CN109510552B - A method for suppressing speed fluctuation of single-rotor compressor - Google Patents

A method for suppressing speed fluctuation of single-rotor compressor Download PDF

Info

Publication number
CN109510552B
CN109510552B CN201811526531.9A CN201811526531A CN109510552B CN 109510552 B CN109510552 B CN 109510552B CN 201811526531 A CN201811526531 A CN 201811526531A CN 109510552 B CN109510552 B CN 109510552B
Authority
CN
China
Prior art keywords
angular velocity
harmonic
fluctuation
filtering
component
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
Application number
CN201811526531.9A
Other languages
Chinese (zh)
Other versions
CN109510552A (en
Inventor
史为品
刘光朋
赵晓明
苗建
徐勤耀
寇秋莉
董金盛
刘聚科
程永甫
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Qingdao Haier Air Conditioner Gen Corp Ltd
Haier Smart Home Co Ltd
Original Assignee
Qingdao Haier Air Conditioner Gen Corp Ltd
Haier Smart Home Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Qingdao Haier Air Conditioner Gen Corp Ltd, Haier Smart Home Co Ltd filed Critical Qingdao Haier Air Conditioner Gen Corp Ltd
Priority to CN201811526531.9A priority Critical patent/CN109510552B/en
Publication of CN109510552A publication Critical patent/CN109510552A/en
Application granted granted Critical
Publication of CN109510552B publication Critical patent/CN109510552B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P23/00—Arrangements or methods for the control of AC motors characterised by a control method other than vector control
    • H02P23/04—Arrangements or methods for the control of AC motors characterised by a control method other than vector control specially adapted for damping motor oscillations, e.g. for reducing hunting

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Control Of Electric Motors In General (AREA)
  • Feedback Control In General (AREA)

Abstract

本发明公开了一种单转子压缩机转速波动抑制方法，包括根据实时角速度和力矩控制压缩机的过程；根据实时角速度控制压缩机的过程包括：对轴误差作滤波处理，获得角速度补偿量；将角速度补偿量补偿到锁相环调节器的输出角速度中，获得补偿后的角速度输出量；根据所述补偿后的角速度输出量对实时角速度作修正，根据修正后的实时角速度控制压缩机；根据力矩控制压缩机的过程包括：计算目标角速度波动量与所述补偿后的角速度输出量之差，获得第一角速度差值；对所述第一角速度差值作滤波处理，获得滤波角速度；将所述滤波角速度输入至速度环调节器，获得输出力矩；根据所述输出力矩控制压缩机。应用本发明，能够提高压缩机转速波动抑制的有效性。

Figure 201811526531

The invention discloses a method for suppressing speed fluctuation of a single-rotor compressor. The angular velocity compensation is compensated into the output angular velocity of the phase-locked loop regulator, and the compensated angular velocity output is obtained; the real-time angular velocity is corrected according to the compensated angular velocity output, and the compressor is controlled according to the revised real-time angular velocity; according to the torque The process of controlling the compressor includes: calculating the difference between the target angular velocity fluctuation and the compensated angular velocity output to obtain a first angular velocity difference; filtering the first angular velocity difference to obtain a filtered angular velocity; The filtered angular velocity is input to the speed loop regulator to obtain the output torque; the compressor is controlled according to the output torque. By applying the present invention, the effectiveness of suppressing the fluctuation of the compressor rotational speed can be improved.

Figure 201811526531

Description

Method for inhibiting fluctuation of rotating speed of single-rotor compressor
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 for suppressing rotation speed fluctuation of a single-rotor compressor.
Background
When the single-rotor compressor used by the air conditioner runs, the single-rotor 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 controlling the rotating speed of the compressor, the effect of inhibiting the rotating speed fluctuation is not ideal enough, and the problem of the rotating speed fluctuation of the compressor cannot be fundamentally solved.
Disclosure of Invention
The invention aims to provide a method for suppressing the fluctuation of the rotating speed of a single-rotor compressor, which improves the effectiveness of suppressing the fluctuation of the rotating speed of the compressor.
In order to realize the purpose of the invention, the invention is realized by adopting the following technical scheme:
a method for suppressing fluctuation of a rotational speed of a single-rotor compressor includes a process of controlling the compressor according to a real-time angular speed and a process of controlling the compressor according to a torque;
the process of controlling the compressor according to the real-time angular velocity includes:
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 a corrected axis error delta theta 'and an angular speed compensation quantity P _ out corresponding to the corrected axis error delta theta' after at least part of axis error fluctuation is filtered;
compensating the angular velocity compensation quantity P _ out into an output angular velocity delta omega _ PLL of a phase-locked loop regulator in the phase-locked loop for controlling the compressor to obtain compensated angular velocity output quantity delta omega ', and obtaining delta omega' ═ P _ out + delta omega _ PLL;
correcting the real-time angular speed omega 1 for controlling the compressor according to the compensated angular speed output quantity delta omega', and controlling the compressor according to the corrected real-time angular speed omega 1;
the filtering processing is performed on the axis error Δ θ to obtain a corrected axis error Δ θ 'obtained by filtering out at least part of axis error fluctuation and an angular velocity compensation amount P _ out corresponding to the corrected axis error Δ θ', and 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;
the process of controlling the compressor according to the torque includes:
calculating the difference between the target angular velocity fluctuation amount and the compensated angular velocity output amount to obtain a first angular velocity difference value;
filtering the first angular velocity difference to obtain a filtered angular velocity at least filtering part of angular velocity fluctuation;
inputting the filter angular velocity as an input quantity to a speed ring regulator in a speed ring for controlling a compressor, and obtaining an output torque of the speed ring regulator;
controlling the compressor according to the output torque;
the filtering the first angular velocity difference to obtain a filtered angular velocity at least after filtering part of angular velocity fluctuation, specifically comprising:
and extracting partial angular velocity fluctuation in the first angular velocity difference by adopting a velocity fluctuation extraction algorithm, extracting a direct current component of the partial angular velocity fluctuation, calculating a difference between the first angular velocity difference and the direct current component of the partial angular velocity fluctuation, and determining the difference as the filtering angular velocity.
Compared with the prior art, the invention has the advantages and positive effects that: the invention provides a method for suppressing the fluctuation of the rotating speed of a single-rotor compressor, which comprises the steps of performing fluctuation filtering on a shaft error delta theta reflecting the deviation of the actual position and the estimated position of a compressor rotor, compensating an angular speed compensation quantity corresponding to a corrected shaft error after at least part of shaft error fluctuation is filtered into the output angular speed of a phase-locked loop regulator to obtain a compensated angular speed output quantity, correcting the real-time angular speed of the compressor according to the compensated angular speed output quantity, and enabling the fluctuation quantity and the phase position of a target rotating speed to be close to the fluctuation quantity and the phase position of the actual rotating speed when the compressor is controlled by the corrected real-time angular speed so as to enable 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 speed fluctuation, the periodical fluctuation of the shaft error is reduced by filtering the fluctuation of the shaft error at the front end, the speed fluctuation can be directly and quickly inhibited, and the effectiveness of speed control is improved. On the other hand, when extracting the harmonic component in the axis error Δ θ, the phase compensation angle is used to adjust the phase of the harmonic component, and the phase characteristics of the phase-locked loop are changed, so that the ripple suppression effect during the full-frequency-domain operation of the compressor can be improved, and the stability of the full-frequency-domain operation can be improved. In addition, the difference value between the compensated angular speed output quantity and the target angular speed fluctuation quantity is subjected to filtering processing, and the filtered angular speed at least part of which is filtered out of the angular speed fluctuation is input into the speed loop regulator as an input quantity, so that the fluctuation of the output torque of the speed loop regulator can be reduced, and when the compressor is controlled according to the output torque, the fluctuation of the rotating speed of the compressor can be reduced, and the running of the compressor is more stable; the compressor operates stably, and the effects of energy conservation and vibration reduction can be achieved.
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 partial flow chart of an embodiment of a method for suppressing a fluctuation in a rotational speed of a single-rotor compressor according to the present invention;
FIG. 2 is another partial flowchart of an embodiment of a method for suppressing rotational speed fluctuation of a single-rotor compressor according to the present invention;
FIG. 3 is a control block diagram based on the method embodiment of FIGS. 1 and 2;
FIG. 4 is a logic block diagram of a specific example of the axis error fluctuation filtering algorithm of FIG. 3;
FIG. 5 is a logic block diagram of a specific example of the speed fluctuation extraction algorithm of FIG. 3.
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.
Fig. 1 and 2 are partial flow charts showing an embodiment of a method for suppressing a fluctuation in the rotational speed of a single-rotor compressor according to the present invention. Specifically, the rotational speed fluctuation suppression method of the embodiment includes two processes: one is a process for controlling the compressor according to the real-time angular velocity, and the flow chart is shown in fig. 1; one is a process of controlling the compressor according to the torque, and the flowchart is shown in fig. 2. Specific implementations of these two processes are described below based on a control block diagram shown in fig. 1 and 2 in conjunction with fig. 3.
Referring to fig. 1, a partial flowchart of an embodiment of a method for suppressing rotation speed fluctuation of a single-rotor compressor according to the present invention, specifically a flowchart for controlling a compressor according to a real-time angular velocity, is shown, and the embodiment employs a process including the following steps to control the compressor according to the real-time angular velocity:
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 the target phase by a phase-locked loop (PLL) control technique, the control block of which is shown in fig. 3. 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. 3P_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. 3), 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:
Figure BDA0001904594370000051
in the formula, the first step is that,
Figure BDA0001904594370000052
and
Figure BDA0001904594370000053
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,
Figure BDA0001904594370000054
is the q-axis inductance, omega, of the compressor1Is the real-time angular frequency of the compressor. Among the parameters, Id、IqAnd 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 a corrected axis error delta theta' after at least part of axis error fluctuation is filtered.
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 a corrected axis error Δ θ' after filtering at least a part of axis error fluctuation.
Step 13: the angular velocity compensation amount P _ out is obtained from the corrected shaft error Δ θ'.
The implementation of the above step 12 and step 13 is reflected in the control block diagram of fig. 3, and an axis error Δ θ fluctuation filtering algorithm is adopted to obtain the angular velocity compensation amount P _ out.
Specifically, the filtering processing is performed on the axis error Δ θ to obtain a corrected axis error Δ θ 'obtained by filtering out at least part of axis error fluctuation and an angular velocity compensation amount P _ out corresponding to the corrected axis error Δ θ', and 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);
respectively connecting the function expressions with 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 by using an integrator to obtain a filtering result, and realizing filtering processing on an axis error delta theta;
respectively comparing the result of filtering out d-axis component of partial harmonic and the result of filtering out 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-PnThe phase compensation angle for the nth harmonic.
The more specific filtering process is described in detail later with reference to fig. 4.
Step 14: the angular velocity compensation amount P _ out is compensated to the output angular velocity delta omega _ PLL of the phase-locked loop regulator in the phase-locked loop for controlling the compressor, and the compensated angular velocity output amount delta omega' is obtained. Specifically, the compensated angular velocity output amount Δ ω' ═ P _ out + Δ ω _ PLL.
Step 15: and correcting the real-time angular speed omega 1 for controlling the compressor according to the compensated angular speed output quantity, and controlling the compressor according to the corrected real-time angular speed omega 1.
Specifically, the method of determining the real-time angular velocity corresponding to the target angular velocity fluctuation amount of 0 in the following velocity loop control is: referring to fig. 3, the compensated angular velocity output amount Δ ω' is added to the angular velocity command ω × in, and the real-time angular velocity ω 1 for controlling the compressor is output. 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. The target angular velocity fluctuation quantity of the speed loop is 0, and the real-time angular velocity is determined based on the output angular velocity delta omega _ PLL of the phase-locked loop regulator and the given angular velocity command omega _ in, so that the compressor is controlled more accurately and stably.
Referring to a partial flow chart of an embodiment of a method for suppressing rotation speed fluctuation of a single-rotor compressor based on the present invention shown in fig. 2, specifically, a flow chart for controlling a compressor according to a torque, the embodiment employs a process including the following steps to control the compressor according to the torque:
step 21: and calculating the difference between the target angular velocity fluctuation amount and the compensated angular velocity output amount to obtain a first angular velocity difference value.
In compressor control, the rotational speed of the compressor rotor can be controlled to approach a set rotational speed by a speed loop (ASR) control technique. Referring to the block diagram of FIG. 3, the speed loop includes a speed loop regulator, typically a proportional integral regulator, see K of FIG. 3P_ASRAnd KI_ASR/S。
In this step, a compensated output amount of angular velocity Δ ω'; then, a difference between the target angular velocity fluctuation amount and the compensated angular velocity output amount Δ ω' is calculated, and the difference therebetween is determined as a first angular velocity difference Δ ω 2. Here, the target angular velocity fluctuation amount is a desired angular velocity fluctuation amount and is a known input amount. As a preferred embodiment, in this example, the target angular velocity fluctuation amount is 0.
Step 22: and performing filtering processing on the first angular velocity difference to obtain a filtered angular velocity after at least part of angular velocity fluctuation is filtered.
The first angular velocity difference is used as an input to the velocity loop regulator to affect the output torque at the velocity loop output. If the first angular speed difference value fluctuates greatly, the fluctuation of the output torque is large, and further the fluctuation of the rotating speed of the compressor is large. After the first angular velocity difference is obtained in step 21, a filtering process is performed on the first angular velocity difference to filter out at least part of the angular velocity fluctuation component, so as to obtain a filtered angular velocity Δ ω _ K.
Specifically, as shown in the block diagram of fig. 3, the filtering processing is performed on the first angular velocity difference Δ ω 2 to obtain a filtered angular velocity Δ ω _ K at least after part of the angular velocity fluctuation is filtered, which specifically includes: extracting partial angular velocity fluctuation K _ out in the first angular velocity difference delta omega 2 by adopting a velocity fluctuation extraction algorithm, and extracting a direct current component K _ DC of the partial angular velocity fluctuation K _ out; then, a difference between the first angular velocity difference Δ ω 2 and the direct current component K _ DC of the partial angular velocity fluctuation is calculated, and the difference is determined as a filtered angular velocity Δ ω _ K. The extraction of the DC component K _ DC of the partial angular velocity fluctuation K _ out can be realized by using the existing technology of extracting the DC component, for example, by using a low-pass filter to extract the DC component K _ DC of the partial angular velocity fluctuation K _ out. For a more preferable filtering processing manner, refer to the description of the following preferred embodiments.
Step 23: inputting the angular speed of the filter as input quantity to a speed loop regulator in a speed loop for controlling the compressor to obtain the output torque tau of the speed loop regulatorM。
Step 24: and controlling the air conditioner compressor according to the output torque. The specific control process refers to the prior art.
By adopting the method of the embodiment formed by the above-mentioned fig. 1 and fig. 2, the double loop control of the speed loop and the phase-locked loop of the compressor is realized. In addition, in the phase-locked loop control, the fluctuation filtering is carried out on the shaft error delta theta reflecting the deviation between the actual position and the estimated position of the compressor rotor, the angular speed compensation quantity corresponding to the corrected shaft error after at least part of the shaft error fluctuation is filtered is compensated to the output angular speed of the phase-locked loop regulator, the compensated angular speed output quantity is obtained, the real-time angular speed of the compressor is corrected according to the compensated angular speed output quantity, and when the compressor is controlled by the corrected real-time angular speed, the variation quantity and the phase of the target rotating speed can be close to the variation quantity 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 speed fluctuation, the periodical fluctuation of the shaft error is reduced by filtering the fluctuation of the shaft error at the front end, the speed fluctuation can be directly and quickly inhibited, and the effectiveness of speed control is improved. In the control of the speed ring, the difference value between the compensated angular speed output quantity and the target angular speed fluctuation quantity is subjected to filtering treatment, and the filtered angular speed with at least part of angular speed fluctuation filtered out is input into the speed ring regulator as an input quantity, so that the fluctuation of the output torque of the speed ring regulator can be reduced, and when the compressor is controlled according to the output torque, the fluctuation of the rotating speed of the compressor can be reduced, and the running of the compressor is more stable; the compressor operates stably, and the effects of energy conservation and vibration reduction can be achieved.
In some other embodiments, the filtering the axis error Δ θ to obtain a corrected axis error Δ θ' after at least part of the axis error fluctuation is filtered, specifically 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 a corrected axis error delta theta' of which at least the first harmonic component is filtered. As a more preferable embodiment, the method for obtaining the corrected axis error 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 a corrected axis error delta theta' of 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. 4 is a logic block diagram showing a specific example of the axis error fluctuation filtering algorithm in fig. 3, specifically, a logic block diagram showing a specific example of obtaining the angular velocity compensation amount P _ out corresponding to the corrected axis error 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. 4, the specific process of the angular velocity compensation amount P _ out corresponding to the corrected axis error Δ θ' after filtering the first harmonic component and the second harmonic component in the axis error Δ θ is as follows:
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:
Figure BDA0001904594370000081
in the formula,. DELTA.theta.DCIs the direct component of the axis error, θd_n＝θpeak_ncosφn，θq_n＝θpeak_nsinφn，
Figure BDA0001904594370000082
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, a low-pass filtering method or an integration method may be used to express from a functionThe first harmonic component and the second harmonic component are extracted from the formula. With particular reference to FIG. 4, 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 of the first harmonic and the q-axis component of the second harmonic of the axis error delta theta are extracted by filtering through a low-pass filter or taking an integral average value in a period through an integrator. 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-P2Are respectively oneThe phase compensation angle of the subharmonic and the phase compensation angle of the second harmonic. 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.
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. 4, 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 correction axis error 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 filtering the first harmonic and the second harmonic, the whole axis error filtering function is turned off, and the angular velocity compensation amount P _ out cannot be output. If one of the enable switches is in the state of turning on the filtering algorithm function, and the other enable switch is in the 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 the state of turning on the filtering first harmonic function, and the Gain _2 enable switch is in the 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 the state of turning off the filtering first harmonic function, and the Gain _2 enable switch is in the state of turning on the filtering second harmonic function).
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. 4 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. 4 and will not be repeated herein.
In some other preferred embodiments, the extracting, by using a speed fluctuation extraction algorithm, a part of the angular velocity fluctuation in the first angular velocity difference specifically includes: and extracting at least a first harmonic component in the first angular velocity difference value by adopting a velocity fluctuation extraction algorithm to serve as a part of angular velocity fluctuation. As a more preferable embodiment, the extracting, by using a speed fluctuation extraction algorithm, part of the angular speed fluctuation in the first angular speed difference includes: and extracting a first harmonic component and a second harmonic component in the first angular velocity difference value by adopting a velocity fluctuation extraction algorithm, and taking the sum of the first harmonic component and the second harmonic component as part of angular velocity fluctuation. After the difference value is obtained between the first angular velocity difference value and the first harmonic component, most of fluctuation components in the first angular velocity difference value can be filtered, the calculated amount is moderate, and the filtering speed is high.
Fig. 5 is a logic block diagram showing a specific example of the speed fluctuation extraction algorithm in fig. 3, specifically, a logic block diagram showing a specific example of extracting the first harmonic component and the second harmonic component from the first angular velocity difference value to form a partial angular velocity fluctuation. Referring to fig. 5, this specific example obtains a partial angular velocity fluctuation containing a first harmonic component and a second harmonic component by the following method:
firstly, a Fourier series expansion is carried out on the first angular velocity difference delta omega 2 to obtain the first angular velocity difference delta omega 2 relative to the mechanical angle thetamIs used for the functional expression of (1). This process can be implemented using existing technology and is not described in detail here.
Then, the first harmonic component and the second harmonic component are extracted from the functional expression, respectively.
Specifically, as shown in FIG. 5, the functional expression is related to cos θm1After the multiplication is carried out, the obtained product is subjected to the reaction,passing through a low pass filter
Figure BDA0001904594370000111
Filtering, and performing inverse Fourier transform on a filtering result to obtain a d-axis component of the first harmonic; multiplying the functional expression by-sin θm1After multiplication, pass through a low-pass filter
Figure BDA0001904594370000112
Filtering, and performing inverse Fourier transform on a filtering result to obtain a q-axis component of a first harmonic; then, the d-axis component and the q-axis component of the first harmonic are added to obtain a first harmonic component K _ out1 in the first angular velocity difference. Similarly, the functional expression is related to cos θm2After multiplication, pass through a low-pass filter
Figure BDA0001904594370000113
Filtering, and performing inverse Fourier transform on a filtering result to obtain a d-axis component of a second harmonic; multiplying the functional expression by-sin θm2After multiplication, pass through a low-pass filter
Figure BDA0001904594370000114
Filtering, and performing inverse Fourier transform on a filtering result to obtain a q-axis component of a second harmonic; then, the d-axis component and the q-axis component of the second harmonic are added to obtain a second harmonic component K _ out2 in the first angular velocity difference. Finally, the first harmonic component K _ out1 is added to the second harmonic component K _ out2, and the resulting sum forms part of the angular velocity fluctuation K _ out. Wherein, thetam1Mechanical angle of first harmonic, theta, in a functional expression developed as a Fourier seriesm2Mechanical angle of the second harmonic in a functional expression developed as a Fourier series, and θm2＝2θm1，T_PD_filterIs the time constant of the low pass filter.
After obtaining the partial angular velocity fluctuation K _ out containing the first harmonic component and the second harmonic component, calculating a difference between the first angular velocity difference Δ ω 2 and the partial angular velocity fluctuation K _ out as a filtered angular velocity Δ ω _ K, where the filtered angular velocity Δ ω _ K is the filtered angular velocity after the first harmonic component and the second harmonic component are filtered out.
As a preferred embodiment, the control of the harmonic extraction can also be achieved by adding an enable switch. Specifically, in the block diagram of fig. 5, Gain _1 and Gain _2 are enable switches for determining whether to turn on/off the extraction algorithm function. Under the condition that the enabling switch states of the Gain _1 and the Gain _2 are on, the functions of extracting the first harmonic and extracting the second harmonic are obtained, and partial angular velocity fluctuation formed by the first harmonic component and the second harmonic component is obtained: k _ out is K _ out1+ K _ out 2. If the enable switch states of Gain _1 and Gain _2 are the functions of extracting the first harmonic and extracting the second harmonic, the whole speed fluctuation extraction algorithm function is turned off, and part of the angular speed fluctuation is 0. If one of the enable switches is in the state of opening the extraction algorithm function, and the other enable switch is in the state of closing the extraction algorithm function, the obtained part of the angular speed fluctuation is only a first harmonic component in the first angular speed difference (the state of the Gain _1 enable switch is in the state of opening the extraction first harmonic function, and the state of the Gain _2 enable switch is in the state of closing the extraction second harmonic function) or only a second harmonic component in the first angular speed difference (the state of the Gain _1 enable switch is in the state of closing the extraction first harmonic function, and the state of the Gain _2 enable switch is in the state of opening the extraction second harmonic function).
In the embodiment of extracting only the first harmonic component, the process of extracting the first harmonic component in fig. 5 may be directly employed; of course, the control of the first harmonic extraction may also be implemented by adding an enable switch, and the specific implementation manner is also shown in fig. 5, which is not repeated herein.
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)

1.一种单转子压缩机转速波动抑制方法，其特征在于，所述方法包括根据实时角速度控制压缩机的过程和根据力矩控制压缩机的过程；1. a single-rotor compressor rotational speed fluctuation suppression method, is characterized in that, described method comprises the process of controlling compressor according to real-time angular velocity and the process of controlling compressor according to torque; 所述根据实时角速度控制压缩机的过程包括：The process of controlling the compressor according to the real-time angular velocity includes: 获取反映压缩机转子的实际位置和推定位置的偏差的轴误差△θ；Obtain the shaft error Δθ reflecting the deviation between the actual position and the estimated position of the compressor rotor; 对所述轴误差△θ作滤波处理，获得至少滤除部分轴误差波动后的修正轴误差△θ'以及与所述修正轴误差△θ'相对应的角速度补偿量P_out；Perform filtering processing on the shaft error Δθ to obtain a corrected shaft error Δθ' after filtering out at least part of the shaft error fluctuation and an angular velocity compensation amount P_out corresponding to the corrected shaft error Δθ'; 将所述角速度补偿量P_out补偿到压缩机控制用锁相环内锁相环调节器的输出角速度Δω_PLL中，获得补偿后的角速度输出量Δω’，Δω’＝P_out+Δω_PLL；Compensating the angular velocity compensation amount P_out into the output angular velocity Δω_PLL of the phase-locked loop regulator in the phase-locked loop for compressor control to obtain the compensated angular velocity output amount Δω', Δω'=P_out+Δω_PLL; 根据所述补偿后的角速度输出量Δω’对压缩机控制用的实时角速度ω1作修正，根据修正后的实时角速度ω1控制压缩机；The real-time angular velocity ω1 used for compressor control is corrected according to the compensated angular velocity output Δω', and the compressor is controlled according to the corrected real-time angular velocity ω1; 所述对所述轴误差△θ作滤波处理，获得至少滤除部分轴误差波动后的修正轴误差△θ'以及与所述修正轴误差△θ'相对应的角速度补偿量P_out，具体包括：The filtering process on the shaft error Δθ to obtain the corrected shaft error Δθ' after filtering out at least part of the shaft error fluctuation and the angular velocity compensation amount P_out corresponding to the corrected shaft error Δθ', specifically includes: 将所述轴误差△θ作傅里叶级数展开，得到轴误差关于机械角θm的函数表达式；Expand the axis error Δθ as a Fourier series to obtain the function expression of the axis error with respect to the mechanical angle θ m ; 将所述函数表达式分别与cosθmn和-sinθmn相乘后，提取出△θ的n次谐波的d轴分量和q轴分量；θmn为n次谐波的机械角；After multiplying the function expression with cosθmn and -sinθmn respectively, extract the d-axis component and the q-axis component of the nth harmonic of Δθ; θmn is the mechanical angle of the nth harmonic; 采用积分器滤除部分谐波的d轴分量和q轴分量，获得滤除结果，实现对所述轴误差△θ的滤波处理；Adopt the integrator to filter out the d-axis component and the q-axis component of some harmonics, obtain the filtering result, and realize the filtering processing of the axis error Δθ; 将所述滤除结果中滤除部分谐波的d轴分量后的结果和滤除部分谐波的q轴分量后的结果分别与cos(θmn+θshift-Pn)和-sin(θmn+θshift-Pn)相乘作傅里叶逆变换，获得与滤除部分谐波成分的修正轴误差△θ'相对应的角速度补偿量P_out；θshift-Pn为n次谐波的相位补偿角；The result of filtering out the d-axis component of some harmonics and the result of filtering out the q-axis component of some harmonics are compared with cos(θ mn +θ shift-Pn ) and -sin (θ mn ) respectively. +θ shift-Pn ) is multiplied for inverse Fourier transform to obtain the angular velocity compensation amount P_out corresponding to the corrected axis error Δθ' that filters out some harmonic components; θ shift-Pn is the phase compensation of the nth harmonic horn; 所述根据力矩控制压缩机的过程包括：The process of controlling the compressor according to the torque includes: 计算目标角速度波动量与所述补偿后的角速度输出量之差，获得第一角速度差值；Calculate the difference between the target angular velocity fluctuation and the compensated angular velocity output to obtain the first angular velocity difference; 对所述第一角速度差值作滤波处理，获得至少滤除部分角速度波动后的滤波角速度；Perform filtering processing on the first angular velocity difference to obtain a filtered angular velocity after filtering out at least part of the angular velocity fluctuation; 将所述滤波角速度作为输入量输入至压缩机控制用速度环中的速度环调节器，获得所述速度环调节器的输出力矩；Inputting the filtered angular velocity as an input to a speed loop regulator in the compressor control speed loop to obtain the output torque of the speed loop regulator; 根据所述输出力矩控制压缩机；controlling the compressor according to the output torque; 所述对所述第一角速度差值作滤波处理，获得至少滤除部分角速度波动后的滤波角速度，具体包括：The filtering process on the first angular velocity difference to obtain a filtered angular velocity after filtering out at least part of the angular velocity fluctuation specifically includes: 采用速度波动提取算法提取出所述第一角速度差值中的部分角速度波动，提取所述部分角速度波动的直流成分，计算所述第一角速度差值与所述部分角速度波动的直流成分的差值，该差值确定为所述滤波角速度。A velocity fluctuation extraction algorithm is used to extract part of the angular velocity fluctuation in the first angular velocity difference, extract the DC component of the partial angular velocity fluctuation, and calculate the difference between the first angular velocity difference and the DC component of the partial angular velocity fluctuation , the difference is determined as the filtered angular velocity. 2.根据权利要求1所述的方法，其特征在于，所述对所述轴误差△θ作滤波处理，获得至少滤除部分轴误差波动后的修正轴误差△θ'，具体包括：2. The method according to claim 1, characterized in that, performing filtering processing on the shaft error Δθ to obtain a corrected shaft error Δθ' after filtering out at least part of the shaft error fluctuation, specifically comprising: 对所述轴误差△θ作滤波处理，至少滤除△θ中的一次谐波的d轴分量和q轴分量，实现对△θ的一次谐波成分的滤波，获得至少滤除一次谐波成分的修正轴误差△θ'。Perform filtering processing on the axis error Δθ, at least filter out the d-axis component and the q-axis component of the first harmonic in Δθ, realize the filtering of the first harmonic component of Δθ, and obtain at least filter out the first harmonic component. The corrected axis error Δθ'. 3.根据权利要求2所述的方法，其特征在于，所述对所述轴误差△θ作滤波处理，获得至少滤除部分轴误差波动后的修正轴误差△θ'，还包括：滤除△θ中的二次谐波的d轴分量和q轴分量，实现对△θ的一次谐波成分和二次谐波成分的滤波，获得滤除一次谐波成分和二次谐波成分的修正轴误差△θ'。3 . The method according to claim 2 , wherein filtering the shaft error Δθ to obtain a corrected shaft error Δθ' after filtering out at least part of the shaft error fluctuation, further comprising: filtering out The d-axis component and the q-axis component of the second harmonic in △θ, realize the filtering of the first harmonic component and the second harmonic component of △θ, and obtain the correction to filter out the first harmonic component and the second harmonic component Axial error Δθ'. 4.根据权利要求1所述的方法，其特征在于，所述将所述函数表达式分别与cosθmn和-sinθmn相乘后，提取出△θ的n次谐波的d轴分量和q轴分量，具体包括：将所述函数表达式分别与cosθmn和-sinθmn相乘后，采用低通滤波法或者积分法，提取出△θ的n次谐波的d轴分量和q轴分量。4. The method according to claim 1, characterized in that, after the functional expression is multiplied by cosθmn and -sinθmn respectively, the d-axis component and q of the n-th harmonic of Δθ are extracted. axis component, specifically including: after multiplying the function expression by cosθmn and -sinθmn respectively, using low-pass filtering method or integration method to extract the d-axis component and q-axis component of the n-th harmonic of Δθ . 5.根据权利要求1所述的方法，其特征在于，所述n次谐波的相位补偿角θshift-Pn根据所述锁相环的闭环增益参数KP_PLL、KI_PLL和所述锁相环的角速度指令ω*_in确定，且满足：5 . The method according to claim 1 , wherein the phase compensation angle θ shift-Pn of the n-th harmonic is based on closed-loop gain parameters K P_PLL , K I_PLL of the phase-locked loop and the phase-locked loop. 6 . The angular velocity command ω*_in is determined and satisfies: θshift-Pn＝(aKP_PLL+bKI_PLL+cKP_PLL/KI_PLL+dω*_in)*π，a、b、c、d为常数系数。θ shift-Pn =(aK P_PLL +bK I_PLL +cK P_PLL /K I_PLL +dω*_in)*π, a, b, c, and d are constant coefficients. 6.根据权利要求1至5中任一项所述的方法，其特征在于，所述采用速度波动提取算法提取出所述第一角速度差值中的部分角速度波动，具体包括：6. The method according to any one of claims 1 to 5, wherein the extracting part of the angular velocity fluctuations in the first angular velocity difference using a velocity fluctuation extraction algorithm specifically includes: 采用速度波动提取算法，至少提取出所述第一角速度差值中的一次谐波成分，作为所述部分角速度波动。Using a velocity fluctuation extraction algorithm, at least the first harmonic component in the first angular velocity difference is extracted as the partial angular velocity fluctuation. 7.根据权利要求6所述的方法，其特征在于，所述采用速度波动提取算法，提取出所述第一角速度差值中的一次谐波成分，具体包括：7 . The method according to claim 6 , wherein the extraction of the first harmonic component in the first angular velocity difference by using a velocity fluctuation extraction algorithm specifically includes: 8 . 将所述第一角速度差值作傅里叶级数展开，得到关于机械角θm的函数表达式；Expand the first angular velocity difference as a Fourier series to obtain a functional expression about the mechanical angle θ m ; 从所述函数表达式中分别提取出一次谐波的d轴分量和q轴分量；Extract the d-axis component and the q-axis component of the first harmonic respectively from the functional expression; 将所述一次谐波的d轴分量和q轴分量相加，获得所述第一角速度差值中的一次谐波成分。The d-axis component and the q-axis component of the first harmonic are added to obtain the first harmonic component in the first angular velocity difference. 8.根据权利要求6所述的方法，其特征在于，所述采用速度波动提取算法提取出所述第一角速度差值中的部分角速度波动，还包括：采用速度波动提取算法，提取出所述第一角速度差值中的二次谐波成分，将所述一次谐波成分和所述二次谐波成分之和作为所述部分角速度波动。8 . The method according to claim 6 , wherein the extracting part of the angular velocity fluctuation in the first angular velocity difference by using a velocity fluctuation extraction algorithm further comprises: using a velocity fluctuation extraction algorithm to extract the For the second harmonic component in the first angular velocity difference, the sum of the first harmonic component and the second harmonic component is used as the partial angular velocity fluctuation. 9.根据权利要求8所述的方法，其特征在于，所述采用速度波动提取算法，提取出所述第一角速度差值中的二次谐波成分，具体包括：9 . The method according to claim 8 , wherein the extraction of the second harmonic component in the first angular velocity difference by using a velocity fluctuation extraction algorithm specifically includes: 10 . 将所述第一角速度差值作傅里叶级数展开，得到关于机械角θm的函数表达式；Expand the first angular velocity difference as a Fourier series to obtain a functional expression about the mechanical angle θ m ; 从所述函数表达式中分别提取出二次谐波的d轴分量和q轴分量；Extract the d-axis component and the q-axis component of the second harmonic respectively from the functional expression; 将所述二次谐波的d轴分量和q轴分量相加，获得所述第一角速度差值中的二次谐波成分。The d-axis component and the q-axis component of the second harmonic are added to obtain the second harmonic component in the first angular velocity difference. 10.根据权利要求1所述的方法，其特征在于，所述目标角速度波动量为0；所述根据所述补偿后的角速度输出量Δω’对压缩机控制用的实时角速度ω1作修正，根据修正后的实时角速度ω1控制压缩机，具体包括：将所述补偿后的角速度输出量Δω’与给定的角速度指令相加，相加的结果确定为所述修正后的实时角速度ω1，根据所述修正后的实时角速度ω1控制压缩机。10. The method according to claim 1, wherein the target angular velocity fluctuation is 0; the real-time angular velocity ω1 used for compressor control is corrected according to the compensated angular velocity output Δω', according to The modified real-time angular velocity ω1 controls the compressor, which specifically includes: adding the compensated angular velocity output Δω' to a given angular velocity command, and the addition result is determined as the corrected real-time angular velocity ω1, according to the The modified real-time angular velocity ω1 controls the compressor.
CN201811526531.9A 2018-12-13 2018-12-13 A method for suppressing speed fluctuation of single-rotor compressor Active CN109510552B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811526531.9A CN109510552B (en) 2018-12-13 2018-12-13 A method for suppressing speed fluctuation of single-rotor compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811526531.9A CN109510552B (en) 2018-12-13 2018-12-13 A method for suppressing speed fluctuation of single-rotor compressor

Publications (2)

Publication Number Publication Date
CN109510552A CN109510552A (en) 2019-03-22
CN109510552B true CN109510552B (en) 2021-10-29

Family

ID=65752424

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811526531.9A Active CN109510552B (en) 2018-12-13 2018-12-13 A method for suppressing speed fluctuation of single-rotor compressor

Country Status (1)

Country Link
CN (1) CN109510552B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7843154B2 (en) * 2007-02-26 2010-11-30 Jtekt Corporation Motor controller and electric power steering apparatus
CN102522941A (en) * 2011-12-21 2012-06-27 海尔集团公司 Method for suppressing low-frequency vibration of compressor and system for suppressing low-frequency vibration of compressor
CN104038127A (en) * 2013-03-07 2014-09-10 日立空调·家用电器株式会社 Motor control device
EP2387145A3 (en) * 2010-05-03 2015-05-27 Hamilton Sundstrand Corporation Synchronous disturbance suppression in a variable speed motor drive
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
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

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7843154B2 (en) * 2007-02-26 2010-11-30 Jtekt Corporation Motor controller and electric power steering apparatus
EP2387145A3 (en) * 2010-05-03 2015-05-27 Hamilton Sundstrand Corporation Synchronous disturbance suppression in a variable speed motor drive
CN102522941A (en) * 2011-12-21 2012-06-27 海尔集团公司 Method for suppressing low-frequency vibration of compressor and system for suppressing low-frequency vibration of compressor
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
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
CN109510552A (en) 2019-03-22

Similar Documents

Publication Publication Date Title
CN109586643B (en) Method for speed fluctuation control of single rotor compressor
CN109724297B (en) Compressor speed fluctuation control method
CN109458336B (en) Method for controlling the speed of a single rotor compressor
CN109698647B (en) A kind of air conditioning compressor rotational speed fluctuation suppression method
CN109510553B (en) Method for controlling the speed fluctuation of air conditioner compressor
CN109660173B (en) Method and device for suppressing speed fluctuation of single-rotor compressor
CN109458339B (en) Method for speed control of single rotor compressor
CN109724300B (en) Method for compressor speed control
CN109724308B (en) A kind of compressor speed control method
CN109742994B (en) Methods of Suppressing Speed Fluctuation of Single-Rotor Compressor
CN109742996B (en) Method for controlling fluctuation of rotating speed of air conditioner compressor
CN109458338B (en) Single-rotor compressor speed control method
CN109469613B (en) Method for suppressing fluctuation of rotational speed of compressor
CN109724312B (en) Air conditioner compressor rotating speed control method
CN109724306B (en) Compressor speed control method
CN109724319B (en) A kind of air conditioner compressor speed control method
CN109713965B (en) Method and device for suppressing speed fluctuation of air conditioner compressor
CN109404284B (en) Method and device for suppressing speed fluctuation of air conditioner single-rotor compressor
CN109510552B (en) A method for suppressing speed fluctuation of single-rotor compressor
CN109742995B (en) Control Method of Rotational Speed Fluctuation of Single-Rotor Compressor
CN109724304B (en) How to control compressor speed
CN109724309B (en) A kind of compressor speed fluctuation control method
CN109698645B (en) Method for controlling speed fluctuation of single rotor compressor
CN109458337B (en) A method of controlling the speed of a single-rotor compressor
CN109724301B (en) A kind of compressor speed fluctuation suppression method

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

Effective date of registration: 20210928

Address after: 266101 Haier Industrial Park, 1 Haier Road, Laoshan District, Shandong, Qingdao

Applicant after: QINGDAO HAIER AIR CONDITIONER GENERAL Corp.,Ltd.

Applicant after: Haier Smart Home Co., Ltd.

Address before: 266101 Haier Industrial Park, 1 Haier Road, Laoshan District, Shandong, Qingdao

Applicant before: QINGDAO HAIER AIR CONDITIONER GENERAL Corp.,Ltd.

TA01 Transfer of patent application right
GR01 Patent grant
GR01 Patent grant