CN109667762B - Method and device for inhibiting rotating speed fluctuation of single-rotor compressor - Google Patents
Method and device for inhibiting rotating speed fluctuation of single-rotor compressor Download PDFInfo
- Publication number
- CN109667762B CN109667762B CN201811531819.5A CN201811531819A CN109667762B CN 109667762 B CN109667762 B CN 109667762B CN 201811531819 A CN201811531819 A CN 201811531819A CN 109667762 B CN109667762 B CN 109667762B
- Authority
- CN
- China
- Prior art keywords
- axis
- filtering
- harmonic
- theta
- error
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
- F04C28/00—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
- F04C28/08—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids characterised by varying the rotational speed
Abstract
The invention discloses a method and a device for inhibiting the rotation speed fluctuation of a single-rotor compressor, wherein the method comprises the following steps: obtaining a shaft error reflecting a deviation of an actual position and an estimated position of a compressor rotor; filtering the axis error to obtain an axis error compensation quantity after at least filtering part of axis error fluctuation; inputting the shaft error compensation quantity as an input quantity to a phase-locked loop regulator in a phase-locked loop for controlling the compressor; and correcting the real-time angular speed for controlling the compressor by using the output angular speed of the phase-locked loop regulator, and controlling the compressor according to the corrected real-time angular speed. By applying the invention, the effectiveness of inhibiting the fluctuation of the rotating speed of the compressor can be improved.
Description
Technical Field
The invention belongs to the technical field of motor control, particularly relates to a compressor control technology, and more particularly relates to a method and a device for inhibiting the rotation speed fluctuation of a single-rotor compressor.
Background
When the compressor used by the air conditioner runs, the compressor is influenced by the working principle and the control technology of the air conditioner serving as a load, so that the load torque of the compressor is extremely unstable, large rotation speed fluctuation is easily caused, and the running of the compressor is not stable. The unstable operation of the compressor can cause the unstable operation of the whole air conditioner system, resulting in various adverse effects. And unstable operation can also produce great operating noise, can not satisfy relevant noise standard requirement, influences air conditioner and uses the travelling comfort. This phenomenon is particularly serious in a single-rotor compressor. Although the prior art also has a method for inhibiting the fluctuation of the rotating speed of the compressor, the fluctuation inhibiting effect is not ideal enough, and the problem of the fluctuation of the rotating speed of the compressor cannot be fundamentally solved.
Disclosure of Invention
The invention aims to provide a method and a device for inhibiting the rotation speed fluctuation of a single-rotor compressor, and the effectiveness of the fluctuation inhibition is improved.
In order to achieve the purpose of the invention, the method provided by the invention is realized by adopting the following technical scheme:
a method of suppressing fluctuations in the rotational speed of a single-rotor compressor, comprising:
acquiring a shaft error delta theta reflecting a deviation between an actual position and an estimated position of a compressor rotor;
filtering the axis error delta theta to obtain an axis error compensation quantity delta theta' after at least part of axis error fluctuation is filtered;
inputting the shaft error compensation quantity delta theta' as an input quantity to a phase-locked loop regulator in a phase-locked loop for controlling the compressor;
correcting the real-time angular velocity omega 1 for controlling the compressor by using the output angular velocity delta omega _ PLL of the phase-locked loop regulator, and controlling the compressor according to the corrected real-time angular velocity omega 1;
the filtering processing is performed on the axis error delta theta to obtain an axis error compensation quantity delta theta' after at least part of axis error fluctuation is filtered, and the method specifically comprises the following steps:
performing Fourier series expansion on the axis error delta theta to obtain the mechanical angle theta of the axis errormThe functional expression of (a);
the function expressions are respectively related to cos thetamnAnd-sin θmnAfter multiplication, extracting d-axis components and q-axis components of n-th harmonic waves of delta theta; thetamnMechanical angle for nth harmonic;
filtering a d-axis component and a q-axis component of partial harmonic waves by using an integrator to obtain a filtering result, and realizing filtering processing of the axis error delta theta;
filtering out the filter junctionThe result after filtering the d-axis component of partial harmonic and the result after filtering the q-axis component of partial harmonic in the result are respectively compared with cos (theta)mn+θshift-Pn) And-sin (theta)mn+θshift-Pn) Multiplying and performing inverse Fourier transform to obtain an angular velocity compensation quantity P _ out corresponding to the correction axis error delta theta' of the filtered partial harmonic component; thetashift-PnPhase compensation angle for nth harmonic;
and converting the angular velocity compensation amount P _ out into an angle to obtain the shaft error compensation amount delta theta'.
In the above method, the filtering processing is performed on the axis error Δ θ to obtain an axis error compensation amount Δ θ' obtained by filtering at least part of the axis error fluctuation, specifically including:
and performing filtering processing on the axis error delta theta, at least filtering a d-axis component and a q-axis component of a first harmonic in the delta theta, realizing filtering of a first harmonic component of the delta theta, and obtaining an axis error compensation quantity delta theta' for at least filtering the first harmonic component.
Further, the filtering processing on the axis error Δ θ to obtain an axis error compensation amount Δ θ' after at least part of the axis error fluctuation is filtered out, further includes: and filtering d-axis components and q-axis components of second harmonic in the delta theta, realizing filtering of first harmonic components and second harmonic components of the delta theta, and obtaining axial error compensation quantity delta theta' for filtering the first harmonic components and the second harmonic components.
The method as described above, said function expression being respectively related to cos θmnAnd-sin θmnAfter multiplication, extracting d-axis components and q-axis components of n-th harmonics of delta theta, and specifically comprising the following steps: the function expressions are respectively related to cos thetamnAnd-sin θmnAfter multiplication, a d-axis component and a q-axis component of the nth harmonic of Δ θ are extracted by a low-pass filtering method or an integration method.
Further, the phase compensation angle theta of the nth harmonic waveshift-PnAccording to the closed loop gain parameter K of the phase-locked loopP_PLL、KI_PLLAnd the angular speed command ω _ in of the phase-locked loop is determined and satisfies:
θshift-Pn＝(aKP_PLL+bKI_PLL+cKP_PLL/KI_PLL+ d ω _ in) × pi, a, b, c, d are constant coefficients.
In order to achieve the purpose, the device provided by the invention adopts the following technical scheme:
an apparatus for suppressing rotation speed fluctuation of a single-rotor compressor, comprising:
a shaft error acquisition unit for acquiring a shaft error Δ θ reflecting a deviation of an actual position and an estimated position of a compressor rotor;
the shaft error compensation quantity acquisition unit is used for filtering the shaft error delta theta to obtain a shaft error compensation quantity delta theta' after at least part of shaft error fluctuation is filtered;
the control unit is used for inputting the shaft error compensation quantity delta theta' as an input quantity to a phase-locked loop regulator in a phase-locked loop for controlling the compressor, correcting the real-time angular speed omega 1 for controlling the compressor by utilizing the output angular speed delta omega _ PLL of the phase-locked loop regulator, and controlling the compressor according to the corrected real-time angular speed omega 1;
the shaft error compensation quantity obtaining unit performs filtering processing on the shaft error Δ θ to obtain a shaft error compensation quantity Δ θ' after at least part of shaft error fluctuation is filtered, and the method specifically includes:
performing Fourier series expansion on the axis error delta theta to obtain the mechanical angle theta of the axis errormThe functional expression of (a);
the function expressions are respectively related to cos thetamnAnd-sin θmnAfter multiplication, extracting d-axis components and q-axis components of n-th harmonic waves of delta theta; thetamnMechanical angle for nth harmonic;
filtering a d-axis component and a q-axis component of partial harmonic waves by using an integrator to obtain a filtering result, and realizing filtering processing of the axis error delta theta;
respectively comparing the result of filtering out the d-axis component of partial harmonic and the result of filtering out the q-axis component of partial harmonic with cos (theta)mn+θshift-Pn) And-sin (theta)mn+θshift-Pn) Multiplying by inverse Fourier transform to obtain and filter out the partAn angular velocity compensation amount P _ out corresponding to the correction axis error Delta theta' of the harmonic component; thetashift-PnPhase compensation angle for nth harmonic;
and converting the angular velocity compensation amount P _ out into an angle to obtain the shaft error compensation amount delta theta'.
In the above apparatus, the axial error compensation amount obtaining unit performs filtering processing on the axial error Δ θ to obtain an axial error compensation amount Δ θ' after at least part of axial error fluctuation is filtered out, specifically including:
and performing filtering processing on the axis error delta theta, at least filtering a d-axis component and a q-axis component of a first harmonic in the delta theta, realizing filtering of a first harmonic component of the delta theta, and obtaining an axis error compensation quantity delta theta' for at least filtering the first harmonic component.
Further, the shaft error compensation amount obtaining unit performs filtering processing on the shaft error Δ θ to obtain a shaft error compensation amount Δ θ' after at least part of shaft error fluctuation is filtered, and the method further includes: and filtering d-axis components and q-axis components of second harmonic in the delta theta, realizing filtering of first harmonic components and second harmonic components of the delta theta, and obtaining axial error compensation quantity delta theta' for filtering the first harmonic components and the second harmonic components.
In the above-described device, the axis error compensation amount obtaining unit may respectively relate the function expressions to cos θmnAnd-sin θmnAfter multiplication, extracting d-axis components and q-axis components of n-th harmonics of delta theta, and specifically comprising the following steps: the function expressions are respectively related to cos thetamnAnd-sin θmnAfter multiplication, a d-axis component and a q-axis component of the nth harmonic of Δ θ are extracted by a low-pass filtering method or an integration method.
Further, the phase compensation angle theta of the nth harmonic waveshift-PnAccording to the closed loop gain parameter K of the phase-locked loopP_PLL、KI_PLLAnd the angular speed command ω _ in of the phase-locked loop is determined and satisfies:
θshift-Pn＝(aKP_PLL+bKI-PLL+cKP_PLL/KI_PLL+ d ω _ in) × pi, a, b, c, d are constant coefficients.
Compared with the prior art, the invention has the advantages and positive effects that: the invention provides a method and a device for inhibiting the fluctuation of the rotating speed of a single-rotor compressor, which filters the fluctuation of a shaft error delta theta reflecting the deviation of the actual position and the estimated position of a compressor rotor, inputs the shaft error compensation quantity after filtering at least part of the shaft error fluctuation into a phase-locked loop regulator as an input quantity, and the shaft error compensation quantity after filtering part of the fluctuation can compensate the shaft error, reduce the fluctuation of the shaft error and then input into the phase-locked loop regulator, thereby reducing the fluctuation of the real-time angular speed of the compressor corrected by the output angular speed of the phase-locked loop regulator, and enabling the fluctuation quantity and the phase of the target rotating speed to be close to the fluctuation quantity and the phase of the actual rotating speed when the compressor is controlled by the corrected real-time angular speed, and enabling the operation of the compressor to tend to be stable; moreover, because the fluctuation of the shaft error is a front end direct factor causing the speed fluctuation, the periodical fluctuation of the shaft error is reduced by filtering the fluctuation of the shaft error at the front end, the rotation speed fluctuation can be more directly and quickly suppressed, and the effectiveness of the rotation speed fluctuation suppression is improved. On the other hand, when the axis error delta theta is filtered, the phase compensation angle is adopted to adjust the phase, the phase characteristic of the phase-locked loop is changed, the fluctuation suppression effect in the full-frequency-domain operation process of the compressor can be improved, and the stability of the full-frequency-domain operation can be improved.
Other features and advantages of the present invention will become more apparent from the following detailed description of the invention when taken in conjunction with the accompanying drawings.
Drawings
FIG. 1 is a flow chart of one embodiment of a method of suppressing rotational speed fluctuations of a single rotor compressor in accordance with the present invention;
FIG. 2 is a control block diagram based on the embodiment of the method of FIG. 1;
FIG. 3 is a logic block diagram of a specific example of the axis error fluctuation filtering algorithm of FIG. 2;
fig. 4 is a block diagram showing the structure of an embodiment of the apparatus for suppressing the rotation speed fluctuation of the single rotor compressor according to the present invention.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in further detail with reference to the accompanying drawings and examples.
Referring to fig. 1, a flow chart of an embodiment of a method for suppressing rotational speed ripple of a single rotor compressor according to the present invention is shown.
As shown in fig. 1, in conjunction with a control block diagram shown in fig. 2, this embodiment achieves compressor speed ripple suppression using a process including the steps of:
step 11: a shaft error Delta theta reflecting a deviation between an actual position and an estimated position of a compressor rotor is acquired.
In the control of the compressor, the phase of the compressor rotor can be locked to a target phase by a phase-locked loop (PLL) control technique, the control block of which is shown in fig. 2. In the prior art, a phase-locked loop regulator, typically a proportional-integral regulator, is included in the phase-locked loop of the compressor, see K of fig. 2P_PLLAnd KI_PLLand/S. Wherein, KP_PLL、KI_PLLIs the closed loop gain parameter of the phase locked loop. The axis error Δ θ is used as an input of the PLL regulator, and specifically, the axis error Δ θ is subtracted from a target angular fluctuation amount (0 shown in fig. 2), and the difference is input to the PLL regulator, and the output of the PLL regulator is an output angular velocity Δ ω _ PLL. Based on the output angular velocity Δ ω _ PLL of the phase-locked loop regulator, the phase-locked loop outputs a real-time angular velocity ω 1 for compressor control, and the rotor position is controlled using the real-time angular velocity ω 1. The shaft error Δ θ, which reflects the deviation between the actual position and the estimated position of the compressor rotor, can be calculated by the following equation:
in the formula, the first step is that,
and
respectively a d-axis voltage set value and a q-axis voltage set value of the compressor, IdAnd IqReal-time d-axis current and real-time q-axis current, r, of the compressor, respectively*Is the resistance of the motor of the compressor,
is the q-axis inductance, omega, of the compressor1Is the real-time angular frequency of the compressor. Among the parameters, Id、IaAnd ω1The detection is carried out in real time by the detection means in the prior art, and other parameter values are known values.
Step 12: and filtering the axis error delta theta to obtain an axis error compensation quantity delta theta' after at least filtering part of axis error fluctuation.
Since the shaft error is used as an input to the phase locked loop, the real-time angular velocity of the compressor at the output of the phase locked loop is affected. If the shaft error fluctuation is large, the real-time angular speed output by the phase-locked loop is unstable, so that the rotor phase locking is unstable, and further, the compressor has faults of overcurrent, step loss and the like.
After the axis error Δ θ is obtained in step 11, filtering is performed on the axis error Δ θ to filter at least a part of fluctuation components, so as to obtain an axis error compensation amount Δ θ' after at least a part of axis error fluctuation is filtered. Reflected in the control block diagram of fig. 2, is to use an axis error Δ θ fluctuation filtering algorithm to obtain an axis error compensation amount Δ θ'.
Specifically, the filtering processing is performed on the axis error Δ θ to obtain an axis error compensation amount Δ θ' after at least part of axis error fluctuation is filtered, and the method specifically includes:
firstly, Fourier series expansion is carried out on the axis error delta theta to obtain the mechanical angle theta of the axis errormIs used for the functional expression of (1).
Then, the function expressions are respectively related to cos thetamnAnd-sin θmnAfter multiplication, extracting d-axis components and q-axis components of n-th harmonic waves of delta theta; thetamnIs the mechanical angle of the nth harmonic.
Then, filtering out d-axis components and q-axis components of partial harmonic waves by using an integrator to obtain a filtering result, and realizing filtering processing on the axis error delta theta;
then, the result of filtering out the d-axis component of partial harmonic and the result of filtering out the q-axis component of partial harmonic in the filtering result are respectively compared with cos (theta)mn+θshift-Pn) And-sin (theta)mn+θshift-Pn) Multiplying and performing inverse Fourier transform to obtain an angular velocity compensation quantity P _ out corresponding to the correction axis error delta theta' of the filtered partial harmonic component; thetashift-PnThe phase compensation angle for the nth harmonic.
Finally, the angular velocity compensation amount P _ out is converted into an angle, and a shaft error compensation amount Δ θ' is obtained.
The more detailed filtering process is described in detail later with reference to fig. 3.
Step 13: the shaft error compensation amount Δ d' is input as an input amount to a phase-locked loop regulator in a phase-locked loop for compressor control.
That is, in this embodiment, the input amount of the phase-locked loop regulator includes not only the axis error Δ θ and the target angle fluctuation amount (0 shown in fig. 2), but also the axis error compensation amount Δ θ'.
Step 14: and correcting the real-time angular speed omega 1 for controlling the compressor by using the output angular speed delta omega _ PLL of the phase-locked loop regulator, and controlling the compressor according to the corrected real-time angular speed omega 1.
Specifically, referring to fig. 2, the phase-locked loop regulator performs proportional-integral adjustment based on the input shaft error Δ θ, the target angle fluctuation amount, and the shaft error compensation amount Δ θ', and outputs an angular velocity Δ ω _ PLL. The angular velocity Δ ω -PLL is added to the angular velocity command ω × in to output the real-time angular velocity ω 1 for compressor control, thereby correcting the real-time angular velocity ω 1 using the output angular velocity Δ ω _ PLL of the phase-locked loop. The angular velocity command ω _ in is a given angular velocity value of the compressor control system, and the determination method of the value of the given angular velocity command ω _ in is implemented by using the prior art.
By adopting the method of the embodiment, the shaft error delta theta reflecting the deviation between the actual position and the estimated position of the compressor rotor is subjected to fluctuation filtering, the shaft error compensation quantity after at least part of the shaft error fluctuation is filtered is input into the phase-locked loop regulator as an input quantity, the shaft error compensation quantity after part of the fluctuation is filtered can compensate the shaft error, the fluctuation of the shaft error is reduced, and then the shaft error is input into the phase-locked loop regulator, and further, the fluctuation of the real-time angular speed of the compressor corrected by the output angular speed of the phase-locked loop regulator can be reduced. When the compressor is controlled by the corrected real-time angular speed, the variation and the phase of the target rotating speed can be close to the variation and the phase of the actual rotating speed, so that the operation of the compressor tends to be stable. Moreover, because the fluctuation of the shaft error is a front end direct factor causing the speed fluctuation, the periodical fluctuation of the shaft error is reduced by filtering the fluctuation of the shaft error at the front end, the rotation speed fluctuation can be more directly and quickly suppressed, and the effectiveness of the rotation speed fluctuation suppression is improved. On the other hand, when the axis error delta theta is filtered, the phase compensation angle is adopted to adjust the phase, the phase characteristic of the phase-locked loop is changed, the fluctuation suppression effect in the full-frequency-domain operation process of the compressor can be improved, and the stability of the full-frequency-domain operation can be improved.
In some other embodiments, the filtering processing is performed on the axis error Δ θ to obtain an axis error compensation amount Δ θ' after at least part of the axis error fluctuation is filtered, specifically including: and performing filtering processing on the axis error delta theta, at least filtering a d-axis component and a q-axis component of a first harmonic in the delta theta, realizing filtering of a first harmonic component of the delta theta, and obtaining an axis error compensation quantity delta theta' for at least filtering the first harmonic component. As a more preferable embodiment, the method for obtaining the axis error compensation amount Δ θ' after filtering at least part of the axis error fluctuation by filtering the axis error Δ θ further includes: and filtering d-axis components and q-axis components of second harmonic in the delta theta, realizing filtering of first harmonic components and second harmonic components of the delta theta, and obtaining axial error compensation quantity delta theta' for filtering the first harmonic components and the second harmonic components. Most of fluctuation components in the delta theta can be filtered out by filtering out the first harmonic component or the first harmonic component and the second harmonic component in the delta theta, the calculated amount is moderate, and the filtering speed is high.
Fig. 3 is a logic block diagram showing a specific example of the axis error fluctuation filtering algorithm of fig. 2, specifically, a logic block diagram showing a specific example of obtaining the angular velocity compensation amount P _ out corresponding to the axis error compensation amount Δ θ' after filtering the first harmonic component and the second harmonic component in the axis error Δ θ. According to the logic block diagram shown in fig. 3, in this embodiment, the angular velocity compensation amount P _ out is obtained by the following procedure:
firstly, the axis error delta theta is subjected to Fourier series expansion to obtain the axis error delta theta relative to the mechanical angle thetamIs used for the functional expression of (1). The method comprises the following specific steps:
in the formula,. DELTA.theta.DCIs the direct component of the axis error, θd_n＝θpeak_n cosφn，θq_n＝θpeak_n sinφn，
Δθpeak_nFor the n harmonic axis error fluctuation amplitude, thetam1、θm2Is the first harmonic mechanical angle. And second harmonic mechanical angle thetam2Expressed as: thetam2＝2θm1。
And then, extracting a first harmonic component and a second harmonic component from the function expression, and filtering the first harmonic component and the second harmonic component by adopting an integrator to obtain a filtering result.
Specifically, the first harmonic component and the second harmonic component can be extracted from the functional expression by a low-pass filtering method or an integration method. With particular reference to FIG. 3, the functional expressions are each related to cos θm1And cos θm2After multiplication, a low-pass filter is used for filtering or an integrator is used for taking an integral average value in a period, and a d-axis component of a first harmonic and a d-axis component of a second harmonic of an axis error delta theta are extracted; respectively comparing the function expressions with-sin thetam1And-sin θm2After multiplication, the q-axis component and the second harmonic of the first harmonic of the axis error delta theta are extracted by filtering with a low-pass filter or taking the integral average value in the period through an integratorThe q-axis component of the wave. Then, the d-axis component and the q-axis component of the first harmonic and the d-axis component and the q-axis component of the second harmonic are respectively subtracted from 0, and the resultant is input to an integrator KI_PAnd performing integral filtering treatment in the/S, filtering d-axis components and q-axis components of the first harmonic and d-axis components and q-axis components of the second harmonic, obtaining filtering results of the first harmonic component and the second harmonic component, and realizing filtering treatment on the axis error delta theta. Also, the filtering result becomes an angular velocity.
Then, each filtering result is subjected to inverse fourier transform, and an angular velocity compensation amount P _ out corresponding to the correction axis error Δ θ' in which the first harmonic component and the second harmonic component are filtered is obtained. Specifically, the filtering result of the d-axis component and the filtering result of the q-axis component are respectively equal to cos (θ)m1+θshift-P1) And-sin (theta)m1+θshift-P1) Multiplying the sum of the results after the Fourier inverse transformation to form an angular velocity compensation quantity P _ out1 corresponding to the correction axis error with the first harmonic component filtered; the filtering result of the d-axis component and the q-axis component are respectively compared with cos (theta)m2+θshift-P2) And-sin (theta)m2+θshift-P2) Multiplying the sum of the results after the Fourier inverse transformation to form an angular velocity compensation quantity P _ out2 corresponding to the correction axis error with the second harmonic component filtered; the sum of the two angular velocity compensation amounts forms an angular velocity compensation amount P _ out of P _ out1+ P _ out2 corresponding to the correction axis error Δ θ' in which the first harmonic component and the second harmonic component are filtered out. Wherein, thetashift-P1And thetashift-P2The phase compensation angle of the first harmonic and the phase compensation angle of the second harmonic are respectively. The angle numbers of the two phase compensation angles can be equal or unequal preset fixed values, and can also be variable angle values.
As a preferred embodiment, two phase compensation angles θshift-P1And thetashift-P2Equal and according to the closed-loop gain parameter K of the phase-locked loopP_PLL、KI_PLLAnd determining the angular speed command omega _ in of the phase-locked loop. Furthermore, it is necessary to satisfy: thetashift-Pn＝(aKP_PLL+bKI-PLL+cKP_PLL/KI_PLL+ d ω in) pi. Wherein a, b, c and d are constant coefficients, and the constant coefficients are determined for a determined control system.
Finally, the angular velocity compensation amount P _ out is converted into an angle, and specifically, the angular velocity compensation amount P _ out is converted according to time, so that the shaft error compensation amount Δ θ' after the first harmonic component and the second harmonic component are filtered out can be obtained.
As a preferred embodiment, the control of harmonic filtering can also be achieved by adding an enable switch. Specifically, in the block diagram of fig. 3, Gain _1 and Gain _2 are enable switches for determining whether to turn on/off the filtering algorithm function. In the case where the enable switch states of Gain _1 and Gain _2 are the functions of filtering the first harmonic and filtering the second harmonic, the angular velocity compensation amount P _ out corresponding to the axis error compensation amount Δ θ' of filtering the first harmonic component and the second harmonic component is obtained as P _ out1+ P _ out 2. If the enable switch states of Gain _1 and Gain _2 are the functions of cutting off and filtering the first harmonic and cutting off and filtering the second harmonic, the whole axis error filtering function is cut off, the angular velocity compensation amount P _ out cannot be output, and then the axis error compensation amount Δ θ' cannot be obtained. If one of the enable switches is in a state of turning on the filtering algorithm function and the other enable switch is in a state of turning off the filtering algorithm function, the obtained angular velocity compensation quantity P _ out is only the angular velocity compensation quantity for filtering the first harmonic (the Gain _1 enable switch is in a state of turning on the filtering first harmonic function and the Gain _2 enable switch is in a state of turning off the filtering second harmonic function) or is only the angular velocity compensation quantity for filtering the second harmonic (the Gain _1 enable switch is in a state of turning off the filtering first harmonic function and the Gain _2 enable switch is in a state of turning on the filtering second harmonic function); accordingly, the axis error compensation amount Δ θ' is only the axis error compensation amount after the first harmonic is filtered out or only the axis error compensation amount after the second harmonic is filtered out.
In the embodiment of filtering only the first harmonic component, the process of extracting the first harmonic component and filtering the first harmonic component in fig. 3 may be directly adopted. Of course, in the embodiment of filtering only the first harmonic component, the control of filtering the first harmonic component may also be implemented by adding an enable switch, and the specific implementation manner is also referred to fig. 3 and will not be repeated herein.
Referring to fig. 4, there is shown a block diagram illustrating an embodiment of an apparatus for suppressing a rotation speed fluctuation of a single rotor compressor according to the present invention.
As shown in fig. 4, the apparatus of this embodiment includes the following structural units, connection relationships between the units, and functions of the units:
a shaft error acquisition unit 21 for acquiring a shaft error Δ θ reflecting a deviation of the actual position and the estimated position of the compressor rotor.
And an axis error compensation amount obtaining unit 22, configured to perform filtering processing on the axis error Δ θ to obtain an axis error compensation amount Δ θ' after at least part of axis error fluctuation is filtered.
And a control unit 23, configured to input the shaft error compensation amount Δ θ' acquired by the shaft error compensation amount acquisition unit 22 as an input amount to a phase-locked loop regulator in a phase-locked loop for compressor control, correct the real-time angular velocity ω 1 for compressor control by using an output angular velocity Δ ω _ PLL of the phase-locked loop regulator, and control the compressor according to the corrected real-time angular velocity ω 1.
The device with the structural units can be applied to compressor products such as air conditioners, corresponding software programs are operated, the device works according to the process of the method embodiment and the preferred embodiment, the rotation speed fluctuation of the compressor is restrained, and the technical effect of the method embodiment is achieved.
The above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions.
Claims (10)
1. A method of suppressing fluctuations in the rotational speed of a single-rotor compressor, the method comprising:
acquiring a shaft error delta theta reflecting a deviation between an actual position and an estimated position of a compressor rotor;
filtering the axis error delta theta to obtain an axis error compensation quantity delta theta' after at least part of axis error fluctuation is filtered;
inputting the shaft error compensation quantity delta theta' as an input quantity to a phase-locked loop regulator in a phase-locked loop for controlling the compressor;
correcting the real-time angular velocity omega 1 for controlling the compressor by using the output angular velocity delta omega _ PLL of the phase-locked loop regulator, and controlling the compressor according to the corrected real-time angular velocity omega 1;
the filtering processing is performed on the axis error delta theta to obtain an axis error compensation quantity delta theta' after at least part of axis error fluctuation is filtered, and the method specifically comprises the following steps:
performing Fourier series expansion on the axis error delta theta to obtain the mechanical angle theta of the axis errormThe functional expression of (a);
the function expressions are respectively related to cos thetamnAnd-sin θmnAfter multiplication, extracting d-axis components and q-axis components of n-th harmonic waves of delta theta; thetamnMechanical angle for nth harmonic;
filtering a d-axis component and a q-axis component of partial harmonic waves by using an integrator to obtain a filtering result, and realizing filtering processing of the axis error delta theta;
respectively comparing the result of filtering out the d-axis component of partial harmonic and the result of filtering out the q-axis component of partial harmonic with cos (theta)mn+θshift-Pn) And-sin (theta)mn+θshift-Pn) Multiplying and performing inverse Fourier transform to obtain an angular velocity compensation quantity P _ out corresponding to the correction axis error delta theta' of the filtered partial harmonic component; thetashift-PnPhase compensation angle for nth harmonic;
and converting the angular velocity compensation amount P _ out into an angle to obtain the shaft error compensation amount delta theta'.
2. The method according to claim 1, wherein the filtering the axis error Δ θ to obtain an axis error compensation amount Δ θ' after at least part of the axis error fluctuation is filtered includes:
and performing filtering processing on the axis error delta theta, at least filtering a d-axis component and a q-axis component of a first harmonic in the delta theta, realizing filtering of a first harmonic component of the delta theta, and obtaining an axis error compensation quantity delta theta' for at least filtering the first harmonic component.
3. The method according to claim 2, wherein the filtering the axis error Δ θ to obtain an axis error compensation amount Δ θ' after filtering at least part of the axis error fluctuation, further comprises: and filtering d-axis components and q-axis components of second harmonic in the delta theta, realizing filtering of first harmonic components and second harmonic components of the delta theta, and obtaining axial error compensation quantity delta theta' for filtering the first harmonic components and the second harmonic components.
4. The method of claim 1, wherein said functional expressions are each related to cos θmnAnd-sin θmnAfter multiplication, extracting d-axis components and q-axis components of n-th harmonics of delta theta, and specifically comprising the following steps: the function expressions are respectively related to cos thetamnAnd-sin θmnAfter multiplication, a d-axis component and a q-axis component of the nth harmonic of Δ θ are extracted by a low-pass filtering method or an integration method.
5. Method according to any one of claims 1 to 4, characterized in that the phase compensation angle θ of the nth harmonicshift-PnAccording to the closed loop gain parameter K of the phase-locked loopP_PLL、KI_PLLAnd the angular speed command ω _ in of the phase-locked loop is determined and satisfies:
θshift-Pn＝(aKP_PLL+bKI_PLL+cKP_PLL/KI_PLL+ d ω _ in) × pi, a, b, c, d are constant coefficients.
6. An apparatus for suppressing rotation speed fluctuation of a single-rotor compressor, comprising:
a shaft error acquisition unit for acquiring a shaft error Δ θ reflecting a deviation of an actual position and an estimated position of a compressor rotor;
the shaft error compensation quantity acquisition unit is used for filtering the shaft error delta theta to obtain a shaft error compensation quantity delta theta' after at least part of shaft error fluctuation is filtered;
the control unit is used for inputting the shaft error compensation quantity delta theta' as an input quantity to a phase-locked loop regulator in a phase-locked loop for controlling the compressor, correcting the real-time angular speed omega 1 for controlling the compressor by utilizing the output angular speed delta omega _ PLL of the phase-locked loop regulator, and controlling the compressor according to the corrected real-time angular speed omega 1;
the shaft error compensation quantity obtaining unit performs filtering processing on the shaft error Δ θ to obtain a shaft error compensation quantity Δ θ' after at least part of shaft error fluctuation is filtered, and the method specifically includes:
performing Fourier series expansion on the axis error delta theta to obtain the mechanical angle theta of the axis errormThe functional expression of (a);
the function expressions are respectively related to cos thetamnAnd-sin θmnAfter multiplication, extracting d-axis components and q-axis components of n-th harmonic waves of delta theta; thetamnMechanical angle for nth harmonic;
filtering a d-axis component and a q-axis component of partial harmonic waves by using an integrator to obtain a filtering result, and realizing filtering processing of the axis error delta theta;
respectively comparing the result of filtering out the d-axis component of partial harmonic and the result of filtering out the q-axis component of partial harmonic with cos (theta)mn+θshift-Pn) And-sin (theta)mn+θshift-Pn) Multiplying and performing inverse Fourier transform to obtain an angular velocity compensation quantity P _ out corresponding to the correction axis error delta theta' of the filtered partial harmonic component; thetashift-PnPhase compensation angle for nth harmonic;
and converting the angular velocity compensation amount P _ out into an angle to obtain the shaft error compensation amount delta theta'.
7. The apparatus according to claim 6, wherein the axis error compensation amount obtaining unit performs filtering processing on the axis error Δ θ to obtain an axis error compensation amount Δ θ' after at least part of axis error fluctuation is filtered out, specifically including:
and performing filtering processing on the axis error delta theta, at least filtering a d-axis component and a q-axis component of a first harmonic in the delta theta, realizing filtering of a first harmonic component of the delta theta, and obtaining an axis error compensation quantity delta theta' for at least filtering the first harmonic component.
8. The apparatus according to claim 7, wherein the axis error compensation amount obtaining unit performs filtering processing on the axis error Δ θ to obtain an axis error compensation amount Δ θ' after at least part of axis error fluctuation is filtered, and further comprises: and filtering d-axis components and q-axis components of second harmonic in the delta theta, realizing filtering of first harmonic components and second harmonic components of the delta theta, and obtaining axial error compensation quantity delta theta' for filtering the first harmonic components and the second harmonic components.
9. The apparatus according to claim 6, wherein the axis error compensation amount obtaining unit respectively relates the function expressions to cos θmnAnd-sin θmnAfter multiplication, extracting d-axis components and q-axis components of n-th harmonics of delta theta, and specifically comprising the following steps: the function expressions are respectively related to cos thetamnAnd-sin θmnAfter multiplication, a d-axis component and a q-axis component of the nth harmonic of Δ θ are extracted by a low-pass filtering method or an integration method.
10. The apparatus of any one of claims 6 to 9, the nth harmonic phase compensating angle θshift-PnAccording to the closed loop gain parameter K of the phase-locked loopP_PLL、KI_PLLAnd the angular speed command ω _ in of the phase-locked loop is determined and satisfies:
θshift-Pn＝(aKP_PLL+bKI_PLL+cKP_PLL/KI_PLL+ d ω _ in) × pi, a, b, c, d are constant coefficients.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811531819.5A CN109667762B (en) | 2018-12-13 | 2018-12-13 | Method and device for inhibiting rotating speed fluctuation of single-rotor compressor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811531819.5A CN109667762B (en) | 2018-12-13 | 2018-12-13 | Method and device for inhibiting rotating speed fluctuation of single-rotor compressor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109667762A CN109667762A (en) | 2019-04-23 |
| CN109667762B true CN109667762B (en) | 2021-07-23 |
Family
ID=66143924
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811531819.5A Active CN109667762B (en) | 2018-12-13 | 2018-12-13 | Method and device for inhibiting rotating speed fluctuation of single-rotor compressor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109667762B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112564571B (en) * | 2019-09-25 | 2022-09-27 | 杭州先途电子有限公司 | Control method, control device and controller |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103967794A (en) * | 2013-02-05 | 2014-08-06 | 广东美的制冷设备有限公司 | Vibration compensation method for single-rotor compressor and controller |
| CN104038127A (en) * | 2013-03-07 | 2014-09-10 | 日立空调·家用电器株式会社 | Motor control device |
| CN105529978A (en) * | 2014-10-14 | 2016-04-27 | 日立空调·家用电器株式会社 | Motor control device, compressor, air conditioner and program |
| CN106356874A (en) * | 2016-09-14 | 2017-01-25 | 国电南瑞科技股份有限公司 | Synchronous oscillation inhibiting method of wind turbine generator and inhibiting system |
| CN106788071A (en) * | 2017-01-06 | 2017-05-31 | 南京航空航天大学 | A kind of method for improving permanent-magnet synchronous motor rotor position estimated accuracy |
-
2018
- 2018-12-13 CN CN201811531819.5A patent/CN109667762B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103967794A (en) * | 2013-02-05 | 2014-08-06 | 广东美的制冷设备有限公司 | Vibration compensation method for single-rotor compressor and controller |
| CN104038127A (en) * | 2013-03-07 | 2014-09-10 | 日立空调·家用电器株式会社 | Motor control device |
| CN105529978A (en) * | 2014-10-14 | 2016-04-27 | 日立空调·家用电器株式会社 | Motor control device, compressor, air conditioner and program |
| CN106356874A (en) * | 2016-09-14 | 2017-01-25 | 国电南瑞科技股份有限公司 | Synchronous oscillation inhibiting method of wind turbine generator and inhibiting system |
| CN106788071A (en) * | 2017-01-06 | 2017-05-31 | 南京航空航天大学 | A kind of method for improving permanent-magnet synchronous motor rotor position estimated accuracy |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109667762A (en) | 2019-04-23 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN109450331B (en) | Method and device for inhibiting fluctuation of rotating speed of compressor | |
| CN109724335B (en) | Method and device for suppressing fluctuation of rotation speed of compressor | |
| CN109510555B (en) | Method and device for inhibiting fluctuation of rotating speed of compressor | |
| CN109458336B (en) | Method for controlling rotation speed of single-rotor compressor | |
| CN109586643B (en) | Method for controlling speed fluctuation of single-rotor compressor | |
| CN109510553B (en) | Method for controlling fluctuation of rotating speed of air conditioner compressor | |
| CN109667762B (en) | Method and device for inhibiting rotating speed fluctuation of single-rotor compressor | |
| CN109660172B (en) | Method and device for inhibiting fluctuation of rotating speed of compressor | |
| CN109560739B (en) | Method and device for controlling rotating speed of compressor | |
| CN109724300B (en) | Method for controlling rotational speed of compressor | |
| CN109458339B (en) | Method for controlling rotating speed of single-rotor compressor | |
| CN109713965B (en) | Method and device for inhibiting fluctuation of rotating speed of air-conditioning compressor | |
| CN109724325B (en) | Method for controlling rotation speed of air conditioner compressor | |
| CN109724308B (en) | Compressor rotating speed control method | |
| CN109660173B (en) | Method and device for suppressing rotation speed fluctuation of single-rotor compressor | |
| CN109723645B (en) | Method and device for controlling rotating speed of single-rotor compressor | |
| CN109469615B (en) | Method and device for controlling rotating speed of compressor | |
| CN109723647B (en) | Method and device for inhibiting rotating speed fluctuation of air conditioner single-rotor compressor | |
| CN109450332B (en) | Method and device for inhibiting fluctuation of rotating speed of air conditioner compressor | |
| CN109654021B (en) | Method and apparatus for controlling rotation speed of single rotor compressor | |
| CN109713966B (en) | Method and device for inhibiting fluctuation of rotating speed of air conditioner compressor | |
| CN109404284B (en) | Method and device for inhibiting rotating speed fluctuation of air conditioner single-rotor compressor | |
| CN109469616B (en) | Method and apparatus for controlling rotational speed of compressor | |
| CN109672388B (en) | Method and device for inhibiting fluctuation of rotating speed of air-conditioning compressor | |
| CN109441821B (en) | Method for controlling rotational speed of compressor |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20210705 Address after: No.1 Gangcheng South Road, Jiangbei District, Chongqing, 400026 Applicant after: CHONGQING HAIER AIR-CONDITIONER Co.,Ltd. Applicant after: QINGDAO HAIER AIR CONDITIONER GENERAL Corp.,Ltd. Applicant after: Haier Zhijia Co.,Ltd. Address before: 266101 Haier Industrial Park, 1 Haier Road, Laoshan District, Shandong, Qingdao Applicant before: QINGDAO HAIER AIR CONDITIONER GENERAL Corp.,Ltd. |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant |