CN111397877B - Rotary machine beat vibration fault detection and diagnosis method - Google Patents

Rotary machine beat vibration fault detection and diagnosis method Download PDF

Info

Publication number
CN111397877B
CN111397877B CN202010256575.5A CN202010256575A CN111397877B CN 111397877 B CN111397877 B CN 111397877B CN 202010256575 A CN202010256575 A CN 202010256575A CN 111397877 B CN111397877 B CN 111397877B
Authority
CN
China
Prior art keywords
frequency
beat
signal
fault
beat vibration
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202010256575.5A
Other languages
Chinese (zh)
Other versions
CN111397877A (en
Inventor
瞿雷
刘金颂
焦渊
苏晓峰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xian University of Architecture and Technology
Original Assignee
Xian University of Architecture and Technology
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Xian University of Architecture and Technology filed Critical Xian University of Architecture and Technology
Priority to CN202010256575.5A priority Critical patent/CN111397877B/en
Publication of CN111397877A publication Critical patent/CN111397877A/en
Application granted granted Critical
Publication of CN111397877B publication Critical patent/CN111397877B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M13/00Testing of machine parts
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H17/00Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves, not provided for in the preceding groups
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M13/00Testing of machine parts
    • G01M13/02Gearings; Transmission mechanisms
    • G01M13/028Acoustic or vibration analysis

Abstract

A rotary machine beat vibration fault detection and diagnosis method comprises the steps of firstly, carrying out bilateral continuation preprocessing on an axis vibration displacement signal at a fault response sensitive sensing point, and decomposing a fault signal into a plurality of eigenmode functions by using a VMD (virtual machine decomposition) method, so that the mode aliasing problem existing in the existing characteristic signal extraction method is solved; then, qualitatively detecting whether the eigenmode function with the center frequency closest to the rotor power frequency is a beat vibration signal by using a oscillogram; finally, Hilbert demodulation analysis is carried out on the resolved beat vibration signals, fault characteristic information is extracted by comprehensively adopting analysis tools such as a Hilbert demodulation spectrum and an instantaneous frequency spectrum, so that accurate beat vibration fault characteristic frequency is obtained, and the problem that the beat vibration fault characteristic frequency cannot be effectively identified due to too low frequency resolution is solved; the method well makes up the defects of detecting and diagnosing the beat vibration fault of the rotary machine by traditional methods such as a oscillogram, a spectrogram and the like, and is favorable for improving the accuracy of fault diagnosis.

Description

Rotary machine beat vibration fault detection and diagnosis method
Technical Field
The invention belongs to the technical field of mechanical fault diagnosis, and particularly relates to a method for detecting and diagnosing a beat vibration fault of a rotary machine.
Background
The beat vibration fault is a special phenomenon in the rotating machinery, and is mainly characterized in that the envelope amplitude of the vibration waveform of the rotor slowly changes periodically along with time. In the rotating machinery equipment, when the frequency of a certain excitation component is close to the power frequency of the rotor, no matter whether the frequency is greater than or less than the power frequency, the beat phenomenon of the rotor can be caused, and therefore the beat phenomenon is easily induced. For example, in a dual-rotor aircraft engine, the inner and outer rotors often have different operating speeds, and when the rotating speeds of the two rotors are relatively close to each other, the engine may generate beat vibration; in a rotor system supported by a magnetic suspension bearing, if the rotating speed of a main shaft is closer to the frequency of a frequency converter or the natural frequency of the rotor system, the beat vibration phenomenon of the main shaft can be caused; in a common industrial turbine device such as a steam turbine and a compressor, the loosening of a rotating part of a rotor, fluid excitation and the like often induce such a failure. This unstable vibration behavior is extremely harmful to the healthy and smooth operation of the equipment, often resulting in equipment downtime and shortened equipment service life. During the operation of the equipment, it is necessary to monitor the vibration characteristics of the rotor in real time so as to detect and early warn the beat vibration fault symptoms of the rotor at an early stage.
At present, the common tools for detecting the rotor beat vibration phenomenon mainly include time domain oscillogram and frequency spectrogram. Although they can help to some extent identify rotor beat faults, they all have their own drawbacks. As in the time domain oscillogram, the characteristics of the beat signal are often overwhelmed by the rotor subharmonics, higher harmonics, and noise signals, and it is difficult for the diagnostic engineer to directly observe the characteristics of the beat signal from the time domain oscillogram. Although some adaptive signal decomposition methods such as EMD and EEMD can extract a plurality of eigenmode functions from the original signal, because they all have mode aliasing phenomena of different degrees, the beat signal is difficult to be extracted independently and completely as a single component. In addition, the observation of the beat phenomenon by the waveform alone is not sufficient to fully diagnose the root cause of the fault, and the beat fault signature frequency needs to be determined. In the process of spectrum analysis, when the sampling frequency is too large or the number of sampling points is too small, the frequency resolution is easily too low, two component components of the beat signal cannot be effectively separated in a spectrogram, and a diagnostic engineer may often mistake the beat signal as a characteristic component, thereby causing misdiagnosis or missed diagnosis. Therefore, how to more effectively detect and identify the beat vibration fault of the rotor is an urgent problem to be solved for improving the fault diagnosis efficiency and accuracy of the rotating machinery.
Disclosure of Invention
In order to overcome the defects of the prior art, the invention aims to provide a beat vibration fault detection and diagnosis method for a rotary machine, which can effectively separate and detect beat vibration fault signals from original vibration displacement signals of a rotor, eliminate the interference of harmonic waves and noise signals and accurately identify the beat vibration fault characteristic frequency.
In order to achieve the purpose, the invention adopts the technical scheme that:
a beat vibration fault detection and diagnosis method for a rotary machine comprises the following steps:
1) selecting a rotor shaft vibration displacement signal x (t) at a fault response sensitive sensing point as an analysis object, and performing bilateral continuation preprocessing on the signal x (t);
2) decomposing the signal x (t) after the bilateral continuation preprocessing in the step 1) by using a VMD (spatial Mode decomposition) method to obtain a plurality of eigenmode functions u (t) corresponding to the signal x (t)k(t) and its center frequency fkK is 1,2, …, N denotes the number of eigenmode functions;
3) from the plurality of eigenmode functions u of step 2)k(t) selecting an eigenmode function with the center frequency closest to the rotor power frequency omega, and marking the eigenmode function as uj(t); observe uj(T) if the waveform envelope amplitude has a periodic variation rule and the variation period T isbIf u is more than or equal to 4/omega, then u is judgedj(t) continuing to execute step 4 for the beat vibration signal; otherwise, u is determinedj(t) if not, the beat vibration detection process is finished;
4) to beat vibration signal uj(t) performing spectral analysis, calculating the frequency resolution Δ f of the spectrum, and determining uj(t) waveform envelope amplitude variation frequency ωbRelation to Δ f; if ω isbU is greater than or equal to 4 delta fj(t) the spectrogram can express the beat vibration fault characteristic frequency omegafAnd the diagnosis is finished; otherwise, the beat vibration fault characteristic frequency omega is caused due to the fact that the frequency resolution is too lowfThe identification can not be effectively realized, and the step 5 needs to be continuously executed;
5) to beat vibration signal uj(t) carrying out Hilbert transformation to obtain a corresponding analytic signal, and then obtaining a Hilbert demodulation spectrum and an instantaneous frequency spectrum of the analytic signal; according to beat vibration signal uj(t) analyzing the characteristic frequency omega of beat vibration fault by the characteristics of Hilbert demodulation spectrum and instantaneous frequency spectrumfRelation with power frequency omega to obtain omegafThe exact value of (c).
The measurement mode of the rotor shaft vibration displacement signal in the step 1) is non-contact measurement, and the continuation preprocessing of the signal adopts a support vector machine method.
The VMD method in the step 2) needs to preset an eigenmode function u when being executedkThe number N of (t) is determined according to the spectrogram characteristics of the signal x (t).
The beat vibration signal u in the step 5)j(t) the frequency corresponding to the dominant component in the Hilbert demodulation spectrum is the frequency omega of the change of the waveform envelope amplitudebThe frequency is a beat signal ujThe difference in frequency between the two component components in (t), i.e. ωb=|ω-ωf|;uj(t) the instantaneous frequency exhibits a periodic variation, under the condition that the power frequency component is the dominant component, if uj(t) when the maximum value of the instantaneous frequency of the sensor occurs at the beat valley and the minimum value of the instantaneous frequency of the sensor occurs at the beat peak, the beat vibration fault characteristic frequency omegaf<Omega; if u isj(t) when the maximum value of the instantaneous frequency appears at the beat peak and the minimum value appears at the beat valley, the beat vibration fault characteristic frequency omegaf>Omega; the beat signal ujAnd (t) providing a judgment basis for determining the beat vibration fault characteristic frequency by virtue of the characteristics of the Hilbert demodulation spectrum and the instantaneous frequency change.
The invention has the beneficial effects that:
according to the method, firstly, the VMD is utilized to decompose an original vibration signal into a plurality of eigenmode functions, so that the mode aliasing problem existing in the existing characteristic signal extraction methods such as EMD and EEMD is solved, the characteristics of the beat vibration signal can be more clearly expressed in the time domain, and the beat vibration fault can be better qualitatively detected by utilizing a oscillogram; and then Hilbert demodulation analysis is carried out on the separated beat vibration signals, and analysis tools such as Hilbert demodulation spectrums and instantaneous frequency spectrums are comprehensively utilized to extract fault information, so that the problem that the beat vibration fault characteristic frequency of the traditional spectrogram caused by too low frequency resolution cannot be effectively identified is solved.
Drawings
FIG. 1 is a flow chart of an embodiment of the present invention.
FIG. 2 is a schematic of an embodiment beat signal.
FIG. 3 is a waveform diagram of the simulation signal x (t) in the embodiment; the graph (b) is a spectrum diagram of the simulation signal x (t) in the embodiment.
FIG. 4 is a diagram of the VMD effect of the simulation signal x (t) in the embodiment.
FIG. 5 shows eigenmode function u in an example1Spectrum diagram of (a).
FIG. 6 is an example eigenmode function u1Hilbert demodulation spectrum of (1).
FIG. 7 shows eigenmode function u in an example1Hilbert instantaneous frequency spectrum.
Detailed Description
The invention is explained in more detail below with reference to the figures and examples.
In the embodiment, the effectiveness of the invention is verified by simulating the shaft vibration displacement simulation signal of the rotor beat vibration fault, the expression of the simulation signal is shown as the formula (1), and the simulation signal consists of a component x1(t)、x2(t)、x3(t), n (t), wherein: x is the number of1(t) represents the subsynchronous component of the rotor at a frequency of 15 Hz; x is the number of2(t) simulating a beat signal, as shown in FIG. 2, which is obtained by superimposing two vibration components, the first component being a vibration signal at 50Hz of power frequency ω, the second component being a vibration signal at 50Hz of power frequency ωThe component being the frequency omegafA fault signal of 48 Hz; x is the number of3(t) represents a double harmonic component of power frequency; n (t) represents a random noise interference signal with a standard deviation of 2;
x(t)=x1(t)+x2(t)+x3(t)+n(t) (1)
wherein:
Figure BDA0002437564860000031
the simulation signal is subjected to discrete sampling, the sampling frequency of the simulation signal is set to be 1024Hz, the sampling time length of the simulation signal is set to be 1s, the waveform and the frequency spectrum of the simulation signal are shown in figure 3, and in a waveform diagram (a), due to the interference of noise and other harmonic components, an obvious beat vibration phenomenon is difficult to observe directly from a time domain waveform; whereas in spectrogram (b), the frequency resolution of the spectrogram is only 1Hz due to the limited number of sampled data points. The frequency of the fault component in the simulation signal is 48Hz, the frequency of the power frequency component is 50Hz, and the frequency values of the two components are very close to each other. Due to the fact that the frequency resolution is too low, the frequency resolution is easily mistaken for one frequency component, the real fault component is covered by the power frequency component, and the beat vibration fault cannot be accurately identified. The simulation signal is analyzed by the method of the invention, and the effectiveness of the simulation signal on beat vibration fault detection and diagnosis is verified.
Referring to fig. 1, a method for detecting and diagnosing a beat vibration fault of a rotary machine includes the following steps:
1) taking the simulation signal x (t) as an analysis object, and performing bilateral continuation preprocessing operation on the signal x (t) by using a support vector machine method;
2) performing spectrum analysis on the signal x (t), as shown in a graph (b) in fig. 3, wherein 3 obvious frequency components and noise components can be obviously observed from the spectrum graph; according to the spectrogram characteristics of the signal x (t), setting the number N of decomposition modes to be 4 and the penalty factor to be 5000, and then decomposing the signal x (t) after bilateral prolongation by using a VMD method to obtain u1、u2、u3、u4A total of 4 eigenMode function, as shown in FIG. 4: eigenmode function u1、u2、u3The corresponding center frequencies are 49.6Hz, 100.0Hz and 14.9Hz in sequence, and respectively correspond to the component x in the simulation signal2(t)、x3(t)、x1(t),u4Corresponding to a random noise signal n (t); as can be seen from fig. 4, although the signal components are not arranged in sequence according to the frequency, the time domain waveforms of the signal components are relatively regular and clear, no obvious modal aliasing occurs, and all the 3 fundamental mode components contained in the signal x (t) can be well extracted;
3) in the simulation signal, the power frequency is set to 50Hz due to the eigenmode function u1The center frequency of the eigenmode function u is closest to the power frequency1Is a detection object; by observing u in FIG. 41Can see u1The waveform amplitude envelope has periodic and slow change and shows the characteristic of beat vibration phenomenon, and u is calculated by referring to a schematic diagram 2 of beat vibration signals1Waveform amplitude envelope variation period TbThe period of rotation of the rotor is 0.02s, so T is 0.5sbIf > 0.08s, then u is determined1Continuing to execute the step 4 for the beat vibration signal;
4) to beat vibration signal u1Performing a spectral analysis, as shown in fig. 5; the frequency resolution Deltaf in the spectrogram is still 1Hz, u1Waveform envelope amplitude variation frequency ωb=1/Tb2Hz, due to ωb<4 delta f, the frequency resolution is too low, so that the beat vibration fault characteristic frequency cannot be effectively identified; it can be observed from fig. 5 that the eigenmode function u1The spectrogram of (a) seems to have only one significant frequency component, the frequency of which is 50Hz, and other fault components are not significant, and step 5 needs to be continuously performed;
5) to beat vibration signal u1Hilbert transformation is carried out to obtain corresponding analytic signals, and then Hilbert demodulation spectrums and instantaneous frequency spectrums of the analytic signals are obtained and are respectively shown in fig. 6 and fig. 7; in FIG. 6, a very distinct spectral peak exists at a frequency of 2Hz, with an amplitude of 9.566, indicating that the difference in frequency between the two component components of the beat signal is 2Hz, since the power frequency is known to be 50Hz, the fault characteristic frequency ωfOnly 48Hz or 52Hz is possible; while in FIG. 7, u1The instantaneous frequency of the fault is slowly changed with the period of 0.5s along with the time, the instantaneous frequency value reaches the maximum at the valley beating position, and the characteristic shows that the fault characteristic frequency omega is the dominant component on the premise that the power frequency component is the dominant componentfAnd finally determining that the beat vibration fault characteristic frequency is 48Hz when the beat vibration fault characteristic frequency is smaller than 50Hz of the power frequency, wherein the analysis conclusion is completely consistent with the theoretical assumption of the simulation signal. It follows that even in the case of too low frequency resolution, the diagnostic information provided by the Hilbert demodulation spectrum, instantaneous frequency spectrum, etc. of the beat signal can be used to determine its fault signature frequency.

Claims (3)

1. A beat vibration fault detection and diagnosis method for a rotary machine is characterized by comprising the following steps:
1) selecting a rotor shaft vibration displacement signal x (t) at a fault response sensitive sensing point as an analysis object, and performing bilateral continuation preprocessing on the signal x (t);
2) decomposing the signal x (t) after the bilateral continuation preprocessing in the step 1) by using a VMD (spatial Mode decomposition) method to obtain a plurality of eigenmode functions u (t) corresponding to the signal x (t)k(t) and its center frequency fkK is 1,2, …, N denotes the number of eigenmode functions;
3) from the plurality of eigenmode functions u of step 2)k(t) selecting an eigenmode function with the center frequency closest to the rotor power frequency omega, and marking the eigenmode function as uj(t); observe uj(T) if the waveform envelope amplitude has a periodic variation rule and the variation period T isbIf u is more than or equal to 4/omega, then u is judgedj(t) continuing to execute step 4) for beat vibration signals; otherwise, u is determinedj(t) if not, the beat vibration detection process is finished;
4) to beat vibration signal uj(t) performing spectral analysis, calculating the frequency resolution Δ f of the spectrum, and determining uj(t) waveform envelope amplitude variation frequency ωbRelation to Δ f; if ω isbU is greater than or equal to 4 delta fjFrequency of (t)Spectrogram capable of expressing beat vibration fault characteristic frequency omegafAnd the diagnosis is finished; otherwise, the beat vibration fault characteristic frequency omega is caused due to the fact that the frequency resolution is too lowfCan not be effectively identified, and the step 5) needs to be continuously executed;
5) to beat vibration signal uj(t) carrying out Hilbert transformation to obtain a corresponding analytic signal, and then obtaining a Hilbert demodulation spectrum and an instantaneous frequency spectrum of the analytic signal; according to beat vibration signal uj(t) analyzing the characteristic frequency omega of beat vibration fault by the characteristics of Hilbert demodulation spectrum and instantaneous frequency spectrumfRelation with power frequency omega to obtain omegafThe exact value of (c).
2. The method for detecting and diagnosing the beating fault of the rotary machine according to claim 1, wherein: the measurement mode of the rotor shaft vibration displacement signal in the step 1) is non-contact measurement, and the continuation preprocessing of the signal adopts a support vector machine method.
3. The method for detecting and diagnosing the beating fault of the rotary machine according to claim 1, wherein: the beat vibration signal u in the step 5)j(t) the frequency corresponding to the dominant component in the Hilbert demodulation spectrum is the frequency omega of the change of the waveform envelope amplitudebThe frequency is a beat signal ujThe difference in frequency between the two component components in (t), i.e. ωb=|ω-ωf|;uj(t) the instantaneous frequency exhibits a periodic variation, under the condition that the power frequency component is the dominant component, if uj(t) when the maximum value of the instantaneous frequency of the sensor occurs at the beat valley and the minimum value of the instantaneous frequency of the sensor occurs at the beat peak, the beat vibration fault characteristic frequency omegaf<Omega; if u isj(t) when the maximum value of the instantaneous frequency appears at the beat peak and the minimum value appears at the beat valley, the beat vibration fault characteristic frequency omegaf>Omega; the beat signal ujAnd (t) providing a judgment basis for determining the beat vibration fault characteristic frequency by virtue of the characteristics of the Hilbert demodulation spectrum and the instantaneous frequency change.
CN202010256575.5A 2020-04-02 2020-04-02 Rotary machine beat vibration fault detection and diagnosis method Active CN111397877B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010256575.5A CN111397877B (en) 2020-04-02 2020-04-02 Rotary machine beat vibration fault detection and diagnosis method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010256575.5A CN111397877B (en) 2020-04-02 2020-04-02 Rotary machine beat vibration fault detection and diagnosis method

Publications (2)

Publication Number Publication Date
CN111397877A CN111397877A (en) 2020-07-10
CN111397877B true CN111397877B (en) 2021-07-27

Family

ID=71434768

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010256575.5A Active CN111397877B (en) 2020-04-02 2020-04-02 Rotary machine beat vibration fault detection and diagnosis method

Country Status (1)

Country Link
CN (1) CN111397877B (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112949524B (en) * 2021-03-12 2022-08-26 中国民用航空飞行学院 Engine fault detection method based on empirical mode decomposition and multi-core learning
CN114544188B (en) * 2022-02-22 2023-09-22 中国航发沈阳发动机研究所 Vibration fluctuation fault identification and elimination method caused by multisource beat vibration of aero-engine
CN115683644B (en) * 2022-10-13 2024-01-05 中国航发四川燃气涡轮研究院 Dual-source beat vibration characteristic identification method for aeroengine
CN115597901B (en) * 2022-12-13 2023-05-05 江苏中云筑智慧运维研究院有限公司 Bridge expansion joint damage monitoring method
CN116358864B (en) * 2023-06-01 2023-08-29 西安因联信息科技有限公司 Method and system for diagnosing fault type of rotary mechanical equipment

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5469745A (en) * 1993-06-01 1995-11-28 Westinghouse Electric Corporation System for determining FOVM sensor beat frequency
KR20090019274A (en) * 2007-08-20 2009-02-25 재단법인서울대학교산학협력재단 Method of beat tuning in a slightly asymmetric ring-type structure
JP2009068841A (en) * 2007-09-10 2009-04-02 Tohoku Univ Vibration displacement measuring device for micro mechanical-electric structure (mems)
CN101619729A (en) * 2009-06-17 2010-01-06 广东美的电器股份有限公司 Control method and operation method for optimizing beaten sound of parallel propeller fan systems
CN102650658A (en) * 2012-03-31 2012-08-29 机械工业第三设计研究院 Time-varying non-stable-signal time-frequency analyzing method
CN102967414A (en) * 2012-11-07 2013-03-13 郑州大学 Method for extracting imbalanced components of micro-speed-difference double-rotor system based on frequency spectrum correction
CN105699072A (en) * 2016-01-11 2016-06-22 石家庄铁道大学 Cascade empirical mode decomposition-based gear fault diagnosis method
CN106197655A (en) * 2016-07-27 2016-12-07 中国水利水电科学研究院 A kind of distinguish the method that true and false bat is shaken
CN110454942A (en) * 2019-08-21 2019-11-15 珠海格力电器股份有限公司 A kind of anti-control method for clapping vibration of more noise source devices and control device

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5469745A (en) * 1993-06-01 1995-11-28 Westinghouse Electric Corporation System for determining FOVM sensor beat frequency
KR20090019274A (en) * 2007-08-20 2009-02-25 재단법인서울대학교산학협력재단 Method of beat tuning in a slightly asymmetric ring-type structure
JP2009068841A (en) * 2007-09-10 2009-04-02 Tohoku Univ Vibration displacement measuring device for micro mechanical-electric structure (mems)
CN101619729A (en) * 2009-06-17 2010-01-06 广东美的电器股份有限公司 Control method and operation method for optimizing beaten sound of parallel propeller fan systems
CN102650658A (en) * 2012-03-31 2012-08-29 机械工业第三设计研究院 Time-varying non-stable-signal time-frequency analyzing method
CN102967414A (en) * 2012-11-07 2013-03-13 郑州大学 Method for extracting imbalanced components of micro-speed-difference double-rotor system based on frequency spectrum correction
CN105699072A (en) * 2016-01-11 2016-06-22 石家庄铁道大学 Cascade empirical mode decomposition-based gear fault diagnosis method
CN106197655A (en) * 2016-07-27 2016-12-07 中国水利水电科学研究院 A kind of distinguish the method that true and false bat is shaken
CN110454942A (en) * 2019-08-21 2019-11-15 珠海格力电器股份有限公司 A kind of anti-control method for clapping vibration of more noise source devices and control device

Non-Patent Citations (5)

* Cited by examiner, † Cited by third party
Title
Changes in rotor response characteristics based diagnostic method and its application to identification of misalignment;Qu Lei 等;《MEASUREMENT》;20190531;第138卷;第91-105页 *
内燃动车组辅助机组拍振现象分析;贺小龙 等;《噪声与振动控制》;20160228;第36卷(第1期);第83-87,105页 *
基于HHT的二滩拱坝工作性态识别及其拍振;李成业;《中国博士学位论文全文数据库工程科技Ⅱ辑》;20141215(第12(2014)期);第C037-15页 *
应用EEMD和小波包分解的压力脉动信号时域特征提取方法;李瑞 等;《现代制造工程》;20180731(第7(2018)期);第1-6,11页 *
泄洪水流诱发泄流结构拍振特性及机理研究;杜磊;《中国优秀硕士学位论文全文数据库工程科技Ⅱ辑》;20190115(第1(2019)期);第C037-237页 *

Also Published As

Publication number Publication date
CN111397877A (en) 2020-07-10

Similar Documents

Publication Publication Date Title
CN111397877B (en) Rotary machine beat vibration fault detection and diagnosis method
US4408294A (en) Method for on-line detection of incipient cracks in turbine-generator rotors
Zhao et al. Generalized Vold–Kalman filtering for nonstationary compound faults feature extraction of bearing and gear
CN110763462B (en) Time-varying vibration signal fault diagnosis method based on synchronous compression operator
US9016132B2 (en) Rotating blade analysis
CN101603854A (en) The rotating machinery non-stationery vibration signal instantaneous frequency estimation algorithm in start and stop period
JPH09113416A (en) Method for diagnosing damage of rolling bearing
Corne et al. Comparing MCSA with vibration analysis in order to detect bearing faults—A case study
JPH1026580A (en) Method and device for diagnosing speed-change-type rotary mechanical equipment
Lin et al. A review and strategy for the diagnosis of speed-varying machinery
CN105865793A (en) Method for improving vibration monitoring precision of rotor aeroengine
JPH0141928B2 (en)
Krause et al. Asynchronous response analysis of non-contact vibration measurements on compressor rotor blades
JP2019101009A (en) Diagnostic method and diagnostic system for rotating machine structure abnormality
CN112345827A (en) Graphical differentiation of spectral frequency families
Shi et al. A dual-guided adaptive decomposition method of fault information and fault sensitivity for multi-component fault diagnosis under varying speeds
CN111562126B (en) Rotary mechanical frequency doubling fault diagnosis method based on three-dimensional holographic difference spectrum
Wang et al. The method for identifying rotating blade asynchronous vibration and experimental verification
CN112465068A (en) Rotating equipment fault feature extraction method based on multi-sensor data fusion
Grądzki et al. Rotor blades diagnosis method based on differences in phase shifts
CN115683644B (en) Dual-source beat vibration characteristic identification method for aeroengine
JPH04204021A (en) Apparatus for diagnosing vibration and sound of rotating machine
Zhang et al. Research on the identification of asynchronous vibration parameters of rotating blades based on blade tip timing vibration measurement theory
JP6283591B2 (en) Automatic vibration diagnostic equipment for rotating machinery
Loukis et al. A procedure for automated gas turbine blade fault identification based on spectral pattern analysis

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant