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FAULT TOLERANT PERMENANT MAGNET MACHINE DRIVES Document By SANTOSH BHARADWAJ REDDY Email: [email protected] Engineeringpapers.blogspot.com More Papers and Presentations available on above site Abstract: The project examines the use of permanent magnet machine drives in high performance, safety-critical applications. Likely fault modes are identified and mac hin e des ign s are dev elo ped for fault- tolera nt ope rat ion , wit hou t severely compromising the drive performance. Fault tolerance is achieved by adopting a modular approach to the drive, with each phase electrically, magne tical ly, therma lly and phys icall y indep enden t of all others. Power converter requirements are discussed and methods for controlling a faulted phase developed to minimize the impact of a machine or power converter fault.

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FAULT TOLERANT PERMENANT MAGNET

MACHINE DRIVES

Document By

SANTOSH BHARADWAJ REDDY

Email: [email protected]

Engineeringpapers.blogspot.com

More Papers and Presentations available on above site

Abstract:

The project examines the use of permanent magnet machine drives in high

performance, safety-critical applications. Likely fault modes are identified

and machine designs are developed for fault-tolerant operation, without

severely compromising the drive performance. Fault tolerance is achieved

by adopting a modular approach to the drive, with each phase electrically,

magnetically, thermally and physically independent of all others. Power 

converter requirements are discussed and methods for controlling a faulted

phase developed to minimize the impact of a machine or power converter 

fault.

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List of symbols

Aerospace applications demand drives with both high reliability and large

power to mass ratios. Recent research in the USA [l-31 has led to the

development of switched reluctance drives for the aerospace market because

of their inherent fault tolerance, despite an arguably reduced power density

compared to other machine types. Research by the current authors [4] has

questioned the justification of abandoning high performance permanent

magnet drives. This paper describes experimental results from a permanent

magnet machine, which has been designed with fault tolerance in mind. The

main thrust of this contribution is concerned with demonstrating that the

fault-tolerant electromagnetic performance can be achieved. The machine

must be designed so that even with a winding or switching device short

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circuit the fault currents are limited to a level within steady state thermal

limits. Penalties must be considered in terms of machine volume and power 

switching device rating, although it is shown that these penalties are not

severe.

There are many potential faults which can occur in a drive system:

inevitably within this work the range of faults under consideration must be

restricted. For example, a design which is insensitive to the failure of a

position transducer would probably require sensorles operation, which is

beyond the scope of this paper. The principal electromagnetic faults which

may occur within the machine are:

(i) winding open circuit

(ii) winding short circuit (phase-ground or within a

phase)

(iii) winding short circuit at the terminals.

eration are:

(i) power device open circuit

(ii) power device short circuit

(iii) DC link capacitor failureThe aim is to develop a drive which can continue to operate with any one of 

these faults. It has become clear that the most successful design approach

involves a multiple phase drive in which each phase may be regarded as a

single module. The operation of any one module must have minimal impact

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upon the others, so that in the event of that module failing the others can

continue to operate unaffected. The above modular approach requires that

there  should  be  minimal  electrical,  magnetic  and  thermal  interac

between phases of the drive. This philosophy must extend to both the

machine and the power converter. The requirements are naturally met in a

switched reluctance motor [3]; separate half bridges are used for each phase

and so the phases are electrically decoupled, and there is low mutual

magnetic coupling between phases. Because the SRM is a singly excited

machine, fault current will not continue to be driven into a faulted phase,

once excitation of that phase is removed. Furthermore, there is reduced

likelihood of a phase-phase fault because the end windings do not overlap.

However, it must be noted that two phases do occupy the same slot, so that

thermal isolation between phases is limited.

A conventional permanent magnet machine has a significantly greater 

specific output than a switched reluctance machine, but it has none of the

inherent fault-tolerant capabilities. The following Section will address how a

permanent magnet drive may be designed to enhance its fault tolerance.

The requirements outlined in the previous Section naturally fix certain

features of the machine design and drive configuration. These requirements

will be considered for a voltage fed inverter drive.

3.1 Complete electrical isolation between phases

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This can be shown to be an essential requirement if continued operation is to

occur with either a power device or winding short-circuited. For instance, in

a star connected system the star point may rise to the DC link voltage, so

that no net torque capability remains. The clear alternative is to drive each

phase from a separate single-phase bridge [SI. This doubles the number of 

power devices but only marginally increases the total power electronic

device volt-ampere rating, because each device need only withstand the

phase voltage rather than the line voltage of star connected systems.

3.2 Implicit limiting of fault currents

The most difficult machine fault to accommodate is a winding short-circuit.

Section 7 shows that a power electronic device short-circuit failure produces

a similar condition to a winding terminal short circuit, except that the fault

current flows through the converter as well as the winding. Thus, a phase

terminal short-circuit has received particular attention. The system was

designed without any fuses incorporated into the drive, as the reliability of 

fuses is generally poor. This leaves two possibilities for dealing with the

above fault conditions. (a) The machine can be deliberately designed with a

low per unit inductance, so that a large fault current flows. Thus, a winding

short-circuit fault will result in a very large winding short-circuit fault

current, the faulted winding will overheat and subsequently produce an

open-circuit. Equally a device short circuit will produce a very large faulted

device current, and the subsequent heating will eventually produce an open-

circuit condition. Alternatively, (b) the machine can be designed with a d

axis per unit inductance approaching 1.0 per unit, so that a phase terminal

short circuit will not result in steady state motor currents beyond 1.0 per 

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unit. The thermal limit of the faulted winding will not be exceeded and the

short circuit can be accommodated over an extended period. Torque ripple

resulting from the short-circuit current in the faulted phase will inevitably be

large unless special measures are employed. The second of the above

approaches provides a more reliable, fault-tolerant solution, as the first

option allows very large per unit fault currents to flow in failed power 

electronic devices until they turn open circuit. The faulted device will

experience large thermal stresses, which may lead to disintegration of the

packaging and propagation of the fault into surrounding power devices.

Producing an effective d axis inductance of one per unit is generally

considered difficult to achieve in a small permanent magnet machine, but it

is shown in a later section that this can in fact be achieved relatively easily.

3.3 Magnetic isolation between phases

Without magnetic isolation, fault currents in one phase induce large voltages

in other phases, preventing adequate control of them [4]. Furthermore, the

current flowing in unfaulted phases supplements the magnet MMF and so

increases the EMF driving fault current. Thus it becomes clear that for a

given unfaulted armature reaction field the single phase short-circuit fault

current is substantially greater when there is mutual coupling between

phases. A torque controller has been developed to minimize the machine

output torque ripple when operating in the faulted condition. The controller 

identifies  current  profiles   which  produce  a  given   torque  demand

minimum i2R loss under both normal and faulted conditions, thus giving

closed loop torque control. This torque control was found to be severely

impaired by substantial phase-phase mutual coupling. The above results

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show that both the faulted and unfaulted phases perform substantially worse

when there is mutual coupling between phases, so the machine should be

designed with minimal phase-phase mutual coupling. In surface mounted

magnet designs the air gap flux due to armature reaction is small and a

substantial amount of the phase inductance arises due to cross-slot leakage

flux. If this is to remain solely a self inductance component then each slot

should contain the conductors of one phase only. The component of 

armature reaction flux which crosses the air gap will always contain an

element which links the other phases. However, if a surface mounted magnet

design with a nonmagnetic retaining sleeve is employed, then the presence

of the sleeve, combined with relatively deep magnets, greatly reduces the air 

gap component of the armature reaction field, so that in effect the mutual

coupling is insignificant.

3.4 Effective thermal isolation between

phasesIf the stator outer surface is well cooled then the dominant temperature rise

in the machine is within each slot. By ensuring that each slot contains only a

single phase winding then thermal interaction between phases is minimized.

3.5 Physical isolation between phases

A phase-phase fault is especially serious, since it will disable two phases. By

placing each winding round a single tooth then all phase windings (including

the end windings) are physically separated, thus virtually

eliminating the possibility of a phase to phase fault.

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3.6 Number of phasesThe basic criteria used is that the drive should continue to produce rated

power in the event of the failure of one phase. Hence, if there are n phases,

each phase must be overrated by a fault-tolerant rating factor, F, where F =

n/ (n - 1). Thus, if there are three phases, each drive must be overrated by

50% in order to give full capability when faulted. Clearly, F falls as the

number of phases rises, but this must be balanced against the increasing

complexity of a high phase number and the inevitably greater chance of a

failure.

3.7 Summary

With regard to the machine design, the essential conclusions are that the

machine should have (i) a surface mounted magnet rotor design, (ii) a one

per-unit armature self inductance, (iii) each winding wound around a single

tooth and (iv) only one phase winding per slot.

The first two conclusions appear to be in conflict because a surface mounted

magnet machine generally has a low per unit reactance. However, the key to

achieving these requirements is to design a machine with a large leakage

inductance  by  controlling  the  depth  and  width  of   the  slot  op

commonly called the stator reactance slot. In the event of a phase winding

short circuit then one half of the magnet flux which normally passes up one

tooth must be shunted across each reactance slot. To avoid undue saturation

the reactance slot depth is designed to be approximately one half of the tooth

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width, with the reactance slot width chosen according to the required

inductance.

4 Analysis of machine winding failures

In the above discussion a winding short circuit at the terminals is considered,

but no consideration is made of the more difficult case, where the short

occurs between two adjacent turns of a winding. The single turn short circuit

is a troublesome fault for all machine types and its detection is a topic of 

ongoing research. In a switched reluctance machine it is necessary to detect

the fault quickly and subsequently remove excitation from the faulted phase.

In a permanent magnet machine it is equally important to have fast fault

detection, but once detected a different course of action is appropriate.

For simplicity of explanation consider a simple case where a winding of N

turns has a sinusoidally varying flux-linkage from the magnet of magnitude

Yf per unit, and a per unit self inductance, Lpu (assume no phase phase

mutual coupling in this case). The peak per unit current which flows in theevent of a terminal short circuit is given by

In all but small, slow speed machines the per unit resistive effect is almost

negligible, so that a terminal short circuit produces very little mean braking

torque, and the fault current is limited by the inductance. Clearly if Lpu is

equal to Yf then l.0pu current will flow.

Now consider the case where the short is across just one turn of the N turn

winding. The induced current in this turn is given by

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Thus if the inductive term remains greater than the resistive one the fault

current in the shorted turn will be N pu. In reality the resistive term is

generally now dominant, but the fault current remains very large and will

cause very high localized heating. This can be explained in general terms by

the realization that the MMF of the single faulted turn is trying to produce a

component of flux which cancels out the magnet flux linkage. It appears,

therefore, that while a terminal short circuit can be accommodated, a single

turn short circuit cannot. However, if the shorted turn can be detected

quickly then the situation can be returned to one analogous to a terminal

short circuit by shorting the terminals through the power converter. This

forces all the turns to share the winding MMF and reduces the current in the

single faulted turn back to rated value. Of course such action is dependant

upon fault detection and subsequent application of the terminal short circuit

in less time than the faulted turn reaches its thermal limit, which may be

considerably under one second.

Section 3 indicates that there should be only one phase winding per slot to

maximize thermal isolation and minimize mutual coupling between phases.

However, to prevent phase-phase faults it was also concluded that each coil

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should be wound around a single tooth, thus eliminating overlapping end-

windings. These two conclusions make an unusual combination. If each coil

is wound around a single tooth and each slot is to contain a single phase then

a winding configuration arises in which only every other tooth has a coil

enclosing it. This arrangement is illustrated in Fig. 1.

 

This may at first appear to be a rather inefficient form of winding, but in

practice it is not. Every slot remains fully filled and the teeth without coils

are still being utilized as flux return paths. The arrangement is particularly

good in terms of thermal isolation, since all the phases are spaced out, with a

tooth   separating   adjoining   phases.   The   additional   advantage  

nonoverlapping end-windings in this arrangement makes a phase-phase fault

exceptionally unlikely. To maintain a high winding pitch factor it is

necessary to ensure that each tooth spans a significant pole arc. In this

design each tooth has been chosen to span 120 electrical degrees, resulting in

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three teeth per pole pair. The winding pattern repeats every two pole pairs,

with 240 electrical degrees between adjacent phases.

To illustrate the magnetic field distribution, Figs. 2 and 3 show magnetic

flux plots for this type of design, operating first on no-load, and then with a

single phase short-circuit fault. It is clear that flux linking the faulted phase

is effectively reduced to zero by the fault, and that all the flux which would

have travelled up the tooth enclosed by the faulted phase is now diverted

across the reactance slots. The flux in the adjoining teeth is substantially

changed, but no coils link these teeth. The flux linking all other coils

remains virtually unchanged.

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The choice of phase number has been discussed earlier: a final choice of six

phases has been decided as a compromise between undue redundancy and

additional complexity. As three phase coils of this machine occupy four 

poles then the full six coils occupy eight poles. Thus, the complete motor 

must be a multiple of eight poles. High pole numbers occupy reduced space,

but at the expense of higher electrical frequencies. Because the machine is to

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rotate at a relatively high speed, producing a high rotational frequency, a

choice of eight active poles has been made. In terms of the machine design

the major penalty of incorporating fault tolerance is associated with the high

per unit reactance required to limit a short-circuit fault current. Under 

normal operation, with rated current in the q-axis, there is a 42 increase in

total machine flux due to the additional armature reaction flux. This

increases the required width of the stator teeth by up to 40%, compared to a

machine with negligible reactance. The increase in tooth width, combined

with deeper reactance slots results in a 10-20% increase in the total active

mass of the machine. In order to validate the principles two small prototype

machines have been built and tested. These two machines differ solely in the

magnitude of the armature inductance. Results from the first machine are

given in [7] and results from the second machine presented below. The

knowledge gained from these prototypes has led to the design of a 16kW

machine and drive to meet an aircraft fuel pump drive specification.

The six phase prototype machine was designed to give a per phase open-

circuit voltage of 55V RMS at 12000rpm and has a rated phase current of 

7.OA RMS. The machine was designed to minimize mutual inductance

between phases, whilst achieving a high per unit self inductance in order to

limit the short-circuit fault current. The machine has a phase resistance of 

0.27Q2, which is 0. 0 2 8 ~ ~ . The phase inductances were measured with

the machine stationary, exciting a single phase and monitoring the phase

current and the induced voltages in the other phases. On this basis the per-

phase self inductance was determined to be 1.25pu, with the maximum

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phase-phase mutual inductance never exceeding 0. 0 4 4 ~ ~Th. us, it can be

seen that the objective of minimizing mutual coupling between phases has

been achieved. The machine was then run unloaded and the terminal voltage

monitored. The no-load terminal voltage of three physically adjacent phases

is shown in Fig. 4. Note that because the three phases are isolated some third

harmonic components of voltage are evident.

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The test was then repeated, but with one phase shorted at its terminals.

These results, along with the current in the shorted phase are given in Fig. 5.

From comparison with Fig. 4 it is clear that the terminal voltage of the

unfaulted phases is virtually unaffected by the faulted phase current. The

RMS fault current is equal to the design value. Note that the fault current

lags the open-circuit voltage of that phase by 90", as the fault current is

predominantly limited by the phase inductance. The machine can operate

indefinitely  in  this  condition,  with  the   other  phases  still  capab

generating torque, so that the ability to withstand a short circuit across any

one phase has been

demonstrated.

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Particular emphasis has been placed upon a power device short-circuit

failure, as this imposes the most arduous conditions upon the drive.

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With regard to Fig. 6-8, consider a short-circuit failure of transistor T1. The

most obvious action is to immediately inhibit the gate drive signals of the

other devices, T2, T3 and T4, which drive that phase. However, because of 

the continuation of an induced phase EMF from the magnets, unidirectional

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current continues to flow through the failed device, T1, and the diode, D3, as

shown in Fig. 7. Fig. 9 shows measurements of the prototype machine with

one phase failed in this manner. This diagram shows how the current in the

faulted phase is unidirectional with an AC component of approximately the

same peak magnitude as the DC component. A better strategy for dealing

with this fault is to continuously hold on transistor T3, so that the winding is

effectively shorted at the terminals, and giving the additional current path

shown in Fig. 8. The faulted phase current is as in the winding terminal

short-circuit shown in Fig. 5, and no longer contains any DC component.

The RMS current in the phase winding and in the faulted device is reduced

by 43 and the peak current halved. However, in order to take this action it is

essential that the fault is both quickly and accurately identified [6].

This paper has discussed the requirements for a fault tolerant permanent

magnet machine drive. The work has shown that the machine should bedriven  from  separate   single  phase  bridges,  and  must   be  capab

withstanding a short-circuit terminal fault. A design topology has been

produced in which there is effective magnetic, thermal and physical isolation

between phases. This has been demonstrated by a series of tests performed

upon a small six phase prototype machine. The machine is capable of 

withstanding open and short-circuit terminal conditions, with the unfaulted

phases continuing to deliver torque. The necessary action required to deal

with adjacent turn short-circuits has also been discussed. Remedial converter 

action to control a phase with a short-circuit power device has also been

discussed and demonstrated.

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1. RICHTER, E.: ‘Switched reluctance machines for high performance

operations in a harsh environment - a review paper’. Proceedings of the

ICEM Boston, MA, 1990

2.  RICHTER,  E.:  ‘High  temperature   switched  reluctance  motors  

generators for  future aircraft  engine applications’. Proceedings  of  the

American control conference, Atlanta, June 1988, pp. 1846--1851

3.  STEPHENS, C.M.: ‘Fault detection and management system for fault-

tolerant switched reluctance motor drives’, IEEE Trans. Ind.

4.  JACK, A.G., and MECROW, B.C.: ‘Safety critical drives for aerospace

applications’. Proceedings of the ICEM 1994, Paris, 1994, Appl., NOV.

1991, 27, (6), pp. 1098-1102 Vol. 1, pp. 91-96

5. JAHNS, T.M.: ‘Improved reliability in solid state AC drives by 7

MECROW,  B.C.,  JACK,  A.G., and HAYLOCK, J.A.:  ‘Fault tolerant

permanent magnet machine drives’. IEE 7th international conference on

Electrical  machines and drives, Oxford, 1995, pp. means of multiple

independent phase-drive units’, IEEE Trans., May 1980, IAS-16, (3), pp.

321-331

6. CRAIG, E., MECROW, B.C., ATKINSON, D.J.,and JACK, A.G.: ‘A

fault   detection   procedure   for   single   phase   bridge   converters’.   E

Conference ’93, Brighton, 1993, Vol. 4, pp. 466-471

7. MECROW, B.C., JACK, A.G., and HAYLOCK, J.A.: ‘Fault tolerant

permanent magnet machine drives’. IEE 7th international conference on

Electrical machines and drives, Oxford, 1995, pp.433-467.

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Document By

SANTOSH BHARADWAJ REDDY

Email: [email protected]

Engineeringpapers.blogspot.com

More Papers and Presentations available on above site