CN111428386B - Elevator traction machine rotor fault diagnosis information fusion method based on complex network - Google Patents

Elevator traction machine rotor fault diagnosis information fusion method based on complex network Download PDF

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CN111428386B
CN111428386B CN202010320015.1A CN202010320015A CN111428386B CN 111428386 B CN111428386 B CN 111428386B CN 202010320015 A CN202010320015 A CN 202010320015A CN 111428386 B CN111428386 B CN 111428386B
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徐晓滨
胡家豪
章振杰
王琪冰
茹晓英
侯平智
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Hangzhou Dianzi University
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Abstract

The invention relates to an elevator traction machine rotor fault diagnosis information fusion method based on a complex network. The correlation of the characteristic parameters is obtained by calculating the Pearson coefficients among the characteristic parameters, and the characteristic parameters are grouped according to the strength of the correlation; respectively calculating the similarity between sample data vectors according to the fault sample data of each group, and constructing a fault data complex network; acquiring a likelihood belief table and a reference center vector of each group by using a complex network community division method, and further acquiring corresponding reference evidence; and respectively activating the diagnostic evidences of each group aiming at the fault characteristic vector acquired on line, carrying out evidence fusion by using a Dempster combination rule, and making a fault decision by using the fused evidences to obtain a fault type corresponding to the on-line fault characteristic data. The invention carries out fusion reasoning of fault diagnosis evidence on the basis of a complex network and effectively improves the fault diagnosis precision of the elevator traction machine rotor by utilizing multi-source diagnosis information.

Description

Elevator traction machine rotor fault diagnosis information fusion method based on complex network
Technical Field
The invention relates to a complex network-based elevator traction machine rotor fault diagnosis information fusion method, and belongs to the technical field of elevator equipment state monitoring and fault diagnosis.
Background
The tractor is the power equipment of the elevator, is composed of a motor, a brake, a coupling, a reduction gearbox, a traction sheave, a frame and the like, and has the function of conveying and transmitting power to enable the elevator to normally run. Because the running working conditions of the elevator are complex and changeable, and uncertain factors in the installation, operation and maintenance processes are added, the traction machine serving as an elevator heart has frequent faults, the safe running of the elevator is influenced, even safety accidents are caused, and casualties and economic losses are caused. Therefore, it is imperative to monitor the state of the hoisting machine and accurately and efficiently diagnose the root cause of the failure.
The existing elevator traction machine mostly adopts a permanent magnet synchronous gearless traction machine, which comprises a machine base, a stator, a rotor body, a brake and the like, wherein the permanent magnet is fixed on the inner wall of the rotor body, the rotor body is arranged on a shaft through a key, and the shaft is arranged on a bilateral sealing deep groove ball bearing on a rear machine base and a self-aligning roller bearing on a front machine base. Identifying faults by vibration signals is a common mechanical equipment diagnosis strategy. During the operation of the traction machine, a plurality of components vibrate, and how to effectively utilize the vibration signals is the key for realizing accurate fault diagnosis. Considering the relevance and diversity among the collected vibration signal sample data, if such characteristics of the data can be deeply mined and utilized, the effectiveness of the diagnosis result must be improved.
As an emerging theoretical tool, the complex network can effectively model and analyze the incidence relation between entities (data), and provides support for solving the problem of data incidence analysis. Meanwhile, the information fusion method can properly dispose diversified data through integration of multi-source diagnosis data. Therefore, the invention provides an elevator traction machine rotor fault diagnosis information fusion method based on a complex network.
Disclosure of Invention
Aiming at the defects of the prior art, the invention provides an elevator traction machine rotor fault diagnosis information fusion method based on a complex network.
The correlation of the characteristic parameters is obtained by calculating the Pearson coefficients among the characteristic parameters, and the characteristic parameters are grouped according to the strength of the correlation; respectively calculating the similarity among sample data vectors according to the fault sample data of each group, and constructing a fault data complex network; acquiring a likelihood belief table and a reference center vector of each group by using a complex network community division method, and further acquiring corresponding reference evidence; the method comprises the steps of respectively activating diagnosis evidences of all groups aiming at fault feature vectors acquired on line, carrying out evidence fusion by using Dempster combination rules, making a fault decision by using the fused evidences, and obtaining a fault type corresponding to the on-line fault feature data.
The invention provides an elevator traction machine rotor fault diagnosis information fusion method based on a complex network, which comprises the following steps:
(1) Setting a fault set theta = { F) of an elevator tractor rotor 1 ,…,F i ,…,F N |i=1,2,…,N},F i And (3) representing the ith fault in the fault set theta, wherein N is the number of the fault modes contained in the elevator traction machine rotor.
(2) Let f 1,i ,f 2,i And f 3,i To reflect each fault F in the set of faults Θ i The characteristic parameters are acceleration signals and are respectively provided by acceleration sensors at the fan end, the motor base and the motor shell driving end;
will f is 1,i ,f 2,i ,f 3,i And F i Expressed as a set of samples M i ={[f 1,i ,f 2,i ,f 3,i F i ]|t=1,2,3,…,S i In which [ f ] 1,i (t),f 2,i (t),f 3,i (t),F i ]Is a sample vector, S i Denotes that the fault is F i Sample data in the State, and denoted F i Number of samples in state, take S i Not less than 100; respectively sampling sample data under each fault state and representing the sample data in a set form
Figure BDA0002461009260000021
The total number of delta samples can be obtained>
Figure BDA0002461009260000022
| M | represents the number in the set M.
(3) Will fail F i Sample data f acquired in state 1,i (t)、f 2,i (t) and f 3,i (t) is expressed as a sample set M i ′={[f 1,i (t),f 2,i (t),f 3,i (t)]|t=1,2,…,S i Respectively sampling sample data in each fault state, and expressing the sample data in a set form
Figure BDA0002461009260000023
Satisfy delta = | M | = | M i ′|,|M i ' | denotes the set M i ' the number of elements in the list.
(4) Carrying out correlation analysis on the sample fault characteristic parameters, and specifically calculating as follows:
Figure BDA0002461009260000024
two characteristic parameters with larger Pearson coefficients are grouped into the same group and marked as G A The characteristic parameters with less correlation are classified into another group, denoted as G B
(5) For two groups of characteristic data G obtained in the step (4) A And G B Respectively constructing data complex network Net A And Net B Described in similarity matrices A and B, a i,j ,b i,j Are elements in the matrices A and B, respectively, representing the sample x in each set of feature data i And x j Distance d between i,j Is defined as formula (2):
a i,j =exp(-15×d i,j ),b i,j =exp(-15×d i,j ) (2)
in the formula (d) i,j With the euclidean distance metric, the similarity of the sample itself is defined as 0, i.e. a when i = j i,j =0,b i,j =0。
(6) The complex network Net of data is divided by using the complex network community division principle A And Net B Is divided into K 1 And K 2 Class, is marked as
Figure BDA0002461009260000031
Grouping M sample vectors into>
Figure BDA0002461009260000032
To obtain K 1 Class-corresponding sample Q k1 ={[f 1,k1 (u k1 ),f 2,k1 (u k1 ),f 3,k1 (u k1 ),F k1 (u k1 )]|u k1 =1,2,…,U k1 },U k1 Represents T k1 Number of sample vectors in class, with Q k1 ∈M,/>
Figure BDA0002461009260000033
Figure BDA0002461009260000034
F k1 (u k1 ) E.g. theta, and can be represented by K 1 Obtaining K corresponding to the sample set M by taking the mean value of each sample-like vector 1 A reference center vector, which may be denoted as C k1 =[c k1,1 ,c k1,2 ,c k1,3 ]Where K1=1,2, …, K 1
The same can put the sample vector in M into
Figure BDA0002461009260000035
In order to obtain K 2 Class correspondence sample Q k2 ={[f 2,k2 (u k2 ),f 2,k2 (u k2 ),f 3,k2 (u k2 ),F k2 (u k2 )]|u k2 =1,2,…,U k2 },U k2 Represents T k2 Number of sample vectors in class, with Q k2 ∈M,/>
Figure BDA0002461009260000036
F k2 (u k2 ) E.g. theta, and can be represented by K 2 Obtaining K corresponding to the sample set M by taking the mean value of each sample-like vector 2 A reference center vector, which may be denoted as C k2 =[c k2,1 ,c k2,2 ,c k2,3 ]Where K2=1,2, …, K 2
(7) F obtained according to the step (2), the step (3), the step (5) and the step (6) i And T k1 、T k2 The relational table shown in Table 1 and Table 2 is constructed to show F i And T k1 、F i And T k2 The corresponding relation between the two; n is a radical of k1,i 、N k2,i Respectively represents T k1 、T k2 The sample set corresponding to the class has a fault F i In combination with
Figure BDA0002461009260000037
And &>
Figure BDA0002461009260000038
And
Figure BDA0002461009260000039
wherein N is more than or equal to 0 k1,i 、N k2,i ≤S i
TABLE 1F i And T k1 Table of corresponding relationship between
Figure BDA00024610092600000310
TABLE 2F i And T k2 Table of corresponding relationship between
Figure BDA0002461009260000041
(8) According to the corresponding relation table obtained in the step (7), when the fault is F i When the sample data is classified into the k1 and k2 likelihood functions, the likelihood functions are as follows:
Figure BDA0002461009260000042
and is provided with
Figure BDA0002461009260000043
Then the reference evidence of the i-th type fault corresponding to the k 1-th and k 2-th types can be defined as:
Figure BDA0002461009260000044
obtaining two parts of fault diagnosis reference evidence as
e p1 =[e p1,1 ,e p1,2 ,…,e p1,N ],e p2 =[e p2,1 ,e p2,2 ,…,e p2,N ] (5)
Constructing likelihood confidence tables as shown in tables 3 and 4 to describe T k1 、T k2 And F i The relationship between them.
TABLE 3T k1 Similar confidence table
Figure BDA0002461009260000045
TABLE 4T k2 Similar confidence table
Figure BDA0002461009260000046
Figure BDA0002461009260000051
(9) When the online monitoring obtains a fault characteristic parameter vector X (t) = [ f ] at t moment 1,i (t),f 2,i (t),f 3,i (t)]Thereafter, an importance weight w of the evidence is defined k Description of evidence e k Respectively solving the fault characteristic parameter vector and K according to the relative importance of the fault characteristic parameter vector and other evidences 1 、K 2 A reference central vector
Figure BDA0002461009260000056
Euclidean distance between them and normalizing them to obtain Dis k1 And Dis k2 The calculation is as follows:
Figure BDA0002461009260000052
definition of w k1 =Dis k1 ,w k2 =Dis k2
(10) Using importance weights w of evidence k To activate the reference evidence e p The calculation is as follows:
e p_1 =w k1 *e p1 =[e p1,1 ′,e p1,2 ′,…,e p1,N ′],
e p_2 =w k2 *e p2 =[e p2,1 ′,e p2,2 ′,…,e p2,N ′] (7)
e is to be p_1 、e p_2 Respectively carrying out normalization to obtain diagnosis evidence e p1 ′、e p2 ′。
(11) Using Dempster combination rule pair e p1 ′、e p2 ' fusion is performed, and the fused diagnosis results are:
Figure BDA0002461009260000053
in the formula m 1 、m 2 Let reference evidence m for two quality functions defined on Θ 1 =e p1 ′,m 2 =e p2 ' definition
Figure BDA0002461009260000054
Is a combined quality function>
Figure BDA0002461009260000055
Indicating that Dempster combination rules can act on two or more quality functions, and A, B, C are all fault type modes;
the diagnostic evidence after fusion was:
e p =[m(1),m(2),…,m(N)] (9)
in the formula, m (1), m (2) and m (N) respectively represent the fault types which are normalized after fusion and are F 1 、F 2 、F N And (5) reliability.
(12) Using the diagnostic evidence e obtained in step (11) p And diagnosing the fault of the elevator traction machine rotor: e.g. of the type p F corresponding to the maximum confidence value i Is a faultThe characteristic parameter vector X (t) is the actual occurring failure mode.
In conclusion, the method comprises the steps of firstly determining a fault set and fault characteristic parameters of an elevator tractor rotor, and respectively sampling sample data in each fault state to obtain a fault characteristic data sample set; the correlation of the characteristic parameters is obtained by calculating Pearson coefficients among the characteristic parameters, and the characteristic parameters are grouped according to the strength of the correlation; respectively calculating the similarity between sample data vectors according to the fault sample data of each group, and constructing a fault data complex network; acquiring likelihood credibility tables and reference center vectors of all groups by using a complex network community division method, and further acquiring corresponding reference evidences; and respectively activating the diagnostic evidences of each group aiming at the fault characteristic vector acquired on line, carrying out evidence fusion by using a Dempster combination rule, and making a fault decision by using the fused evidences to obtain a fault type corresponding to the on-line fault characteristic data. The program (compiling environment Matlab) compiled by the method can run on a monitoring computer, and is combined with hardware such as a sensor, a data collector and the like to form an online monitoring system for carrying out real-time monitoring and fault diagnosis on the rotor state of the elevator traction machine.
The invention has the beneficial effects that: 1. grouping the characteristic data by calculating a Pearson coefficient, so that the constructed complex network community is more accurate; 2. the acquired reference center point is more accurate by using complex network community division, so that the acquisition of the reference evidence is more convenient and faster; 3. and defining the Euclidean distance from the sample vector to the community center as the evidence weight, thereby solving the defect of manually setting the evidence weight in the prior art.
Drawings
FIG. 1 is a block flow diagram of the method of the present invention.
Fig. 2 is a diagram of an elevator machine rotor fault diagnostic system.
Fig. 3 is a block diagram of an elevator traction machine rotor fault diagnosis system in an example of the method of the present invention.
Detailed Description
The invention relates to an elevator traction machine rotor fault diagnosis information fusion method based on a complex network, the flow chart of which is shown in figure 1, and the method comprises the following steps:
(1) Setting a fault set theta = { F) of an elevator traction machine rotor 1 ,…,F i ,…,F N |i=1,2,…,N},F i And (3) representing the ith fault in the fault set theta, wherein N is the number of the fault modes contained in the elevator traction machine rotor.
(2) Let f 1,i ,f 2,i And f 3,i To be able to reflect each fault F in the set of faults Θ i The characteristic parameter is an acceleration signal, and the acceleration signals are respectively provided by acceleration sensors at the fan end, the motor base and the motor shell driving end, and f is measured by a sensor 1,i ,f 2,i ,f 3,i And F i Expressed as a set of samples M i ={[f 1,i ,f 2,i ,f 3,i F i ]|t=1,2,3,…,S i In which [ f) 1,i (t),f 2,i (t),f 3,i (t),F i ]Is a sample vector, S i Indicates that the fault is F i Sample data in the State, and denoted F i Number of samples in state, take S i Not less than 100; respectively sampling sample data under each fault state and representing the sample data in a set form
Figure BDA0002461009260000071
The total number of delta samples can be obtained>
Figure BDA0002461009260000072
| M | represents the number in the set M.
(3) Will fail F i Sample data f acquired in state 1,i (t)、f 2,i (t) and f 3,i (t) is expressed as a sample set M i ′={[f 1,i (t),f 2,i (t),f 3,i (t)]|t=1,2,…,S i And respectively sampling sample data in each fault state, and representing the sample data in a set form
Figure BDA0002461009260000073
Satisfy delta = | M | = | M i ′|,|M i ' | denotes the set M i ' number of elements in.
(4) Carrying out correlation analysis on the sample fault characteristic parameters, and specifically calculating as follows:
Figure BDA0002461009260000074
two characteristic parameters with larger Pearson coefficients are classified into the same group and marked as G A The characteristic parameters with less correlation are classified into another group, which is marked as G B
(5) For two groups of characteristic data G obtained in the step (4) A And G B Respectively constructing data complex network Net A And Net B Described in similarity matrices A and B, a i,j ,b i,j Are elements in the matrices A and B, respectively, representing the sample x in each set of feature data i And x j Distance d between i,j Is defined as formula (2):
a i,j =exp(-15×d i,j ),b i,j =exp(-15×d i,j ) (2)
in the formula (d) i,j With the euclidean distance metric, the similarity of the sample itself is defined as 0, i.e. a when i = j i,j =0,b i,j =0。
(6) The complex network Net of data is divided by using the complex network community division principle A And Net B Is divided into K 1 And K 2 Class, is marked as
Figure BDA0002461009260000075
Grouping M sample vectors into `>
Figure BDA0002461009260000076
To obtain K 1 Class-corresponding sample Q k1 ={[f 1,k1 (u k1 ),f 2,k1 (u k1 ),f 3,k1 (u k1 ),F k1 (u k1 )]|u k1 =1,2,…,U k1 },U k1 Represents T k1 Number of sample vectors in class, with Q k1 ∈M,/>
Figure BDA0002461009260000077
Figure BDA0002461009260000078
F k1 (u k1 ) E.g. theta, and can be represented by K 1 Obtaining K corresponding to the sample set M by taking the mean value of each sample-like vector 1 A reference center vector, which may be denoted as C k1 =[c k1,1 ,c k1,2 ,c k1,3 ]Where K1=1,2, …, K 1
The same can put the sample vector in M into
Figure BDA0002461009260000079
In order to obtain K 2 Class-corresponding sample Q k2 ={[f 2,k2 (u k2 ),f 2,k2 (u k2 ),f 3,k2 (u k2 ),F k2 (u k2 )]|u k2 =1,2,…,U k2 },U k2 Represents T k2 Number of sample vectors in class, with Q k2 ∈M,/>
Figure BDA00024610092600000710
F k2 (u k2 ) E.g. theta, and can be represented by K 2 Obtaining K corresponding to the sample set M by averaging the class sample vectors 2 A reference center vector, which may be denoted as C k2 =[c k2,1 ,c k2,2 ,c k2,3 ]Wherein K2=1,2, …, K 2
(7) F obtained according to the step (2), the step (3), the step (5) and the step (6) i And T k1 、T k2 The relational table shown in Table 1 and Table 2 is constructed to show F i And T k1 、F i And T k2 The corresponding relation between the two; n is a radical of k1,i 、N k2,i Respectively represents T k1 、T k2 The sample set corresponding to the class has a fault F i In combination with
Figure BDA0002461009260000081
And &>
Figure BDA0002461009260000082
And
Figure BDA0002461009260000083
wherein N is more than or equal to 0 k1,i 、N k2,i ≤S i
TABLE 1F i And T k1 Table of corresponding relationship between
Figure BDA0002461009260000084
TABLE 2F i And T k2 Table of corresponding relationship between
Figure BDA0002461009260000085
For the convenience of understanding the correspondence table shown in table 1 and table 2, this is exemplified here. The elevator traction machine rotor shown in fig. 2 has N =3 failure modes F i : eccentric F of tractor rotor 1 Imbalance of the rotor of the traction machine F 2 Loosening of parts of tractor rotor F 3 Then the fault set Θ = { F 1 ,F 2 ,F 3 Their common characteristic parameter f 1,i ,f 2,i And f 3,i And vibration signals are provided for acceleration sensors mounted at the fan end, the motor base and the motor housing drive end. Get S 1 =600,S 2 =300,S 3 =120, sample data in each fault state is acquired through step (2), δ =1020 sample data are sampled in total, and f can be calculated through step (3) and step (4) 1 、f 2 、f 3 Has a Pearson coefficient of r (f) 1 ,f 2 )=0.0202,r(f 1 ,f 3 )=-0.0907,r(f 2 ,f 3 ) = -0.1092, knows that f 2 And f 3 Has strong correlation, can convert f 2 、f 3 Composition feature data G A ,f 1 Is another set of characteristic data G B Obtaining Net through the calculation of the step (5) A And Net B Net is performed by the step (6) A Is divided into 4 communities with the community center of C 11 =[0.0162,-0.115,0.0023],C 12 =[-0.0256,0.0196,0.064],C 13 =[0.0129,0.1764,-0.0044],C 14 =[-0.0191,0.0358,-0.0324]The samples in M are classified as T in Table 1 in step (6) 1 、T 2 、T 3 、T 4 Will Net B Is divided into 6 communities with the community center of C 21 =[-0.0272,-0.0407,0.002],C 22 =[-0.0695,0.0028,0.006],C 23 =[0.0542,0.0286,0.008],C 24 =[1.6053,0.0178,0.031],C 25 =[-0.2823,0.0438,0.0023],C 26 =[-0.6934,0.0225,0.0119]The samples in M are classified as T in Table 2 in step (6) 1 、T 2 、T 3 、T 4 、T 5 、T 6 As follows:
TABLE 3F i And T k1 Table of corresponding relationship between
Figure BDA0002461009260000091
TABLE 4F i And T k2 Table of corresponding relationship between
Figure BDA0002461009260000092
(8) According to the corresponding relation table obtained in the step (7), when the fault is F i When the sample data is classified into the k1 and k2 likelihood functions, the likelihood functions are as follows:
Figure BDA0002461009260000093
and is provided with
Figure BDA0002461009260000094
Then the reference evidence of the i-th type fault corresponding to the k 1-th and k 2-th types can be defined as:
Figure BDA0002461009260000095
obtaining two parts of fault diagnosis reference evidence as
e p1 =[e p1,1 ,e p1,2 ,…,e p1,N ],e p2 =[e p2,1 ,e p2,2 ,…,e p2,N ] (5)
Constructing likelihood confidence tables as shown in tables 3 and 4 to describe T k1 、T k2 And F i The relationship between them.
TABLE 5T k1 Similar confidence table
Figure BDA0002461009260000101
TABLE 6T k2 Similar confidence table
Figure BDA0002461009260000102
For the convenience of understanding the correspondence table shown in table 5 and table 6, this example is given here. According to the corresponding relation table obtained in the step (7), when the fault state is F, the corresponding relation table is obtained through the formula (4) in the step (8) i Hour is put into T in Table 5 1 、T 2 、T 3 、T 4 Likelihood function value of class
Figure BDA0002461009260000103
Figure BDA0002461009260000104
Figure BDA0002461009260000105
T in Table 6 1 、T 2 、T 3 、T 4 、T 5 、T 6 Likelihood function values of class are
Figure BDA0002461009260000106
Figure BDA0002461009260000107
Figure BDA0002461009260000108
Obtaining the fault F from the formula (4) in the step (8) 1 Evidence e p1,1 =[0.331,0.167,0.361,0.141] T ,e p2,1 =[0.223,0.31,0.257,0,0.2083,0.0017] T Similarly, F can be obtained 2 、F 3 Corresponding fault reference evidence e p1,2 =[0.397,0.113,0.383,0.107] T ,e p1,3 =[0.283,0.192,0.442,0.083] T ,e p2,2 =[0.17,0.283,0.153,0.007,0.32,0.067] T ,e p2,3 =[0.092,0.333,0.117,0.0167,0.283,0.158] T Meanwhile, likelihood confidence tables such as table 7 and table 8 can be constructed to describe class T k1 、T k2 And F i The relationship between:
TABLE 7T k1 Similar confidence table
Figure BDA0002461009260000111
TABLE 8T k2 Similar confidence table
Figure BDA0002461009260000112
(9) When the online monitoring obtains a fault characteristic parameter vector X (t) = [ f ] at the moment t 1,i (t),f 2,i (t),f 3,i (t)]Thereafter, an importance weight w of the evidence is defined k Description of evidence e k Respectively solving the fault characteristic parameter vector and K according to the relative importance of the fault characteristic parameter vector and other evidences 1 、K 2 A reference central vector
Figure BDA0002461009260000113
And normalizing the Euclidean distance to obtain the Dis k1 And Dis k2 CalculatingThe following were used:
Figure BDA0002461009260000114
definition of w k1 =Dis k1 ,w k2 =Dis k2
(10) Using importance weights w of evidence k To activate the reference evidence e p The calculation is as follows:
Figure BDA0002461009260000115
e is to be p_1 、e p_2 Respectively carrying out normalization to obtain diagnosis evidence e p1 ′、e p2 ′。
(11) Combining rule pairs e by Dempster p1 ′、e p2 ' fusion is performed, and the fused diagnosis results are:
Figure BDA0002461009260000121
in the formula m 1 、m 2 Let reference evidence m for two quality functions defined on Θ 1 =e p1 ′,m 2 =e p2 ' definition
Figure BDA0002461009260000122
Is a combined quality function>
Figure BDA0002461009260000123
Indicating that Dempster combination rules can act on two or more quality functions, and A, B, C are fault type modes;
the diagnostic evidence after fusion is:
e p =[m(1),m(2),…,m(N)] (9)
in the formula, m (1), m (2) and m (N) respectively represent the fault type F subjected to normalization after fusion 1 、F 2 、F N And (7) reliability.
(12) Using the diagnostic evidence e obtained in step (11) p And diagnosing the fault of the elevator traction machine rotor: e.g. of the type p F corresponding to the maximum confidence value i Namely the fault mode of the real fault characteristic parameter vector X (t).
In order to deepen the importance weight w corresponding to the sample vector X (t) k The understanding of (1) is that the fault characteristic parameter vector X (t) = [0.0421,0.1695, -0.0864 at the moment of online acquisition t =1]Substituting the obtained data into formula (6) in step (9) to obtain fault characteristic vectors X (t) and K at the time t =1 1 、K 2 The Euclidean distance between the central vectors is normalized to obtain the importance weight w k1 =[0.2045,0.1139,0.2911,0.3905],w k2 =[0.2345,0.0884,0.4876,0.0527,0.0835,0.053]Obtaining the reference evidence e after activation through formula (7) in the step (10) p_1 ′=[0.2471,0.2473,0.2409],e p_2 ′=[0.2225,0.1704,0.1409]. Normalized to obtain e p1 ′=[0.3362,0.3369,0.3269],e p2 ′=[0.4168,0,3192,0.264]. E obtained in step (10) p1 ' and e p2 ' substitution of equation (8) into step (11) yields fused diagnostic evidence e p =[0.4155,0.3230,0.2615]And diagnosing the fault of the elevator traction machine rotor: e.g. of a cylinder p F corresponding to m (1) with maximum confidence coefficient value 1 Namely the fault mode of the fault characteristic parameter vector X (t) which really occurs.
The embodiments of the present invention will be described in detail below with reference to the accompanying drawings:
the flow chart of the method of the invention is shown in figure 1, and the core part is as follows: calculating Pearson coefficients of the characteristic parameters to obtain the correlation of the characteristic parameters, and grouping the characteristic parameters according to the strength of the correlation; respectively calculating the similarity between sample data vectors according to the fault sample data of each group, and constructing a fault data complex network; acquiring a likelihood belief table and a reference center vector of each group by using a complex network community division method, and further acquiring corresponding reference evidence; and respectively activating the diagnostic evidence of each group aiming at the online acquired fault feature vector, carrying out evidence fusion by using a Dempster combination rule, and making a fault decision by using the fused evidence to obtain a fault type corresponding to the online fault feature data.
The steps of the method of the present invention will be described in detail below with reference to the preferred embodiment of the elevator machine rotor fault diagnosis system of fig. 2.
1. Example of setting up simulation experiment table of elevator traction device
As shown in the structure diagram of the elevator traction machine rotor fault diagnosis system in fig. 3, the vibration acceleration sensors are respectively installed at the drive end of the motor shell, the fan end and the motor base to collect vibration signals, the vibration signals collected by the three sensors are transmitted to the HG-8902 data collection box, processed by the signal conditioning circuit, and finally output to the monitoring computer through the a/D converter, and then the elevator traction machine rotor time domain vibration acceleration signals are obtained as fault characteristic signals by using HG-8902 data analysis software in the Labview environment.
2. Elevator traction machine rotor fault setting and fault characteristic parameter selection
According to the specific characteristics of the experiment table, 3 typical failure modes are respectively set on the experiment table: the tractor rotor is eccentric, the tractor rotor is unbalanced, and the tractor rotor part is not hard up. And collecting vibration signals as fault characteristic parameters by mounting the vibration signals at a motor shell driving end, a fan end and a motor base.
3. Correlation analysis, complex network community division and corresponding relation table construction
Get S 1 =600,S 2 =300,S 3 =120, sample data in each fault state is acquired through step (2), δ =1020 sample data are sampled in total, and f can be calculated through step (3) and step (4) 1 、f 2 、f 3 Has a Pearson coefficient of r (f) 1 ,f 2 )=0.0202,r(f 1 ,f 3 )=-0.0907,r(f 2 ,f 3 ) = -0.1092, see f 2 And f 3 Has strong correlation, can convert f 2 、f 3 Composition feature data G A ,f 1 Is the characteristic data G B Calculating to obtain Net through the step (5) A And Net B Through the step (6) willNet A Divided into 4 communities, community center C 11 =[0.0162-0.115,0.0023],C 12 =[-0.0256,0.0196,0.064],C 13 =[0.0129,0.1764,-0.0044],C 14 =[-0.0191,0.0358,-0.0324]. The samples in M are classified into T in Table 1 in step (6) in the same way 1 、T 2 、T 3 、T 4 Will Net B Is divided into 6 communities with the community center of C 21 =[-0.0272,-0.0407,0.002],C 22 =[-0.0695,0.0028,0.006],C 23 =[0.0542,0.0286,0.008],C 24 =[1.6053,0.0178,0.031],C 25 =[-0.2823,0.0438,0.0023],C 26 =[-0.6934,0.0225,0.0119]The samples in M are classified as T in Table 2 in step (6) 1 、T 2 、T 3 、T 4 、T 5 、T 6
As follows:
TABLE 9F i And T k1 Table of corresponding relationship between
Figure BDA0002461009260000141
TABLE 10F i And T k2 Table of corresponding relationship between
Figure BDA0002461009260000142
5. Constructing a likelihood belief table and obtaining diagnostic evidence
According to the corresponding relation table obtained in the step (7), when the fault state is F, the formula (4) in the step (8) can obtain i Time is put in Table 5 1 、T 2 、T 3 、T 4 Likelihood function values of class are
Figure BDA0002461009260000143
Figure BDA0002461009260000144
Figure BDA0002461009260000145
T in Table 6 1 、T 2 、T 3 、T 4 、T 5 、T 6 The likelihood function value of a class is->
Figure BDA0002461009260000146
Figure BDA0002461009260000147
Figure BDA0002461009260000148
Figure BDA0002461009260000149
Obtaining corresponding F from the formula (4) in the step (8) 1 Reference evidence of failure e p1,1 =[0.331,0.167,0.361,0.141] T ,e p2,1 =[0.223,0.31,0.257,0,0.2083,0.0017] T Similarly, F can be obtained 2 、F 3 Corresponding fault reference evidence e p1,2 =[0.397,0.113,0.383,0.107] T ,e p1,3 =[0.0.283,0.192,0.442,0.083] T ,e p2,2 =[0.17,0.283,0.153,0.007,0.32,0.067] T ,e p2,3 =[0.092,0.333,0.117,0.0167,0.283,0.158] T Meanwhile, likelihood confidence tables such as table 7 and table 8 can be constructed to describe class T k1 、T k2 And F i The relationship between:
TABLE 11T k1 Similar confidence table
Figure BDA0002461009260000151
TABLE 12T k2 Similar confidence table
Figure BDA0002461009260000152
Acquiring a fault characteristic parameter vector X (t) = [0.0421,0.1695 ] at the moment t =1 online,-0.0864]Substituting the above into formula (6) in step (8) to obtain fault feature vectors X (t) and K at time t =1 1 、K 2 The Euclidean distance between the central vectors is normalized to obtain the importance weight
w k1 =[0.2045,0.1139,0.2911,0.3905],
w k2 =[0.2345,0.0884,0.4876,0.0527,0.0838,0.0530],
Obtaining the activated reference evidence through the formula (7) in the step (9)
Figure BDA0002461009260000153
Figure BDA0002461009260000154
Normalized to obtain e p1 ′=[0.3362,0.3369,0.3269],e p2 ′=[0.4168,0,3192,0.264]。
6. Fault diagnosis
E obtained in step (10) p1 ' and e p2 ' substitution of equation (8) into step (11) yields fused diagnostic evidence e p =[0.4155,0.3230,0.2615]And diagnosing the fault of the elevator traction machine rotor: e.g. of a cylinder p F corresponding to m (1) with maximum confidence value 1 The fault mode of the fault characteristic parameter vector X (t) is consistent with the real fault mode set by the collected fault characteristic parameter vector, and the decision result is correct.

Claims (3)

1. The elevator traction machine rotor fault diagnosis information fusion method based on the complex network is characterized by comprising the following steps:
(1) Setting a fault set theta = { F) of an elevator traction machine rotor 1 ,…,F i ,…,F N |i=1,2,…,N},F i The ith fault in the fault set theta is represented, and N is the number of fault modes contained in the elevator tractor rotor;
(2) Let f 1,i ,f 2,i And f 3,i To be able to reflect each fault F in the set of faults Θ i The characteristic parameter is accelerationSignals are provided by acceleration sensors at a fan end, a motor base and a motor shell driving end respectively;
will f is 1,i ,f 2,i ,f 3,i And F i Expressed as a set of samples M i ={[f 1,i ,f 2,i ,f 3,i F i ]|t=1,2,3,…,S i In which [ f) 1,i (t),f 2,i (t),f 3,i (t),F i ]Is a sample vector, S i Indicates that the fault is F i Sample data in the State, and denoted F i Sampling number in the state, taking S i Not less than 100; respectively sampling sample data under each fault state and representing the sample data in a set form
Figure FDA0002461009250000011
The total number of delta samples can be obtained>
Figure FDA0002461009250000012
| M | represents the number in the set M;
(3) Will fail F i F obtained under the state 1,i (t)、f 2,i (t) and f 3,i (t) is expressed as a sample set M i ′={[f 1,i (t),f 2,i (t),f 3,i (t)]|t=1,2,…,S i And respectively sampling sample data in each fault state, and representing the sample data in a set form
Figure FDA0002461009250000013
Satisfy delta = | M | = | M i ′|,|M i ' | denotes the set M i ' number of elements in;
(4) Carrying out correlation analysis on the sample fault characteristic parameters to obtain a Pearson coefficient; two characteristic parameters with larger Pearson coefficients are grouped into the same group and marked as G A The characteristic parameters with less correlation are classified into another group, which is marked as G B
(5) For two groups of characteristic data G obtained in the step (4) A And G B Respectively constructing data complex network Net A And Net B Described in similarity matrices A and B, a i,j ,b i,j Are elements in the matrices A and B, respectively, representing the sample x in each set of feature data i And x j Distance d between i,j A function of (a);
(6) The complex network Net of data is divided by using the complex network community division principle A And Net B Is divided into K 1 And K 2 Class, is marked as
Figure FDA0002461009250000014
Grouping M sample vectors into>
Figure FDA0002461009250000015
To obtain K 1 Class correspondence sample Q k1 ={[f 1,k1 (u k1 ),f 2,k1 (u k1 ),f 3,k1 (u k1 ),F k1 (u k1 )]|u k1 =1,2,…,U k1 },U k1 Represents T k1 Number of sample vectors in class, with Q k1 ∈M,/>
Figure FDA0002461009250000016
Figure FDA0002461009250000017
F k1 (u k1 ) E.g. theta, and can be represented by K 1 Obtaining K corresponding to the sample set M by taking the mean value of each sample-like vector 1 A reference center vector, which may be denoted as C k1 =[c k1,1 ,c k1,2 ,c k1,3 ]Wherein K1=1,2, …, K 1
The same can put the sample vector in M into
Figure FDA0002461009250000021
In (b) to obtain K 2 Class correspondence sample Q k2 ={[f 2,k2 (u k2 ),f 2,k2 (u k2 ),f 3,k2 (u k2 ),F k2 (u k2 )]|u k2 =1,2,…,U k2 },U k2 Represents T k2 Number of sample vectors in class, with Q k2 ∈M,/>
Figure FDA0002461009250000022
F k2 (u k2 ) E.g. theta, and can be represented by K 2 Obtaining K corresponding to the sample set M by averaging the class sample vectors 2 A reference center vector, which may be denoted as C k2 =[c k2,1 ,c k2,2 ,c k2,3 ]Wherein K2=1,2, …, K 2
(7) F obtained according to the step (2), the step (3), the step (5) and the step (6) i And T k1 、T k2 The relational table shown in Table 1 and Table 2 is constructed to show F i And T k1 、F i And T k2 The corresponding relation between the two; n is a radical of k1,i 、N k2,i Respectively represents T k1 、T k2 The failure in the sample set corresponding to the class is F i In combination with
Figure FDA0002461009250000023
And &>
Figure FDA0002461009250000024
And &>
Figure FDA0002461009250000025
Wherein N is more than or equal to 0 k1,i 、N k2,i ≤S i
TABLE 1F i And T k1 Table of corresponding relationship between
Figure FDA0002461009250000026
TABLE 2F i And T k2 Table of corresponding relationship between
Figure FDA0002461009250000027
(8) According to the corresponding relation table obtained in the step (7), when the fault is F i When the sample data is classified into the k1 and k2 likelihood functions, the likelihood functions are as follows:
Figure FDA0002461009250000031
and is provided with
Figure FDA0002461009250000032
Defining the reference evidence of the ith type fault corresponding to the kth 1 and the kth 2 as follows:
Figure FDA0002461009250000033
obtaining two parts of fault diagnosis reference evidence as
e p1 =[e p1,1 ,e p1,2 ,…,e p1,N ],e p2 =[e p2,1 ,e p2,2 ,…,e p2,N ]
Constructing likelihood confidence tables as shown in tables 3 and 4 to describe T k1 、T k2 And F i The relationship between;
TABLE 3T k1 Similar confidence table
Figure FDA0002461009250000034
TABLE 4T k2 Similar confidence table
Figure FDA0002461009250000035
(9) When the online monitoring obtains a fault characteristic parameter vector X (t) = [ f ] at t moment 1,i (t),f 2,i (t),f 3,i (t)]Thereafter, an importance weight w of the evidence is defined k Description of evidence e k Respectively obtaining the fault characteristic parameter vector and K compared with the relative importance of other evidences 1 、K 2 A reference center vector
Figure FDA0002461009250000036
And normalizing the Euclidean distance to obtain the Dis k1 And Dis k2 Definition of w k1 =Dis k1 ,w k2 =Dis k2
(10) Using importance weights w of evidence k To activate the reference evidence e p To obtain e p_1 、e p_2 A 1, e p_1 、e p_2 Respectively carrying out normalization to obtain diagnosis evidence e p1 ′、e p2 ′;
(11) Combining rule pairs e by Dempster p1 ′、e p2 ' performing fusion to obtain fused diagnosis results as follows:
Figure FDA0002461009250000041
in the formula m 1 、m 2 Let reference evidence m for two quality functions defined on Θ 1 =e p1 ′,m 2 =e p2 Definition m = m 1 ⊕m 2 For the combined quality function, the speed indicates that the Dempster combination rule can act on two or more quality functions, and A, B, C is a fault type mode;
the diagnostic evidence after fusion was:
e p =[m(1),m(2),…,m(N)] (9)
in the formula, m (1), m (2) and m (N) respectively represent the fault type F subjected to normalization after fusion 1 、F 2 、F N Reliability;
(12) Using the diagnostic evidence e obtained in step (11) p And diagnosing the fault of the elevator traction machine rotor: e.g. of the type p F corresponding to the maximum confidence value i Namely the fault mode of the real fault characteristic parameter vector X (t).
2. The elevator traction machine rotor fault diagnosis information fusion method based on the complex network as claimed in claim 1, characterized in that: in step (5), a i,j ,b i,j The definition is as follows:
a i,j =exp(-15×d i,j ),b i,j =exp(-15×d i,j )
in the formula (d) i,j With the euclidean distance metric, the similarity of the sample itself is defined as 0, i.e. a when i = j i,j =0,b i,j =0。
3. The complex network-based elevator traction machine rotor fault diagnosis information fusion method according to claim 1, characterized in that: step (10) of e p_1 、e p_2 Is calculated as follows:
e p_1 =w k1 *e p1 =[e p1,1 ′,e p1,2 ′,…,e p1,N ′],
e p_2 =w k2 *e p2 =[e p2,1 ′,e p2,2 ′,…,e p2,N ′]。
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Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014123443A1 (en) * 2013-02-06 2014-08-14 Ivanov Alexandr Vladimirovich Method and device for vibration diagnosis and forecasting sudden engine failure
CN108069308A (en) * 2017-12-05 2018-05-25 暨南大学 A kind of electric staircase failure diagnosis method based on sequential probability
CN110196165A (en) * 2019-04-29 2019-09-03 杭州电子科技大学 A kind of rotating machinery ball bearing method for diagnosing faults based on K-means cluster and evidential reasoning

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100049343A1 (en) * 2008-08-25 2010-02-25 International Business Machines Corporation Non-intrusive acoustic monitoring for equipment diagnostic and fault reporting

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014123443A1 (en) * 2013-02-06 2014-08-14 Ivanov Alexandr Vladimirovich Method and device for vibration diagnosis and forecasting sudden engine failure
CN108069308A (en) * 2017-12-05 2018-05-25 暨南大学 A kind of electric staircase failure diagnosis method based on sequential probability
CN110196165A (en) * 2019-04-29 2019-09-03 杭州电子科技大学 A kind of rotating machinery ball bearing method for diagnosing faults based on K-means cluster and evidential reasoning

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
徐晓滨 ; 郑进 ; 徐冬玲 ; 杨剑波 ; .基于证据推理规则的信息融合故障诊断方法.控制理论与应用.2015,(第09期),全文. *

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