, "Study of Performancepotential production costs. This involves and Certain Special Aspects of Electronicallyexploring lower cost magnet material, Commutated Brushless D.C. Motors for Electricinvestigating high power transistor technology Vehicles" Masters Thesis, Virginia Polytechnic

• further, and simplifying the present motor Institute and State University, May 1980.designs. 8. D. J. Shortt, R. A. Carter, and F. C.

REFERENCES Lee, "A Transistorized Chopper-lnverterControllerfor Electric Vehicle Propulsion," Proceedings ofthe 2nd InternationalPower Conversion

I. "Electric Vehicle Test Procedure-SAE Conference, Intertec Communications Inc., paperJ_R27a"Society of Automotive Engineers, Inc., 6.1, Munich, Germany, September 1980.February 1976. 9. J. Ingaki, M. Kuniyoshi, and S.

2. J. A. Ross and G. D. Wooldridge, Tadakuma, "Commutators Get the Brushoff," IEEE"Preliminary Power Train Design for a Spectrum, volume lO, no. 6, pp. 52-58, June 1973.State-of-the-ArtElectric Vehicle," RohrIndustries Inc. (Contract NAS3-20592), RHR-78-035DOE/NASA/0592-78-1,NASA CR-135340, April 1978.

Table l-Electronically Commutated Motors Designed for DOE/NASA

VPI/RECO-I VPI/RECO-2 VPI/FERRITE AR/RECO AR/FERRITE

i lagnet material SmCo5 SmCo5 Strontium SmCo5 StrontiumFerrite 8 Ferrite 8

Magnetic (BH)max. kj/m 3 140 140 26 175 26Magnet weight, kg (Ibs.) 2.4 (5.3) 1.5 (3.2) 4.4 (9.6) 1.4 (3.0) 5.9 (13.0)No. of poles 4 6 6 4 6Rated speed, rpm 7650 8600 9000 26,000 22,000Peak power, kW (hp) 26 (35) 26 (35) 26 (35) 26 (35) 30 (40) (*)Machine weight, kg (Ibs.) 40 (88) 27 (60) 58 (127) 15 (33) 34 (75) (**)

(**)f_achineefficiency, %estimated 93.4 95.9 95.8 93.0 93.0tested 93.0 93.0 -Inverter type Transistor Transistor Transistor SCR SCR

(*) Note the higher rated design

(**) External cooling fan required for this motor at an additional weight of 2.7 kg (6.0 Ibs.)

Table 2-Efficiencies Expected Over the SAE, Schedule D, Driving Cycle-J227a

Efficiency VPI/RECO-I AR/RECO

Machine 0.90 0.93Power Conditioner 0.85* 0.94System 0.77 0.88

*Includes Anomalous Losses in Power Conditioner

Maslowski

Page 10: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the
Page 11: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

I I I I 1CURRENT r CURRENT ICONTROL" I SENS,NO I

I __[__SYNCHRONOUSi

_ ELECTRON,C'MAC.,N_DC- De SWITCHCONVERTER [STATIC[CHOPPER] INVERTER], / I

I f / I

I _.,.(/SHAFTI GAT,NGt--'-UUPOS,T,ONII CIRCUITRY IL .I SENSORj

Figure1. - Electronicallycommutateddcmotor.

Figure2. - Componentpartsofmachineforelectronicallycommutateddcmotor.

Page 12: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

800 600 400 200 0DEMAGNETIZINGFORCEH, kA/m

Figure3. - Demagnetizationcurvesof four selectedmagneticmaterials.

Figure4. - Rotorwithpermanentmagnetsattached.

Page 13: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

Figure5. - Assembledrotor.

C-80-4297

Figure6. - Statorlaminationstack.

Page 14: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

Figure7. - Partiallyassembledstatorshowingarmaturecoils.

I iIII

ROTORPOSITION0 60 120 180 240 300 0 60 120 180

HALLSWITCHNO.1

HALLSWITCHNO.2

HALLSWITCHNO.3

Figure8. - Rotorpositionsensor.

Page 15: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

Figure9. - EndViewof machineshowingrotor positionassembly.

CHOKE

Lcov+-- [CURRENT T INVERTER

120V CONTROL

: '11 L I III

U i ii+oICONTROL SENSOR CONTROL POSITIONCIRCUITS CIRCUITS SENSOR

I ,ILIMITER

I DC- DC CURRENTCOMMANDCONVERTER , i

i I CE--+ l i +f"_ CIRCUITRY

Figure10. - Completeblockdiagramof transistorinverterpowerconditioner.

Page 16: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

POWERSUPPLY

LIERCAPACITOR FINVERTERBRIDGEtrCHOPPER /i /I /

0O 60012001800240030003600420o DEG.ELEC.I I I I I I I

iA .... ,-.-kl i i { I,vvvvvvv I I --

, l I

' ' I I ' II I I III I., { I I I I

• I IIB I g I , , I

' ' ' I II t | I I

ic "", I ] ' I , ,' , , I I IK.. I I_

Figure11.- Transistorinverterpowerconditionerschematicandidealizedmotorcurrents.

SWI

D_ "--!105-1.40_L ;.rQ]. Q30_867Hz_

!:'_-_I; 'Q" 5 6" _ o7- EMF POSITION

-- " , SENSE SENSE

THYRISTORI{cHOPPERLOGICI- I DRIVER(3) I

t I

!SEQUENCELOGICH INVERTERLOGICI_-I

LOWVOLTAGEPWR I I PROTECTLOGICI

Figure12.- SCRinverterpowerconditionerschematic.

Page 17: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

C.80-_9

Figure13. - BreadboardversionofSCRinverterpowerconditioner.

C-80-2667

Figure 14. - Thecompletedhigh-speedmachine.

Page 18: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

C-79-3363

Figure15.- Thecompletedmedium-speedmachine.

I_'_'_.1l_'_'_.1POI PO_

°_,.-_AC_,_k_-l_.__A,_

DY_10MOTOR BOX

I F,EtJI PO_ER

Figure10.- Blockdiagramoflaboratorytestsystem.

Page 19: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

% OFRATEDSPEED1007P50

, 50-- _ -- 100

4(]-- -... -- 80_;

20 ..,.-.. -- 40

10 ......-.".._-_ ..... 20

I --"F--r 1 I I I /-o0 I0 20 30 40 50 60 I0 80

TORQUE,in.Ib

Figure17.-Performanceofhigh-speedmotorduringdrivemode.

% OFRATEDSPEED

O 10075PO25

P0-- --100

....... .O

30 I "/ o 60'_' 20 /.. 40

"""" --"-'T" I "', 0 10 20 30 40 50 60 70 80

TORQUE,in.Ib

Figure18.-Performanceofhigh-speedmotorduringbrake(regeneration)mode.

Page 20: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

TAPPOSITION

O 2[] 3Z_ 4

100-- --.20

80- -- 16 '

_. 60-- -- 12

g _

20-- _ _ Z 4

l l I I l l-o0 40 80 120 160 200 240

TORQUE,in.Ib

Figure19.-Performanceofmedium-speedmachineduringdrivemode.

TAPPOSITION

O 2[] 3/x 4

100- -- 20

80 -- 16b--

,,, 60 -- 12 "_" E

40- -8_

" Ky _"' ri,

I

I I I'°I I I o0 40 80 120 160 200 240

TORQUE,in.Ib

Figure20.-Performanceofmediumspeedmachineduringbrake(regeneration)mode.

Page 21: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the
Page 22: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

1. Report No. 2. Government Accession No. 3. Recipient's Catalog No.NASA TM-81654

4. Title and Subtitle 5. Report DateELECTRONICALLY COMMUTATED dc MOTORS

FOR ELECTRIC VEHICLES 6. PerformingOrganizationCode778-36-06

7. Author(s) 8. Performing Organization Report No.

Edward A. Maslowski E-657 ,

10. Work Unit No.9. Performing Organization Name and Address

NationalAeronauticsand Space Administration

Lewis Research Center 11. Contract or Grant No.

Cleveland, Ohio 4413513. Type of Report and Period Covered

12. SponsoringAgency Name and Address

U.S. Department of Energy Technical MemorandumOffice of Transportation Programs 14. SponsoringAgency_,ede Report No.

Washington, D.C. 20545 DOE/NASA/51044-1415. Supplementary Notes

Prepared under Interagency Agreement DE-AI01-77CS51044. Prepared for Society of Auto-

motive Engineers International Congress and Exposition, Detroit, Michigan. February 23-27,1981,

16. Abstract

A motor development program to explore the feasibility of electronically commutated dc motors

(also known as brushless) for electric cars is described. Two different design concepts and a

number of design variations based on these concepts are discussed. One design concept is based

on a permanent magnet, medium-speed, machine rated at 7000-9000 rpm and powered via a

transistor-inverter power conditioner. The other concept is based on a permanent magnet, high

speed, machine rated at 22,000-26,000 rpm and powered via a thyristor-inverter power con-

ditioner. Test results are presented for a medium-speed motor and for a high-speed motor eac[

of which have been fabricated using samarium-cobalt permanent magnet material.

17. Key Words (Suggested by Author(s)) 18. Distribution Statement

Electric vehicles; Electric motors; Unclassified - unlimited

Transportation;Motor controllers STAR Category 44

DOE Category UC-96

19. Security Classif. (of this report) 20. Security Classif. (of this page) 21. No. of Pages 22. Price*Unclassified Unc las sified

* ForsalebytheNationalTechnicalInformationService,Springfield,Virginia22161

NASA-C-168 (Rev. I0-75)

Page 23: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the
Page 24: DOE NASAfractional slot winding, that is, an odd number of coils, was used. Fifteen slots were used in a four-pole, three-phase design giVing 1.25 slots per-pole-per-phase. In the

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