A MOTOR ENERGIZING CIRCUIT

Abstract: Drive system for a variable reluctance motor having a pulsated drive. The motor has a stator provided with one or more windings for one or more phases, and a rotor which, upon rotation, co-acts with the magnetic circuit in each stator phase and produces in the magnetic circuit for each stator winding a permeance which changes with changes in the rotor angle. A sensing and control circuit (1-10) senses the inductance in the phase winding (L1, L2, L3) in each phase, at least during a part of a rotor revolution. Upon the indication of a pre-determined inductance Lk, the circuit permits the rotational position of the rotor at which the determined inductance Lk was indicated to constitute a starting point for determining a rotational position ( theta OFF) for changing the energized state of the phase winding.

Description: A motor energizing circuit The present invention relates to an energizing circuit for a reluctance motor of the kind disclosed in the preamble of Claim 1, ' The most common method of commuting from one phase to another in variable reluctance motors, particularly so-called switched type drive motors, is to utilize at least one rotor sensor which is adapted to produce control signals that correspond to the rotational position of the rotor. This method, however, involves the provision of additional elements on the rotor, which in practice has been found to be encumbered with a number of drawbacks and also to give rise to errors, particularly in troublesome environments. Brushless d.c. motors which operate with variable reluct¬ ance are well known to the art. The kind of variable reluctance motor to which the invention relates has a stator with one or more excitation windings arranged in one or more phases, with ' separate activation or energiza¬ tion of the respective phase windings. The stator and rotor form a magnetic circuit for generating a mechanical torque, which is essentially proportional to the square of the ampereturn of the activated or energized winding and to the permeance change time, which is a function of the rotor shift in the motor. A shift in the position of the rotor relative to the stator results in a variation in the reluctance, and subsequently also the permeance, in the magnetic circuit of the stator winding. Torque is obtained in the drive direction of the motor solely when the ampere-turn of the winding is maintained over a time interval in which the permeance increases with rotor displacement or shift. Consequently, it is endeavou¬ red to hold each winding energized solely during one such period for said each winding. For reasons pertaining to drive techniques, it is convenient, although not totally necessary, to activate solely one stator phase at a time. Commutation from one phase to another can be effected so that each phase winding is activated, or energized, during one rotor-position-interval in which supply of current to the winding results in an increased permeance with rotor displacement or shift. The supply to each phase winding is preferably discontinued, or decreased, during each rotor- position-interval in which the ampere-turn of the winding results in a decrease in permeance with rotor displacement or shift. As beforementioned, the most usual method in this regard is to use additional rotor sensors for sensing continuously the rotor position and controlling the ener¬ gizing supply with, the aid of a sensor-controlled circuit. There is a general desire, however, to find ways and means which will allow these rotor-position-sensors to be dis¬ pensed with. Several attempts have been made to utilize the variation in the current or voltage characteristics of the stator windings and surrounding circuits to provide an indication of suitable time points at which the energizing voltage can be switched on and off. A particular problem encountered with switched reluctance motors of the drive motor.type is that they can be operated at both high and low speeds. The majority of known systems which incor¬ porate a facility for sensing motor characteristics for the purpose of controlling the energizing voltage are pri¬ marily intended for stepping motors and while functioning satisfactorily at relatively low motor speeds have a poorer performance, or no performance at all in -respect of speeds which exceed 50 of the maximum motor speed. In one known reluctance motor control system, described in US Patent Specification No. 3,980,933, there is sensed the electromotive force (EMF) induced in the stator winding as the rotor rotates and when the output from a switching device is non-conducting. The output of the switching device is made conductive when the EMF reaches a predeter¬ mined level. This motor requires a considerable bias current in order to afford interference margins. This results in power losses. Furthermore, because no energiz- ing current passes through the winding during the time period in which the rotor position is sensed, it is not possible to load the motor to its maximum. Consequently, an exciting or energizing current must be passed con¬ stantly through one of the phase windings. In the case of * another reluctance motor control system, described in US Patent Specification No. 4,520,302, means are provided for measuring the time during which the flow of current through a stator winding rises or falls from one level to another, in order to provide an indicatio -of the rotor position. Thus, solely the current flow is sensed during this control. This system, which has been designed for controlling a stepping motor, affords poor resolution at high speeds, e.g. speeds exceeding 50$ of the maximum motor speed. The object of the invention is to provide a reluctance motor drive circuit in which no rotor sensors are used but which, nevertheless, is capable of driving the motor at all speeds and loads. This object is achieved with an energizing circuit having the characteristic features set forth in Claim 1. Further features of the invention are disclosed in the remaining claims. In accordance with the invention, at speeds above a given speed v a signal for interrupting the supply of voltage to a winding is derived directly from both the current passing through and the voltage lying across said winding, without the motor drive being affected directly by the measuring process. In this way there is obtained a func¬ tion which at speeds above v corresponds fully to that obtained for a rotor position sensor. As the rotor rota¬ tes, the inductance of each stator winding changes in accordance with a given curve shape, due to variation in permeance during this rotation. In accordance with the invention, the time at which the inductance of a winding has a pre-determined value, L. , is sensed for each phase winding. ; calculating unit then calculates a time point subsequent to the sensed time point, for interrupting the supply of energizing voltage to the winding. The invention will now be described in more detail with reference to the accompanying drawings, i which Fig. 1 is a circuit diagram which illustrates one embodi- ment of the control system according to the invention; Figs. 2-5 are diagrams which illustrate the manner in which the invention operates; Fig. 6 illustrates a circuit for supplementing the circuit shown in Fig. 1; and Fig. 7 is a further diagram which illustrates the manner of operation of the invention. Fig. 1 illustrates three phase windings LI, L2, L3 on the stator of a three-phase reluctance motor. The invention is not restricted to the number of phases of the motor, and three phases are illustrated solely by way of example. The motor is driven by a d.c. voltage V, which may be 310 V for example, this voltage being normal for drive-type and switch-type reluctance motors. Between earth and the posi¬ tive terminal of the voltage source the phase winding LI lies in a circuit which incorporates a current measuring resistor Rl, the source-drain-path of a power transistor Tal, the phase winding 1, and a power transistor Tbl. In this circuit the lower transistor Tal is biased to satura¬ tion during the whole of the time period over which the phase winding LI is energized, while the upper transistor Tbl is pulsed during the energizing interval of the phase, in the manner normal with switched reluctance motors, with which each energizing pulse for one phase is divided into part pulses. The process of dividing a drive pulse into part pulses does not form part of the actual invention and will not therefore be described in more detail. A diode Dal is connected with its anode to earth and its cathode to the part of the phase winding LI remote from the tran- ■ sistor Tal, in order to maintain the current through the phase winding LI throughout the whole of the energizing pulse interval. A diode Dbl is connected with its anode to the part of the phase winding LI remote from the transis¬ tor Tbl and the positive terminal, in order to provide a current circuit in which current can be rapidly drained from the phase winding LI as soon as the transistor Tal is deactivated, i.e. blocked. Each of the remaining phase windings L2 and L3 are connec¬ ted to a respective circuit of the same kind. Thus, the phase winding L2 is incorporated in a circuit comprising a current measuring resistor R2, two power transistors Ta2, Tb2 and two diodes Da2, Db2, and the phase winding L3 is incorporated in a circuit comprising a current measuring resistor R3, two power diodes Ta3, Tb3 and two diodes Da3, Db3. Switching of the transistors to their respective on-andoff modes is controlled by a control unit 1. The control unit is preferably a microprocessor or microcomputer, although a circuit constructed from conventional circuit components may also be used instead. The control unit 1 has six out¬ puts, each of which is connected, via a respective ampli- fier 2, to the gating means of a respective transistor Tal, Ta2, Ta3, Tbl, Tb2, Tb3, for the purpose of gating each transistor individually. In accordance with the invention, there is determined for each phase winding the time point Θ at which the induc¬ tance L in the phase winding on an upwardly extending part of the inductance curve passes through a pre-determined inductance value L, . For the purpose of testing the condition L>L, , the integrated voltage across the phase winding is compared with a product of the current through the winding and the sensed inductance value L.. The L, -condition, hereinafter referred to ' as the funda¬ mental condition, can be derived in accordance with the following: The differential equation for the winding current is where U is the voltage across the phase winding, across that transistor Tal, Ta2 and Ta3 which is excited during the whole of the activation time of the phase concerned, and across the current measuring resistor Rl, R2 and R3 respectively, (the voltage drop across the transistor can be ignored herewith) , R is the resistance of the respec¬ tive current measuring resistor Rl, R2, R3, added to the resistance in the phase winding and the resistance in the continuously activated transistor, L is the inductance of the respective phase winding LI, L2, L3 and i_ is the current through the phase winding. Equat ion 1 i s re-wr i t ten as t If one integrates from the time of initiating the energizing voltage to the phase (t Q =0) to the time _t and assumes that i t =0, i.e. that no current flows in the winding when^ a phase is activated, the equation (L-i). = 0 is obtained, since i t =0. From this there is obtained the condition L(t) > L(k) gives r (U-R.i)dτ > i(t) \ l .e (U-R.i)dτ > L k .i(t) (2) The equation (2) gives the aforementioned L^-condition or fundamental condition according to the invention. For the purpose of testing the fundamental condition according to equation (2) continuously, which needs be tested for each phase solely from the time of initial activation of the phase to the ^ time at which the fundamental condition is fulfilled, the following circuit is provided for each phase: For the purpose of sensing the voltage U continuously, a voltage divider comprising two resistors Ral, Rbl and Ra2, Rb2 and Ra3, Rb3 respectively are connected between earth and the upper end of the phase winding in Fig. 1. The voltage divider has a relatively high total resistance, in order not to load the phase winding circuit unnecessarily. A suitable fraction of the voltage U, i.e. k.U is taken out over the respective earthed resistor Ral, Ra2 and Ra3. * multiplex unit 3 has an input connected to the output " of .each of the three voltage dividers. The multiplex unit 3 is controlled by the control unit 1 such as to couple to the output of unit 3 the signal from the voltage divider for the phase winding whose inductance is to be measured. This can only be effected with one control conductor and the switching process thus takes place in a cyclic sequen- ce for each "l"-signal on the control conductor. In order to reach the voltage U, the output signal from the unit 3 is divided with k in a dividing circuit 4. A multiplex unit 5 has three inputs connected to a respec- tive resistor Rl, R2, R3, all of which have the resistance R " . The fourth input will be described hereinafter. The multiplex unit 5 is controlled by the control unit 1 synchronously with the control of the multiplex unit 3. In this case, however, the control unit 1 produces a digital signal which indicates which input shall be connected to the output. The output signal from the multiplex unit 5 is applied to a multiplicator 6, which multiplicates by the resistance R for the whole winding circuit divided by the resistance R ? . The output signal from the circuit 6 has the value Rl. The output of the dividing- circuit 4 having the voltage U is connected to the (+)-input and the output to the multi¬ plicator circuit 6 having the voltage Rl is connected to the (-)-input of a differentiator 7, so that the voltage on its output is (U-Ri). This signal is supplied to an integrating circuit 8, which integrates the signal from the circuit 7 during times determined by the control circuit 1. The circuit 8 commences a new integration with the control signal obtained from the control circuit 1. This control signal is supplied to the circuit 8 each time a phase is activated. The output of the multiplex unit 5 is also connected to a multiplicator 9, which multiplies the signal R' with L, /R' . The output signal from the unit 9 thus obtains the value L, .i , where L, is the inductance to be detecte . The signals from the integrator 8 and the multiplication circuit 9 are each fed to a respective input of a compara- tor 10, which produces a "l"-signal on its output as soon as the value of the signal from the integrator 8 exceeds the value of the signal from the circuit 9. When the control unit 1 receives a signal from the compa- ' rator 10 and this signal does not lie within an unpermit- ted time interval, as described in more detail herein¬ after, sensing of the property applicable to the phase concerned is complete. The control unit 1 can then send a control signal direct to the multiplex units 3 and 5, causing these units to be activated to allow signals from the next phase in turn to be sensed to pass through. Alternatively, the units can be switched upon activation of the next phase. As will be understood, the whole calculation of the funda¬ mental condition can be carried out with factors which are k times the values, therewith obviating the need for the circuit 4. It should be observed, however, that the control unit 1 does not immediately de-activate the phase in question upon fulfillment of the fundamental condition according to the equation (2) , as will be explained in more detail hereinafter with reference to the diagrams of Figs. 2-5. Instead, the control unit 1 carries out calculations according to pre-set conditions, in order to establish the time at which the phase shall be activated. These conditions are partly dependent on the rotational speed v of the rotor and partly on the current _i_. Consequently, the value of the current i_ must be fed directly to the control unit 1. The output of the multi¬ plex unit 5 is therefore connected to an analogue/digital converter 11 and is fed to a separate input on the control unit 1, which divides the value obtained by R', in order to obtain the value of i_. The value of i_ is also used when driving the motor within the low speed range, as will be described In more detail hereinafter. As beforementioned, the L, -condition, or fundamental condition, in the equation (2) gives an L, -condition angle k , which is dependent on the current strength in the winding, i.e. in the phase winding which has just been driven by the control unit 1. This is because the induc¬ tance is not solely a function of the rotor position, but also of the current i_. This is illustrated in Fig. 2, which shows the variation σf the inductance L in one ohase as a function of the rotor angle Θ over slightly more than one revolution * The diagram shows four different curves 1, , l , l , In, of which each curve is drawn for a separate constant current strength, where 1 is drawn for a very low current strength and l is drawn for a very high current strength. The current strengths, in turn, are contingent, inter alia, on the extent to which the motor is loaded or driven. The fact that the curve shape becomes flatter with increasing current strengths is because the iron in the magnetic circuit of the motor is saturated to progressively greater extents. It is not a constant current strength which determines the actual curve shape of the inductance L, but the fact that the inductance L varies in accordance with the prevailing or momentary current i_ , although Fig. 2 illustrates how the inductance varies with current strength. It will be seen from Fig. 2 that Θ, for detected or sensed L, is displaced to the right with increasing current strengths. Consequently, compensation is made for the current, in accordance with the invention. The current _i is therefore measured by the control unit when the L, -condition is fulfilled. A delay of 0 after Θ is introduced, this delay Θ being dependent on the current i_ in the winding. A low current results in a long delay and a high current in a short delay. The dependency is not totally linear with the current _i_ and, to some extent, is dependent on the motor construction. The control unit 1 contains the relationship between the current i_ for 0. for the motor concerned and effects the delay in accor¬ dance therewith. The angle QF p, i.e. the rotor position angle, at which excitation or activation of the phase concerned is discon- tinued, should also vary with the rotational speed of the motor. At constant Q n „„ the motor obtains a series motor OFF characteristics, i.e. the power is inversely proportional to the speed. If 0FF is permitted to decrease with increasing speeds, the motor obtains a flatter torque/ speed characteristic and it Is possible to obtain a motor with, e.g., constant power, by controlling 0 p. This is achieved by introducing a further delay 0 in addition to 0 prior to shutting down the ω s phase at Q nFF .» this delay depending upon rotational speed. Fig. 3 illustrates a curve shape of the inductance L as a function of 0 for a motor driven with a low current and at high speed, whereas Fig. 4 illustrates a curve shape of inductance L as a function of 0 for a motor driven by a high current and at high speed. Thus, it will be seen from Fig. 3 that both ® , which is the current- dependent current compensation factor, and 0 ω , which is the speed-dependent compensation factor, are low, so that the time between 0 and FF is relatively long. Fig. 4 shows that both ©s„ and Θω are short,' and hence the time between Θ, and Θ 0FF Will also be short. The range of variation for the aforesaid compensation may be relatively large in the case of a number of motors, in which case the fundamental condition L>L, must be ful¬ filled at an early stage. It is even conceivable that the compensating times will exceed the integration times _t. This is illustrated in Fig. 3 where the combined time of θs_ and 0ω is greater than the time between 0 n O.N n ' which represents the rotational angle at which the phase is activated or excited, and 0.. Since the drive circuit according to the invention is intended to replace a sensor circuit for a reluctance motor, and the control unit 1 is preferably a microprocessor, it is suitable in one practi¬ cal application to manufacture a reference motor which is provided with normal sensor control and to investigate where the motor equipped with sensor control de-activates the phase at ø QFF » b operating the motor at different speeds and at different loads, and indicating S, and storing the delays between 0 , and Θ QFF in a. ixed memory in the microprocessor. As beforementioned, it is convenient from the aspect of drive techniques to permit ø to constitute a commutating angle at which transi¬ tion from the excitation of one phase to the excitation of the next phase takes place immediately. At high rotor speeds, commutation shall take place very early, and the delay 0 therewith moves towards 0. It is possible that phase activation at f nM for the next phase L QN is greater than the fundamental condition inductance L.k. LO„ λ N T may J also be g °reater than L,k when the current level j. in a preceding phase is high at the time that commutation takes place, so that θ becomes small. Fig. 5 illustrates this circumstance. The broken line curve illustrates the variation of the inductance L as a func¬ tion of 0 for i=0 and the full line curve illustrates the variation L as a function of 0 when i=i, =0. When a phase is activated, i=0 is included in this phase. The inductance then follows the broken line curve. At the rotation angle 9 the inductance in the phase winding is LON M . As will be seen from the left-hand side of the diagram, L n „ can be greater than L. and also much greater than when the current i, flows in the winding (see the full line curve). The current jL_ rises relatively slowly from the value 0 upon activation of the phase at 0, ™ , and is relatively low during the first part of the activation period during which L^L . . The inductance in this case roughly follows the broken line curve. Thus, an interval of the L-curve can be found right at the beginning of a phase supply, i.e. from 0 nM to Q Q in Fig. 5, during which the fundamental condition L>L^ is fulfilled. It is important to prevent the phase from being de-activated during this interval. Consequently, in accordance with the invention, sensing of the fundamental condition can be blocked for a given period of time sub¬ sequent to activation, up to a rotational angle Θ„, spaced from 0 Q by a good margin. This additional blockaging feature can be inserted, e.g., for speeds above a pre-set level and/or for currents i, above a pre-set Level. Such blocking may also be made a general feature. Interference margins are also improved with such blocking, as opposed to when blocking is not utilized, since it is then no longer necessary to compare L, .i and for small drive angles, during which both magnitudes are small. As mentioned in the aforegoing, the L, -condition accord¬ ing to equation (2) was derived under the proviso that the current i_ in the winding must be zero ampere at the time of phase activation. This can prove problematic since back emf flows in the phase winding long after a phase has been deactivated at Θ 0FFJ as will be seen from the right-hand part of the curve _i in the Fig. 5 diagram. in order to . guarantee that there is no current In the phase winding at the time of activation, phase activation is blocked in accordance with the invention until it is sure that the current is zero. This current is not measu¬ red across the current measuring resistors Rl, R2, R3, when the phase is unactivated, since the lower transistor Tal, Ta2, Ta3, (Fig. 1) is switched off prior to activa¬ tion. A phase activation blocking function can be obtained in at least two different ways. The first method of obtaining a blocking function is illustrated in Fig. 6, which shows the third phase winding L3 and associated energizing circuits Ta3, Tb3, R3, Da3, Db3, together with the control unit 1, and the amplifiers 2 in accordance with Fig. 1, and with additions to this circuit for providing the activation blocking facility. Each phase winding circuit in Fig. 1 shall be provided with the same addition means as those illustrated in Fig. 6. This means includes a so-called "pull-up" resistor R which is connected between the upper part of the phase winding L3 and the positive terminal of the supply 0 voltage. A voltage divider Re and Rd is connected in series with the "pull-up" resistor Rp and earth. The outlet on the voltage divider Re and Rd is connected to a comparator 12, which has a reference voltage U f coupled to its other input. The voltage over the voltage ,5 divider is approximately OV for as long as back emf prevails. Upon termination of the back emf, the voltage rises via R to approximately the level of the supply voltage V. 0 The comparator 12 will transmit a logic signal "0" for as long as back emf continues, and transmits a "l"-signal as soon as the back emf is terminated. Naturally, an equally good result can be obtained by sensing the lower winding outlet on the phase winding with a so-called "pull-down" 5 resistor, or by using the same principle with some other winding configuration, e.g. a bifilar winding. This has not been shown in the Figure, however. The other method of blocking phase activation is one of 0 utilizing the fact that the back emf time is constantly shorter than the drive time at a constant supply voltage V. This can be seen from the curve i_ in Fig. 5 . - The phase winding is deactivated when the rotor angle is Θ Subsequent hereto the current _i_ falls along an exponential 5 curve and reaches the value 0 at the rotation ang σ le 0m. The time between Q U n τr ? -Γ and 0m is therewith always shorter than the time between θON and θOFF. Conse¬ quently, there is measured the total time for which V is applied over the energizing circuit of the phase winding concerned, i.e. the time between 0 0N and 0 QFF> and activation of this phase is then blocked until back emf has continued for the same period of time. Although this implies an overestimation of the back emf time, it lacks all practical significance. Practical tests have shown that this type of blockaging facility has no practical influence on the acceleration of the motor. The aforedescrlbed drive arrangement provides positive commutation under normal motor operation. At very high currents, however, there is a chance that commutation will be excluded due to non-fulfilment- of the condition accord¬ ing to equation (2). This will occur when the current is so high as to prevent the inductance reaching to the level L, . This is illustrated in Fig. 2 by the lower curve Ln. The three Inductance curves 1, , 1~, 1-, reach and exceed the level L, . Commutation will then take place. The curve 1 4„ fails to reach the level L.k. In this case there is * no commutation. The problem is parti¬ ally solved by selecting L, at a low Inductance and to combine this lower value of L. with the aforesaid delays 0 and 0 ω , as illustrated in Figs. 3 and 4. This provides a satisfactory solution when a chopping function is incorporated for pulsing the drive of the phase wind¬ ings, as effected with the upper transistors Tbl, Tb2, Tb3 in Fig. 1. This limits the current to a sufficiently low value. There are times, however, when this is ' not suffi¬ cient, particularly when the peak current is much higher than the maximum current with commutation. Such a curve shape is illustrated in Fig. 5, where the current i_ reaches a peak value i , which lies far above the P' current i, , measured at β .. In order to guarantee that commutation will always take place even with extreme overcurrents, there is utilized a high current limiting level. This high current limiting level must always be found in a motor, in order to protect the electronics thereof, and this level is now used in accordance with the invention to provide a commutating signal in the manner described in more detail herebelow. As illustrated in Fig. 1, the current in the activated phase winding is sensed continuously by the control unit 1 via the analogue/digital converter 11. When sensing the lower current limiting value, the upper power transistor Tbl, Tb2, or Tb3 is switched-off. The current jL then falls normally. Subsequent to switching-off the one power tran- sistor in the winding circuit, current is only able to rise when the inductance of the motor decreases. If the current should rise subsequent to switching-off the upper power transistor, this would mean that the position of maximum inductance of the inductance curve has been passed without commutation taking place and that there has been reached an angular position which lies somewhere on the negative flank of the inductance curve. The motor will then produce a drive-emf and the current will increase. Thus, if the current increases subsequent to sensing maxi- mum current, commutation shall take place immediately. The diagram in Fig. 7 illustrates an example of the shape of the curve i(0) in the case of commutation when L, is not sensed. At the rotation position the overcurrent or excess current i max is sensed. The upper power tran¬ sistor Tbl, Tb2 or Tb3 is therewith switched off. The current i(ø) then falls. The upper power transistor is again switched-on at 0, and the current rises and again reaches imax at the rotational position 0e,' the up^per power transistor again being switched off. The inductance curve, however, has now passed its maximum, as shown in the full line curve L(0,i). The current i(0) now no longer falls, but instead rises relatively slowly. At the rota¬ tion position 0 nFF there is sensed a current i- which is higher than imax. Commutation to the next phase then takes place immediately. Instead of sensing maximum current through the analogue/- digital converter ll r it Is possible as is usual in such circumstances, to provide an additional comparator circuit constructed to sense excess current separately and to indicate directly to the control unit 1 when excess current or overcurrent Is ' reached. There is therefore illustrated in broken lines in the circuit shown In Fig. 1 a voltage dividing circuit which includes three series- connected resistors Re, Rf, Rg between the positive terminal on the voltage source V and earth. The outlet between the resistors Rf and Rg is connected to a referen¬ ce voltage input on a comparator 13 and the outlet between the resistors Re and Rf is connected to a reference volta- ge input on a comparator 14. The output from the multiplex unit 5 is coupled to the (+)-input of both comparators 13 and 14. The voltage across Rg is so selected that the comparator 13 will produce a "l"-signal as soon as the pre-set maximum permitted current level ima„x has been reached. The reference voltage to the comparator 14 is somewhat higher than that for the comparator 13. Conse¬ quently, the comparator 14 will produce a "l"-signal for a current level which is slightly higher than the maximum permitted level i__„. Each of the outputs of the compa- rators 13 and 14 is connected to a respective input on the control unit 1, which controls in the manner afore- described. As will be seen from Fig. 1, the control unit 1 is also supplied with a control signal from without on a parallel input. This control signal indicates to the control arrangement the speed desired. The control signal also indicates to the control arrangement when the motor is to be started and stopped. A special start function is required for starting the motor. The simplest method in this regard is for the control arrangement to impose a current pulse on a phase by steering the two power transistors in the phase for a second or two, so that the motor locks in the maximum inductance state for this phase. Forced commutation is then effected to the next phase, whereafter subsequent commutations are effected in the aforedescribed manner. The aforedescribed sensing and control principle operates satisfactorily at high and average rotational speeds and provides equally as good commutation as will a' conventio¬ nal sensor. Theoretically the principle can function right down to rotational speeds of zero revolutions per second. In this latter regard, however, it is necessary to carry out precise compensation of the winding resistance, which resistance obtains ^ an increasing significance at precisely low speeds. It is difficult to determine the winding resistance exactly, however, since the resistance varies, inter alia, with motor temperature. Consequently, it is difficult in practice to carry out accurate compensation at low speeds. Tests have shown that the aforedescribed sensing and control principle functions satisfactorily down to 5$ to 10$ of the maximum speed of the motor, and is able to function at still lower speeds, including zero speed conditions, provided that the motor is only subjected to small loads. However, in order to obtain a control system which will operate satisfactorily under all conditions throughout the whole of the speed range, the system according to the invention is constructed to monitor the motor speed and to detect or sense when the motor holds a pre-determined, relatively low speed v , e.g. a speed which is 20$ of the maximum motor speed. At speeds above V the circuit illustrated in Fig. 1 operates in accordance with the aforedescribed principle, by determining the inductance of the phase winding which is activated to find an inductance value L. which forms a starting point for determining the time for deactivating the phase. At speeds beneath the speed V it is suitable instead to sense the inductance of the phase which is to be activated in order to detect an inductance value at which commuta¬ tion shall take place for activating the phase. Since no current will normally flow in an unactivated winding, the winding inductance must be indicated in a manner different to that described above. Consequently, high frequency pulses of short duration are supplied to the gating means of the power transistors in the drive circuit for that winding which Is next in turn for activa¬ tion. Each pulse is of a given duration _t, which is short in relation to the period time, so that the current is able to fall to zero between each pulse. The current is measured by the analogue/digital converter at the end of each pulse. The current rise over the duration of each pulse provides a measurement of the momentary inductance. Thus, within this speed range the control unit 1 instructs the multiplex unit 5 to supply voltage across the resis¬ tors Rl, R2, R3 incorporated in the phase circuit which is next in turn for activation and not in the prevailing activating phase circuit as in the case of the high speed range. The control unit 1 determines the inductance by approxi¬ mating the equation (U-Ri)=d/dτ(Li) with U=L.di/dτ, which is a good approximation for small currents i_ and low speeds, i.e. low dL/dτ. The US Patent Specification 4,520,302 mentioned in the introduction describes a system m which measures time for current change in a non-exciting phase, which in practice implies measuring the inductance in this phase. Conse- quently, according to this prior publication commutation is effected when the inductance in the phase on which measurements are made has reached a pre-determined value. In this known control system it is assumed that the drive voltage is constant. In practice, however, the drive voltage V can vary radically, partly due to normal voltage variations and partly due to the voltage ripple obtained when +V is a rectified a.c. voltage. The inductance in a non-exciting phase is also contingent on the current strength of the exciting phase. Neither , does the US Patent Specification 4,520,302 take into account those variations in inductance which are due to current level, which renders it difficult to drive the: motor described therein at different loads. As discussed in the aforegoing, the inductance in a phase is highly dependent on the current prevailing therein. Parts of the iron circuit of present day reluctance motors are most often common to the various phases. Saturation, and there- with reduced inductance in a phase (see Fig. 2), therefore results in partial saturation and therewith reduced induc¬ tance also in remaining phases. Consequently, Fig. 2 can, in principle, also be said to describe the inductance in a phase as a function of the current i_ in another phase, particularly when the current is low in the phase on which the measurement is made. Thus, the various curves in Fig. 2 can be said to corres¬ pond to different currents in the exciting phase when a non-exciting phase is measured. Consequently, in accordance with a further development of the invention, compensation is made within the low speed range, i.e. speeds beneath v , both for varying supply voltage +V and for varying voltage in the energized winding. A voltage divider comprising two series-connected resistors R and R is connected between the positive terminal at +V on the voltage source and earth. The R , R outlets of the voltage divider are connected to the y fourth input of the multiplex unit 5..The voltage U' measured across R is therewith proportional to +V. y For each pulse of short duration transmitted to the monitored winding the control unit 1 will now steer the multiplex unit 5 in a selected sequence the voltage across the resistor Rl, R2 or R3 in the monitσred phase, the voltage over the measuring resistor Rl, R2, R3 in the energized phase and the voltage U' over the resistor R . The control unit 1 thus indicates the momentary current at the end of each short-duration pulse sent to the monitored winding in the non-energized phase, by supplying a control pulse to the control input of the analogue/digital conver¬ ter 11 upon termination of the short duration pulse. In conjunction herewith, i.e. immediately before or after, an indication is also given of the current in the energized phase and the voltage U' by steering the multiplex unit 5 and the analogue/digital converter 11 at appropriate time points. The control unit 1 then receives on its inputs connected to the analogue/digital converter 11 signals having known proportions to those signals which are desired to be measured. In order to obtain a rotor position point 0 nFF which is as constant as possible for a selected rotor speed, It is fully possible to carry out compensation with varying compensation in a manner analogous with the manner carried out with 0 within the high speed range. This cannot be effected, however, when the motor is stationary, i.e. when actually starting the motor. Consequently, it is more advantageous to determine instead the momentary inductance, or a value proportional thereto and to compensate the inductance value determined. The function L (0,i b ), i.e. the inductance in a phase a. as a function of the current in a phase b_, is not linear with i, . A good approximation for the majority of types of reluctance motors is most often a (0 c ,0)/L b (θ c ,i b ) = (l + c.i b ) where the constant o_ is determined individually for each motor, so as to ' maintain © 0FF constant. 0 now corres¬ ponds to 0^ within the high speed range. Θg FF is preferably equal to 0 within the low speed range. , ' Natu- C I rally, this will apply provided that compensation of the inductance is effected in the aforedescribed manner. The commutating condition to be fulfilled upon compensating the inductance for both momentary supply voltage level and energizing current level is then: L=L c —^> (l+c.i b ).U.T/i=L c This enables a purely static commutation to be obtained irrespective of the current strength of the energized phase and the supply voltage. Static commutation which is independent of rotor rotation in the aforesaid manner can also be obtained provided that the speed is low. Firstly it is necessary that the approximation d/dτ (L.i)=L.di/dτ applies (i.e. in dL/dτ<<Ldi)/dτ) , and secondly it is necessary for the frequency of the inductance-sensing pulses to be much higher than the motor commutating frequency, since this frequency determines the time division in the commutating process. In practice these limitations imply that the motor can be driven solely between 20$ and 50$ of Its maximum speed when applying this commutating method. At speeds beneath this limit, however, there is obtained a function which corresponds completely with the function obtained with a rotor position sensor. The rotor point 0 QF p has been discussed in the afore¬ going with reference to Figs. 3 and 4. It will be under- stood that each phase winding can be energized individual¬ ly and in a manner to operate optionally, with overlap between the phases, such that two phases are driven simul¬ taneously during given intervals. If, however, overlap between the phases Is not employed by that commutation is effected at the rotation angle 0 QFF from one phase to another, 0 0M will be displaced within the rotor angle in the same manner as 0 O.-.,F-,_F. In Fig. 3, where Q 0FF lies relatively close to the upper part of the inductance curve, 0 QN lies within a range of the inductance curve in which the inductance is lowest. At high speeds and high currents Θ 0FF will move further to the left i.e. downwardly on the rising part of the inductance curve, as illustrated in Fig. 4. 0~ M will therewith also move to the left, as illustrated in Fig. 4, and in the case of normal operation will actually occur at an Interval on the inductance curve in which the curve has a negative slope. This is also illustrated in both Fig. 5 and Fig. 7. In the case of extremely low speeds it may be suitable in the aforedescribed energizing process for the low speed range to activate or energize the phase immediately at the beginning of the rising part of the L-curve, although in the case of somewhat higher speeds within the low speed range, and in particular when the speed approaches the speed v , it may instead be suitable to move the rotation-position 0,-,., at which activation is initiated farther to the left, so that activation already takes place on the negative flank of the inductance curve imme¬ diately prior to the region of very low inductance. This results in improved and smoother functioning of the motor, particularly when the motor passes the speed v , where the drive circuit switches from a driving or energi- zed mode in the low speed range to a driving or energi¬ zed mode in the high speed range, Displacement of the activation point Θ QN from a rising flank of the induc¬ tance curve to a falling flank of said curve can be carried out continuously. It Is difficult, however, to sense an inductance differential during the next straight part of the inductance curve when inductance is very low, and consequently it may be suitable instead to move 0 0M continuously during the rising and falling parts of the inductance curve and to execute stepwise movement between these locations. The activation point may also be moved stepwise in a number of stages. The possibility of dis¬ placing the activation point becomes more significant with fewer phases. Consequently, the greatest significance of this displacement possibility lies with motors having two or three phases. The control unit 1 is therefore conveniently provided with a program for the low speed range in which the inductance value and the sign for inductance change for giving 0 0M is different for different speeds or speed ranges within the low speed range. The boundary speed v at which the control system switches between sensing modes can be selected with a relative degree of freedom, although it preferably lies within the range of 10-20$ of the maximum speed. Naturally, this switching between the sensing modes takes place with a given hysteresis in speed. With a suitably selected boundary speed v , which boun¬ dary speed may- be different with different motor construc- tions, it is possible to obtain commutation over the whole speed range of the motor, this commutation corresponding totally to the commutation obtained with a rotor position sensor. Conseqeuently, variable a reluctance motor provi¬ ded with the control system according to the invention can be driven at all speeds from a stationary state to a state of maximum rotor speed under optimum operating conditions. Many modifications are possible within the scope of the invention.

Claims: CLAIMS 1. An energizing system for a variable reluctance motor comprising a stator which is provided with one or more windings for one or more phases, and further comprising a rotor which upon rotation co-acts with the magnetic cir- cuits in each stator phase and generates in the magnetic circuits of each stator winding a permeance which changes with rotor angle, characterized by a sensing and control circuit (1-10) constructed to sense the inductance in the ' phase winding (LI, L2, L3) or a magnitude clearly related to the inductance in each phase at least during a part of the revolution of the rotor when a respective phase is an energized phase, and which when indicating a pre-determi- ned inductance L, permits the rotational position of the rotor, when the pre-determined inductance L, is indica- ted, to constitute a starting point for determining a rotational position for changing the energized or excita¬ tion state of the phase winding. 2. An energizing system according to Claim 1, characteri- zed in that when the inductance level L, is reached the sensing and control circuit (1-10) deactivates the phase energization subsequent to a time delay which is dependent on predetermined operating parameters of the motor at the moment concerned. 3. An energizing system according to Claim 2, characteri¬ zed in that one of the operating parameters is the pre¬ vailing current strength in the phase winding. 4. An energizing system according to Claim 2, characteri¬ zed in that one of the operating parameters is the pre¬ vailing motor speed. 5. An energizing system according to any of the preceding claims, characterized in that for each phase, at least during the time of monitoring said phase, the current in the phase winding is arranged to be indicated over a resistor (Rl, R2, R3) connected in series with the winding (LI, L2, L3) ; in that the voltage across the winding and the resistor is arranged to be indicated; and in that the sensing and monitoring arrangement (1-10) continuously forms and makes a comparison between the following values where U is the indicated voltage, j_ is the indicated current, R is the resistance of the resistor (Rl, R2, R3) added with the resistance of the phase winding, and L^-, is a constant, the time t=0 being set upon activation or energizing of the phase; and in that the sensing and control arrangement is constructed to indicate the rotor position when the comparison indicates that the inductance of the phase winding is L^.. 6. An energizing system according to Claim 5, characteri¬ zed in that the sensing and control arrangement (1-10) is constructed so as not to begin to respond to the compari¬ son until the rotor has rotated through a pre-deter ined rotor angle subsequent to energizing (at Θ 0M ) the par- ticular phase being monitored. 7. An energizing system according to any of the preceiding claims, characterized in that the sensing and control arrangement (1-10) is constructed to prevent the energiz- ing of a desenergized phase until after a time point at which the current through the phase winding is 0. 8. An energizing system according to Claim 7, characteri¬ zed in that the sensing and control arrangement is con¬ structed to determine the time between energizing (at 0 QFF and desenergization (at Θ Q FF^ anc n0 ^ ^° s ^ eer the phase to energization the next time until there is reached a time point which at least equals the time lapse after the time of desenergization (at Θ ) . 9. An energizing system according to any of the preceding claims, characterized in that the sensing and control circuit (1-10) is constructed in a known manner to sense when the current passing through the winding in the ener¬ gized phase reaches a pre-determined highest permitted current level, and to adjust energizing of the phase by supplying pulses to the winding; in that the sensing and control circuit (1-10) is constructed to effect commuta¬ tion to energizing of the next phase when the current in . the monitored phase winding during a pulse pause having a pre-determined level exceeds the pre-determined highest current level. 10. An energizing system according to any of the preceding claims, characterized in that the sensing and control arrangement is constructed to indicate rotor speed; in that said detecting and control arrangement is construc¬ ted, at speeds above a pre-determined speed v , to moni¬ tor the inductance in the energized phase winding such as to indicate an inductance L. which can constitute a starting point for calculating desenergizing of the phase, and at a speed beneath the pre-determined speed v is constructed to indicate the inductance in the phase wind¬ ing of the phase which is next in turn to be energized, in order to obtain a time point for energizing of said phase. 11. An energizing system according to Claim 10, characte¬ rized in that at least at speeds beneath the pre-determi- ned speed v the point of the inductance curve at which the control arrangement steers the phase to energizing is different for low and high speeds within said speed range, such that the sensing and control arrangement (1-10) steers the phases to energizing at a rotor position in which the inductance curve has a positive flank, at very low speeds, and at a rotor position in which the induc¬ tance curve has a negative flank, at speeds which lie, relatively close to vn 12. An energizing system according to Claim 10 or 11, characterized in that at speeds beneath the pre-determined speed (v ) the sensing and control circuit (1-10) senses the current in the phase winding in the energized phase and corrects the indicated inductance in the phase winding in the phase which is next in turn for energizing with a factor which is dependent on the current in the energized phase. 13. An energizing system according to any of Claims 10-12, characterized in that at speeds beneath the pre-determined speed (v ) the sensing and control circuit (1-10) senses the momentary drive voltage level and corrects the indica¬ ted inductance in the phase winding in the phase which is next in turn for energizing with a factor which is depen¬ dent on the prevailing drive voltage level. 14. An energizing system according to any of Claims 10-13, characterized in that at speeds beneath the pre-determined speed (v ) the sensing and control circuit (1-10) is constructed to supply voltage pulses of short duration over the phase winding in the phase next in turn to be energized, and for each pulse to measure the current level i_ in said phase winding upon termination of the pulse, the duration of which is _t, and to measure the current i, in the phase winding in the energized phase and to measure the drive voltage U' in conjunction with measuring ia,' aanndd ttoo mmaakkee tthhee fftollowing inductance calculation at each measuring moment L=(l+c.i b ) U'.t/i where k is a constant contingent on the motor concerned, and to compare the calculated inductance with an induc¬ tance value Lc ,' for which commutation shall take place.

Inventors: HEDLUND GUNNAR, LUNDBERG HENRIK, HEDLUND, GUNNAR, LUNDBERG, HENRIK
Applicants: EMS ELECTRONIC MOTOR SYSTEMS, EMS ELECTRONIC MOTOR SYSTEMS AB
Application year: 1987
Main classification: H02P6
IPC codes: H02P6, H02P25