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    • 专利摘要:
    CONTROLLER AND METHOD FOR TRANSITION BETWEEN CONTROL ANGLE.The present invention relates to a system that includes a pulse width module (PWM), a subtraction module, an error reduction module, and a sum module. The PWM module controls switching of an inverter that energizes a motor. The PWM module controls switching based on a first angle in a first mode and a second angle in a second mode. The subtraction module determines a difference between the first and the second angle. The error reduction module (i) stores the difference when a transition from the first mode to the second mode is commanded and (ii) decreases a magnitude of the stored difference to zero. The sum module calculates a sum of the stored difference and the second angle. The PWM module controls switching based on the sum in the second mode.
    公开号:BR112012003132A2
    申请号:R112012003132-5
    申请日:2010-08-10
    公开日:2020-08-11
    发明作者:Charles E. Green；Joseph G. Marcinkiewicz
    申请人:Emerson Climate Technologies, Inc.；
    IPC主号:
    专利说明:

    Invention Patent Descriptive Report for "CONTROLLER AND METHOD FOR TRANSITION BETWEEN CONTROL ANGLE".
    Cross Reference to Related Orders The present invention claims priority for US Utility Application No. 12 / 852,625, filed on August 8, 2010 and Provisional Application No. 61 / 232,633, filed on August 10, 2009, whose descriptions are fully incorporated into the present by way of example.
    Field This description relates to electric motor control systems and methods.
    Background The background description provided here is intended to present the context of the description without details. The work of the currently named inventors, as far as is described in that background section, as well as aspects of the description that might not otherwise qualify as state of the art at the time of deposit, are neither expressed nor implicitly admitted as prior art against the present description.
    Electric motors are used in a wide variety of industrial and residential applications including, but not limited to, heating, ventilation and air conditioning (HVAC) systems. For example, an electric motor can drive a compressor in an HVAC system. One or more additional electric motors can also be implemented in the HVAC system. Just as an example, the HVAC system can include another electric motor that drives a fan associated with a condenser. Another electric motor can be included in the HVAC system to drive a fan associated with an evaporator.
    The energy factor is an indicator of the relationship between the current and voltage in a circuit, or how a circuit effectively uses real energy compared to storage and return energy for an energy source.
    The energy factor can be expressed as a value between zero and one.
    The use of the actual effective energy circuit divided by the total amps of | - voltage across the circuit may increase as the power factor approaches one.
    In several implementations, an energy factor correction (PFC) system can be implemented. PFC systems generally operate to increase a circuit energy factor to one, thereby increasing the circuit's use of real energy as compared to the amount of reactive energy the circuit stores and returns to the source. .
    Summary A system includes a 'pulse width modulation' (PWM) module, a subtraction module, an error reduction module, and a module. sum module.
    The PWM module controls the switching of an inverter that powers a motor.
    The PWM module controls switching based on a first angle in a first mode and a second angle in a second mode.
    The subtraction module determines a difference between the first and second angles.
    The error reduction module (i) stores the difference when a transition from the first mode to the second mode is commanded and (ii) decreases a magnitude of the stored difference to zero.
    The sum module — calculates a sum of the stored difference and the second angle.
    The PWM module controls switching based on the sum in the second mode.
    In other aspects, the system also comprises a commanded angle generation module.
    The angle generation module controls the first angle based on a commanded speed.
    In still other aspects, the first angle is generated by the integration of the commanded speed.
    In additional aspects, the system also comprises a limitation module.
    The limiting module generates the speed controlled by limiting the index of a requested speed.
    In yet additional aspects, the system also comprises an evaluator module.
    The evaluator module determines the second angle with |
    | 3/35. . | based on measured engine parameters.
    The measured parameters include at least one of measured currents and measured voltages. - In other respects, the evaluator module determines an evaluated speed.
    The PWM module controls switching based on the rated speed after the transition from the first mode to the second mode. | In still other aspects, the error reduction module decreases the magnitude of a predetermined amount of periodic intervals.
    In additional aspects, the system also comprises a transition module.
    The transition module commands the transition from the first mode to the second mode when an rated engine speed is greater than a predetermined speed. | . In yet additional aspects, the system also comprises a 'transition module.
    The transition module controls the transition from - the first mode to the second mode when the engine has run for more than the predetermined period.
    One method includes: controlling the switching of an inverter that energizes a motor based on a first angle in a first mode and a second angle in a second mode; determine a difference between the first and second angles; store the difference when a transition from the first mode to the second mode is commanded; decrease the stored difference to zero; calculate a sum of the stored difference and the second angle; and control the switching based on the sum of the second mode.
    In other respects, the method also includes generating the first — angle based on a commanded speed.
    In still other aspects, the method also includes generating the first angle by integrating the commanded speed.
    In additional aspects, the method also includes generating the speed commanded by limiting the index of a requested speed.
    In additional aspects, the method also includes determining the second angle based on the measured parameters of the engine.
    The measured parameters include at least one of the measured currents and the
    | . . 4/35 | | measured voltages.
    In other respects, the method also includes determining one. rated speed and control switching based on the rated speed after the transition from the first mode to the second mode.
    In still other aspects, the method also includes decreasing the magnitude by a certain amount at periodic intervals.
    In additional aspects, the method also includes commanding the transition from the first mode to the second mode when an rated engine speed is greater than a predetermined speed.
    In still additional aspects, the method also includes commanding the transition from the first mode to the second mode when the engine is out. has been running for longer than a predetermined period.
    A system includes a control module, an angle determination module and a reduction module.
    The control module controls: a motor based on a first rotor angle in a first mode and controls the motor based on a second rotor angle in a second mode.
    The angle determination module (i) determines the second rotor angle based on a sum of a stored value and a third rotor angle and (ii) after the second mode is selected, defines the stored-air value for a difference between the first rotor angle and the third | rotor angle.
    The reduction module reduces a magnitude of the stored value to zero over a different period of zero after selecting the second mode.
    Other areas of applicability of this description will become clear from the detailed description provided here.
    It should be understood that the detailed description and specific examples are only intended to illustrate and not to limit the scope of the description.
    Brief Description of the Drawings This description will be fully understood from the detailed description and the accompanying drawings, in which: figure 1 is a functional block diagram of an exemplary cooling system; |
    . . 5/35 figure 2 is a functional block diagram of an exemplary drive controller and an exemplary compressor; . Figures 3a to 3c are simplified schematics of exemplary energy factor correction (PFC) modules; figures 4a to 4c are simplified schemes of exemplary power inverter modules and motors; figure 5 is a functional block diagram of a motor control module according to the present description; figure 6 is a functional block diagram of an angle determination module according to the present description; Figure 7 illustrates a transition from open loop to closed loop operation in accordance with the present description; and figure 8 illustrates a method for the transition of the la- operation. open section for closed loop operation according to the present description. Detailed description The following description is of an illustrative nature only and is not intended in any way to limit the description, its application or uses. For the sake of clarity, the same numerical references in the drawings will be used to identify similar elements. As used in the context, the phrase at least one of A, B and C must be considered as a logic (A, B or C) using a non-exclusive logic or it must be understood that they can be executed within an orderly method without changing the principles of this description.
    As used here, the term module can refer to, be part of, or include an Application Specific Integrated Circuit (ASIC); an electronic circuit; a combinatorial logic circuit; a programmable field door arrangement (FPGA); a processor (shared, dedicated, or group) that executes code; other suitable components that provide the described functionality; or a combination of part or all of the above, such as a chip system. The term module can include memory (shared, dedicated, or group) that stores code executed by the processor |
    | 6/35 | ache. i The term code, as used in the context, can include soft-. ware, hardware programming, and / or microcode, and can refer to programs, routines, functions, classes, and / or objects. The shared term, | S as used in context, means that some or all of the code from multiple modules can be executed using a single (shared) processor. In addition, some or all codes of multiple modules can be stored by a single (shared) memory. The term group, as used in the context, means that some or all of the codes in a single module can be executed using a group of processors. In addition, some or all codes from a single module can. be stored using a group of memories. The devices and methods described in the context can be im-. supplemented by one or more computer programs run by one or more processors. Computer programs can include instructions executable by a processor that are stored in a non-transitory, tangible computer-readable medium. Computer programs can also include stored data. The non-limiting examples of the non-transient tangible computer-readable medium are volatile memory, magnetic storage and optical storage.
    Referring now to Figure 1, a functional block diagram of a cooling system 100 is shown. The cooling system 100 can include a compressor 102, a condenser 104, an expansion valve 106, and an evaporator 108. In accordance with the principles of the present description, the cooling system 100 can include additional and / or alternative components. In addition, this description is applicable to other types of refrigeration systems including, but not limited to, heating, ventilation, and air conditioning (HVAC) systems, thermal pump, and cooler. Compressor 102 receives refrigerant in the form of steam and compresses the refrigerant. Compressor 102 provides pressurized cooling and steam form to condenser 104. Compressor 102 includes
    | an electric motor that drives a pump. Just as an example, pump i of compressor 102 may include a scrollable compressor or a compressor. alternative pressor. All or part of the pressurized refrigerant is converted into liquid form inside condenser 104. Condenser 104 transfers heat out of the refrigerant, thereby cooling the refrigerant, When the refrigerant vapor is cooled to a temperature below! a saturation temperature, the refrigerant turns into a refrig- | liquid (or liquefied). Condenser 104 may include an electric fan that increases the heat transfer rate out of the refrigerator. rante. | . Condenser 104 supplies the refrigerant to the evaporator | 108 through expansion valve 106. Expansion valve 106 controls | 7 la the flow rate at which refrigerant is supplied to evaporator 108. | Expansion valve 106 may include a thermostatic expansion valve | ca or can be controlled electronically, for example, by a system controller '130. A pressure drop caused by the expansion valve 106 can cause a part of the liquefied refrigerant to return to steam. In this way, evaporator 108 can receive a mixture of refrigerant vapor and liquefied refrigerant. The refrigerant absorbs heat in the evaporator 108. The liquid refrigerant turns into vapor when heated to a temperature that is higher than the saturation temperature of the refrigerant. Evaporator 108 may include an electric fan that increases heat transfer to the refrigerant. A 120 utility supplies power to the cooling system
    100. Just as an example, utility 120 can provide single phase alternating current (AC) power at approximately 230 Volts (V) mean square value (RMS) or at another suitable voltage. In several implementations, utility 120 can supply three-phase power at approximately 400 Volts or 480 Volts RMS at a line frequency of, for example, 50 or 60 Hz. Utility 120 can supply AC power to the | system controller 130 via an AC line. AC power can also be supplied to a drive controller 132 via the line. B.C. System controller 130 controls the cooling system
    100. Just as an example, system controller 130 can control cooling system 100 based on user inputs and / or parameters measured by various sensors (not shown). The sensors can include pressure sensors, temperature sensors, current sensors, voltage sensors, etc. The sensors can also include feedback information from the drive controller, such as motor current or torque, over a serial data bus or other suitable data bus. A user interface 134 provides user inputs “for system controller 130. User interface 134 can additionally or alternatively provide user inputs for drive controller 132. User inputs can include , for example, a desired temperature, requests related to the operation of a fan (for example, the evaporator fan), and / or other suitable inputs. System controller 130 can control the operation of condenser fans 104, evaporator 108, and / or the expansion valve
    106. Drive controller 132 can control compressor 102 based on commands from system controller 130. Just as an example, system controller 130 can instruct drive controller 132 to operate the compressor motor at a given speed. nity. In various implementations, drive controller 132 can also control the condenser fan. Referring now to figure 2, a block diagram of drive controller 132 and compressor 102 is shown. An electromagnetic interference (EMI) filter 202 reduces EMI that could otherwise be injected back into the AC line by the drive controller
    132. Offiltro EMI 202 can also filter EMI carried on the AC line.
    A power factor correction module (PFC) 204 receives AC power from the AC line as filtered by the EMI 202 filter. The PFC module. 204 (described in more detail with reference to figures 3a, 3b and 3c) rectifies the AC energy, thus converting the AC input energy into direct current (DC) energy. The generated DC power is supplied in positive and negative terminals of the PFC module. The PFC 204 module also selectively provides power factor correction between the incoming AC power and the generated DC power.
    The PFC 204 module selectively boosts AC power to a DC voltage that is greater than a peak AC power voltage. Just as an example, the PFC module can operate in a passive mode,: where the DC voltage generated is less than the peak voltage of the AC power. The PFC 204 module can also operate in an active mode, where the DC voltage * generated is greater than the peak voltage of the AC power. The DC voltage that is greater than the peak voltage of the AC power can be referred to as the driven DC voltage.
    AC power that has an RMS voltage of 230 V has a peak voltage of approximately 325 V (230 V multiplied by the square root of 2). Just as an example, when operating AC power that has an RMS voltage of 230 V, the PFC 204 module can generate DC voltages between approximately 350 V and approximately 410 V. Only as an example, the lower limit of 350 V can be imposed to avoid unstable operating regimes of the PFC 204 module. Limits may vary, such as the actual AC input voltage value. In several implementations, the PFC 204 module may be able to achieve boosted DC voltages higher than 410 V. However, the upper limit may be imposed to improve the long-term reliability of components that experience higher voltage stress. higher, such as the components in a DC 206 filter. In many implementations, the upper - and / or lower limits can be varied.
    The DC 206 filter filters the DC energy generated by the PFC 204 module. The DC 206 filter minimizes ripple voltage present in the DC energy that results from converting AC power to DC energy. In several implementations, the DC 206 filter can include one or more filter capacitors - in series or parallel connected between the positive and negative terminals of the PFC 204 module. In such implementations, the positive and negative terminals of the PFC 204 module can be connected directly to the positive and negative terminals of a 208 inverter power module.
    The inverter power module 208 (described in more detail with reference to figures 4a, 4b and 4c) converts the DC energy, filtered through the DC filter 206, into AC energy that is supplied to the compressor motor.
    Just as an example, the inverter power module 208 can convert the DC power into three-phase AC power and supply the phases of the AC power to. three respective windings of the compressor motor 102. In other implementations, the inverter energy module 208 can convert + DC energy into more or less energy phases. The DC-DC 220 power supply can also receive filtered DC power. The DC-DC 220 power supply converts DC power into one or more DC voltages that are suitable for various components and functions. Just as an example, the DC-DC power supply 220 can reduce the DC power voltage to a first DC voltage that is suitable for digital logic power and a second DC voltage that is suitable for controlling switches within the PFC 204 module. For example, the second DC voltage can be selectively applied to switch terminals port terminals. In various implementations, DC power can be supplied by another DC power source (not shown) - for example, a DC voltage derived through a main VAC 230 input transformer.
    In several implementations, the first DC voltage can be approximately 3.3 V and the second DC voltage can be approximately 15 V. In many implementations, the DC-DC 220 power supply can also generate a third voltage A.D. Just as an example, the third DC voltage can be approximately 1.2 V. The third DC voltage can be derived from the first DC voltage using a voltage regulator. Just as an example, the third DC voltage: can be used for digital core logic and the first DC voltage can. be used for input / output circuits of a PFC i 250 control module and a 260 motor control module. The PFC 250 control module controls the PFC 204 module, and the 260 motor control module controls the power module inverter
    208. In several implementations, the PFC 250 control module controls the switching of the switches within the PFC 204 module, and the motor control module 260 controls the switching of the switches within the 208 inverter power module. The PFC 204 module can be implemented with 1.23 or more phases. . A supervisor control module 270 can communicate with system controller 130 through a communications module 272. O. communications module 272 can include an input / output port and other suitable components to serve as an interface between system controller 130 and supervisor control module 270. communications module 272 can implement wired and / or wireless protocols . The supervisor control module 270 provides several commands for the PFC control module 250 and the motor control module 260. For example, the supervisor control module 270 can provide a commanded speed for the motor control module 260. The commanded speed corresponds to a desired rotational speed of the compressor motor 102. In several implementations, the commanded compressor speed can be supplied to the supervisor control module 270 by the system controller 130. In several implementations, the module supervisor control 270 can determine or adjust the commanded compressor speed based on the inputs provided via the communications module 272 and / or parameters measured by various sensors (ie sensor inputs). The supervisor control module 270 can also adjust the commanded compressor speed based on feedback from the PFC 250 control module and / or from the motor control module 260.
    The supervisor control module 270 can also provide other commands for the PFC 250 control module and / or the motor control module 260. For example, based on the commanded speed, the control module supervisor control 270 can command the PFC control module to produce a commanded bus voltage. The supervisor control module 270 can adjust the commanded bus voltage based on additional inputs, such as operating parameters of the inverter power module 208 and the measured voltage of the input AC line.
    The supervisor control module 270 can diagnose faults in various systems of the drive controller 132. Just as an example, the supervisor control module 270 can receive information from. failure of the PFC 250 control module and / or the motor control module
    260. The supervisor control module 270 can also receive fault information via the communications module 272. The supervisor control module 270 can manage reports and fault compensation between drive controller 132 and system controller 130.
    Responsive to fault information, the supervisor display module 270 can instruct the PFC control module 250 and / or the motor control module 260 to enter a fault mode. Just as an example, in failure mode, the PFC 250 control module can stop the switching of the PFC 204 module switches, while the motor control module 260 can stop the switching of the inverter power module 208 switches. In addition, the motor control module 260 can directly provide fault information to the control module PFC 250.
    In this way, the PFC 250 control module can respond to a fault identified by the motor control module 260 even if the supervisor control module 270 is not operating correctly and vice versa.
    The PFC 250 control module can control switching on the PFC 204 module using pulse width modulation (PWM). Specifically, the PFC 250 control module can generate PWM signals that are applied to the switches in the PFC 204 module. The duty cycle of the PWM signals is varied to produce desired currents in the switches in the PFC 204 module. The desired currents are calculated based on: an error between the measured DC bus voltage and a desired DC bus voltage. In other words, the desired currents are calculated to achieve the desired DC bus voltage. The desired currents can also be based on the range of the power factor correction parameters, such as the shapes of the current waveforms in the PFC 204 module. The PWM signals generated by the PFC 250 control module can be referred to such as PWM PFC signals.
    The motor control module 260 can control the switches in the inverter power module 208 using PWM to achieve the commanded compressor speed. The PWM signals generated by the module. motor control 260 can be referred to as inverter PWM signals. The duty cycle of the inverter PWM signals controls the current through the. motor windings (i.e., motor currents) of compressor 102. Motor currents control motor torque, and motor control module 260 can control motor torque to achieve commanded compressor speed. In addition to sharing fault information, the PFC 250 control module and the motor control module 260 can also share data. As an example only, the PFC 250 control module can receive data from the motor control module 260 such as load, motor currents, rated motor torque, inverter temperature, duty cycle of the inverter PWM signals, and other suitable parameters . The PFC 250 control module can also receive data from the motor control module —260, such as the measured DC bus voltage. The motor control module 260 can receive data from the PFC control module 250 such as an AC line voltage, current (s) through the PFC 204 module, rated AC power, PFC temperature, commanded bus voltage, and others appropriate parameters. In various implementations, some or all of the PFC 250 control module, motor control module 260, and supervisor control module 270 can be implemented on an integrated circuit (IC) 280. A-
    . As an example, the IC 280 may include a digital signal processor - (DSP), a programmable field gate arrangement (FPGA), a micropro-. terminator, etc.
    In several implementations, additional components can be included in the IC 280. In addition, several functions can be implemented within the IC 280 in figure 2 outside the IC 280, such as in a second IC or in a discrete circuit.
    Just as an example, the supervisor control module 270 can be integrated with the motor control module 260. Figure 3a is a schematic of an example implementation of the PFC 204 module. The PFC 204 module receives AC power via the first and second AC input terminals 302 and 304. AC power can be, for example, the AC power output through the EMI filter 202. In several implementa-. tions, the signals at the first and second AC 302 and 304 input terminals may vary in time with respect to a ground.
    The 'PFC 204 module generates DC power for filter 206 and the inverter power module 208 via a positive DC terminal 306 and a negative DC terminal 308. An anode of a first rectifier diode 310 is connected to the second input terminal 304, and a cathode of the first rectifier diode 310 is connected to the positive DC terminal 306. an anode of a second rectifier diode 312 is connected to the negative DC terminal 306, and a cathode of the second rectifier diode 312 is connected to the second AC 304 input terminal. Rectifier diodes 310 and 312 can be implemented as one or more individual diodes in series or parallel.
    A switch block 320 is connected between positive and negative DC terminals 306 and 308. Switch block 320 includes a first leg PFC 330 that includes first and second switches 332 and 334. Each switch 332 and 334 includes a first terminal , a second terminal and a control terminal.
    In various implementations, each switch 332 and 334 can be implemented as an isolated gate bipolar transistor (IGBT). In such implementations, the first, the second and the control terminals can correspond to collector, emitter and port terminals, respectively.
    The first terminal of the first switch 332 is connected to the
    . positive DC terminal 306. The second terminal of the first switch 332 is - connected to the first terminal of the second switch 334. The second terminal of the second switch 334 can be connected to the negative DC terminal 308. In various implementations, the second terminal of the second switch 334 can be connected to the negative DC terminal 308 via a shunt resistor to allow measurement of the current flowing through the first leg PFC 330. The control terminals of switches 332 and 334 receive PWM PFC signals generally complementary to the PFC control module
    250. In other words, the PWM PFC signal supplied to the first switch 332 is opposite in polarity to the PWM PFC signal supplied to the se-. second switch 334. The short circuit current can flow when the connection of one of the switches 332 and 334 overlaps with the switching off of the other switch 332 and 334. Therefore, the two switches 332 and 334 can be switched off during a dead time before or any of switches 332 and 334 are turned on. Therefore, generally complementary means that two signs are opposite in most of their periods. However, around transitions, both signals may be low or high for some period of transition.
    The first PFC 330 leg can include first and second diodes 336 and 338 connected antiparallel to switches 332 and 334, respectively. In other words, an anode of the first diode 336 is connected to the second terminal of the first switch 332, and a cathode of the first diode 336 is connected to the first terminal of the first switch 332. An —anode of the second diode 338 is connected to the second terminal of the second switch 334, and a cathode of the second diode 338 is connected to the first terminal of the second switch 334.
    Switch block 320 may include one or more additional PFC legs. In various implementations, switch block 320 may include one or more additional PFC legs. As shown in figure 3a, switch block 320 includes second and third legs 350 and 360. The number of legs PFC included in switch block 320 can be chosen based on performance and cost, just as an example, the magnitude of: ripple (voltage and current) at the DC output of module 204 may decrease as the number of PFC legs increases. In addition, the amount of ripple current in the AC line current may decrease as the number of PFC legs increases. However, parts costs and implementation complexity may increase as which increases the number of PFC legs. The second and third legs PFC 350 and 360 of switch block 320 can be similar to the first leg PFC 330. Just as an example, the second and third legs PFC 350 and 360 can include compose respective components for switches 332 and 334, diodes 336 and 338, e. respective branch resistors connected in the same way as the first PFC 330 leg. 7 The PWM PFC signals provided for the additional PFC leg switches can also be of a complementary nature. The PWM PFC signals provided for the additional PFC legs can be phase shifted from each other and the PWM PFC signals provided for the first PFC 330 leg. Just as an example, the phase shift of the PFC PFC signals can be determined by dividing 360 ( º) by the number of PFC legs. For example, when switching block 320 includes three PFC legs, the PWM PFC signals can be phase shifted 120 ° (or 180 ° for two phases, or 90 ° for four phases, etc.). The phase shift of the PWM PFC signals can cancel the ripple in the AC line current as well as in the DC output.
    The PFC 204 module includes a first inductor 370. The first inductor 370 is connected between the first AC 302 input terminal and the second terminal of the first switch 332. Additional inductors can connect the first AC 302 input terminal to the legs Additional PFCs. Just as an example, figure 3a illustrates a second inductor 372 and a third inductor 374 that connects the first AC input terminal 302 to the second and third legs PFC 350 and 360, respectively.
    A voltage can be measured via the shunt resistor
    380 to determine current through the first leg PFC 330 according to: Ohm law. An amplifier (not shown), such as an amplifier -. operational, can amplify the voltage through the shunt resistor
    380. The amplified voltage can be digitized, isolated, and / or filtered to determine the current through the first PFC leg 330. The current through other PFC legs can be determined using respective tap resistors. Additionally or alternatively, a resistor 382 can be connected in series with the negative DC terminal 308, as shown in figure 3b. The current through resistor 382 can therefore indicate a total current output from the PFC 204 module. The current through each PPC leg: 330, 350, and 360 can be inferred from the total current based on the known phase timing. of current through legs PFC 330, 350, and 360.. Any method of measuring or perceiving current across any or all legs PFC 330, 350, 360 can be used. For example, in several implementations, the current through the first PFC 330 leg can be measured using a sensor current sensor 387 (as shown in figure 3c). As an example only, the current sensor 387 can be implemented in series with the first inductor 370. In several implementations, the current sensor 387 can include a Hall effect sensor that measures the current through the first leg PFC 330 based in magnetic flux around the first inductor 370. The current through the legs PFC 350 and 360 can also be measured using the associated current sensors 388 and 389, respectively.
    The PFC 204 module can also include first and second secondary circuit diodes 390 and 392. An anode of the first secondary circuit diode 390 is connected to the first input terminal AC 302, and a cathode of the first secondary circuit diode 390 is connected to the positive DC terminal 306. An anode of the second secondary circuit diode 392 is connected to the negative DC terminal 308, and a cathode of the second secondary circuit diode 392 is connected to the first AC input terminal 302.
    Secondary circuit diodes 390 and 392 can be diodes of
    . energy, which can be designed to operate at low frequencies, such as, for example, frequencies less than approximately 100 Hz or. approximately 200 Hz. The resistance of secondary circuit diodes 390 and 392 may be less than the resistance of inductors 370, 372 and
    374. Therefore, when switches 332 and 334 within switch block 320 are not being switched, current can flow through secondary circuit diodes 390 and 392 instead of diodes 336 and 338. When the PFC module 204 is operating to create a driven DC voltage, the driven DC voltage will be greater than a peak voltage on the AC line. Therefore, secondary circuit diodes 390 and 392 will not be directly polarized and will remain inactive. Secondary circuit 390 and 392 diodes can provide lightning protection and power surge protection. 7 In various implementations, secondary circuit diodes 390 and 392 can be implemented with rectifier diodes 310 and 312 in a single package. Just as an example, The Vishay model Rectifier number 26MT or 36MT or International, model number 26MB or 36MB can be used for secondary circuit diodes 390 and 392 and rectifier diodes 310 and 312. Rectifier diodes 310 and 312 carry current whether the PFC 204 module is generating a boosted DC voltage or not. Therefore, in various implementations, each rectifier diode 310 and 312 can be implemented as physical diodes connected in parallel. Current sensors can be used to measure PFC phase currents in series with inductors 370, 372 and 374.
    Referring now to figure 4a, a simplified schematic of an engine 400 is presented and an exemplary implementation of the inverter energy module 208. Engine 400 is a component of compressor 102 in figure 2. However, the principles of figures 4a to 4c can apply other motors, including a capacitor motor 104. The inverter power module 208 includes a switch block 402. In several implementations, switch block 402 and switch block 320 of module 204 can be implemented using a similar part. Just like e-
    . For example, in figure 4a, the first inverter leg 410 includes first and second switches 420 and 422 and first and second diodes 424 and 426, which are. similarly arranged on switches 332 and 334 and diodes 336 and 338 of figure 3a. Switch block 402 receives the filtered DC voltage from the DC filter 206 via a positive DC terminal 404 and a negative DC terminal
    406. The first terminal of the first switch 420 can be connected to the positive DC terminal 404, while the second terminal of the second switch 422 can be connected to the negative DC terminal 406. The control terminals of the switch 420 and 422 generally receive reverse PWM signals - complementary sensors of the engine control module 260.. The switch block 402 may include one or more additional inverter legs. In various implementations, switch block 402 may 'include one or more reversing leg for each phase or motor winding
    400. Just as an example, switch block 402 may include second and third inverter legs 430 and 440, as shown in Figure 4a. The inverter legs 410, 430 and 440 can supply current to the motor windings 450, 452 and 454, respectively. Windings 454, 452 and 450 can be referred to as windings a, b and c, respectively. The voltage applied to windings 454, 452 and 450 can be referred to as Va, Vb and Vc, respectively. The current through windings 454, 452 and 450 can be referred to as la, lb, lc, respectively. Just as an example, the first ends of the windings 450, 452 and 454 can be connected in a common node. The second ends of the windings 450, 452 and 454 can be connected to the second terminal of the first switch 420 of the inverter legs 410, 430 and 440, respectively. The inverter power module 208 may also include a branch resistor 460 that is associated with the first branch leg 410. Branch resistor 460 can be connected between the second terminal of the second switch 422 and the negative DC terminal 406. In several implementations, the respective shunt resistors can be located between
    : of the inverter leg 430 and 440 and the negative DC terminal 406. Just like. For example, the current through the first winding 450 of the motor 400 can - be determined based on the voltage across the shunt resistor 460 of the first inverter leg 410. In several implementations, the shunt resistor in one of the inverter legs 410, 430, or 440 can be omitted. In such implementations, the current can be inferred based on the measurements of the remaining shunt resistors. Additionally or alternatively, a resistor 462 can be connected in series with a negative DC terminal 406, as shown in figure 4b. The current through resistor 462 can therefore indicate a total current consumed by the inverter energy module 208. The current through each inverter leg 410, 430 and 440 can be inferred from the total current in the known phase timing of the current through inverter legs 410, 430 and 440. Additional comments on the determinant currents in an inverter can be found in US Patent No.
    7,193,388, commonly assigned, deposited on March 20, 2007, the description of which is incorporated herein as an example. Any method of measuring and perceiving current through any or all of the reversing legs 410, 430, and
    440. For example, in various implementations, the current through the first inverter leg 410 can be measured using a current sensor 487 (illustrated in figure 4c). Just as an example, the current sensor 487 can be implemented between the first inverter leg 410 and the first winding 450. The current through the inverter legs 430 and 440 can also be measured using associated current sensors 488 and 489, respectively. In several implementations, current sensors can be associated with two of the inverter legs 410, 430 and 440. The current through the other of the inverter legs 410, 430 and 440 can be determined based on an assumption of than the current in the domotorsome windings zero. Referring now to figure 5, an exemplary implementation of the engine control module 260 in figure 2 is illustrated.
    . motor control 260 controls the switches within the e- module. inverter energy 206 to control the voltages applied to the windings - 454, 452, 450 (then the “windings, to 2”) of motor 400. This can also be referred to as inverter power module control 206 or as motor control 400.
    For example, when the motor 400 includes a three-phase motor, the motor control module 260 can apply voltages V, a c to the windings, à., Respectively. Voltages V, c can be referred to collectively as input voltages. The chains |, a. are generated in the windings, a., respectively, when voltages V, a c are applied to the windings, a and. The chains |, a. can be collectively re-. wounds like winding chains. The chains in the chains |; a c produce magnetic flux around currents |, a. and vice versa. Motor control module 260 generates output voltages to control winding currents and / or to control magnetic flux.
    Motor 400 includes a rotor (not shown) that rotates in response to winding currents. The motor control module 260 controls the amplitude, duty cycle, and / or frequency of the output voltages to control the rotor torque and speed. The motor control module 260 can control the output voltages based on a controlled motor speed, which represents a desired motor speed of the rotor.
    Motor control module 260 can implement field-oriented control of motor 400. Therefore, motor control module 260 can map motor drive variables in various reference structures. Motor drive variables can include current / voltage values required to control motor 400 as well as measured currents / voltages. For example, motor drive variables may include currents 1, a, measured across the windings x a, 7voltages requested used by the motor control module 260 to apply voltages V, a to the windings. to c.
    The engine control module 260 can map the drive variables
    . motor drive in an abc reference frame (FOR), an ab. FoR, and a FOR qdr. The abc FoR can represent, for example, a structure. three-phase stator structure based on the xa ce windings. Each of the currents |; a - can be mapped on the respective geometric axes a, b, and c of the abcFoR. In addition, the motor control module 260 can map voltages corresponding to voltages V, a c in abc FoR. AB FoR includes fixed coordinates, based on stator x and y in which the motor drive variables are projected. The qdr FOR is a FOR rotation that corresponds to the rotor and rotates in synchronization with the rotor. Therefore, the qdr FOR is based on a rotor angle.
    The engine control module 260 can transform the variables. motor drive from one FoR to another FOR. For example, the motor control module 260 can transform currents represented 'in abc FOR into currents represented in aB FoR and vice versa. The motor control module 260 can transform the motor drive variables of the abc FoR to «B FoR using a numerical transformation. The motor control module 260 can transform the motor drive variables from a «B FoR to qdr FoR based on the angle of the rotor.
    Motor control module 260 controls inverter power module 208 based on the commanded speed of supervisor control module 270 of figure 2. In various implementations, filter module 501 can filter the commanded speed of supervisor control module 270 of figure 2. In these implementations, the output of the filter module 501 is referred to below as the uv commanded speed.
    In open loop mode, the actual speed of the rotor will generally follow the commanded speed uw ,, assuming that the commanded speed w does not change too fast. As a result, the low pass filter coefficients of the filter module 501 can be chosen so that the acceleration of the rotor can be maintained with changes in the commanded speed w, output from the filter module 501. Otherwise, rotor synchronization may be lost. In several implementations, the 501 filter module can implement a ramp function, which
    : updates the commanded speed ww, up to a maximum increment during ca-. of the predetermined time interval.
    - Motor control module 260 can control motor 400 based on a commanded FoR (for example, a FoR qdv) when operating in —opened loop mode. The FoR qdv is associated with the commanded speed ww, of the rotor and a commanded angle (Bv) of the rotor. A command angle generation module 502 can determine the command angle 9, such as by integrating the commanded speed u ,. The motor control module 260 can operate in various ways, such as open loop mode or closed loop mode. Just as an example, the motor control module 260 can operate in open loop R mode at motor 400 start and later transition to operate in closed loop mode. When operating in closed loop mode, the rotor will tend to synchronize with the commanded speed u, especially when the motor control module 260 is operating the rotor at slower speeds. However, the actual rotor angle may differ from the commanded angle 9, due to a load applied to the motor 400. For example, a change in load while operating in open loop mode can change a phase difference between the commanded angle 9, and the actual rotor angle.
    A transition module 503 determines when to transition to motor control module 260 from open loop mode to closed loop mode. Just as an example, the transition module 503 can terminate when transiting based on at least one of the commanded speed w ,, a motor operating time 400, a motor-driven acceleration, and / or a feedback evaluator 504.
    For example, the 503 transition module can predict the rotor speed based on the commanded acceleration and / or the operating time. The transition module 503 can transition from open to closed loop when the predicted speed is greater than a speed limit. In various implementations, the transition module 503 can transition from open loop to closed loop mode when a time elapsed from when engine 400 started exceeds a predetermined period.
    . The evaluator mode 504 evaluates the speed (west) & angle (9est). of the rotor. The evaluator module 504 can determine the evaluated speed. West based on the Best rated angle. For example, the evaluator module 504 can differentiate and filter the Best evaluated angle over a period of time to determine the assessed speed west. The transition module 503 can transition from open to closed loop mode when the evaluator module 504 has achieved stable evaluations of the evaluated 8est angle and the evaluated West speed. In various implementations, the transition module 503 can transition from open loop mode to closed loop mode when divergence has occurred in the evaluator module 504 that can be indicated, for example, by flow assessments. . Alternatively, the transition module 503 can transition from open loop mode to closed loop mode when the co-sent speed w is greater than the speed limit. Alternatively or in addition, the transition module 503 can initiate a transition when the rated speed west of the rotor is greater than a predetermined speed. Other factors that affect the transition can include a load on the motor 400 and motor drive variables. The 504 evaluator module can determine the Best evaluated angle based on several motor drive variables. For example, motor drive variables can include Va a «to be applied to the windings, a. e la a «measured in the windings x a ce. In addition, the evaluator module 504 can determine the evaluated angle Sest based on the commanded speed w ,. The evaluator module 504 can implement a state observer (for example, a Luenberger observer) to determine the evaluated angle Best AND the evaluated speed west based on the motor drive variables. Additional description of sensorless control systems and methods can be found in U.S. Patents
    6,756,757, issued on June 29, 2004, 7,208,895, issued on April 24, 2007, 7,342,379, issued on March 11, 2008, and 7,375,485, issued on May 20, 2008, whose descriptions are hereby incorporated by way of example.
    . A current determination module 506 can measure the currents |, the «of the windings, the c (hereinafter“ measured currents ”). The millstone. evaluator module 504 can use the measured currents to evaluate est € West.
    An angle / speed determination module 508 generates an output angle 6, and an output speed w, based on the currently enabled mode, such as open loop or closed loop mode.
    The angle / speed determination module 508 can define the exit angle 6, equal to the commanded angle 0, when operating in open loop mode and can define the exit angle 89, equal to the evaluated angle Ses when operating in closed loop mode.
    When the 503 transition module instructs a mo- transition. From open loop to closed loop mode, the angle / speed determination module 508 gradually adjusts the exit angle 9, from the commanded angle 8, to the evaluated angle est.
    This gradual adjustment can minimize transient current demands when transitioning from open loop to closed loop mode, which can avoid interrupting current control (described below) and / or evaluating the evaluated angle Gest.
    The gradual adjustment can therefore improve stability during transitions and allow engine 400 to start more reliably, especially under high loads.
    The angle / speed determination module 508 can set the output speed w, equal to the commanded speed 9, when operating in open loop mode.
    The angle / speed determination module 508 can define the output speed w, equal to the evaluated speed West when operating in closed loop mode.
    In motor drive variables, the angle / speed determination module 508 can immediately switch output speed w, from commanded speed w, to the rated speed west when the transition module 503 instructs a mode transition open loop to closed loop mode.
    The transition module 503 can also instruct a change from closed loop mode to open loop mode.
    Just as an example, a transition back to open loop mode can be performed
    . when error conditions, such as when a lost rotor + is observed, or abnormal operating conditions. The angle / speed determination module 508 can therefore also switch the output speed w, from the rated speed west back to the commanded speed ww, and switch the output angle 8, from the rated angle Best back to the angle commanded 6 ,. In motor drive variables, in the same way as the transition from open loop mode to closed loop mode, switching output speed w can be carried out immediately, while switching output angle 9 can be carried out gradually.
    In many implementations, additional modes can be supported. Just as an example, three, four or more modes can be supported. The transition module 503 can instruct the angle / speed determination module 508 to transition from one mode to another. During each transition, the 508 angle / speed determination module can switch output speed w immediately to a corresponding speed for the selected mode. Alternatively, the output speed w can rise towards the speed of the selected mode. In addition, the angle / speed determination module 508 raises the exit angle 6, towards a corresponding angle for the selected mode. The transition module 503 can instruct the angle / speed determination module 508 to transition from one mode to another using a transition signal. For example, the transition signal may specify a target mode to which the 508 angle / velocity determination module must transition. A speed loop control module 510 generates a demanded torque signal calculated to match output speed w, for commanded speed w ,. In various implementations, the speed loop control module 510 can be bypassed in open loop mode. In closed loop mode, output speed w is equal to the rated speed west of motor 400. Therefore, the speed loop control module 510 can generate the torque signal required to maintain speed.
    . motor city 400 approximately equal to the commanded speed w ,. . Just as an example, when the output speed w is less than the - commanded speed uw, the speed loop control module 510 i can increase the required torque, and vice versa.
    An injection module Idr 512 generates a d-axis current demand d (Idr) based on the DC bus voltage, the required torque signal, and the commanded speed w ,. The Ildr demand is used by the current control, described below, for Idr injection, which can also be referred to as field weakening or phase advance. In various implementations, the Idr 512 injection module can adjust the Idr demand based on a voltage signal output (OOV), described below, and measured current BR.
    A torque mapping module 514 generates a 'q-axis current demand (Iqr) based on the demanded torque signal. The torque can also be generated by the demand ldr and therefore the torque mapping module 514 can determine the demand Igr also based on the demand Idr. Just as an example, the torque mapping module 514 can implement a maximum current limit. In several implementations, the torque mapping module 514 can compare a combination of ldr demand and Iqr demand to the maximum current limit, and reduce one or both demands when the combination exceeds the maximum current limit. In many implementations, the 514 torque mapping module can only limit the Igr demand. Just as an example, the maximum current limit can be an average square root limit, such as 25 Ampsnms.
    When the torque mapping module 514 is limiting the demand Igr to meet the maximum current limit, the torque mapping module 514 can output a limit signal to the speed loop control module 510. When the signal limit limit is recovered, the speed loop control module 510 can temporarily suspend the required torque increase. In addition, the speed loop control module 510 can also temporarily suspend
    . torque demanded based on the OOV signal. . Just as an example, the speed loop control module 510 can try to match the output speed w ;, to a reduced version of the commanded speed wu.
    Alternatively or in addition, the speed loop control module 510 can selectively suspend the sum of error and / or integration operation that would increase the required torque.
    In other words, when the torque mapping module indicates, via the limit signal, that the maximum current limit is reached, the speed loop control module 510 can increase the required torque because the torque existing demand can no longer be reached at the maximum current limit. . A current control module 516 determines the voltage commands Vqr and Vdr, in qdr FoR, based on current demands Igr 'and dr.
    The controlled voltages Vqr and Vdr can be a voltage command q-axis and a voltage command d-axis, respectively.
    In various implementations, the current control module 516 can determine the voltage commands Vqr and Vdr based on the measured currents.
    In several implementations, the current control module 516 can try to match the measured currents for the Iqr and Idr demands by adjusting the voltage commands Vqr and Vdr.
    In various implementations, the current control module 516 can also receive output speed ww.
    An abc module for qdr 520 maps the measured currents |; a c for the qdr FOR based on the exit angle 8 ,. The resulting mapped current can be referred to as Iqdr, and can include the components Iqr and Idr.
    The currents measured by the components of the motor control module 260, such as the current control module 516, can therefore use the Iqgdr representation of the measured currents.
    A qdr module for the B 522 can transform the voltage commands Vqr and Vdr from qdr FoR to the «B FoR, thus generating a voltage request on the aB FoR (hereinafter“ voltage request ”). The voltage request can indicate the voltages to be applied for bearings x a .. The qdr module for aB 522 can perform the transformation
    . based on the exit angle 8 ,, and in various implementations it can carry out. the transformation based on the output speed w ,. - A pulse width modulation (PWM) module 524 generates duty cycle signals to control the inverter power module 208 using PWM. Just as an example, the PWM switching frequency can be approximately 5 kHz or approximately 10 kHz. In several implementations, the inverter power module 208 and the motor 400 have three phases, and the PWM 524 module generates three duty cycle signals, one for each inverter leg. In several implementations, each leg of the inverter power module 208 includes a first rotor angle of complementary switches, and each duty cycle signal is therefore converted into complementary duty cycle signals, one for each complementary switch. - 'tar. As an example only, referring to figure 4a, switch 420 and switch 422 of the first inverter leg 410 can be controlled with complementary duty cycles.
    In several implementations, to avoid short circuit condition, where the two switches 420 and 422 are connected simultaneously, the complementary duty cycles can be adjusted so that one switch is not switched on at the same time that the other switch is switching off . In other words, the off times for the two switches are partially overlapping.
    The PWM 524 module determines duty cycle signals based on the DC bus voltage and voltage requests from the dqr module to of 522. Just as an example, PWM 524 module can transform the voltage request from aB FoR to determine three of - voltage commands, hereinafter Vra, Vrv, and Vrc (collectively Vr, a.) corresponding to the windings, a., respectively.
    When voltage demands cannot be met due to the presence of DC bus voltage, drive controller 132 is set to operate in the OOV state. Just as an example, a maximum duty cycle can be defined in the PWM 524 module.
    . voltage demands result in one of the duty cycles being greater than the maximum duty cycle, 6 drive controller 132 is operating in the OOV state.
    In implementations, the maximum duty cycle can be set to less than 100%, such as 96%, 95% or 92%. The maximum duty cycle limit can be defined based on the requirements for accurate measurement of winding currents |; The . A minimum duty cycle limit can also be set.
    Just as an example, the minimum duty cycle limit can be equal to one minus the maximum duty cycle limit.
    In several implementations, the motor 400 may not respond to the BR winding voltages themselves, but instead to differences between the winding voltages.
    As a simplistic example, applying 50 Volts' to a first winding and 150 Volts to a second winding can be equivalent to applying O Volts to the first winding and 100 Volts to the second winding.
    Therefore, even if one of the voltage demands exceeds an available voltage, the PWM 524 module can offset the voltage demands when generating the duty cycles.
    In such implementations, the PWM module 524 can determine that the drive controller 132 is in the OOV state when a difference between any two of the three voltage demands is greater than the available voltage.
    Just as an example, the available voltage can be equal to the DC bus multiplied by the maximum duty cycle.
    In various implementations, the PWM 524 module can shift duty cycles so that one of the duty cycles is set to zero.
    Alternatively, the PWM 524 module can shift duty cycles so that duty cycles are centered around an intermediate duty cycle, such as 50%. In several implementations, the PWM 524 module can shift work cycles using one or the other of these - approaches, depending on a mode of operation.
    Just as an example, the PWM 524 module can shift duty cycles so that the lowest duty cycle is set to zero when the engine 400
    : operating at speeds above a predetermined limit. 'In the OOV state, the difference between the corresponding work cycles | Regarding the voltage demands is greater than the difference enters | minimum and maximum duty cycles.
    Therefore, when operating in the OOV state, the —PWM 524 module can scale voltage demands down before generating duty cycles.
    In the same way, the PWM 524 module can scale duty cycles.
    In several implementations, the PWM! 524 can scale duty cycles or demands for the lowest voltage | possible, so that one of the work cycles is defined for the cycle | minimum duty cycle, and one of the duty cycles is defined for the maximum duty cycle. . The scaling factor is an indication of the OOV distance the drive controller 132 is currently in.
    The scale factor can be referred to as the OOV magnitude, and can be included in the OOV signal.
    In the OOV state, the PWM 524 module sets an OOV flag to a first value, such as 1. When not in the OOV state, the PWM 524 module sets the OOV flag to a second value, such as 0. The OOV flag can - to be included in the OOV signal.
    An amount of OOV can be determined based on the OOV signal.
    For example, the amount of OOV can indicate the frequency of the drive controller 132 is operating OOV.
    For illustrative purposes only, the inverter power module 208 may define a molded operating region as a hexagon.
    Voltage demands can be considered as circles within the hexagon.
    If the circles are centered inside the hexagon, as the circles expand, they touch the sides of the hexagon.
    When the circles expand beyond the hexagon, the circles become more and more stuck on each face of the hexagon.
    The hold can correspond to the OOV state.
    As a result, the proportion of time that voltage demands are held (production of OOV state) indicates how far OOV is from trigger driver 132. | The OOV quantity can represent a part of the time that the
    , 32/35. drive controller 132 is spending in the OOV state.
    The OOV quantity can be determined by applying a filter, such as a digital low pass filter, to the OOV flag.
    Just as an example, the OOV quantity can be determined by applying a | moving average for the OOV flag.
    When the OOV flag assumes values from O to 1, the OOV quantity will then vary between and including 1.
    When multiplied by 100, the OOV amount is the percentage of time that drive controller 132 is spending in the OOV state.
    The engine control module 260 can use several approaches to minimize OOV operation, or keep OOV operation below a predetermined limit.
    In various implementations, the 'Idr 512 injection module can use the OOV quantity in determining how to adjust the Idr demand.
    The speed loop control module 510 can also 'use the OOV amount to determine when to suspend the increase in torque required.
    The current control module 516 can suspend the increase for one or both Vqr and Vdr commands based on the OOv flag.
    Referring now to figure 6, an exemplary implementation of the angle / speed determination module 508 includes a subtraction module 602, an error reduction module 604, a sum module 606, a first multiplexing module 608, and a second multiplexing module 612. During open loop mode, the transition signal from the transition module 503 instructs the first multiplexing module 608 to output the commanded angle & ,. When transitioning from open loop to closed loop mode, the transition signal instructs the first multiplexing module 608 to output a sum of the sum module 606 as the output angle O, .. This sum will eventually be equal Best rated angle.
    However, at the time of transition, the commanded angle 9, and the evaluated angle Gest may not be the same.
    To avoid discontinuities in the exit angle 6, at the time of transition, the sum of the sum module 606 is controlled to be equal to the commanded angle 8 ,. This can be done by calculating the difference (Gero) between the commanded angle 8, and the evaluated angle
    . Best, and adding the angle error to the evaluated Gest angle. The Best evaluated angle that is added cancels out with the Best evaluated angle that was subtracted, and the result is still the commanded angle 8, at the moment of transition. The subtraction module 602 generates the angle error Berror- The error reduction module 604 stores the value of the angle error at the moment of transition, and, over time, reduces the absolute value of the stored value to zero. The stored value leaves the error reduction module 604 as 8 ;. When the stored value reaches zero, the sum of the sum module 606 will be equal to the evaluated angle Best and the transition is completed.
    In several implementations, the 604 error reduction module. it can decrease the magnitude of the stored value by predetermined reductions at predetermined intervals until the stored value reaches zero. In other words, the error reduction module 604 decreases the magnitude deb, decreasing Bs, without considering the sign of 95. For example, the error reduction module 604 can subtract the predetermined increment 9; when 9; it is a positive value. The error reduction module 604 can add the predetermined increment to 9; when 8; it is a negative value. Just as an example, the error reduction module 604 can decrease the magnitude of debs. by 0.5 degrees at intervals us up to 0; reach zero.
    During open loop mode, the transition signal instructs the second multiplexing module 612 to emit wu, such as uwr. When transitioning from open loop to closed loop mode, the transition signal instructs the second multiplexing module 612 to output West as wWwr. Normally, west E & Ww will be the same, and therefore switching directly from one to the other will not result in an abrupt change in w ,.
    Referring now to figure 7, an example of transition from open loop to closed loop mode is graphically illustrated. The thin dashed line tracks the commanded angle 8, used in open loop mode. The thin chia line traces the Best rated angle in closed loop mode. The bold line is the output of the 508 angle / speed determination module, the exit angle 9, .. The exit angle 8, follows the angle
    . commanded 9, until the transition from open loop mode to 'closed loop mode' begins.
    The exit angle 6, then ascends towards the angle: rated Best.
    In fact, as soon as the transition begins, the exit angle 8 follows the Best evaluated angle.
    However, the exit angle 9 is following the evaluated angle O. plus an offset (9;). This shift is reduced over the course of the transition.
    When the displacement reaches zero, the exit angle 6, follows the evaluated angle est for the remainder of figure 7. Although the fusion system is described as controlling a transition from the commanded angle 9, in the open loop mode to the evaluated angle G.st EM Closed loop mode, the fusion system can be general-. Applicable for transition between any engine control angles.
    For example, when a first sensorless control system controls based on a first angle (891) and a second sensor control system controls based on a second angle (62), the fusion system can control a transition from 81 to 62 when controlling the transitions from the first to the second sensorless control system.
    Alternatively, the fusion system can control a transition from 62 to 91 when the control switches from the second sensorless control system to the first sensorless control system.
    The first sensorless control system can be a system that controls the rotor in a first speed variation, while the second sensorless control system can be a system that controls the rotor in a second speed variation.
    Therefore, the system and fusion can transition between 91 and 82 based on the speed of the rotor.
    In some implementations, the fusion system can control an open loop mode transition to the first sensorless control system, so it controls the transitions between the first sensorless control system and the second based on the speed of the sensor. rotor.
    The fusion system can control transitions from any of the N modes to other N modes, where N is an integer greater than or equal to 2. Just as an example, N can be equal to or 2, 3, 4 or more.
    . Referring now to figure 8, a method for transitioning from 'open loop to closed loop mode' starts at 802. In 802, the control operates motor 400 in open loop mode based on the co-angle. warrant 89, ew ,. In 804, the control determines whether to switch from open loop mode to closed loop mode. If true, the control proceeds to 806, otherwise the control remains at 804. At 806, the control controls the Seror error angle based on a difference between the commanded angle 8 and the evaluated angle 8est. In 808, the control stores the error angle of error as Bs.
    In 810, the control operates engine 400 based on Wes: E at S0- from 8est E Os. Since processing is not instantaneous, 810 is technically. performed after the transition from the open loop to the closed loop was instructed by 804. However, the delay can be negligible. In 812, the control determines whether 9; is equal to zero. If false, control proceeds to
    814. If true, control continues to 818. In 814, control holds for a predetermined interval. In 816, the control decreases the magnitude of 8; for a predetermined quantity and returns to 812. In 818, the control operates engine 400 based on west E at the rated angle Best. The control remains at 818. However, if an error occurs, the control can return (not shown) to 802. Operation in open loop mode can allow error conditions to be recovered.
    The broad teachings of the description can be implemented in several ways. Therefore, although this description includes particular examples, the true scope of the description should not be limited to the same since other modifications will become clear to that person skilled in the art when studying the drawings, the report and the claims in question. attachment.
    权利要求:
    Claims (19)
    [1]
    . CLAIMS "1. System comprising:: a pulse width modulation (PWM) module that controls switching of an inverter that powers a motor, where the - PWM module controls switching based on a first angle at a prime - r mode and a second angle in a second mode; a subtraction module that determines a difference between the first and second angles; an error reduction module that (i) stores the difference when a transition from the first mode to the second and (ii) decreases a magnitude of the stored difference to zero, e. a sum module that calculates a sum of the stored difference and the second angle, in which the PWM module controls the switching 'based on the sum in the second mode.
    [2]
    2. System according to claim 1, additionally comprising a commanded angle generation module that generates the first angle based on a commanded speed.
    [3]
    3. System according to claim 2, in which the first angle is generated by the integration of the commanded speed.
    [4]
    A system according to claim 3, further comprising an index limiting module that generates the command speed by limiting the index to a requested speed.
    [5]
    5. System according to claim 1, additionally comprising an evaluator module that determines the second angle based on measured motor parameters, in which the measured parameters include at least one of the measured currents and measured voltages.
    [6]
    6. System according to claim 5, in which the evaluator module determines an evaluated speed, and in which the PWM module controls the switching based on the evaluated speed after the transition from the first mode to the second mode.
    [7]
    7. System according to claim 1, in which the error reduction module decreases the magnitude by a predetermined amount
    [8]
    . at periodic intervals. 8. The system according to claim 1, further comprising J a transition module that controls the transition from the first mode to the second mode when an evaluated motor speed is greater than a predetermined speed.
    [9]
    A system according to claim 1, further comprising a transition module that controls the transition from the first mode to the second mode when the engine has been running for longer than a predetermined period.
    [10]
    10. Method comprising: control the switching of an inverter that energizes a motor. based on a first angle in a first mode and a second angle in a second mode; 'determine a difference between the first and second angles; store the difference when a transition from the first mode to the second mode is commanded; decrease a magnitude of the stored difference to zero; calculate a sum of the stored difference and the second angle; and control switching based on the sum in the second mode.
    [11]
    A method according to claim 10, further comprising generating the first angle based on a commanded speed.
    [12]
    A method according to claim 11, further comprising generating the first angle by integrating the commanded speed.
    [13]
    13. The method of claim 12, further comprising generating the commanded speed by limiting a requested speed.
    [14]
    14. The method of claim 10, further comprising determining the second angle based on measured engine parameters, wherein the measured parameters include at least one
    [15]
    . measured currents and measured voltages. 15. The method of claim 14, further comprising SY: determining an evaluated velocity; and controlling switching based on the speed evaluated after the transition from the first mode to the second mode.
    [16]
    16. The method of claim 10, further comprising decreasing the magnitude by a certain amount at periodic intervals.
    [17]
    17. The method of claim 10, further comprising commanding the transition from the first mode to the second mode. when a rated motor speed is greater than a predetermined speed. '
    [18]
    18. The method of claim 10, further comprising commanding the transition from the first mode to the second mode when the engine has been running for longer than a predetermined period.
    [19]
    19. System comprising: a control module that controls a motor based on a first rotor angle in a first mode and that controls the motor based on a second rotor angle in a second mode; an angle determination module that (i) determines the second rotor angle based on a sum of a stored value and a third rotor angle and (ii) after the second mode is selected, stored value for a difference between the first rotor angle and the third rotor angle; and a reduction module that reduces a magnitude of the stored value to zero for a period other than zero after selecting the second mode.
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    Ez vo 7; i oB <Z 3 i i 3 38 E i i F- 8. so ES i; = so ç ES ê: i É K 3 EO i i 5 5 sES i i o Ps SS os; : ss 3 3 Í: 2 2 o =; : 2 oo o o cT; ; = [85S8 o 2 Ss 8 ES i H 5 lots Ss is ES: H Ses El So DS i o t 2 Sr 5 SS o37T | O i: 85 i o co ”: BS i SO00) r o 282: SS: 2 = 8S 3 o | ZE E i = 383 Bifi — o: Ss ) So; SE: - "e E sfe— o: DO: o 1 ET O i £ EBE 280 j i numbers in Oo 5 t
    '3 o ia PP: is 8 Í i XÁ MEN j si E S i 3:; po (+): 38:; $ o à io i is: o -A. io *: 1st o; % FE +: * io:. 1> 86 H DS IS; ie: is; : It is the 3rd
    DG E H S Do 2 o: o> vo H 2 o) o; Ss to 16 E 3 S 8Eio BD i ss O 6; o o o; o - poe => 1; ”LL PE o) 3 VC i E o À &Oo; = i2: o Fr) i io i 18 = H io 3 i is oO i: 3 Õ i 1e and i = Ú:; ; qn 3; Ss:; what : ds i DP:; ; :> o o o õ == S rr o Te i o) bh í o "í & .. i õ“.; oO ".. i 2. io "e H o A í% = rr i £ E ff É SC o Te Po. o = goremeesaeeenta ra Mia Sar tsetaSaRASRRIANIANTAAARAISSNINSAAESRRAARAS ARA A Ran AA: o is E AT NY & o> ooo A, as IS S o 8 ". Fr Es “. the <“. & 2a —— ho - C to 8 T "TTTTTTTT 7 TTTOA BS. O - O oO S an—” o | 8 E o = = IS -> o
    ES o "o s
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    法律状态:
    2020-08-18| B06U| Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]|
    2020-12-08| B11B| Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements|
    2021-11-03| B350| Update of information on the portal [chapter 15.35 patent gazette]|
    优先权:
    申请号 | 申请日 | 专利标题
    US23263309P| true| 2009-08-10|2009-08-10|
    US61/232,633|2009-08-10|
    US12/852,625|2010-08-09|
    US12/852,625|US8264192B2|2009-08-10|2010-08-09|Controller and method for transitioning between control angles|
    PCT/US2010/045041|WO2011019730A2|2009-08-10|2010-08-10|Controller and method for transitioning between control angles|
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