CN111797518B - Load solving method under low-frequency torque compensation of compressor - Google Patents

Load solving method under low-frequency torque compensation of compressor Download PDF

Info

Publication number
CN111797518B
CN111797518B CN202010578495.1A CN202010578495A CN111797518B CN 111797518 B CN111797518 B CN 111797518B CN 202010578495 A CN202010578495 A CN 202010578495A CN 111797518 B CN111797518 B CN 111797518B
Authority
CN
China
Prior art keywords
compressor
frequency
moment
load
frequency point
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
CN202010578495.1A
Other languages
Chinese (zh)
Other versions
CN111797518A (en
Inventor
王培丞
童玲
高博
宫珣
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.)
University of Electronic Science and Technology of China
Original Assignee
University of Electronic Science and Technology of China
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 University of Electronic Science and Technology of China filed Critical University of Electronic Science and Technology of China
Priority to CN202010578495.1A priority Critical patent/CN111797518B/en
Publication of CN111797518A publication Critical patent/CN111797518A/en
Application granted granted Critical
Publication of CN111797518B publication Critical patent/CN111797518B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/10Complex mathematical operations
    • G06F17/15Correlation function computation including computation of convolution operations
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02BCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
    • Y02B30/00Energy efficient heating, ventilation or air conditioning [HVAC]
    • Y02B30/70Efficient control or regulation technologies, e.g. for control of refrigerant flow, motor or heating

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Computational Mathematics (AREA)
  • Mathematical Analysis (AREA)
  • Mathematical Optimization (AREA)
  • Pure & Applied Mathematics (AREA)
  • Data Mining & Analysis (AREA)
  • Mathematical Physics (AREA)
  • Algebra (AREA)
  • Software Systems (AREA)
  • Databases & Information Systems (AREA)
  • Computing Systems (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • Geometry (AREA)
  • Control Of Positive-Displacement Pumps (AREA)

Abstract

The invention discloses a load solving method under compressor low-frequency torque compensation, which is used for calculating each operating frequency point f under a non-torque compensation state i Compressor load M of i Then at the frequency f of the loading torque compensation i Within the range of (2), each vibration maximum frequency point f is calculated j At each frequency point f of compressor operation i Moment compensation coefficient lambda of ij Fitting each frequency point f by MATLAB fitting tool i Moment compensation coefficient lambda of ij Establishing a library function of a moment compensation coefficient, and finally directly calculating the load M 'of the compressor under the low-frequency torque compensation by calling the library function of the moment compensation coefficient without repeatedly testing' i

Description

Load solving method under low-frequency torque compensation of compressor
Technical Field
The invention belongs to the technical field of compressor low-frequency torque compensation, and particularly relates to a load solving method under compressor low-frequency torque compensation.
Background
In order to reduce low-frequency vibration and noise, a low-frequency torque compensation technology is an important means in the matching process of the piping of the air-conditioning compressor. The compressor is used as an excitation source, the load characteristic of the compressor can be used as the input of pipe vibration simulation, and the quality of a design scheme is evaluated in the conceptual design stage of the pipe. The low-frequency torque compensation is generally in the range of below 40Hz of the operation of the compressor, and the essence of the low-frequency torque compensation technology is to give an optimal compensation angle, so that the resisting torque of the compressor piping system at the vibration maximum operation frequency point is compensated, and the vibration of the compressor piping system is further reduced. Correspondingly, the change of the piping structure may cause the change of the maximum vibration frequency point of the piping system of the compressor, namely, the optimal compensation angle will be changed.
At present, the method for obtaining the load of the compressor after low-frequency torque compensation is mainly a test method, and the method obtains the load of the compressor by testing the vibration displacement of a suction and exhaust port of a single compressor and performing reverse thrust on a transfer function matrix. The method has great limitation, firstly, in the aspect of selecting the low-frequency torque compensation angle, the compensation angle is selected based on the vibration maximum frequency point of the single compressor, and generally has difference with the compensation angle of the vibration maximum frequency point of a piping system of the compressor; secondly, if the piping scheme is changed, the compensation angle also needs to be changed, and the test needs to be performed again, so that the test period is long.
Disclosure of Invention
The invention aims to overcome the defects of the prior art and provides a load solving method under low-frequency torque compensation of a compressor, which solves the load of the compressor through the vibration maximum frequency point of a compressor piping system.
In order to achieve the purpose, the invention provides a load solving method under compressor low-frequency torque compensation, which is characterized by comprising the following steps of:
(1) Calculating each operating frequency point f under the state of no moment compensation i Load M of compressor i
M i =M di -M gi
Wherein i represents the number of operating frequency points of the compressor, M di For compressor operating frequency f i Instantaneous drive torque, M gi For compressor operating frequency f i Resistance moment in time;
(2) Establishing a library function of the moment compensation coefficient;
(2.1) calculating the maximum frequency f of each vibration j At each frequency point f of compressor operation i Moment compensation coefficient lambda of ij
If the compressor distribution pipe system is approximately a linear system, then according to the characteristics of the linear system, when the compressor distribution pipe system is at the vibration maximum frequency point f j At each frequency point f of compressor operation i Moment compensation coefficient lambda of ij Equal to the compressor at each frequency point f i Lower moment compensating loadThe ratio of the load to the moment-free compensation load, i.e.:
λ ij =M' i /M i =x' i /x i (1)
wherein, M' i For each operating frequency point f in the state of moment compensation i Compressor load of (M) i For each operating frequency point f in the state of no moment compensation i Compressor load of (x' i Operating frequency points f for a compressor distribution system in the absence of moment compensation i Response of (a), x i Representing each operating frequency point f of the compressor piping system in the state of moment compensation i The response of (c);
(2.2) setting the frequency f of the load moment compensation i The range of (A) is 10 Hz-40 Hz; at f i In the value range of (c), the frequency point f is calculated according to the formula (1) i Moment compensation coefficient lambda of ij
(2.3) fitting each frequency point f by MATLAB fitting tool i Moment compensation coefficient lambda of ij Establishing a library function of the moment compensation coefficient;
λ ij =F n (f i ,f j ) (2)
wherein f is i 、f j ∈[10Hz,40Hz],F n () The library function is represented, specifically as: when f is j Equal to a fixed frequency f 1 * When, lambda ij =F 1 (f i ) (ii) a When f is j Equal to a fixed frequency
Figure BDA0002552205370000021
When, lambda ij =F 2 (f i ) (ii) a By analogy, when f j Is equal to a fixed frequency->
Figure BDA0002552205370000022
When, lambda ij =F n (f i ) (ii) a Wherein +>
Figure BDA0002552205370000023
Vibration of piping system for compressorThe value of the maximum frequency point;
(3) Calling a library function of a moment compensation coefficient, and calculating the load M of the compressor under the low-frequency torque compensation i ';
M' i =M iij (3)
The invention aims to realize the following steps:
the invention relates to a load solving method under low-frequency torque compensation of a compressor, which is used for calculating each operating frequency point f under the state of no torque compensation i Compressor load M of i Then at the frequency f of the loading torque compensation i Within the range of (2), each vibration maximum frequency point f is calculated j At each frequency point f of compressor operation i Moment compensation coefficient lambda of ij Fitting each frequency point f by MATLAB fitting tool i Moment compensation coefficient lambda of ij Establishing a library function of a moment compensation coefficient, and finally directly calculating the load M 'of the compressor under the low-frequency torque compensation by calling the library function of the moment compensation coefficient without repeatedly testing' i
Meanwhile, the load solving method under the low-frequency torque compensation of the compressor further has the following beneficial effects:
(1) Under the condition that the piping design scheme is changed, the load of the compressor in a torque compensation state does not need to be tested, but the load is obtained through quick solution calculation of a torque compensation coefficient, so that the test cost is reduced;
(2) Under the condition that the piping design scheme needs to be changed for many times and matched with the compressor, the problem that the traditional compressor load excitation solving method needs to test for many times is solved, the testing cost is reduced, and load input is rapidly provided for vibration simulation.
Drawings
FIG. 1 is a flow chart of a load solving method under low frequency torque compensation of a compressor according to the present invention;
FIG. 2 is a moment compensation coefficient function for a maximum frequency of vibration of 25 Hz;
FIG. 3 is a function of the moment compensation coefficient for a maximum frequency of vibration of 30 Hz.
Detailed Description
The following description of the embodiments of the present invention is provided in order to better understand the present invention for those skilled in the art with reference to the accompanying drawings. It is to be expressly noted that in the following description, a detailed description of known functions and designs will be omitted when it may obscure the subject matter of the present invention.
Examples
FIG. 1 is a flow chart of a load solving method under low-frequency torque compensation of a compressor according to the invention.
In this embodiment, as shown in fig. 1, the method for solving the load under the low-frequency torque compensation of the compressor of the present invention includes the following steps:
s1, solving and calculating to obtain each operating frequency point f of the compressor under the condition of no moment compensation through a theoretical formula i The rotational inertia moment is calculated, namely, each operating frequency point f under the state of no moment compensation is calculated i Load M of compressor i
M i =M di -M gi
Wherein i represents the number of operating frequency points of the compressor, M di For compressor operating frequency f i Moment of time drive, M gi For compressor operating frequency f i Resistance moment in time;
s2, establishing a library function of the moment compensation coefficient;
s2.1, calculating each vibration maximum frequency point f j At each frequency point f of compressor operation i Moment compensation coefficient lambda of ij
Since the compressor distribution pipe system can be approximately considered as a linear system, according to the characteristics of the linear system, when the compressor distribution pipe system is at the point f of maximum vibration frequency j At each frequency point f of compressor operation i Moment compensation coefficient lambda of ij Equal to the compressor at each frequency point f i The ratio of the lower moment-compensated load to the no moment-compensated load, i.e.:
λ ij =M' i /M i =x' i /x i (1)
wherein, M' i For each operating frequency point f in the state of moment compensation i Compressor load of (M) i For each operating frequency point f in the state of no moment compensation i Compressor load of (x' i Operating frequency points f for a compressor distribution system in the absence of moment compensation i Response of (a), x i Representing each operating frequency point f of the compressor piping system in the state of moment compensation i The response can be displacement, speed, acceleration, stress, strain and the like, and response values can be obtained through vibration testing;
s2.2 setting frequency f of loading moment compensation i The range of (A) is 10 Hz-40 Hz; at f i In the value range of (2), the frequency point f is calculated according to the formula (1) i Moment compensation coefficient lambda of ij
S2.3, compensation factor lambda due to moment ij Is at the point f of maximum frequency of vibration j Related, so that if the point of maximum frequency of vibration changes, the compensation factor λ ij The change will occur, i.e. the point f of maximum frequency of vibration j Determining that the compressor is at each operating frequency point f i Moment compensation coefficient lambda of ij It was also determined that, therefore, each frequency point f was fitted by a MATLAB fitting tool i Moment compensation coefficient lambda of ij Establishing a library function of the moment compensation coefficient;
λ ij =F n (f i ,f j ) (2)
wherein f is i 、f j ∈[10Hz,40Hz],F n () The library function is represented, specifically as: when f is j Equal to a fixed frequency f 1 * When is lambda ij =F 1 (f i ) (ii) a When f is j Equal to a fixed frequency
Figure BDA0002552205370000041
When is lambda ij =F 2 (f i ) (ii) a By analogy, when f j Is equal to a fixed frequency->
Figure BDA0002552205370000042
When is lambda ij =F n (f i ) (ii) a Wherein +>
Figure BDA0002552205370000043
The value of the vibration maximum frequency point of the piping system of the compressor is taken; in the embodiment, n ≧ 2, that is, the established torque compensation coefficient library function should at least include the torque compensation functions at more than two vibration maximum frequency points.
S3, calling a library function of the moment compensation coefficient, and calculating the load M of the compressor under the low-frequency torque compensation i ';
M' i =M iij (3)
Examples of the invention
In the present embodiment, the response obtained by the vibration test is stress, and f is obtained separately j =f 1 * =25Hz、
Figure BDA0002552205370000051
And stress data of the pipeline under the state of moment compensation and no moment compensation are available, namely n =2.
It should be noted that the range of the optimal frequency point for moment compensation is generally in the range of [20Hz,35Hz ], so that the maximum vibration frequency point is selected to establish a moment compensation coefficient function library for 25Hz and 30 Hz.
When f is j =f 1 * And when the frequency is 25Hz, solving to obtain torque compensation coefficient data points at each operating frequency point of the compressor, and performing quasi-function fitting on the data points, wherein the fitting result is shown in figure 2.
λ ij =-7.5E-06f i 4 +7.5E-04f i 3 -2.3E-02f i 2 +2.3E-01f i +0.19(f j =25Hz)
When in use
Figure BDA0002552205370000052
Then, the moment compensation coefficient data points under each operating frequency point of the compressor are obtained by solving, and the data points are subjected to quasi-function fitting, and the fitting result is as followsAs shown in fig. 3.
λ ij =1.01E-05f i 4 -9.6E-04f i 3 +3.5E-02f i 2 -6.2E-01f+4.5(f j =30Hz)
The piping system of the compressor is [10Hz,40Hz]During range operation, the load in the vibration simulation is a constant value torque, the frequency response curve of the actual pipeline is solved through simulation, the frequency point corresponding to the maximum response amplitude is recorded as the maximum vibration frequency point, and in the embodiment, the maximum vibration frequency point f j =23Hz, when the vibration maximum frequency point is at lambda ij There is no corresponding f in the function library j At this time, f can be selected to be away j λ corresponding to the vibration maximum frequency point of =23Hz ij Instead, therefore, we are at λ ij The following functions are selected from the function library:
λ ij =-7.5E-06f i 4 +7.5E-04f i 3 -2.3E-02f i 2 +2.3E-01f i +0.19(f j =25Hz)
and finally, calculating the load of the compressor under the low-frequency torque compensation.
Although illustrative embodiments of the present invention have been described above to facilitate the understanding of the present invention by those skilled in the art, it should be understood that the present invention is not limited to the scope of the embodiments, and various changes may be made apparent to those skilled in the art as long as they are within the spirit and scope of the present invention as defined and defined by the appended claims, and all matters of the invention which utilize the inventive concepts are protected.

Claims (2)

1. A load solving method under low-frequency torque compensation of a compressor is characterized by comprising the following steps:
(1) Calculating each operating frequency point f under the state of no moment compensation i Compressor load M of i
M i =M di -M gi
Wherein i represents the number of operating frequency points of the compressor, M di To compressThe machine operating frequency is f i Moment of time drive, M gi For compressor operating frequency f i Resistance moment in time;
(2) Establishing a library function of the moment compensation coefficient;
(2.1) establishing and calculating each vibration maximum frequency point f j At each frequency point f of compressor operation i Moment compensation coefficient lambda of ij A linear equation of (c);
if the compressor distribution pipe system is approximately a linear system, then according to the characteristics of the linear system, when the compressor distribution pipe system is at the vibration maximum frequency point f j At each frequency point f of compressor operation i Moment compensation coefficient lambda of ij Equal to the compressor at each frequency point f i The ratio of the lower moment-compensated load to the moment-less compensated load, i.e.:
λ ij =M′ i /M i =x′ i /x i (1)
wherein, M' i For each operating frequency point f in the state of moment compensation i Compressor load of (M) i For each operating frequency point f in the state of no moment compensation i Compressor load of x' i Operating frequency points f for a compressor distribution system in the absence of moment compensation i Response of (c), x i Representing each operating frequency point f of the compressor piping system in the state of moment compensation i The response of (c);
(2.2) setting the frequency f of the load moment compensation i The range of (A) is 10 Hz-40 Hz; at f i In the value range of (c), the frequency point f is calculated according to the formula (1) i Moment compensation coefficient lambda of ij
(2.2) fitting each frequency point f by MATLAB fitting tool i Moment compensation coefficient lambda of ij Establishing a library function of the moment compensation coefficient;
λ ij =F n (f i ,f j ) (2)
wherein, f i 、f j ∈[10Hz,40Hz],F n () The library function is represented, specifically as: when f is j Equal to a fixed frequency f 1 * When, lambda ij =F 1 (f i ) (ii) a When f is j Equal to a fixed frequency
Figure QLYQS_1
When is lambda ij =F 2 (f i ) (ii) a By analogy, when f j Is equal to a fixed frequency->
Figure QLYQS_2
When is lambda ij =F n (f i ) (ii) a Wherein it is present>
Figure QLYQS_3
The value of the vibration maximum frequency point of the piping system of the compressor is taken;
(3) Calling a library function of the moment compensation coefficient, and calculating the compressor load M 'under the low-frequency torque compensation' i
M′ i =M iij (3)。
2. Load solving method at low frequency torque compensation of a compressor, according to claim 1, characterized in that said λ ij If the function library of (1) does not find the point of the maximum frequency of vibration, then use the f nearest to the point of the maximum frequency of vibration j Corresponding lambda ij Instead.
CN202010578495.1A 2020-06-23 2020-06-23 Load solving method under low-frequency torque compensation of compressor Active CN111797518B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010578495.1A CN111797518B (en) 2020-06-23 2020-06-23 Load solving method under low-frequency torque compensation of compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010578495.1A CN111797518B (en) 2020-06-23 2020-06-23 Load solving method under low-frequency torque compensation of compressor

Publications (2)

Publication Number Publication Date
CN111797518A CN111797518A (en) 2020-10-20
CN111797518B true CN111797518B (en) 2023-04-18

Family

ID=72804634

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010578495.1A Active CN111797518B (en) 2020-06-23 2020-06-23 Load solving method under low-frequency torque compensation of compressor

Country Status (1)

Country Link
CN (1) CN111797518B (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104728090A (en) * 2013-12-18 2015-06-24 海尔集团公司 Air conditioner inverter compressor frequency-domain constant torque control system and method
CN104753423A (en) * 2013-12-27 2015-07-01 迪尔公司 Methods Of Torque Estimation And Compensation And Systems Thereof
CN106022288A (en) * 2016-05-30 2016-10-12 电子科技大学 Marine oil spill information identification and extraction method based on SAR image
CN108920804A (en) * 2018-06-25 2018-11-30 四川长虹空调有限公司 Refrigeration equipment frequency-changeable compressor excitation load emulated computation method
CN109063246A (en) * 2018-06-25 2018-12-21 四川长虹空调有限公司 Frequency-changeable compressor is piped evaluation of vibration method

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3664118B2 (en) * 2001-08-07 2005-06-22 トヨタ自動車株式会社 Control device for vehicle equipped with internal combustion engine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104728090A (en) * 2013-12-18 2015-06-24 海尔集团公司 Air conditioner inverter compressor frequency-domain constant torque control system and method
CN104753423A (en) * 2013-12-27 2015-07-01 迪尔公司 Methods Of Torque Estimation And Compensation And Systems Thereof
CN106022288A (en) * 2016-05-30 2016-10-12 电子科技大学 Marine oil spill information identification and extraction method based on SAR image
CN108920804A (en) * 2018-06-25 2018-11-30 四川长虹空调有限公司 Refrigeration equipment frequency-changeable compressor excitation load emulated computation method
CN109063246A (en) * 2018-06-25 2018-12-21 四川长虹空调有限公司 Frequency-changeable compressor is piped evaluation of vibration method

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
aleksei vyngre等.calculation of the load of an electric driveof areciprocal compressor of a ship refrigeration unit.《2018 international multi-conference on industrial engineering and modern technologies(FarEastCon)》.2019,第1-4页. *
逯佳旺等. 不同载荷下压缩机的气动特性动态监测与控制.《智能计算机与应用》.2018,(第04期),第48-51+56页. *

Also Published As

Publication number Publication date
CN111797518A (en) 2020-10-20

Similar Documents

Publication Publication Date Title
US8812213B2 (en) Vehicle speed control apparatus
WO2023077704A1 (en) Random stress load spectrum grading method and system based on sn curve, and storage medium
CN111797518B (en) Load solving method under low-frequency torque compensation of compressor
JP5658530B2 (en) Engine test equipment
CN110442931B (en) Motor multi-objective optimization design method based on RSM
CN112528411A (en) Geometric nonlinear structure noise vibration response calculation method based on modal reduction
US20120016602A1 (en) Method and device for determining the pressure upstream from the turbine of a supercharging turbocharger of a thermal engine
CN109408963B (en) Fitting method for piping vibration response function relation of air conditioner under different environmental working conditions
CN110765675A (en) Noise prediction method for automobile exhaust system
CN110672290B (en) Seismic simulation vibrating table iteration control method considering lag time
Venkatesan et al. Experimental validation of a mathematical model of a reed-valve reciprocating air compressor from an automotive-braking system
CN112541276B (en) Dynamic response prediction equivalent method based on scaling model
CN113358678B (en) Semi-quantitative prediction and visualization method for mesoscopic stress and texture in alpha titanium deformation process
CN115859418A (en) Offshore wind power large-diameter single-pile horizontal dynamic response analysis method
CN110348158B (en) Seismic fluctuation analysis method based on partitioned different-step-length solution
CN110470925B (en) Electric drive power assembly reliability testing method based on extension correlation function
WO2020095507A1 (en) Shaft torque control device
CN115795956A (en) Method and system for optimizing flange structure of liquid rocket engine
KR101790733B1 (en) Step length control apparatus with multi-staged clutch damper model and the method thereof
CN113866016B (en) Multi-axis short crack propagation life prediction method considering non-proportional loading additional damage
dos Santos et al. Model based approach by combination of test and simulation methodologies for NVH investigation and improvement of a rear wheel drive vehicle
JPH08200141A (en) Torque estimating method and estimating device
CN108052712B (en) Method for evaluating integrity of aero-generator
Hao et al. Maps Preserving the Norm of the Positive Sum in L p Spaces
CN115791039A (en) Frequency division vibration control method suitable for series excitation system

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
GR01 Patent grant
GR01 Patent grant