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CN111980898A - Air compressor performance identification and group preference joint control system and method - Google Patents

Air compressor performance identification and group preference joint control system and method Download PDF

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CN111980898A
CN111980898A CN202010849924.4A CN202010849924A CN111980898A CN 111980898 A CN111980898 A CN 111980898A CN 202010849924 A CN202010849924 A CN 202010849924A CN 111980898 A CN111980898 A CN 111980898A
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CN111980898B (en
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王海舰
黄梦蝶
田莹
赵雪梅
张强
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Guilin University of Electronic Technology
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B49/00Control, e.g. of pump delivery, or pump pressure of, or safety measures for, machines, pumps, or pumping installations, not otherwise provided for, or of interest apart from, groups F04B1/00 - F04B47/00
    • F04B49/06Control using electricity
    • F04B49/065Control using electricity and making use of computers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B23/00Pumping installations or systems
    • F04B23/04Combinations of two or more pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04BPOSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B51/00Testing machines, pumps, or pumping installations
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Abstract

The invention discloses a system and a method for combined control of air compressor performance identification and group preference, which adopt a plurality of sensors to test vibration signals, current signals, temperature signals and acoustic emission signals of each air compressor in a group, adopt a multi-sensing information fusion technology to fuse the vibration signals, the current signals, the temperature signals and the acoustic emission signals in the operation process of the air compressors, realize effective identification of the current performance of each air compressor, determine the preference sequence and the operation duration of starting and stopping of each air compressor according to the performance of each air compressor, ensure the balanced adjustment of the performance of each air compressor in the air compressor group, avoid serious performance reduction and serious service life attenuation of each air compressor caused by long-term operation of each air compressor, thereby greatly improving the working efficiency of the air compressor group and the service life of each air compressor.

Description

一种空压机性能识别与组群偏好联控系统及方法An air compressor performance identification and group preference joint control system and method

技术领域technical field

本发明涉及空气压缩机性能识别与联动控制领域,特别是涉及基于多传感信息融合的空压机性能识别与组群偏好联控系统及方法。The invention relates to the field of air compressor performance identification and linkage control, in particular to an air compressor performance identification and group preference joint control system and method based on multi-sensor information fusion.

背景技术Background technique

空气压缩机是一种用以压缩气体的设备,广泛应用于工业生产的各个领域,特别是矿山开采领域,空气压缩机是为矿山开采过程中各种气动设备提供气源的重要装置。矿用空气压缩机通常以组群的方式出现,即通过多个空压机组成空压机组群,组群中的各空压机将压缩的气体通过自己的输入管道输送到母管中。由于矿山开采过程中不同时段的用风量差异很大,因此,组群中空压机运行的台数也需要根据用风量的大小进行调整,如果单台空压机经常处于运行状态或启动或与频繁,势必会造成个别空压机寿命的加速衰减,不利于整个空压机组群的高效运行以及压缩气体的优质输出,这就需要建立空压机组群合理的启停顺序、运行时长等联控方法。Air compressor is a kind of equipment for compressing gas, which is widely used in various fields of industrial production, especially in the field of mining. Air compressor is an important device that provides gas source for various pneumatic equipment in the process of mining. Mine air compressors usually appear in groups, that is, a group of air compressors is formed by multiple air compressors, and each air compressor in the group transports the compressed gas to the main pipe through its own input pipeline. Due to the large difference in air consumption in different periods during the mining process, the number of air compressors operating in the group also needs to be adjusted according to the air consumption. It will inevitably lead to the accelerated decay of the life of individual air compressors, which is not conducive to the efficient operation of the entire air compressor group and the high-quality output of compressed gas. method.

专利ZL201710653659.0给出了一种多台联动空压机及其联控备用机待机启动方法,可以通过转动杆,实现一个驱动装置带动多个压缩装置,同时,对各台空压机设定不同的压力阈值,当系统压力不足时,实现空压机的依次顺序启动,而当系统压力过高时,实现空压机依次逆序停机,以满足系统压力的稳定。Patent ZL201710653659.0 provides a method for multiple linked air compressors and their linked standby units to start up. By rotating the lever, one drive device can drive multiple compression devices, and at the same time, set the settings for each air compressor. With different pressure thresholds, when the system pressure is insufficient, the air compressors will be started in sequence, and when the system pressure is too high, the air compressors will be shut down in reverse order to meet the stability of the system pressure.

专利ZL201610071479.7给出了一种空压机触摸屏联控系统及方法采用主站触摸屏作为主站,控制各个从站触摸屏的运行,采用从站触摸屏作为从站,不再由变频器直接作为主站或从站,减少了变频器的运行负担,改善了变频器的控制性能。Patent ZL201610071479.7 gives an air compressor touch screen joint control system and method. The master station touch screen is used as the master station to control the operation of each slave station touch screen. The slave station touch screen is used as the slave station, and the inverter is no longer directly used as the master station. station or slave station, reducing the operating burden of the inverter and improving the control performance of the inverter.

以上两个专利虽然在一定程度上实现了空压机的联动控制,但在控制过程中没有考虑到空压机组群中各台空压机运行时间不同、启动频率不同对各台空压机性能的影响,极易导致部分空压机由于疲劳服役而加速衰老,而另一部分空压机由于启动次数不多,运行时间不长,其性能得不到充分发挥,导致严重的资源浪费,因此,亟需研究一种能够平衡各台空压机性能,实现空压机组群中各台空压机的均衡服役,保证各台空压机性能的最大发挥,有效延长各台空压机的使用寿命。Although the above two patents have realized the linkage control of air compressors to a certain extent, they did not take into account the different operating times and different starting frequencies of each air compressor in the air compressor group during the control process. The impact of performance can easily lead to accelerated aging of some air compressors due to fatigued service, while other air compressors cannot be fully utilized due to the small number of starts and the short running time, resulting in serious waste of resources. , It is urgent to study a method that can balance the performance of each air compressor, realize the balanced service of each air compressor in the air compressor group, ensure the maximum performance of each air compressor, and effectively prolong the service life of each air compressor. service life.

发明内容SUMMARY OF THE INVENTION

针对现有技术的缺陷和不足,本发明提供一种基于多传感信息融合的空压机性能识别与组群偏好联控系统及方法,采用多种传感器测试组群中各台空压机的振动信号、电流信号、温度信号、声发射信号,采用多传感信息融合技术对空压机运行过程中的振动信号、电流信号、温度信号、声发射信号进行融合,实现对各台空压机当前性能的有效识别,并根据各台空压机性能的优劣,确定各台空压机启停的偏好次序与运行时长,保证空压机组群中各台空压机性能的均衡调节,避免由于单台空压机长期运行造成的空压机性能严重下降,寿命严重衰减,从而大大提高空压机组群的工作效率和各台空压机的使用寿命。Aiming at the defects and deficiencies of the prior art, the present invention provides an air compressor performance identification and group preference joint control system and method based on multi-sensor information fusion. Vibration signal, current signal, temperature signal, acoustic emission signal, using multi-sensor information fusion technology to fuse the vibration signal, current signal, temperature signal and acoustic emission signal during the operation of the air compressor, to realize the integration of each air compressor Effective identification of the current performance, and according to the advantages and disadvantages of the performance of each air compressor, determine the preferred order and operation time of each air compressor to start and stop, to ensure the balanced adjustment of the performance of each air compressor in the air compressor group, It avoids the serious decline of air compressor performance and the serious degradation of service life caused by the long-term operation of a single air compressor, thereby greatly improving the working efficiency of the air compressor group and the service life of each air compressor.

为实现上述目的,本发明提供了如下方案:For achieving the above object, the present invention provides the following scheme:

一种空压机性能识别与组群偏好联控系统,包括:An air compressor performance identification and group preference joint control system, comprising:

空压机组群和空压机组群控制系统;Air compressor group and air compressor group control system;

空压机组群包括若干台空压机、母管;The air compressor group includes several air compressors and main pipes;

若干台空压机与所述母管连接;Several air compressors are connected to the main pipe;

空压机组群控制系统包括信号检测模块,数据采集与控制模块,上位机系统模块;The air compressor group control system includes a signal detection module, a data acquisition and control module, and a host computer system module;

信号检测模块用于检测所述空压机组群数据信号;The signal detection module is used to detect the data signal of the air compressor group;

数据采集与控制模块用于空压机群组所述数据信号的采集与空压机群组的工作控制;The data acquisition and control module is used for the acquisition of the data signal of the air compressor group and the work control of the air compressor group;

上位机模块用于所述数据采集与控制模块采集数据的融合识别,并通过控制模块控制空压机群组;The upper computer module is used for the fusion identification of the data collected by the data collection and the control module, and controls the air compressor group through the control module;

优选地,空压机包括:电机、气缸、冷却器、分离器、输出管道;Preferably, the air compressor includes: a motor, a cylinder, a cooler, a separator, and an output pipe;

优选地,电机与气缸连接;Preferably, the motor is connected to the cylinder;

优选地,气缸与冷却器、分离器连接;Preferably, the cylinder is connected with the cooler and the separator;

优选地,分离器具有第一端、第二端、第三端;Preferably, the separator has a first end, a second end and a third end;

优选地,分离器第一端与气缸连接;Preferably, the first end of the separator is connected with the cylinder;

优选地,分离器第二端与气缸连接;Preferably, the second end of the separator is connected to the cylinder;

优选地,分离器第三端与输出管道连接;Preferably, the third end of the separator is connected to the output pipeline;

优选地,若干台空压机的输出管道与所述母管连接;Preferably, the output pipes of several air compressors are connected with the main pipe;

优选地,信号检测模块包括:振动传感器、电流传感器、声发射传感器、温度传感器;Preferably, the signal detection module includes: a vibration sensor, a current sensor, an acoustic emission sensor, and a temperature sensor;

优选地,数据采集与控制模块包括数据采集单元和控制单元;Preferably, the data acquisition and control module includes a data acquisition unit and a control unit;

优选地,上位机模块包括数据融合单元、数据识别单元、数据控制单元;Preferably, the host computer module includes a data fusion unit, a data identification unit, and a data control unit;

优选地,振动传感器与电机连接;Preferably, the vibration sensor is connected to the motor;

优选地,电流传感器与电机连接;Preferably, the current sensor is connected to the motor;

优选地,声发射传感器与气缸连接;Preferably, the acoustic emission sensor is connected to the cylinder;

优选地,温度传感器与冷却器连接;Preferably, the temperature sensor is connected to the cooler;

优选地,数据采集单元与信号检测模块连接;Preferably, the data acquisition unit is connected to the signal detection module;

优选地,数据采集单元与数据融合单元连接;Preferably, the data acquisition unit is connected with the data fusion unit;

优选地,数据融合单元与数据识别单元连接;Preferably, the data fusion unit is connected with the data identification unit;

优选地,数据识别单元与数据控制单元连接;Preferably, the data identification unit is connected with the data control unit;

优选地,数据控制单元与控制单元连接;Preferably, the data control unit is connected to the control unit;

优选地,控制单元与空压机群组连接;Preferably, the control unit is connected to the air compressor group;

优选地,数据采集与控制单元模块,采集信号检测模块检测的多特征信号样本数据,通过上位机系统模块进行数据存储与识别,通过控制单元控制空压机组群的工作时间、工作数量和运行模式;Preferably, the data acquisition and control unit module collects the multi-feature signal sample data detected by the signal detection module, performs data storage and identification through the host computer system module, and controls the working time, number of jobs and operation of the air compressor group through the control unit. model;

优选地,运行模式有N级,分为一级单机运作模式、二级双机联动模式、三级三机协同模式、......N级N机全动模式。Preferably, there are N levels of operation modes, which are divided into a first-level single-machine operation mode, a second-level dual-machine linkage mode, a third-level three-machine cooperative mode, ...... N-level N-machine full-motion mode.

一种空压机性能识别与组群偏好联控方法,包括以下步骤:An air compressor performance identification and group preference joint control method, comprising the following steps:

S1.建立所述空压机组群;S1. Establish the air compressor group;

S2.采集所述空压机的特征样本构建样本数据库;S2. Collect characteristic samples of the air compressor to construct a sample database;

S3.构建融合识别模型,获取空压机性能识别结果,并根据所述空压机性能识别结果确定空压机启停偏好次序和运行时间;S3. Construct a fusion identification model, obtain air compressor performance identification results, and determine the air compressor start-stop preference order and running time according to the air compressor performance identification results;

S4.利用上位机数据融合、识别与控制系统模块反馈所述空压机识别融合结果信息到控制单元,通过所述控制单元实现所述空压机组群的均匀调度;S4. Use the host computer data fusion, identification and control system module to feed back the air compressor identification and fusion result information to the control unit, and realize the uniform scheduling of the air compressor group through the control unit;

优选地,空压机的特征样本包括:振动信号、电流信号、声发射信号以及温度信号;Preferably, the characteristic samples of the air compressor include: vibration signal, current signal, acoustic emission signal and temperature signal;

优选地,振动信号为电机振动信号;Preferably, the vibration signal is a motor vibration signal;

优选地,电流信号为电机电流信号;Preferably, the current signal is a motor current signal;

优选地,声发射信号为气缸声发射信号;Preferably, the acoustic emission signal is a cylinder acoustic emission signal;

优选地,温度信号为冷却器温度信号;Preferably, the temperature signal is a cooler temperature signal;

优选地,利用振动传感器采集的振动信号构建样本数据库1,并结合数据之间相关性求解得到相应的隶属度函数1;Preferably, the sample database 1 is constructed by using the vibration signals collected by the vibration sensor, and the corresponding membership function 1 is obtained by solving the correlation between the data;

优选地,利用电流传感器采集的电流信号构建样本数据库2,并结合数据之间相关性求解得到相应的隶属度函数2;Preferably, the sample database 2 is constructed by using the current signal collected by the current sensor, and the corresponding membership function 2 is obtained by solving the correlation between the data;

优选地,利用声发射传感器采集的声发射信号构建样本数据库3,并结合数据之间相关性求解得到相应的隶属度函数3;Preferably, the sample database 3 is constructed by using the acoustic emission signal collected by the acoustic emission sensor, and the corresponding membership function 3 is obtained by solving the correlation between the data;

优选地,利用温度传感器采集的温度信号构建样本数据库4,并结合数据之间相关性求解得到相应的隶属度函数4;Preferably, the sample database 4 is constructed by using the temperature signal collected by the temperature sensor, and the corresponding membership function 4 is obtained by solving the correlation between the data;

优选地,根据隶属度函数1、隶属度函数2、隶属度函数3、隶属度函数4,获取空压机的一组所述振动信号、电流信号、声发射信号以及温度信号的多信号特征样本数据,作为原始数据的输入,将多信号特征样本数据带入隶属度函数1、隶属度函数2、隶属度函数3、隶属度函数4,得到振动信号、电流信号、声发射信号以及温度信号的隶属度值。Preferably, according to membership function 1, membership function 2, membership function 3, and membership function 4, a group of multi-signal feature samples of the vibration signal, current signal, acoustic emission signal and temperature signal of the air compressor are obtained Data, as the input of the original data, bring the multi-signal feature sample data into membership function 1, membership function 2, membership function 3, membership function 4, and obtain vibration signal, current signal, acoustic emission signal and temperature signal. Membership value.

优选地,将振动信号、电流信号、声发射信号以及温度信号的隶属度值作为D-S证据理论基本概率分配函数的基本输入值进行计算;Preferably, the membership value of the vibration signal, the current signal, the acoustic emission signal and the temperature signal is calculated as the basic input value of the basic probability distribution function of the D-S evidence theory;

优选地,通过所述计算得到每个空压机的基本概率值,将基本概率值采用基于D-S证据理论的融合模型对振动信号、温度信号、压力信号、声发射信号以及电流信号的多特征样本数据进行融合;Preferably, the basic probability value of each air compressor is obtained through the calculation, and the basic probability value adopts the fusion model based on the D-S evidence theory to analyze the multi-feature samples of vibration signal, temperature signal, pressure signal, acoustic emission signal and current signal. data fusion;

优选地,通过多特征样本数据融合获取各空压机性能识别结果的不确定度及信度值,根据融合结果的决策准则确定最终的压机性能识别融合结果;Preferably, the uncertainty and reliability values of each air compressor performance identification result are obtained through multi-feature sample data fusion, and the final compressor performance identification fusion result is determined according to the decision criterion of the fusion result;

根据所述空压机性能识别融合结果,确定空压机启停偏好次序,即融合最大结果值对应的所述空压机性能最佳,融合次大结果值对应的所述空压机性能其次,同理按照融合结果数值大小排序对应上空压机性能次序;According to the results of the air compressor performance identification and fusion, determine the priority order of starting and stopping the air compressor, that is, the performance of the air compressor corresponding to the largest fusion result value is the best, and the performance of the air compressor corresponding to the next largest fusion result value is second , in the same way, according to the numerical value of the fusion result, the corresponding upper air compressor performance sequence is sorted;

优选地,D-S证据理论识别决策准则包括:Preferably, the D-S evidence theory identification decision criteria include:

1)空压机性能识别结果的信度值要大于任意其它故障识别结果的信度值;1) The reliability value of the air compressor performance identification result is greater than that of any other fault identification results;

2)空压机性能识别结果的信度值减去其它任意空压机性能识别结果的信度值要大于阈值K;2) The reliability value of the air compressor performance identification result minus the reliability value of any other air compressor performance identification result must be greater than the threshold K;

3)空压机性能识别结果的不确定度要小于阈值L;3) The uncertainty of the air compressor performance identification result should be less than the threshold value L;

优选地,通过再次获取空压机上的所述多种传感器采集的振动信号、电流信号、声发射信号以及温度信号,生成新的多特征信号样本库及隶属度函数,利用融合识别模型进行新的融合,获取新的融合结果后更新空压机偏好启停顺序和运行时间,实现动态调整空压机组群的服役均衡度。Preferably, by obtaining the vibration signals, current signals, acoustic emission signals and temperature signals collected by the various sensors on the air compressor again, a new multi-feature signal sample library and membership function are generated, and a new multi-feature signal sample library and membership function are generated, and the fusion recognition model is used for new After obtaining the new fusion results, the preferred start-stop sequence and running time of the air compressors are updated, and the service balance of the air compressor unit group can be dynamically adjusted.

本发明的技术效果:Technical effect of the present invention:

(1)利用多种传感器采集多类信号样本,采用多传感信息融合方法对不同的多特征信号进行融合,进一步提高空压机性能识别准确度、精确度;(1) Use a variety of sensors to collect multiple types of signal samples, and use the multi-sensor information fusion method to fuse different multi-feature signals to further improve the accuracy and precision of air compressor performance identification;

(2)下位机和上位机协同配合,完成数据的实时传输及融合,精准监测空压机运行各项指标;(2) The lower computer and the upper computer cooperate to complete the real-time transmission and fusion of data, and accurately monitor various indicators of the air compressor operation;

(3)明确各台空压机启停的偏好次序与运行时长,保证空压机组群中各台空压机性能的均衡调节;(3) Clarify the preferred order and operation time of each air compressor to start and stop, so as to ensure the balanced adjustment of the performance of each air compressor in the air compressor group;

(4)实现空压机组群偏好联动,完成空压机多种工作模式的选择,能够进行多台空压机之间的最佳匹配的筛选,均衡各个空压机的使用寿命,提高空压机组群整个系统的使用效率和产生气体的质量,保证空压机组群高质、高量的运作。(4) Realize the preference linkage of the air compressor group, complete the selection of various working modes of the air compressor, and be able to screen the best match between multiple air compressors, balance the service life of each air compressor, and improve the air compressor. The utilization efficiency of the entire system of the compressor group and the quality of the gas produced ensure the high-quality and high-volume operation of the air compressor group.

附图说明Description of drawings

为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例中所需要使用的附图作简单地介绍,显而易见地,下面描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动性的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the accompanying drawings required in the embodiments will be briefly introduced below. Obviously, the drawings in the following description are only some of the present invention. In the embodiments, for those of ordinary skill in the art, other drawings can also be obtained according to these drawings without creative labor.

图1是本发明实施例中基于多传感信息融合的空压机性能识别与组群偏好联控系统的模型结构示意图。1 is a schematic structural diagram of a model of an air compressor performance identification and group preference joint control system based on multi-sensor information fusion in an embodiment of the present invention.

图2是本发明实施例中基于多传感信息融合的空压机性能识别与组群偏好联控系统的具体过程流向示意图。2 is a schematic diagram of a specific process flow of an air compressor performance identification and group preference joint control system based on multi-sensor information fusion in an embodiment of the present invention.

图3是本发明实施例中基于多传感信息融合的空压机性能识别与组群偏好联控系统的融合识别模型过程示意图。FIG. 3 is a schematic diagram of a fusion recognition model process of an air compressor performance recognition and group preference joint control system based on multi-sensor information fusion in an embodiment of the present invention.

图4是本发明实施例中基于多传感信息融合的空压机性能识别与组群偏好联控系统的信号流向示意图。4 is a schematic diagram of a signal flow of an air compressor performance identification and group preference joint control system based on multi-sensor information fusion in an embodiment of the present invention.

其中,1为第一空压机,2为第二空压机,3为第三空压机,4为第四空压机,Ⅰ为电机,Ⅱ为气缸,Ⅲ为冷却器,Ⅳ为分离器,1-1为第一空压机振动传感器1-2为第一空压机电流传感器,1-3为第一空压机声发射传感器,1-4为第一空压机温度传感器,2-1为第二空压机振动传感器2-2为第二空压机电流传感器,2-3为第二空压机声发射传感器,2-4为第二空压机温度传感器,3-1为第三空压机振动传感器3-2为第三空压机电流传感器3-3为第三空压机声发射传感器,3-4为第三空压机温度传感器,4-1为第四空压机振动传感器4-2为第四空压机电流传感器,4-3为第四空压机声发射传感器,4-4为第四空压机温度传感器。Among them, 1 is the first air compressor, 2 is the second air compressor, 3 is the third air compressor, 4 is the fourth air compressor, I is the motor, II is the cylinder, III is the cooler, IV is the separation 1-1 is the first air compressor vibration sensor, 1-2 is the first air compressor current sensor, 1-3 is the first air compressor acoustic emission sensor, 1-4 is the first air compressor temperature sensor, 2-1 is the second air compressor vibration sensor 2-2 is the second air compressor current sensor, 2-3 is the second air compressor acoustic emission sensor, 2-4 is the second air compressor temperature sensor, 3- 1 is the third air compressor vibration sensor 3-2 is the third air compressor current sensor 3-3 is the third air compressor acoustic emission sensor, 3-4 is the third air compressor temperature sensor, 4-1 is the third air compressor temperature sensor The four-air compressor vibration sensor 4-2 is the fourth air compressor current sensor, 4-3 is the fourth air compressor acoustic emission sensor, and 4-4 is the fourth air compressor temperature sensor.

具体实施方式Detailed ways

下面将结合本发明实施例中的附图,对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

为使本发明的上述目的、特征和优点能够更加明显易懂,下面结合附图和具体实施方式对本发明作进一步详细的说明。In order to make the above objects, features and advantages of the present invention more clearly understood, the present invention will be described in further detail below with reference to the accompanying drawings and specific embodiments.

实施例1:如图1-4所示,本发明是一种空压机性能识别与组群偏好联控系统,包括空压机组群,信号检测模块,数据采集与控制单元,上位机数据融合、识别与控制系统模块。Embodiment 1: As shown in Figures 1-4, the present invention is an air compressor performance identification and group preference joint control system, including an air compressor group, a signal detection module, a data acquisition and control unit, and a host computer data Fusion, identification and control system modules.

空压机组群包含多台空气压缩机,各台空压机的输出管道共同与母管连接,本发明以四台空压机构成的组群进行说明。The air compressor group includes a plurality of air compressors, and the output pipes of each air compressor are jointly connected to the main pipe. The present invention is described with a group composed of four air compressors.

空压机组群的各台空压机采用联动控制,可根据工业上所需要的供气容量,进行空压机之间的最佳配合的筛选,选择具体空压机工作的台数和运行模式,运行模式可分为单机运作、双机联动、三机协同以及四机全动;Each air compressor in the air compressor group adopts linkage control, which can screen the best cooperation between air compressors according to the air supply capacity required in the industry, and select the number and operation mode of specific air compressors. , the operation mode can be divided into single-machine operation, double-machine linkage, three-machine coordination and four-machine full-motion;

信号检测模块即首先通过在空压机的电机部分安装振动传感器和电流传感器,在空压机气缸处安装声发射传感器,在主机排气口即冷却器处安装温度传感器;利用振动传感器、电流传感器、声发射传感器以及温度传感器进行振动信号、电流信号、声发射信号以及温度信号的检测,根据振动传感器、电流传感器、声发射传感器以及温度传感器检测出四种信号的变化情况,掌握当前空压机电机端、气缸部分以及冷却器端的运行情况;The signal detection module first installs a vibration sensor and a current sensor on the motor part of the air compressor, installs an acoustic emission sensor at the air compressor cylinder, and installs a temperature sensor at the exhaust port of the main engine, that is, the cooler; use the vibration sensor and current sensor. , Acoustic emission sensor and temperature sensor to detect vibration signal, current signal, acoustic emission signal and temperature signal. The operation of the motor end, the cylinder part and the cooler end;

数据采集与控制单元模块即利用振动传感器、电流传感器、声发射传感器以及温度传感器采集的振动信号、电流信号、声发射信号以及温度信号,建立空压机组群的振动信号特征数据库、电流信号特征数据库、声发射信号特征数据库和温度信号特征数据库,结合优化算法以及数据间的模糊关系,获取振动、电流、声发射以及温度的多特征信号样本隶属度函数;The data acquisition and control unit module uses the vibration signal, current signal, acoustic emission signal and temperature signal collected by the vibration sensor, current sensor, acoustic emission sensor and temperature sensor to establish the vibration signal characteristic database and current signal characteristic of the air compressor group. Database, acoustic emission signal feature database and temperature signal feature database, combined with optimization algorithm and fuzzy relationship between data, to obtain multi-feature signal sample membership functions of vibration, current, acoustic emission and temperature;

上位机数据融合、识别与控制系统模块即存储所获取的多特征信号样本库,选取一种多传感信息融合的方法,将隶属度函数作为一个目标输入,将多传感信息融合方法与隶属度函数结合,继而进一步优化获取最终融合结果,根据融合结果确定各台空压机性能的优劣,建立各台空压机启停的偏好次序与运行时长,以保证空压机组群中各台空压机性能的均衡调节;并将数据反馈到数据采集与控制单元模块,利用其中的控制单元选择具体空压机工作的台数和运行模式,继而完成空压机性能识别与组群偏好联动。The upper computer data fusion, identification and control system module stores the acquired multi-feature signal sample library, selects a multi-sensor information fusion method, takes the membership function as a target input, and combines the multi-sensor information fusion method with membership According to the fusion results, the performance of each air compressor is determined, and the preference order and operation time of each air compressor are established to ensure that each air compressor in the air compressor group Balanced adjustment of the performance of each air compressor; feedback the data to the data acquisition and control unit module, and use the control unit to select the number and operation mode of the specific air compressor, and then complete the air compressor performance identification and group preference linkage .

(1)多个空压机组合构成空压机组群;(1) Multiple air compressors are combined to form an air compressor group;

如图1所示,Ⅰ电机、Ⅱ气缸、Ⅲ冷却器和Ⅳ分离器构成空压压缩机的主体部分,Ⅰ电机、Ⅱ气缸、Ⅲ冷却器、Ⅳ分离器以及各轴端所需导气管,可构成第一空压机、第二空压机、第三空压机以及第四空压机的总体结构,第一空压机、第二空压机、第三空压机以及第四空压机组成了空压机组群,并通过Ⅴ控制单元将4个空压机进行连接,通过Ⅴ控制单元选择空压机工作时间、数量和运行模式。As shown in Figure 1, I motor, II cylinder, III cooler and IV separator constitute the main part of the air compressor, I motor, II cylinder, III cooler, IV separator and air ducts required for each shaft end, It can constitute the overall structure of the first air compressor, the second air compressor, the third air compressor and the fourth air compressor, the first air compressor, the second air compressor, the third air compressor and the fourth air compressor. The compressors form an air compressor group, and the 4 air compressors are connected through the V control unit, and the working time, quantity and operation mode of the air compressors are selected through the V control unit.

(2)在空压机指定位置上安装振动传感器、电流传感器、声发射传感器以及温度传感器,便于空压机多特征信号检测;(2) Install vibration sensors, current sensors, acoustic emission sensors and temperature sensors on the designated positions of the air compressor to facilitate the detection of multi-signature signals of the air compressor;

在四个空压机上各自安装振动传感器、电流传感器、声发射传感器以及温度传感器,如图1所示,第一空压机的Ⅰ电机部分安装振动传感器1-1以及电流传感器1-2,气缸Ⅱ处安装声发射传感器1-3,冷却器Ⅲ处安装温度传感器1-4;Install a vibration sensor, a current sensor, an acoustic emission sensor and a temperature sensor on each of the four air compressors. As shown in Figure 1, the I motor part of the first air compressor is equipped with a vibration sensor 1-1 and a current sensor 1-2. Acoustic emission sensor 1-3 is installed at cylinder II, and temperature sensor 1-4 is installed at cooler III;

第二空压机的Ⅰ电机部分安装振动传感器2-1以及电流传感器2-2,气缸Ⅱ处安装声发射传感器2-3,冷却器Ⅲ处安装温度传感器2-4;A vibration sensor 2-1 and a current sensor 2-2 are installed in the motor part I of the second air compressor, an acoustic emission sensor 2-3 is installed at the cylinder II, and a temperature sensor 2-4 is installed at the cooler III;

第三空压机的Ⅰ电机部分安装振动传感器3-1以及电流传感器3-2,气缸Ⅱ处安装声发射传感器3-3,冷却器Ⅲ处安装温度传感器3-4;A vibration sensor 3-1 and a current sensor 3-2 are installed in the motor part I of the third air compressor, an acoustic emission sensor 3-3 is installed at the cylinder II, and a temperature sensor 3-4 is installed at the cooler III;

第四空压机的Ⅰ电机部分安装振动传感器4-1以及电流传感器4-2,气缸Ⅱ处安装声发射传感器4-3,冷却器Ⅲ处安装温度传感器4-4。A vibration sensor 4-1 and a current sensor 4-2 are installed in the motor part I of the fourth air compressor, an acoustic emission sensor 4-3 is installed at the cylinder II, and a temperature sensor 4-4 is installed at the cooler III.

振动传感器、电流传感器、声发射传感器以及温度传感器分别用来检测振动信号、电流信号、声发射信号以及温度信号。The vibration sensor, the current sensor, the acoustic emission sensor and the temperature sensor are respectively used to detect the vibration signal, the current signal, the acoustic emission signal and the temperature signal.

(3)通过多种传感器进行实时的信号检测,采集振动、电流、声发射以及温度多信号特征样本,针对四种信号的特征样本构建各自的样本数据库;(3) Real-time signal detection is carried out through a variety of sensors, and multi-signal characteristic samples of vibration, current, acoustic emission and temperature are collected, and their respective sample databases are constructed for the characteristic samples of the four kinds of signals;

如图2所示,利用振动传感器采集的振动信号构建样本数据库1,并结合数据之间相关性求解得到相应的隶属度函数1;As shown in Figure 2, the sample database 1 is constructed by using the vibration signal collected by the vibration sensor, and the corresponding membership function 1 is obtained by combining the correlation between the data;

利用电流传感器采集的电流信号构建样本数据库2,并结合数据之间相关性求解得到相应的隶属度函数2;The sample database 2 is constructed by using the current signal collected by the current sensor, and the corresponding membership function 2 is obtained by solving the correlation between the data;

利用声发射传感器采集的声发射信号构建样本数据库3,并结合数据之间相关性求解得到相应的隶属度函数3;The sample database 3 is constructed by using the acoustic emission signal collected by the acoustic emission sensor, and the corresponding membership function 3 is obtained by solving the correlation between the data;

利用温度传感器采集的温度信号构建样本数据库4,并结合数据之间相关性求解得到相应的隶属度函数4。The sample database 4 is constructed by using the temperature signal collected by the temperature sensor, and the corresponding membership function 4 is obtained by solving the correlation between the data.

建立四个空压机对应的不同特征信号样本所构成的样本数据库,同时获取四个空压机对应样本数据库的不同隶属度函数。A sample database composed of different characteristic signal samples corresponding to four air compressors is established, and different membership functions of the sample database corresponding to the four air compressors are obtained at the same time.

(4)如图3所示,构建融合识别模型,获取空压机性能识别结果,并根据空压机性能识别结果确定空压机启停偏好次序和运行时间;(4) As shown in Figure 3, build a fusion identification model, obtain the air compressor performance identification results, and determine the air compressor start-stop preference order and running time according to the air compressor performance identification results;

1)根据四个空压机对应的隶属度函数,分别获取四个空压机的一组振动、电流、声发射以及温度多信号特征样本数据即10,作为原始数据的输入带入所计算的隶属度函数得到关于振动信号、电流信号、声发射信号以及温度信号的隶属度值即20;1) According to the membership function corresponding to the four air compressors, obtain a set of vibration, current, acoustic emission and temperature multi-signal characteristic sample data of the four air compressors, namely 10, and bring it into the calculated membership as the input of the original data. The degree function obtains the membership value of the vibration signal, the current signal, the acoustic emission signal and the temperature signal, that is, 20;

2)将获取的关于振动信号、电流信号、声发射信号以及温度信号的隶属度值作为D-S证据理论的基本概率分配函数的基本输入值即30,带入后将计算得到每个空压机的基本概率值,采用基于D-S证据理论的融合模型即40对振动、温度、压力、声发射以及电流多特征样本数据进行融合,获取各空压机性能识别结果的不确定度及信度值,根据融合结果的决策准则即50确定最终的压机性能识别融合结果;2) Take the obtained membership value of vibration signal, current signal, acoustic emission signal and temperature signal as the basic input value of the basic probability distribution function of D-S evidence theory, that is, 30. For the basic probability value, the fusion model based on the D-S evidence theory is used to fuse the multi-feature sample data of vibration, temperature, pressure, acoustic emission and current to obtain the uncertainty and reliability values of the performance identification results of each air compressor. The decision criterion of the fusion result is 50 to determine the final press performance identification fusion result;

3)D-S证据理论识别决策准则:3) D-S evidence theory identifies decision-making criteria:

3-1、空压机性能识别结果的信度值要大于任意其它故障识别结果的信度值;3-1. The reliability value of the air compressor performance identification result is greater than that of any other fault identification results;

3-2、空压机性能识别结果的信度值减去其它任意空压机性能识别结果的信度值要大于阈值K;3-2. The reliability value of the air compressor performance identification result minus the reliability value of any other air compressor performance identification result must be greater than the threshold K;

3-3、空压机性能识别结果的不确定度要小于阈值L。3-3. The uncertainty of the air compressor performance identification result should be less than the threshold value L.

4)根据空压机性能识别融合结果,确定空压机启停偏好次序,即融合最大结果值对应的空压机性能最佳,融合次大结果值对应的空压机性能其次,同理按照融合结果数值大小排序对应上空压机性能次序。4) According to the air compressor performance identification fusion results, determine the air compressor start and stop preference order, that is, the air compressor performance corresponding to the largest fusion result value is the best, and the air compressor performance corresponding to the next largest fusion result value is second. The numerical order of the fusion results corresponds to the performance order of the air compressors.

(5)利用上位机数据融合、识别与控制系统模块反馈空压机识别融合结果信息到控制单元,控制空压机工作时间、台数和启停顺序,实现整个空压机组群的均匀调度。(5) Use the upper computer data fusion, identification and control system module to feed back the air compressor identification and fusion result information to the control unit to control the working time, number and start and stop sequence of the air compressors to achieve uniform scheduling of the entire air compressor group.

利用控制系统反馈空压机融合识别结果到Ⅴ控制单元,并设定好所获取的空压机启停偏好次序,再通过Ⅴ控制单元选择空压机工作时间、数量和运行模式,运行模式有四级可细分为一级单机运作、二级双机联动、三级三机协同以及四级四机全动。Use the control system to feed back the air compressor fusion identification result to the V control unit, and set the obtained air compressor start and stop preference order, and then use the V control unit to select the working time, quantity and operation mode of the air compressor. The operation modes include: The four-level can be subdivided into the first-level single-machine operation, the second-level dual-machine linkage, the third-level three-machine coordination, and the fourth-level four-machine full-motion.

考虑到空压机组群中每个空压机启停顺序、运行时间以及使用频率均不一致,将很大程度降低空压机组群整个系统的使用寿命,故根据空压机启停偏好次序,可规律地、均衡地调节空压机组群的使用情况。Considering that the start-stop sequence, running time and frequency of use of each air compressor in the air compressor group are inconsistent, the service life of the entire system of the air compressor group will be greatly reduced, so according to the air compressor start-stop preference order , which can regularly and evenly adjust the use of the air compressor group.

与此同时,可在一定时间间隔内再次获取四个空压机上的多种传感器采集的振动信号、电流信号、声发射信号以及温度信号,重新生成新的多特征信号样本库及隶属度函数,利用融合识别模型进行新的融合,获取新的融合结果后更新空压机偏好启停顺序和运行时间,动态调整空压机组群的服役均衡度。At the same time, the vibration signal, current signal, acoustic emission signal and temperature signal collected by various sensors on the four air compressors can be acquired again within a certain time interval, and a new multi-feature signal sample library and membership function can be regenerated. , use the fusion recognition model to perform new fusion, update the air compressor preference start-stop sequence and running time after obtaining the new fusion result, and dynamically adjust the service balance of the air compressor unit group.

本发明空压机性能识别和偏好联控过程中多特征信号数据具体流向如图4所示:The specific flow of multi-feature signal data in the process of performance identification and preference joint control of the air compressor of the present invention is shown in Figure 4:

第一空压机中振动传感器、电流传感器、声发射传感器以及温度传感器所检测的振动信号、电流信号、声发射信号以及温度信号经S11传递到数据采集与控制模块,即采集振动信号、电流信号、声发射信号以及温度信号的特征样本便于构建第一空压机的多信号特征数据样本库,再经过S21传递到上位机数据融合、识别与控制系统,即处理采集到的数据,利用多传感信息融合方法将其融合后,获取第一空压机启停偏好顺序并由控制系统反馈信息,经S31传递到数据采集与控制模块,最后经S41控制第一空压机的运作;The vibration signal, current signal, acoustic emission signal and temperature signal detected by the vibration sensor, current sensor, acoustic emission sensor and temperature sensor in the first air compressor are transmitted to the data acquisition and control module through S11, that is, the vibration signal and current signal are collected. The characteristic samples of the acoustic emission signal and the temperature signal are easy to construct the multi-signal characteristic data sample library of the first air compressor, and then transmitted to the upper computer data fusion, identification and control system through S21, that is, the collected data is processed and the multi-transmission data is used. After the sensor information fusion method is used to fuse it, the starting and stopping preference sequence of the first air compressor is obtained and the information is fed back by the control system, which is transmitted to the data acquisition and control module through S31, and finally the operation of the first air compressor is controlled through S41;

第二空压机中振动传感器、电流传感器、声发射传感器以及温度传感器所检测的振动信号、电流信号、声发射信号以及温度信号经S12传递到数据采集与控制模块,即采集振动信号、电流信号、声发射信号以及温度信号的特征样本便于构建第二空压机的多信号特征数据样本库,再经过S22传递到上位机数据融合、识别与控制系统,即处理采集到的数据,利用多传感信息融合方法将其融合后,获取第二空压机启停偏好顺序并由控制系统反馈信息,经S32传递到数据采集与控制模块,最后经S42控制第二空压机的运作;The vibration signal, current signal, acoustic emission signal and temperature signal detected by the vibration sensor, current sensor, acoustic emission sensor and temperature sensor in the second air compressor are transmitted to the data acquisition and control module through S12, that is, the vibration signal and current signal are collected. The characteristic samples of the acoustic emission signal and the temperature signal are convenient to build the multi-signal characteristic data sample library of the second air compressor, and then pass it to the upper computer data fusion, identification and control system through S22, that is, to process the collected data and use the multi-transmission data. After the sensor information fusion method is used to fuse it, the starting and stopping preference sequence of the second air compressor is obtained and the information is fed back by the control system, which is transmitted to the data acquisition and control module through S32, and finally the operation of the second air compressor is controlled through S42;

第三空压机中振动传感器、电流传感器、声发射传感器以及温度传感器所检测的振动信号、电流信号、声发射信号以及温度信号经S13传递到数据采集与控制模块,即采集振动信号、电流信号、声发射信号以及温度信号的特征样本便于构建第三空压机的多信号特征数据样本库,再经过S23传递到上位机数据融合、识别与控制系统,即处理采集到的数据,利用多传感信息融合方法将其融合后,获取第三空压机启停偏好顺序并由控制系统反馈信息,经S33传递到数据采集与控制模块,最后经S43控制第三空压机的运作;The vibration signal, current signal, acoustic emission signal and temperature signal detected by the vibration sensor, current sensor, acoustic emission sensor and temperature sensor in the third air compressor are transmitted to the data acquisition and control module through S13, that is, the vibration signal and current signal are collected. The characteristic samples of the acoustic emission signal and temperature signal are convenient to construct the multi-signal characteristic data sample library of the third air compressor, and then transmitted to the upper computer data fusion, identification and control system through S23, that is, the collected data is processed and the multi-transmission data is used. After it is fused by the sensor information fusion method, the starting and stopping preference order of the third air compressor is obtained and the information is fed back by the control system, which is transmitted to the data acquisition and control module through S33, and finally the operation of the third air compressor is controlled through S43;

第四空压机中振动传感器、电流传感器、声发射传感器以及温度传感器所检测的振动信号、电流信号、声发射信号以及温度信号经S14传递到数据采集与控制模块,即采集振动信号、电流信号、声发射信号以及温度信号的特征样本便于构建第四空压机的多信号特征数据样本库,再经过S24传递到上位机数据融合、识别与控制系统,即处理采集到的数据,利用多传感信息融合方法将其融合后,获取第四空压机启停偏好顺序并由控制系统反馈信息,经S34传递到数据采集与控制模块,最后经S44控制第四空压机的运作。The vibration signal, current signal, acoustic emission signal and temperature signal detected by the vibration sensor, current sensor, acoustic emission sensor and temperature sensor in the fourth air compressor are transmitted to the data acquisition and control module through S14, that is, the vibration signal and current signal are collected. The characteristic samples of , acoustic emission signal and temperature signal are convenient to build the multi-signal characteristic data sample database of the fourth air compressor, and then pass it to the upper computer data fusion, identification and control system through S24, that is, process the collected data, use the multi-transmission data After the sensor information fusion method is used to fuse it, the starting and stopping preference order of the fourth air compressor is obtained and the information is fed back by the control system, which is transmitted to the data acquisition and control module through S34, and finally the operation of the fourth air compressor is controlled through S44.

以上所述的实施例仅是对本发明的优选方式进行描述,并非对本发明的范围进行限定,在不脱离本本发明设计精神的前提下,本领域普通技术人员对本发明的技术方案做出的各种变形和改进,均应落入本发明权利要求书确定的保护范围内。The above-mentioned embodiments are only to describe the preferred mode of the present invention, and do not limit the scope of the present invention. Without departing from the design spirit of the present invention, those of ordinary skill in the art can make various Variations and improvements should fall within the protection scope determined by the claims of the present invention.

Claims (10)

1. The utility model provides an air compressor machine performance identification and group preference allies oneself with accuse system which characterized in that includes:
the air compressor group and the air compressor group control system;
the air compressor group comprises a plurality of air compressors and a main pipe;
the air compressor is connected with the main pipe;
the air compressor group control system comprises a signal detection module, a data acquisition and control module and an upper computer system module;
the signal detection module is used for detecting the air compressor group data signals;
the data acquisition and control module is used for acquiring data signals of the air compressor group and controlling the work of the air compressor group;
the upper computer module is used for fusion identification of data acquisition and control module data acquisition, and controls the air compressor group through the control module.
2. The air compressor performance identification and group preference joint control system of claim 1, wherein:
the air compressor machine includes: the device comprises a motor, a cylinder, a cooler, a separator and an output pipeline;
the motor is connected with the air cylinder;
the cylinder is connected with the cooler and the separator;
the separator has a first end, a second end, and a third end;
the first end of the separator is connected with the cylinder;
the second end of the separator is connected with the cylinder;
the third end of the separator is connected with the output pipeline;
and the output pipeline of the platform air compressor is connected with the main pipe.
3. The air compressor performance identification and group preference joint control system of claim 1, wherein:
the signal detection module includes: a vibration sensor, a current sensor, an acoustic emission sensor, a temperature sensor;
the data acquisition and control module comprises a data acquisition unit and a control unit;
the upper computer module comprises a data fusion unit, a data identification unit and a data control unit;
the vibration sensor is connected with the motor;
the current sensor is connected with the motor;
the acoustic emission sensor is connected with the cylinder;
the temperature sensor is connected with the cooler;
the data acquisition unit is connected with the signal detection module;
the data acquisition unit is connected with the data fusion unit;
the data fusion unit is connected with the data identification unit;
the data identification unit is connected with the data control unit;
the data control unit is connected with the control unit;
the control unit is connected with the air compressor group;
the data acquisition and control unit module acquires multi-characteristic signal sample data detected by the signal detection module, performs data storage and identification through the upper computer system module, and controls the working time, the working quantity and the running mode of the air compressor group through the control unit;
the operation mode has N levels and is divided into a first-level single-machine operation mode, a second-level double-machine linkage mode, a third-level three-machine cooperation mode and an N-level N-machine full-motion mode.
4. The air compressor performance identification and group preference joint control method is characterized by comprising the following steps of:
s1, establishing an air compressor group;
s2, collecting a characteristic sample of the air compressor to construct a sample database;
s3, constructing a fusion recognition model, obtaining an air compressor performance recognition result, and determining the start-stop preference order and the operation time of the air compressor according to the air compressor performance recognition result;
and S4, feeding back the information of the air compressor identification fusion result to a control unit by using an upper computer data fusion, identification and control system module, and realizing uniform scheduling of the air compressor group through the control unit.
5. The air compressor performance identification and group preference joint control method according to claim 4, characterized in that:
the characteristic sample of air compressor machine includes: a vibration signal, a current signal, an acoustic emission signal, and a temperature signal;
the vibration signal is the motor vibration signal;
the current signal is the motor current signal;
the acoustic emission signal is the cylinder acoustic emission signal;
the temperature signal is the cooler temperature signal.
6. The air compressor performance identification and group preference joint control method according to claim 4, characterized in that:
constructing a sample database 1 by using vibration signals acquired by the vibration sensor, and solving by combining the correlation among the data to obtain a corresponding membership function 1;
constructing a sample database 2 by using current signals acquired by a current sensor, and solving by combining the correlation among data to obtain a corresponding membership function 2;
constructing a sample database 3 by using acoustic emission signals acquired by an acoustic emission sensor, and solving to obtain a corresponding membership function 3 by combining correlation among data;
and constructing a sample database 4 by using the temperature signals acquired by the temperature sensors, and solving by combining the correlation among the data to obtain a corresponding membership function 4.
7. The air compressor performance identification and group preference joint control method according to claim 6, characterized in that:
according to the membership function 1, the membership function 2, the membership function 3 and the membership function 4, acquiring a group of multi-characteristic signal sample data of the vibration signal, the current signal, the acoustic emission signal and the temperature signal of the air compressor, using the multi-characteristic signal sample data as the input of original data, and substituting the multi-signal characteristic sample data into the membership function 1, the membership function 2, the membership function 3 and the membership function 4 to obtain the membership values of the vibration signal, the current signal, the acoustic emission signal and the temperature signal.
8. The air compressor performance identification and group preference joint control method according to claim 7, characterized in that:
calculating the membership values of the vibration signal, the current signal, the acoustic emission signal and the temperature signal as basic input values of a basic probability distribution function of a D-S evidence theory;
obtaining the basic probability value of each air compressor through calculation, and fusing multi-signal characteristic sample data of the vibration signal, the temperature signal, the pressure signal, the acoustic emission signal and the current signal by adopting a fusion model based on a D-S evidence theory according to the basic probability value;
obtaining uncertainty and confidence value of the performance identification result of each air compressor through the multi-feature sample data fusion, and determining a final performance identification fusion result of the air compressor according to a decision criterion of the fusion result;
and identifying a fusion result according to the performance of the air compressor, and determining the start-stop preference order of the air compressor, namely, fusing the best performance of the air compressor corresponding to the maximum result value, fusing the performance of the air compressor corresponding to the second-largest result value, and similarly, sequencing the performance order of the corresponding air compressor according to the numerical value of the fusion result.
9. The air compressor performance identification and group preference joint control method according to claim 8, characterized in that:
the D-S evidence theory recognition decision criteria include:
1) the reliability value of the performance identification result of the air compressor is greater than the reliability values of any other fault identification results;
2) the reliability value of the performance identification result of the air compressor minus the reliability value of the performance identification result of any other air compressor is greater than a threshold value K;
3) and the uncertainty of the air compressor performance identification result is less than a threshold value L.
10. The air compressor performance identification and group preference joint control method according to claim 4, characterized in that:
and generating a new multi-feature signal sample library and the membership function by acquiring the vibration signals, the current signals, the acoustic emission signals and the temperature signals collected by the various sensors on the air compressor again, performing new fusion by using the fusion recognition model, updating the preferential start-stop sequence and the running time of the air compressor after acquiring a new fusion result, and dynamically adjusting the service balance degree of the air compressor group.
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