CN115528965B - Method for calculating multi-damping loop inductance of permanent magnet motor with rotor provided with damping strips - Google Patents

Method for calculating multi-damping loop inductance of permanent magnet motor with rotor provided with damping strips Download PDF

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CN115528965B
CN115528965B CN202211495556.3A CN202211495556A CN115528965B CN 115528965 B CN115528965 B CN 115528965B CN 202211495556 A CN202211495556 A CN 202211495556A CN 115528965 B CN115528965 B CN 115528965B
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damping
axis
rotor
loop
quadrature
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CN115528965A (en
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周羽
杨小宝
王学庆
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Beihete (Suzhou) Technology Co.,Ltd.
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Chengdu Univos Technology Co ltd
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    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P21/00Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
    • H02P21/14Estimation or adaptation of machine parameters, e.g. flux, current or voltage
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P21/00Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
    • H02P21/14Estimation or adaptation of machine parameters, e.g. flux, current or voltage
    • H02P21/141Flux estimation
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P21/00Arrangements or methods for the control of electric machines by vector control, e.g. by control of field orientation
    • H02P21/34Arrangements for starting
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P25/00Arrangements or methods for the control of AC motors characterised by the kind of AC motor or by structural details
    • H02P25/02Arrangements or methods for the control of AC motors characterised by the kind of AC motor or by structural details characterised by the kind of motor
    • H02P25/022Synchronous motors
    • H02P25/03Synchronous motors with brushless excitation
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P6/00Arrangements for controlling synchronous motors or other dynamo-electric motors using electronic commutation dependent on the rotor position; Electronic commutators therefor
    • H02P6/20Arrangements for starting
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P6/00Arrangements for controlling synchronous motors or other dynamo-electric motors using electronic commutation dependent on the rotor position; Electronic commutators therefor
    • H02P6/34Modelling or simulation for control purposes
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02PCONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P2207/00Indexing scheme relating to controlling arrangements characterised by the type of motor
    • H02P2207/05Synchronous machines, e.g. with permanent magnets or DC excitation

Abstract

The invention discloses a method for calculating the inductance of a multi-damping loop of a permanent magnet motor with a rotor provided with damping strips, which comprises the steps of obtaining the magnetic potential of a rotor direct-axis damping loop and the magnetic potential of a rotor quadrature-axis damping loop of a rotor damping loop according to induced current; obtaining an air gap magnetic field of the direct-axis damping loop according to the magnetic potential of the rotor direct-axis damping loop, and obtaining an air gap magnetic field of the quadrature-axis damping loop according to the magnetic potential of the rotor quadrature-axis damping loop; obtaining self inductance and mutual inductance of a permanent magnet synchronous motor direct-axis damping loop of which the rotor is provided with a damping strip and mutual inductance between a stator winding and the direct-axis damping loop according to an air gap magnetic field of the direct-axis damping loop; obtaining self inductance and mutual inductance of a quadrature axis damping loop of the permanent magnet synchronous motor with the rotor provided with the damping strips and mutual inductance between a stator winding and the quadrature axis damping loop according to an air gap magnetic field of the quadrature axis damping loop; and optimizing the permanent magnet motor with the rotor band damping strip according to the obtained damping loop inductance, and improving the transient performance and the steady-state performance of the permanent magnet motor with the rotor band damping strip in the starting process.

Description

Method for calculating multi-damping loop inductance of permanent magnet motor with rotor provided with damping strips
Technical Field
The invention relates to the technical field of permanent magnet synchronous motors, in particular to a method for calculating the inductance of a multi-damping loop of a permanent magnet motor with a rotor provided with damping strips.
Background
Energy is a very important strategic material for all countries in the world, which not only affects the development of national economy, but also affects the prosperity of national strength, so that all countries in the world regard the energy problem as a major problem affecting the prosperity and the defenceness of the country. The motor is a driving device of various industrial and agricultural production equipment and is widely applied to various fields of industrial and agricultural production. The motor energy conservation plays a significant role in realizing the double-carbon target in China, and the country supports the development of high-efficiency motors, reduces the loss of the motors, can greatly save energy, and improves and relieves the energy pressure.
The self-starting permanent magnet motor is a permanent magnet synchronous motor with a damping strip on a rotor, and is more and more concerned by people, and the main reason is that the self-starting permanent magnet motor has outstanding characteristics compared with the traditional motor: (1) The self-starting permanent magnet synchronous motor is only under the action of a permanent magnet magnetic field and a stator winding magnetic field during steady-state operation, a rotor damping winding does not cut a magnetic field any more and has no damping loss, and the rotating speed during operation is synchronous and is not influenced by a load; (2) The power factor is high, the power factor of the self-starting permanent magnet synchronous motor can be adjusted through reasonable design, the motor can operate under the condition of lagging or leading power factor, and the maximum power factor of the motor can even reach the unit power factor; (3) The motor has small volume and light weight, and the common motor can be replaced by a permanent magnet motor which is 1-2 machine seat numbers smaller than the volume and the weight of the motor; (4) The economic operation range is wide, the economic allowable range of the permanent magnet synchronous motor is 10% -140% of the rated load, the economic allowable range is obviously wider than that of a common induction motor, and the power factor of the permanent magnet synchronous motor can still reach about 0.9 even under the condition of 0.25 times of the rated load; (5) Compared with the induction motor with the same specification, the self-starting permanent magnet synchronous motor has the advantage that the rated efficiency is improved by 4-12%.
In the permanent magnet synchronous motor with the damping strips on the rotor, the analytical calculation method of the damping strip inductance is very important for analytical calculation of the running performance of the permanent magnet synchronous motor with the damping strips on the rotor by applying a multi-damping loop model. In fact, the existing method generally adopts a rotor inductance calculation method of an electrically excited synchronous motor to be directly transplanted into a damping loop of a permanent magnet motor to calculate the rotor inductance, and at present, no accurate analytic calculation method for calculating the related inductances of a direct-axis damping loop and a quadrature-axis damping loop exists.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provides a method for calculating the inductance of a multi-damping loop of a permanent magnet motor with a rotor provided with damping strips, which comprises the following steps:
the method comprises the steps of obtaining induction current of a damping strip on a rotor in the starting process of a permanent magnet synchronous motor with the damping strip on the rotor, and obtaining the magnetic potential of a rotor direct-axis damping loop and the magnetic potential of a rotor quadrature-axis damping loop of a rotor damping loop according to the induction current; obtaining an air-gap magnetic field of the direct-axis damping loop according to the magnetic potential of the rotor direct-axis damping loop, and obtaining an air-gap magnetic field of the quadrature-axis damping loop according to the magnetic potential of the rotor quadrature-axis damping loop;
respectively obtaining the self inductance of the direct-axis damping loop and the mutual inductance of the direct-axis damping loop according to the air gap magnetic field of the direct-axis damping loop; respectively obtaining self inductance of the quadrature axis damping loop and mutual inductance of the quadrature axis damping loop according to the air gap magnetic field of the quadrature axis damping loop;
obtaining mutual inductance between a stator winding of the permanent magnet synchronous motor with the rotor provided with the damping strips and the direct-axis damping loop according to an air-gap magnetic field of the direct-axis damping loop; obtaining mutual inductance between a stator winding of the permanent magnet synchronous motor with the rotor provided with the damping strips and the quadrature axis damping loop according to an air gap magnetic field of the quadrature axis damping loop;
according to the obtained self-inductance of the direct-axis damping loop, the mutual inductance of the direct-axis damping loop, the self-inductance of the quadrature-axis damping loop, the mutual inductance between the stator winding and the direct-axis damping loop and the mutual inductance between the stator winding and the quadrature-axis damping loop, the permanent magnet motor with the rotor band damping strip is optimized, and the transient performance and the steady-state performance of the permanent magnet motor with the rotor band damping strip in the starting process are improved.
Further, the obtaining of the magnetic potential of the rotor direct axis damping loop and the magnetic potential of the rotor quadrature axis damping loop of the rotor damping loop according to the induced current includes the following steps:
when the current of the damping loop isIThen, the magnetic potential distribution of the rotor straight shaft damping loop is shown as follows:
Figure 528286DEST_PATH_IMAGE001
Figure 976585DEST_PATH_IMAGE002
is a straight-axis damping loop and is characterized in that,
Figure 21901DEST_PATH_IMAGE003
in order to provide a quadrature axis damping loop,
Figure 682690DEST_PATH_IMAGE004
are respectively d-axis d 1 、d 2 、d 3 The magnetomotive force of the direct-axis damping circuit,
Figure 513374DEST_PATH_IMAGE005
is the groove pitch angle of the damping strip,
Figure 601416DEST_PATH_IMAGE006
is the spatial electrical angular position;
the magnetic potential distribution of the rotor quadrature axis damping loop is shown as follows:
Figure 134028DEST_PATH_IMAGE007
Figure 332928DEST_PATH_IMAGE008
are respectively q-axis q 1 、q 2 、q 3 Magnetomotive force of the quadrature damping circuit.
Further, the obtaining of the air-gap magnetic field of the direct-axis damping loop according to the magnetic potential of the rotor direct-axis damping loop includes:
straight shaft damping loop
Figure 267386DEST_PATH_IMAGE009
Generating an air-gap magnetic field of
Figure 526329DEST_PATH_IMAGE010
In the above formula, j represents the imaginary part of the complex number,
Figure 546238DEST_PATH_IMAGE011
are respectively d 1 、d 2 、d 3 The resulting radial flux density of the direct axis damping loop,
Figure 548829DEST_PATH_IMAGE012
are respectively d 1 、d 2 、d 3 The resulting tangential magnetic flux density of the direct axis damping loop,
Figure 337793DEST_PATH_IMAGE013
the magnetic permeability of the air is such that,σthe magnetic flux leakage coefficient is obtained by the following steps,h m is half the thickness of the permanent magnet,b m is the width of the permanent magnet or magnets,
Figure 781020DEST_PATH_IMAGE014
is the minimum air gap length and is,
Figure 288224DEST_PATH_IMAGE015
is the distance between the poles of the magnetic field,
Figure 828927DEST_PATH_IMAGE016
the straight-axis basic air gap field can be obtained by the following formula:
Figure 737977DEST_PATH_IMAGE017
wherein the content of the first and second substances,R s is the inner radius of the stator and,R q is to solve the radius of the air gap flux density,
Figure 338723DEST_PATH_IMAGE018
is coefficient of polar arcpIs the number of the pole pairs,
Figure 67644DEST_PATH_IMAGE019
is the air gap length at the position of the Q point in the air gap,
Figure 412038DEST_PATH_IMAGE020
is machineThe mechanical angle of the rotating shaft is changed into the angle,
Figure 175595DEST_PATH_IMAGE021
representing the arctan function.
Further, the obtaining of the air-gap magnetic field of the quadrature axis damping loop according to the rotor quadrature axis damping loop magnetic potential includes:
quadrature damping circuit
Figure 212821DEST_PATH_IMAGE022
The air gap magnetic field generated is:
Figure 179771DEST_PATH_IMAGE023
in the above formula, the first and second carbon atoms are,
Figure 327856DEST_PATH_IMAGE024
are each q 1 、q 2 、q 3 The radial magnetic density generated by the quadrature axis damping loop,
Figure 945919DEST_PATH_IMAGE025
are each q 1 、q 2 、q 3 Generating tangential magnetic flux density of the quadrature axis damping loop;
Figure 154046DEST_PATH_IMAGE026
the quadrature axis basic air gap field can be obtained by the following formula:
Figure 857560DEST_PATH_IMAGE027
wherein the content of the first and second substances,b j is the distance between the adjacent magnetic poles,
Figure 543756DEST_PATH_IMAGE028
is the intermediate variable(s) of the variable,
Figure DEST_PATH_IMAGE029
further, the obtaining of the self inductance of the direct axis damping loop and the mutual inductance of the direct axis damping loop according to the air gap magnetic field of the direct axis damping loop respectively includes:
Figure 547484DEST_PATH_IMAGE030
the self-inductance of the d1, d2, d3 direct axis damping loop is shown as follows:
Figure 660934DEST_PATH_IMAGE031
in the above formula, the first and second carbon atoms are,
Figure 602476DEST_PATH_IMAGE032
the permanent magnet synchronous motor with the damping strips for the rotor has the axial effective length,
Figure 92363DEST_PATH_IMAGE033
are respectively d 1 、d 2 、d 3 Self-flux linkage generated by the direct-axis damping loop;
Figure 419439DEST_PATH_IMAGE034
mutual inductance between the d1 and d2 direct-axis damping loops, mutual inductance between the d2 and d3 direct-axis damping loops, and mutual inductance between the d1 and d3 direct-axis damping loops are respectively shown as follows:
Figure 969370DEST_PATH_IMAGE035
therein
Figure 647476DEST_PATH_IMAGE036
The mutual flux linkage between the d1 and d2 direct-axis damping loops, the mutual flux linkage between the d1 and d3 direct-axis damping loops, and the mutual flux linkage between the d2 and d3 direct-axis damping loops are respectively.
Further, the obtaining of the self-inductance of the quadrature damping loop and the mutual inductance of the quadrature damping loop according to the air-gap magnetic field of the quadrature damping loop respectively includes:
Figure 941054DEST_PATH_IMAGE037
the self-inductance of the quadrature axis damping loop q1, q2 and q3 respectively,
Figure 388215DEST_PATH_IMAGE038
the self-magnetic chains of the quadrature damping loops q1, q2 and q3 respectively are shown as follows:
Figure 843468DEST_PATH_IMAGE039
Figure 759602DEST_PATH_IMAGE040
mutual inductance between q1 and q2 quadrature axis damping loops, mutual inductance between q2 and q3 quadrature axis damping loops, mutual inductance between q1 and q3 quadrature axis damping loops,
Figure 591292DEST_PATH_IMAGE041
are each q 1 And q is 2 Flux linkage, q, between quadrature damping loops 1 And q is 3 Flux linkage between quadrature damping loops, q 2 And q is 3 The flux linkage between the quadrature damping loops is shown as follows:
Figure 158539DEST_PATH_IMAGE042
further, the obtaining of the mutual inductance between the stator winding of the permanent magnet synchronous motor with the rotor having the damping strips and the direct axis damping loop according to the air gap magnetic field of the direct axis damping loop includes:
Figure 784693DEST_PATH_IMAGE043
mutual inductance between the A-phase stator winding and the direct-axis damping loop is obtained according to an air gap magnetic field of the direct-axis damping loop:
Figure 171812DEST_PATH_IMAGE044
wherein the content of the first and second substances,
Figure 807193DEST_PATH_IMAGE045
the number of the branches connected in parallel is equal to that of the branch,qis the number of slots per phase per pole,
Figure 963367DEST_PATH_IMAGE046
the number of turns of the winding in the slot, and P is the number of pole pairs; when the rotor is in the position of
Figure 26001DEST_PATH_IMAGE047
When the utility model is used, the water is discharged,
Figure 900416DEST_PATH_IMAGE048
damping the flux linkage of the air-gap field entering the A-phase winding for the direct axis, an
Figure 93150DEST_PATH_IMAGE049
Figure 369411DEST_PATH_IMAGE050
Wherein the content of the first and second substances,mthe number of the phases is the same as the number of the phases,
Figure 602946DEST_PATH_IMAGE051
is the axial position of phase A in the rotor coordinate system,
Figure 964657DEST_PATH_IMAGE052
the number of the stator slots is the number of the stator slots,
Figure 941840DEST_PATH_IMAGE053
is the short-range coefficient of the signal,
Figure 807028DEST_PATH_IMAGE054
is the slot pitch electrical angle;
when the rotor rotates, the stator winding and the rotorRelative motion exists between the sub-damping loops; when rotor is in electrical angle position
Figure 211465DEST_PATH_IMAGE055
When the rotor is in a rotating state, the direct-axis magnetic field of the stator winding changes, the mutual inductance between the stator winding and the rotor direct-axis damping loop changes simultaneously, the magnetic fields generated by the phases A, B and C have an electrical angle difference of 120 degrees in space, and the mutual inductance between the phase B and the phase C and the direct-axis damping loop can be obtained in the same way.
Further, the mutual inductance between the stator winding of the permanent magnet synchronous motor with the rotor provided with the damping strips and the quadrature axis damping loop is obtained according to the air gap magnetic field of the quadrature axis damping loop:
Figure 60472DEST_PATH_IMAGE056
mutual inductance between the A-phase stator winding and q1, q2 and q3 quadrature axis damping loops is obtained according to air gap magnetic fields of the quadrature axis damping loops:
Figure 575767DEST_PATH_IMAGE057
the mutual inductance between the phase B and the phase C and the quadrature axis damping loop can be obtained in the same way, and when the position of the rotor is
Figure 577352DEST_PATH_IMAGE058
When the temperature of the water is higher than the set temperature,
Figure 152690DEST_PATH_IMAGE059
the air gap magnetic fields of the quadrature axis damping loops q1, q2 and q3 enter the flux linkage of the A phase winding,
Figure 488993DEST_PATH_IMAGE060
the number of the parallel branches is the same as the number of the parallel branches,
Figure 807979DEST_PATH_IMAGE061
the number of the pole pairs is the number of the pole pairs,
Figure 913339DEST_PATH_IMAGE062
the current of the quadrature damping loop, q is the number of slots per phase per pole,
Figure 659578DEST_PATH_IMAGE063
the number of turns of the winding in the slot,
Figure 217598DEST_PATH_IMAGE064
is the radius of the point Q in the air gap,
Figure 340275DEST_PATH_IMAGE065
the axial effective length of the motor is long,
Figure 50873DEST_PATH_IMAGE066
the resulting radial flux densities of the q1, q2, and q3 damping loops, respectively.
Further, the leakage inductance of the damping loop is also included, and is obtained by the following formula: further, the method comprises
Figure 968013DEST_PATH_IMAGE067
In the above formula, the first and second carbon atoms are,pthe number of the pole pairs is the number of the pole pairs,
Figure 278909DEST_PATH_IMAGE068
is a magnetic permeability of air, and
Figure 674118DEST_PATH_IMAGE069
in the above formula, the first and second carbon atoms are,b ro the width of the rotor slot is the width of the rotor slot,h ro the height of the notch of the rotor is high,R rs is the radius of the circular rotor slot, and then the leakage inductance of the damping circuit
Figure 488491DEST_PATH_IMAGE070
The self-inductance of the damping loop is added,
Figure 842111DEST_PATH_IMAGE071
as an arcsine function。
The beneficial effects of the invention are: the invention considers the condition of uneven air gap between the stator and the rotor, and is beneficial to better optimizing the sine of the steady-state current of the permanent magnet synchronous motor with the damping strips on the rotor. The calculation of the damping loop inductance is beneficial to fast and accurate analysis optimization and design of the permanent magnet motor with the damping strips on the rotor, the transient performance in the starting process is improved, such as reduction of starting current multiples and starting torque impact, enhancement of pull-in synchronization capacity and the like, and the steady-state performance is improved, such as enhancement of stability, improvement of efficiency and power factor, and anti-interference capacity.
Drawings
FIG. 1 is a schematic flow chart of a method for calculating the inductance of a multi-damping loop of a permanent magnet motor with a rotor having damping strips;
FIG. 2 is a structural diagram of a rotor of a permanent magnet synchronous motor with damping strips;
FIG. 3 is a schematic diagram of a damping circuit structure;
FIG. 4 is a schematic diagram of the mutual inductance between phase A and damping loop d 1;
FIG. 5 is a schematic diagram of the mutual inductance between phase A and damping loop d 2;
FIG. 6 is a schematic diagram of the mutual inductance between phase A and damping loop d 3;
FIG. 7 is a schematic diagram of the mutual inductance between phase A and the damping loop q 1;
FIG. 8 is a schematic diagram of the mutual inductance between phase A and damping loop q 2;
fig. 9 is a schematic diagram of the mutual inductance between phase a and damping loop q 3.
Detailed Description
The technical solutions of the present invention are further described in detail below with reference to the accompanying drawings, but the scope of the present invention is not limited to the following descriptions.
For the purpose of making the object, technical solution and advantages of the present invention more apparent, the present invention will be further described in detail with reference to the accompanying drawings and embodiments. It should be understood that the detailed description and specific examples, while indicating the preferred embodiment of the invention, are intended for purposes of illustration only and are not intended to limit the scope of the invention. The components of embodiments of the present invention generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.
Thus, the following detailed description of the embodiments of the present invention, as presented in the figures, is not intended to limit the scope of the invention, as claimed, but is merely representative of selected embodiments of the invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments of the present invention without making any creative effort, shall fall within the protection scope of the present invention. It is noted that relational terms such as "first" and "second," and the like, may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions.
Furthermore, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrases "comprising a" \8230; "does not exclude the presence of additional like elements in the process, method, article, or apparatus that comprises the element.
The features and properties of the present invention are described in further detail below with reference to examples.
As shown in fig. 1, a method for calculating inductance of a multi-damping loop of a permanent magnet motor with a damping strip on a rotor includes the following steps:
the method comprises the steps of obtaining induction current of a damping strip on a rotor in the starting process of a permanent magnet synchronous motor with the damping strip on the rotor, and obtaining the magnetic potential of a rotor direct-axis damping loop and the magnetic potential of a rotor quadrature-axis damping loop of a rotor damping loop according to the induction current; obtaining an air-gap magnetic field of the direct-axis damping loop according to the magnetic potential of the rotor direct-axis damping loop, and obtaining an air-gap magnetic field of the quadrature-axis damping loop according to the magnetic potential of the rotor quadrature-axis damping loop;
respectively obtaining the self inductance of the direct axis damping loop and the mutual inductance of the direct axis damping loop according to the air gap magnetic field of the direct axis damping loop; respectively obtaining self inductance of the quadrature axis damping loop and mutual inductance of the quadrature axis damping loop according to the air gap magnetic field of the quadrature axis damping loop;
obtaining mutual inductance between a stator winding of the permanent magnet synchronous motor with the rotor provided with the damping strips and the direct-axis damping loop according to the air gap magnetic field of the direct-axis damping loop; obtaining mutual inductance between a stator winding of the permanent magnet synchronous motor with the rotor provided with the damping strips and the quadrature axis damping loop according to an air gap magnetic field of the quadrature axis damping loop;
and optimizing the permanent magnet motor with the rotor band damping strip according to the obtained self-inductance of the direct-axis damping loop, the self-inductance of the quadrature-axis damping loop, the mutual inductance between the stator winding and the direct-axis damping loop and the mutual inductance between the stator winding and the quadrature-axis damping loop, so that the transient performance and the steady-state performance of the permanent magnet motor with the rotor band damping strip in the starting process are improved.
The method for obtaining the rotor direct axis damping loop magnetic potential and the rotor quadrature axis damping loop magnetic potential of the rotor damping loop according to the induction current comprises the following processes:
when the current of the damping loop isIThen, the magnetic potential distribution of the rotor straight shaft damping loop is shown as follows:
Figure 374724DEST_PATH_IMAGE001
Figure 839203DEST_PATH_IMAGE002
in order to provide a straight-axis damping loop,
Figure 508082DEST_PATH_IMAGE072
in order to form a quadrature axis damping loop,
Figure 783337DEST_PATH_IMAGE004
respectively d axis d 1 、d 2 、d 3 The magnetomotive force of the straight-axis damping circuit,
Figure 803245DEST_PATH_IMAGE005
is the groove pitch angle of the damping strip,
Figure 805836DEST_PATH_IMAGE006
is the spatial electrical angular position;
the magnetic potential distribution of the rotor quadrature axis damping loop is shown as follows:
Figure 594801DEST_PATH_IMAGE007
Figure 290224DEST_PATH_IMAGE008
are respectively q-axis q 1 、q 2 、q 3 Magnetomotive force of the quadrature damping circuit.
The air gap magnetic field of the direct-axis damping loop is obtained according to the magnetic potential of the rotor direct-axis damping loop, and the method comprises the following steps:
straight shaft damping loop
Figure 531850DEST_PATH_IMAGE009
Generating an air-gap magnetic field of
Figure 338132DEST_PATH_IMAGE073
In the above formula, j represents the imaginary part of the complex number,
Figure 247182DEST_PATH_IMAGE011
are respectively d 1 、d 2 、d 3 The radial magnetic density generated by the straight shaft damping loop,
Figure 582348DEST_PATH_IMAGE012
are respectively d 1 、d 2 、d 3 The resulting tangential magnetic flux density of the direct axis damping loop,
Figure 590231DEST_PATH_IMAGE013
the magnetic permeability of the air is such that,σthe magnetic flux leakage coefficient is obtained by the following steps,h m is half the thickness of the permanent magnet,b m is the width of the permanent magnet or magnets,
Figure 669046DEST_PATH_IMAGE014
is the minimum air gap length and is,
Figure 432602DEST_PATH_IMAGE015
is the distance between the poles of the magnetic field,
Figure 469828DEST_PATH_IMAGE016
the straight-axis basic air gap field can be obtained by the following formula:
Figure 951625DEST_PATH_IMAGE017
wherein the content of the first and second substances,R s is the inner radius of the stator and,R q is to solve the radius of the air gap flux density,
Figure 99710DEST_PATH_IMAGE018
is coefficient of polar arcpIs the number of the pole pairs,
Figure 452194DEST_PATH_IMAGE019
is the air gap length at the position of the Q point in the air gap,
Figure 660321DEST_PATH_IMAGE020
is a mechanical angle of view of the device,
Figure 114568DEST_PATH_IMAGE074
representing the arctan function.
The air gap magnetic field of the quadrature axis damping loop obtained according to the rotor quadrature axis damping loop magnetic potential comprises the following steps:
quadrature damping circuit
Figure 800764DEST_PATH_IMAGE022
The air gap magnetic field generated is:
Figure 538913DEST_PATH_IMAGE023
in the above formula, the first and second carbon atoms are,
Figure 652362DEST_PATH_IMAGE024
are each q 1 、q 2 、q 3 The radial magnetic density generated by the quadrature axis damping loop,
Figure 843172DEST_PATH_IMAGE025
are each q 1 、q 2 、q 3 Generating tangential magnetic flux density of the quadrature axis damping loop;
Figure 333059DEST_PATH_IMAGE075
the quadrature axis basic air gap field can be obtained by the following formula:
Figure 925715DEST_PATH_IMAGE027
wherein the content of the first and second substances,b j is the distance between the adjacent magnetic poles,
Figure 475645DEST_PATH_IMAGE028
is a function of the intermediate variable(s),
Figure 904483DEST_PATH_IMAGE076
the step of respectively obtaining the self inductance of the direct axis damping loop and the mutual inductance of the direct axis damping loop according to the air gap magnetic field of the direct axis damping loop comprises the following steps:
Figure 932482DEST_PATH_IMAGE030
the self-inductance of the d1, d2 and d3 direct axis damping loops is shown as the following formula:
Figure 379644DEST_PATH_IMAGE077
in the above formula, the first and second carbon atoms are,
Figure 100475DEST_PATH_IMAGE032
the permanent magnet synchronous motor with the damping strips for the rotor has the axial effective length,
Figure 265877DEST_PATH_IMAGE033
are respectively d 1 、d 2 、d 3 The self-flux linkage generated by the straight-axis damping loop;
Figure 97567DEST_PATH_IMAGE034
mutual inductance between the d1 and d2 direct-axis damping loops, mutual inductance between the d2 and d3 direct-axis damping loops, and mutual inductance between the d1 and d3 direct-axis damping loops are respectively shown as follows:
Figure 399235DEST_PATH_IMAGE035
therein
Figure 290968DEST_PATH_IMAGE036
The mutual magnetic linkage between the d1 and d2 direct-axis damping loops, the mutual magnetic linkage between the d1 and d3 direct-axis damping loops, and the mutual magnetic linkage between the d2 and d3 direct-axis damping loops.
The air gap magnetic field according to quadrature damping return circuit obtain quadrature damping return circuit's self-inductance and quadrature damping return circuit's mutual inductance respectively, include:
Figure 694399DEST_PATH_IMAGE078
the self-inductance of the quadrature axis damping loop q1, q2 and q3 respectively,
Figure 64200DEST_PATH_IMAGE079
the self-magnetic chains of the quadrature damping loops q1, q2 and q3 respectively are shown as follows:
Figure 220375DEST_PATH_IMAGE080
Figure 283009DEST_PATH_IMAGE040
mutual inductance between q1 and q2 quadrature axis damping loops, mutual inductance between q2 and q3 quadrature axis damping loops, mutual inductance between q1 and q3 quadrature axis damping loops,
Figure 157424DEST_PATH_IMAGE081
are each q 1 And q is 2 Flux linkage between quadrature damping loops, q 1 And q is 3 Flux linkage, q, between quadrature damping loops 2 And q is 3 The flux linkage between the quadrature damping loops is shown as follows:
Figure 596496DEST_PATH_IMAGE042
according to the air gap magnetic field of the direct-axis damping loop, the mutual inductance between the stator winding of the permanent magnet synchronous motor with the rotor provided with the damping strip and the direct-axis damping loop is obtained, and the method comprises the following steps:
Figure 872756DEST_PATH_IMAGE043
mutual inductance between the A-phase stator winding and the direct-axis damping loop is obtained according to an air gap magnetic field of the direct-axis damping loop:
Figure 106291DEST_PATH_IMAGE044
wherein, the first and the second end of the pipe are connected with each other,
Figure 468003DEST_PATH_IMAGE045
the number of the branches connected in parallel is equal to that of the branch,qis the number of slots per phase per pole,
Figure 944988DEST_PATH_IMAGE046
the number of turns of the winding in the slot is P, and the number of pole pairs is P; when the rotor is in the position of
Figure 341334DEST_PATH_IMAGE047
When the temperature of the water is higher than the set temperature,
Figure 745770DEST_PATH_IMAGE082
damping the flux linkage of the air-gap field entering the A-phase winding for the direct axis, an
Figure 594778DEST_PATH_IMAGE049
Figure 110073DEST_PATH_IMAGE050
Wherein, the first and the second end of the pipe are connected with each other,mthe number of the phases is the same as the number of the phases,
Figure 360925DEST_PATH_IMAGE051
is the axial position of the phase A in the rotor coordinate system,
Figure 670684DEST_PATH_IMAGE052
is the number of the stator slots, and the number of the stator slots,
Figure 6987DEST_PATH_IMAGE053
is the short-range coefficient of the signal,
Figure 325973DEST_PATH_IMAGE054
is the slot pitch electrical angle;
when the rotor rotates, relative motion exists between the stator winding and the rotor damping loop; when rotor is in electrical angle position
Figure 182065DEST_PATH_IMAGE055
When the rotor is in a rotating state, the direct-axis magnetic field of the stator winding changes, the mutual inductance between the stator winding and the rotor direct-axis damping loop changes simultaneously, the magnetic fields generated by the phases A, B and C have an electrical angle difference of 120 degrees in space, and the mutual inductance between the phase B and the phase C and the direct-axis damping loop can be obtained in the same way.
Further, the mutual inductance between the stator winding of the permanent magnet synchronous motor with the rotor having the damping strips and the quadrature axis damping loop is obtained according to the air gap magnetic field of the quadrature axis damping loop:
Figure 928304DEST_PATH_IMAGE056
mutual inductance between the A-phase stator winding and q1, q2 and q3 quadrature axis damping loops is obtained according to air gap magnetic fields of the quadrature axis damping loops:
Figure 486324DEST_PATH_IMAGE057
the mutual inductance between the phase B and the phase C and the quadrature axis damping loop can be obtained in the same way, and when the position of the rotor is
Figure 609001DEST_PATH_IMAGE083
When the utility model is used, the water is discharged,
Figure 568867DEST_PATH_IMAGE059
the air gap magnetic fields of the quadrature axis damping loops q1, q2 and q3 enter the flux linkage of the A phase winding,
Figure 486007DEST_PATH_IMAGE060
the number of the parallel branches is the same as the number of the parallel branches,
Figure 796903DEST_PATH_IMAGE084
the number of the pole pairs is the number of the pole pairs,
Figure 457691DEST_PATH_IMAGE085
the current of the quadrature axis damping loop, q is the number of slots per pole and phase,
Figure 22796DEST_PATH_IMAGE063
the number of turns of the winding in the slot,
Figure 376417DEST_PATH_IMAGE064
is the radius of the point Q in the air gap,
Figure 909030DEST_PATH_IMAGE065
the axial effective length of the motor is long,
Figure 842350DEST_PATH_IMAGE066
the resulting radial flux densities of the q1, q2, and q3 damping loops, respectively.
Also includes the leakage inductance of the damping loop, which is obtained by the following formula: further, the method comprises
Figure 776808DEST_PATH_IMAGE067
In the above formula, the first and second carbon atoms are,pthe number of the pole pairs is the number of the pole pairs,
Figure 301331DEST_PATH_IMAGE068
is a magnetic permeability of air, and
Figure 55660DEST_PATH_IMAGE069
in the above formula, the first and second carbon atoms are,b ro the width of the rotor slot is the width of the rotor slot,h ro the height of the notch of the rotor is high,R rs radius of the circular rotor slot, and then damping the leakage inductance of the circuit
Figure 323830DEST_PATH_IMAGE070
The self-inductance of the damping loop is added,
Figure 112795DEST_PATH_IMAGE071
is an arcsine function.
Specifically, according to the method for analyzing and calculating the inductance of the multiple damping loops of the permanent magnet synchronous motor with the damping strips on the rotor, as shown in fig. 2, in the starting process, the damping strips generate induced current.
The rotor damping loop and the stator winding are mutually linked, mutual inductance is generated between the stator and the rotor, and self inductance and mutual inductance of the rotor are also generated by the interaction between the rotor damping loops.
The magnetic potential of the damping strip induced current is related to the number of damping strips and the slot pitch. Due to the rotation of the rotor, the relative position between the rotor and the stator changes. The damping bars are divided into direct-axis damping bars and quadrature-axis damping bars to calculate the magnetic field generated by the damping bars. The magnetic potential of the rotor damping strip is direct-axis magnetic potential and quadrature-axis magnetic potential respectively.
The number of damping strips on each pole of the rotor is 6,
Figure 293372DEST_PATH_IMAGE086
in order to provide a straight-axis damping loop,
Figure 800576DEST_PATH_IMAGE087
is a quadrature damping loop. The number of the rotor direct axis damping loops and the number of the quadrature axis damping loops are both 3, and fig. 3 is a structural diagram of the quadrature axis damping loops and the direct axis damping loops.
Because a solid conductor is arranged in the rotor slot, the number of turns of each damping loop of the rotor is 1, and when the current of the damping loop isIIn the meantime, the method for representing the magnetic potential distribution of the rotor direct-axis damping circuit is shown as the following formula
Figure 606858DEST_PATH_IMAGE088
Figure 250329DEST_PATH_IMAGE089
Are respectively d-axis d 1 、d 2 、d 3 The magnetomotive force of the damping circuit,
Figure 116654DEST_PATH_IMAGE090
is the groove pitch angle of the damping strip,
Figure 845576DEST_PATH_IMAGE091
is the spatial electrical angular position. When the angle in this patent is not described, the angle is an electrical angle.
The magnetic potential distribution of the rotor quadrature axis damping loop is shown as the following formula:
Figure 455549DEST_PATH_IMAGE092
in the above formula, the first and second carbon atoms are,
Figure 219105DEST_PATH_IMAGE008
are respectively q-axis q 1 、q 2 、q 3 The magnetomotive force of the damping circuit.
The magnetomotive force in the air gap between the stator and the rotor is shaped as a square wave when current flows in the damping circuit. Then straight shaft damping loop
Figure 738555DEST_PATH_IMAGE093
The air gap magnetic field is generated as
Figure 220352DEST_PATH_IMAGE094
In the above-mentioned formula, the compound has the following structure,
Figure 368436DEST_PATH_IMAGE095
are respectively d 1 、d 2 、d 3 The resulting radial flux density of the damping circuit.
Figure 986499DEST_PATH_IMAGE012
Are respectively d 1 、d 2 、d 3 The resulting tangential magnetic flux density of the damping circuit. ,
Figure 929048DEST_PATH_IMAGE096
the magnetic permeability of the air is such that,σthe magnetic flux leakage coefficient is that the magnetic flux leakage coefficient,h m is half the thickness of the permanent magnet,b m is the width of the permanent magnet or magnets,
Figure 632562DEST_PATH_IMAGE014
is the minimum air gap length and is,
Figure 584337DEST_PATH_IMAGE015
is the distance between the two poles of the wire,
Figure 791327DEST_PATH_IMAGE016
the straight-axis basic air gap magnetic field can be obtained by the following formula.
Figure 170356DEST_PATH_IMAGE097
In the above formula, the first and second carbon atoms are,R s is the inner radius of the stator and,R q is to solve the radius of the air gap flux density,
Figure 111898DEST_PATH_IMAGE018
is coefficient of polar arcpIs the number of the pole pairs,
Figure 601786DEST_PATH_IMAGE019
is the air gap length at the position of the Q point in the air gap,
Figure 194441DEST_PATH_IMAGE098
is a mechanical angle.
Quadrature damping circuit
Figure 744371DEST_PATH_IMAGE099
The air gap field generated is:
Figure 156898DEST_PATH_IMAGE100
in the above formula, the first and second carbon atoms are,
Figure 450476DEST_PATH_IMAGE101
are each q 1 、q 2 、q 3 The resulting radial magnetic density of the damping circuit,
Figure 897638DEST_PATH_IMAGE102
are each q 1 、q 2 、q 3 The generated tangential magnetic flux density of the damping loop;
Figure 618469DEST_PATH_IMAGE075
the quadrature axis basic air gap field can be obtained by the following formula.
Figure 534604DEST_PATH_IMAGE103
Upper typeIn the step (1), the first step,b j is the distance between adjacent magnetic poles and is,
Figure 366293DEST_PATH_IMAGE104
is the intermediate variable(s) of the variable,
Figure 402383DEST_PATH_IMAGE105
1) Self and mutual inductance of damping loops
Since the direct-axis damping loop and the quadrature-axis damping loop are orthogonal, the mutual inductance between the direct-axis loop and the quadrature-axis loop is zero. Only the self-inductance and mutual-inductance of the direct-axis damping loop and the self-inductance and mutual-inductance of the quadrature-axis damping loop exist.
a) Self-inductance and mutual inductance of direct-axis damping loop
Figure 294115DEST_PATH_IMAGE106
For the self-inductance of the direct-axis damping loop, the air-gap magnetic field formula of the direct-axis damping loop can be substituted into the following formula to obtain
Figure 681234DEST_PATH_IMAGE107
In the above-mentioned formula, the compound has the following structure,
Figure 316615DEST_PATH_IMAGE108
the permanent magnet synchronous motor with the damping strips for the rotor has the axial effective length,
Figure 738369DEST_PATH_IMAGE109
is a magnetic linkage.
Figure 801003DEST_PATH_IMAGE110
For the mutual inductance between the straight-axis damping loops, the air-gap magnetic field formula of the straight-axis damping loops can be substituted into the following formula to obtain
Figure 675418DEST_PATH_IMAGE111
b) Self-inductance and mutual-inductance of quadrature damping loop
Figure 599643DEST_PATH_IMAGE078
For the self-inductance of the quadrature axis damping loop, the air-gap magnetic field formula of the quadrature axis damping loop can be substituted into the following formula to obtain
Figure 875903DEST_PATH_IMAGE112
Figure 109439DEST_PATH_IMAGE113
For mutual inductance between the quadrature axis damping loops, the air gap magnetic field formula of the quadrature axis damping loops can be substituted into the following formula to obtain
Figure 471150DEST_PATH_IMAGE114
c) Leakage inductance of damping circuit
Calculating the leakage inductance of the damping circuit by considering the leakage inductance of the slot, wherein the leakage inductance of the damping circuit can be obtained by the following formula
Figure DEST_PATH_IMAGE115
In the above formula, the first and second carbon atoms are,pthe number of the pole pairs is the number of the pole pairs,
Figure DEST_PATH_IMAGE116
is a magnetic permeability of air, and
Figure DEST_PATH_IMAGE117
in the above-mentioned formula, the compound has the following structure,b ro the width of the rotor slot is the width of the rotor slot,h ro the height of the notch of the rotor is high,R rs the radius of a circular rotor slot. Then, handle the resistanceLeakage inductance of damping loop
Figure 245071DEST_PATH_IMAGE118
Adding damping loop self-inductance.
2) Mutual inductance between stator winding and damping circuit
The damping loop is divided into a direct-axis damping loop and a quadrature-axis damping loop. According to the damping loop air gap magnetic field of the permanent magnet synchronous motor with the rotor provided with the damping strips, at different rotor positions, the flux linkage of the interlinkage of the rotor damping loop and the stator armature winding is different, and the mutual inductance between the stator winding and the damping loop can change along with the rotor position.
a) Mutual inductance between stator winding and direct axis damping circuit
The number of the straight shaft damping loops is three,
Figure DEST_PATH_IMAGE119
is mutual inductance between the A-phase stator winding and the direct-axis damping loop, and can be obtained by substituting the air-gap magnetic field formula of the direct-axis damping loop into the following formula
Figure DEST_PATH_IMAGE120
In the above-mentioned formula, the compound has the following structure,
Figure DEST_PATH_IMAGE121
the number of the branches connected in parallel is,qis the number of slots per phase per pole,
Figure DEST_PATH_IMAGE122
the number of turns of the winding in the slot; when the rotor is in the position of
Figure 191817DEST_PATH_IMAGE123
When the utility model is used, the water is discharged,
Figure DEST_PATH_IMAGE124
damping the flux linkage of the air-gap field entering the A-phase winding for the direct axis, an
Figure 861832DEST_PATH_IMAGE125
Figure DEST_PATH_IMAGE126
In the above formula, the first and second carbon atoms are,mthe number of the phases is shown as,
Figure DEST_PATH_IMAGE127
is the axial position of phase A in the rotor coordinate system,
Figure 727151DEST_PATH_IMAGE128
is the number of the stator slots, and the number of the stator slots,
Figure DEST_PATH_IMAGE129
is the short-range coefficient of the signal,
Figure 773605DEST_PATH_IMAGE130
is the slot pitch electrical angle.
When the rotor rotates, there is relative motion between the stator windings and the rotor damping circuit. When rotor is in electrical angle position
Figure DEST_PATH_IMAGE131
In time, the direct axis magnetic field of the stator winding changes during rotation. The mutual inductance between the stator windings and the rotor direct axis damping circuit changes simultaneously. The mutual inductance is calculated at different rotor positions. A. The phase difference of magnetic fields generated by the B phase and the C phase in the space is 120 degrees, and the mutual inductance between the B phase or the C phase and the straight-axis damping loop can be obtained by using the same principle.
b) Mutual inductance between stator winding and quadrature damping circuit
The number of the quadrature axis damping loops is three,
Figure DEST_PATH_IMAGE132
is mutual inductance between the A-phase stator winding and the quadrature axis damping loop, and can be obtained by substituting the air gap magnetic field formula of the quadrature axis damping loop into the following formula
Figure 555616DEST_PATH_IMAGE133
Therefore, the mutual inductance between the B phase or the C phase and the quadrature damping loop can be obtained by using the same principle.
Fig. 4-9 illustrate the mutual inductance between the a-phase winding and the damping loop. As can be seen from FIGS. 4-9, the magnetic field calculated by the analytic method and the finite element method has good goodness of fit, and the correctness of the analytic method adopted by the invention is proved. The method for calculating the inductance of the damping loop of the permanent magnet synchronous motor with the rotor provided with the damping strip can further carry out accurate analytic simulation calculation on the starting performance of the permanent magnet synchronous motor with the rotor provided with the damping strip
The foregoing is illustrative of the preferred embodiments of the present invention, and it is to be understood that the invention is not limited to the precise form disclosed herein and is not to be construed as limited to the exclusion of other embodiments, and that various other combinations, modifications, and environments may be used and modifications may be made within the scope of the concepts described herein, either by the above teachings or the skill or knowledge of the relevant art. And that modifications and variations may be effected by those skilled in the art without departing from the spirit and scope of the invention as defined by the appended claims.

Claims (9)

1. A method for calculating the inductance of a permanent magnet motor with a damping strip on a rotor and multiple damping loops is characterized by comprising the following steps:
the method comprises the steps of obtaining induction current of a damping strip on a rotor in the starting process of a permanent magnet synchronous motor with the damping strip on the rotor, and obtaining the magnetic potential of a rotor direct-axis damping loop and the magnetic potential of a rotor quadrature-axis damping loop of a rotor damping loop according to the induction current; obtaining an air-gap magnetic field of the direct-axis damping loop according to the magnetic potential of the rotor direct-axis damping loop, and obtaining an air-gap magnetic field of the quadrature-axis damping loop according to the magnetic potential of the rotor quadrature-axis damping loop;
respectively obtaining the self inductance of the direct-axis damping loop and the mutual inductance of the direct-axis damping loop according to the air gap magnetic field of the direct-axis damping loop; respectively obtaining self inductance of the quadrature axis damping loop and mutual inductance of the quadrature axis damping loop according to the air gap magnetic field of the quadrature axis damping loop;
obtaining mutual inductance between a stator winding of the permanent magnet synchronous motor with the rotor provided with the damping strips and the direct-axis damping loop according to the air gap magnetic field of the direct-axis damping loop; obtaining mutual inductance between a stator winding of the permanent magnet synchronous motor with the rotor provided with the damping strips and the quadrature axis damping loop according to an air gap magnetic field of the quadrature axis damping loop;
according to the obtained self-inductance of the direct-axis damping loop, the mutual inductance of the direct-axis damping loop, the self-inductance of the quadrature-axis damping loop, the mutual inductance between the stator winding and the direct-axis damping loop and the mutual inductance between the stator winding and the quadrature-axis damping loop, the permanent magnet motor with the rotor band damping strip is optimized, and the transient performance and the steady-state performance of the permanent magnet motor with the rotor band damping strip in the starting process are improved.
2. The method for calculating the inductance of the multiple damping loops of the permanent magnet motor with the damping strips on the rotor according to the claim 1, wherein the method for obtaining the magnetic potential of the direct-axis damping loop and the magnetic potential of the quadrature-axis damping loop of the rotor of the damping loop according to the induced current comprises the following steps:
when the current of the damping loop isIThen, the magnetic potential distribution of the rotor straight shaft damping loop is shown as follows:
Figure QLYQS_1
Figure QLYQS_2
is a straight-axis damping loop and is characterized in that,
Figure QLYQS_3
in order to provide a quadrature axis damping loop,
Figure QLYQS_4
respectively d axis d 1 、d 2 、d 3 The magnetomotive force of the damping circuit,
Figure QLYQS_5
is the groove pitch angle of the damping strip,
Figure QLYQS_6
is the spatial electrical angular position;
the magnetic potential distribution of the rotor quadrature axis damping loop is shown as follows:
Figure QLYQS_7
Figure QLYQS_8
are respectively q-axis q 1 、q 2 、q 3 The magnetomotive force of the damping circuit.
3. The method for calculating the inductance of the multiple damping loops of the permanent magnet motor with the rotor provided with the damping strips according to the claim 2, wherein the step of obtaining the air-gap magnetic field of the direct-axis damping loop according to the magnetic potential of the direct-axis damping loop of the rotor comprises the following steps:
straight shaft damping loop
Figure QLYQS_9
Generating an air-gap magnetic field of
Figure QLYQS_10
In the above formula, j represents the imaginary part of the complex number,
Figure QLYQS_11
are respectively d 1 、d 2 、d 3 The resulting radial flux density of the direct axis damping loop,
Figure QLYQS_12
are respectively d 1 、d 2 、d 3 The resulting tangential magnetic flux density of the direct axis damping loop,
Figure QLYQS_13
the magnetic permeability of the air is such that,σthe magnetic flux leakage coefficient is obtained by the following steps,h m is half the thickness of the permanent magnet and,b m is the width of the permanent magnet or magnets,
Figure QLYQS_14
is the minimum air gap length and is,
Figure QLYQS_15
is the distance between the two poles of the wire,
Figure QLYQS_16
the straight-axis basic air gap field can be obtained by the following formula:
Figure QLYQS_17
wherein the content of the first and second substances,R s is the inner radius of the stator and,R q is to solve the radius of the air gap flux density,
Figure QLYQS_18
is the coefficient of the polar arc,pis the number of the pole pairs,
Figure QLYQS_19
is the air gap length at the position of the Q point in the air gap,
Figure QLYQS_20
is a mechanical angle of view of the device,
Figure QLYQS_21
representing the arctan function.
4. The method for calculating the inductance of the multiple damping loops of the permanent magnet motor with the rotor provided with the damping strips according to the claim 3, wherein the step of obtaining the air-gap magnetic field of the quadrature damping loop according to the rotor quadrature damping loop magnetic potential comprises the following steps:
quadrature damping circuit
Figure QLYQS_22
The air gap magnetic field generated is:
Figure QLYQS_23
in the above formula, the first and second carbon atoms are,
Figure QLYQS_24
are each q 1 、q 2 、q 3 The resulting radial magnetic density of the damping circuit,
Figure QLYQS_25
are each q 1 、q 2 、q 3 The resulting tangential flux density of the damping circuit;
Figure QLYQS_26
the quadrature axis basic air gap field can be obtained by the following formula:
Figure QLYQS_27
wherein, the first and the second end of the pipe are connected with each other,b j is the distance between adjacent magnetic poles and is,
Figure QLYQS_28
is the intermediate variable(s) of the variable,
Figure QLYQS_29
5. the method for calculating the inductance of the multiple damping loops of the permanent magnet motor with the damping strips on the rotor according to the claim 4, wherein the step of respectively obtaining the self inductance of the direct-axis damping loop and the mutual inductance of the direct-axis damping loop according to the air-gap magnetic field of the direct-axis damping loop comprises the following steps:
Figure QLYQS_30
are respectively d1D2, d3 direct axis damping loop self inductance, as shown in the following formula:
Figure QLYQS_31
in the above formula, the first and second carbon atoms are,
Figure QLYQS_32
the permanent magnet synchronous motor with the rotor provided with the damping strips has the axial effective length,
Figure QLYQS_33
are respectively d 1 、d 2 、d 3 The self-flux linkage generated by the straight-axis damping loop;
Figure QLYQS_34
mutual inductance between the d1 and d2 direct-axis damping loops, mutual inductance between the d2 and d3 direct-axis damping loops, and mutual inductance between the d1 and d3 direct-axis damping loops are respectively shown as follows:
Figure QLYQS_35
therein are
Figure QLYQS_36
Figure QLYQS_37
And
Figure QLYQS_38
the mutual magnetic linkage between the d1 and d2 direct-axis damping loops, the mutual magnetic linkage between the d1 and d3 direct-axis damping loops, and the mutual magnetic linkage between the d2 and d3 direct-axis damping loops.
6. The method for calculating the inductance of the multiple damping loops of the permanent magnet motor with the damping strips on the rotor according to the claim 5, wherein the self inductance of the quadrature damping loop and the mutual inductance of the quadrature damping loop are respectively obtained according to the air-gap magnetic field of the quadrature damping loop, and the method comprises the following steps:
Figure QLYQS_39
self-inductance of the quadrature damping loop of q1, q2 and q3 respectively,
Figure QLYQS_40
the self-magnetic chains of the quadrature damping loops q1, q2 and q3 respectively are shown as follows:
Figure QLYQS_41
Figure QLYQS_42
mutual inductance between q1 and q2 quadrature damping loops, mutual inductance between q2 and q3 quadrature damping loops, and mutual inductance between q1 and q3 quadrature damping loops, respectively;
Figure QLYQS_43
Figure QLYQS_44
and
Figure QLYQS_45
are each q 1 And q is 2 Flux linkage, q, between quadrature damping loops 1 And q is 3 Flux linkage between quadrature damping loops, q 2 And q is 3 The flux linkage between the quadrature damping loops is shown as follows:
Figure QLYQS_46
7. the method for calculating the inductance of the multiple damping loops of the permanent magnet motor with the rotor damping strips according to the claim 6, wherein the step of obtaining the mutual inductance between the stator winding of the permanent magnet synchronous motor with the rotor damping strips and the direct-axis damping loops according to the air-gap magnetic field of the direct-axis damping loops comprises the following steps:
Figure QLYQS_47
mutual inductance between the A-phase stator winding and the direct-axis damping loop is obtained according to an air gap magnetic field of the direct-axis damping loop:
Figure QLYQS_48
wherein the content of the first and second substances,
Figure QLYQS_49
the number of the branches connected in parallel is,qis the number of slots per pole per phase,
Figure QLYQS_50
the number of turns of the winding in the slot is P, and the number of pole pairs is P; when the rotor is in the position of
Figure QLYQS_51
When the temperature of the water is higher than the set temperature,
Figure QLYQS_52
damping the flux linkage of the air-gap field entering the A-phase winding for the direct axis, an
Figure QLYQS_53
Figure QLYQS_54
Wherein, the first and the second end of the pipe are connected with each other,mthe number of the phases is the same as the number of the phases,
Figure QLYQS_55
is the axial position of phase A in the rotor coordinate system,
Figure QLYQS_56
the number of the stator slots is the number of the stator slots,
Figure QLYQS_57
is the short-range coefficient of the signal,
Figure QLYQS_58
is the slot pitch electrical angle;
when the rotor rotates, relative motion exists between the stator winding and the rotor damping loop; when the rotor is in electrical angle position
Figure QLYQS_59
When the rotor is rotated, the direct-axis magnetic field of the stator winding changes in the rotating process, the mutual inductance between the stator winding and the rotor direct-axis damping loop changes simultaneously, the magnetic fields generated by the A phase, the B phase and the C phase have an electrical angle difference of 120 degrees in space, and the mutual inductance between the B phase and the C phase and the direct-axis damping loop can be obtained in the same way.
8. The method for calculating the inductance of the multiple damping loops of the permanent magnet motor with the rotor damping strips as claimed in claim 7, wherein the mutual inductance between the stator winding of the permanent magnet synchronous motor with the rotor damping strips and the quadrature damping loops is obtained according to the air-gap field of the quadrature damping loops:
Figure QLYQS_60
mutual inductance between the A-phase stator winding and q1, q2 and q3 quadrature axis damping loops is obtained according to air gap magnetic fields of the quadrature axis damping loops:
Figure QLYQS_61
in the same way, the mutual inductance between the B phase and the C phase and the quadrature axis damping loop can be obtained when the rotor is positioned
Figure QLYQS_63
When the utility model is used, the water is discharged,
Figure QLYQS_67
the air gap magnetic fields of the quadrature axis damping loops q1, q2 and q3 enter the flux linkage of the A phase winding,
Figure QLYQS_69
the number of the parallel branches is the same as the number of the parallel branches,
Figure QLYQS_64
the number of the pole pairs is the number of the pole pairs,
Figure QLYQS_66
the current of the quadrature axis damping loop, q is the number of slots per pole and phase,
Figure QLYQS_68
the number of turns of the winding in the slot,
Figure QLYQS_70
is to solve for the radius of the air gap flux density,
Figure QLYQS_62
the axial effective length of the motor is long,
Figure QLYQS_65
the resulting radial flux densities of the q1, q2, q3 damping loops, respectively.
9. The method for calculating the inductance of the multiple damping loops of the permanent magnet motor with the damping strips on the rotor according to claim 8, further comprising the leakage inductance of the damping loops, which is obtained by the following formula:
Figure QLYQS_71
in the above-mentioned formula, the compound has the following structure,pthe number of the pole pairs is the number of the pole pairs,
Figure QLYQS_72
is a magnetic permeability of air, and
Figure QLYQS_73
in the above formula, the first and second carbon atoms are,b ro the width of the rotor slot is the width of the rotor slot,h ro the height of the notch of the rotor is high,R rs radius of the circular rotor slot, and then damping the leakage inductance of the circuit
Figure QLYQS_74
The self-inductance of the damping loop is added,
Figure QLYQS_75
is an arcsine function.
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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1514314A (en) * 1974-07-12 1978-06-14 Siemens Ag Synchronous machines
US5309089A (en) * 1991-11-12 1994-05-03 Mitsubishi Denki Kabushiki Kaisha Method of measuring unsaturated inductances of an equivalent circuit of a synchronous machine
CN101588118A (en) * 2008-05-20 2009-11-25 上海海事大学 Method for modeling double three-phase permanent-magnetic synchronous motors
CN103853891A (en) * 2014-03-21 2014-06-11 西北工业大学 Finite element analysis-based variable-element permanent magnet synchronous motor modeling method
CN114421830A (en) * 2022-03-29 2022-04-29 南京凌博电子科技有限公司 Motor control method based on virtual damping winding for permanent magnet synchronous motor
CN115021638A (en) * 2022-06-15 2022-09-06 南方电网科学研究院有限责任公司 Electromagnetic transient modeling method, system and equipment of efficient synchronous machine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201112247D0 (en) * 2011-07-15 2011-08-31 Wind Technologies Ltd Brushless doubly fed machines
CN108573094B (en) * 2018-03-21 2019-03-15 华北电力大学 The method for building up and system of the VBR electromagnetic transient simulation model of synchronous generator
CN111654165B (en) * 2020-05-31 2022-04-08 天津工业大学 Built-in permanent magnet synchronous motor magnetic field calculation method based on rotor magnetic potential model
CN113507189B (en) * 2021-07-01 2022-07-26 山东大学 Design parameter optimization method for built-in permanent magnet synchronous motor

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1514314A (en) * 1974-07-12 1978-06-14 Siemens Ag Synchronous machines
US5309089A (en) * 1991-11-12 1994-05-03 Mitsubishi Denki Kabushiki Kaisha Method of measuring unsaturated inductances of an equivalent circuit of a synchronous machine
CN101588118A (en) * 2008-05-20 2009-11-25 上海海事大学 Method for modeling double three-phase permanent-magnetic synchronous motors
CN103853891A (en) * 2014-03-21 2014-06-11 西北工业大学 Finite element analysis-based variable-element permanent magnet synchronous motor modeling method
CN114421830A (en) * 2022-03-29 2022-04-29 南京凌博电子科技有限公司 Motor control method based on virtual damping winding for permanent magnet synchronous motor
CN115021638A (en) * 2022-06-15 2022-09-06 南方电网科学研究院有限责任公司 Electromagnetic transient modeling method, system and equipment of efficient synchronous machine

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
Calculation of the damper winding inductances of a synchronous machine;O. Misir, et al.;《8th IET International Conference on Power Electronics, Machines and Drives (PEMD 2016)》;20161110;第1-6页 *
同步电动机阻尼绕组的参数计算;谢卫,等;《上海大中型电机》;20091231;第14-16页 *
同步电机的混合模型;黄进,等;《电工技术学报》;19900531(第2期);第11-16页 *

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