CN109029689A - A kind of rotating machinery vibration analysis method based on two ends of rotor motion profile - Google Patents

A kind of rotating machinery vibration analysis method based on two ends of rotor motion profile Download PDF

Info

Publication number
CN109029689A
CN109029689A CN201810893544.3A CN201810893544A CN109029689A CN 109029689 A CN109029689 A CN 109029689A CN 201810893544 A CN201810893544 A CN 201810893544A CN 109029689 A CN109029689 A CN 109029689A
Authority
CN
China
Prior art keywords
rotor
vibration
rotating machinery
balance force
radius
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.)
Granted
Application number
CN201810893544.3A
Other languages
Chinese (zh)
Other versions
CN109029689B (en
Inventor
张文涛
房林铁
夏亚磊
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.)
China Datang Corp Science and Technology Research Institute Co Ltd Huazhong Branch
Original Assignee
China Datang Corp Science and Technology Research Institute Co Ltd Huazhong Branch
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 China Datang Corp Science and Technology Research Institute Co Ltd Huazhong Branch filed Critical China Datang Corp Science and Technology Research Institute Co Ltd Huazhong Branch
Priority to CN201810893544.3A priority Critical patent/CN109029689B/en
Publication of CN109029689A publication Critical patent/CN109029689A/en
Application granted granted Critical
Publication of CN109029689B publication Critical patent/CN109029689B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H9/00Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves by using radiation-sensitive means, e.g. optical means

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Testing Of Balance (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Abstract

The present invention relates to a kind of rotating machinery vibration analysis method based on two ends of rotor motion profile, technical solution is, according to obtained in the same direction and reversal of vibrations component value, to judge out-of-balance force pattern on rotor: if AtGreater than outstanding value specified in rotating machinery vibrating standard, out-of-balance force in the same direction is big on rotor;If AfGreater than outstanding value specified in rotating machinery vibrating standard, reversed out-of-balance force is big on rotor;If AtAnd AfBoth greater than outstanding value specified in rotating machinery vibrating standard, the out-of-balance force that pattern is mixed on rotor is big, the method of the present invention is simple, comprehensively consider when vibration analysis and out-of-balance force pattern analysis and has vertically and horizontally vibrated, rather than it is only vibrated only in accordance with single direction, obtained analysis conclusion is the innovation in rotating machinery vibration analysis method comprehensively, reliably.

Description

A kind of rotating machinery vibration analysis method based on two ends of rotor motion profile
Technical field
The present invention relates to a kind of rotating machinery vibrating method for testing and analyzing, and technical staff can be helped according to vibration-testing number According to the distribution pattern of out-of-balance force on analysis rotor, if power is uneven, couple unbalance and mixing are uneven, rotation is carried out in guidance Mechanical dynamic balancing work, main application fields include: all kinds of rotating machineries, such as pump, blower, motor, Turbo-generator Set.
Background technique
Imbalance is the most common vibration fault of rotating machinery, and rotor dynamic balancing is having for rotating machinery vibrating fault treatment Effect means, and the work often to be carried out.It is accurate to determine that dynamic balancing efficiency can be improved in uneven pattern and precision, reduction are opened Machine number is of great significance for improving rotating machinery operation stability and reliability.
Imbalance includes static unbalance, unbalance dynamic and hybrid imbalance.Under static unbalance state, exist in the middle part of rotor Out-of-balance force, or it is equal in magnitude there are one group in two ends of rotor, and the identical power in direction, also known as power are uneven.Unbalance dynamic Under state, in the power that two ends of rotor is equal in magnitude, contrary there are one group, also known as couple unbalance.When in rotor simultaneously There are when power imbalance and couple unbalance, referred to as hybrid imbalance.Before development rotor dynamic balancing, it is necessary to understand turn first The pattern and distribution of out-of-balance force on son.
Under unit actual motion state, out-of-balance force can not be directly tested, is all to diagnose uneven event according to vibration Barrier, and analyze on rotor whether have out-of-balance force.Vibration is big, and out-of-balance force is big;With small vibration, out-of-balance force is small.Equally and root The pattern of out-of-balance force is judged according to the vibration of two ends of rotor.As in two ends of rotor vibration signal there are biggish component in the same direction, Then think that there are power imbalances on rotor;As there are biggish reversed components in two ends of rotor vibration signal, then it is assumed that on rotor There are couple unbalances;As existed simultaneously biggish component in the same direction and reversed in two ends of rotor vibration signal, then it is assumed that on rotor In the presence of the imbalance of mixing pattern.
Judging out-of-balance force pattern all at present is carried out by the vibration on horizontal or vertical single direction.For steamer For the large rotating machineries such as generating set, due to unit vertically and horizontally on support stiffness, damping characteristic etc. exist Larger difference, bear vibration caused by out-of-balance force also has bigger difference in the vertical and horizontal direction on rotor.Practical work Cheng Zhong, it sometimes appear that complete according to vertical vibration and according to the out-of-balance force pattern that judges of horizontal direction vibration Different situations.Therefore, it is imperative to improve and innovate.
Summary of the invention
For above situation, for the defect for overcoming the prior art, the purpose of the present invention is just to provide a kind of based on rotor two The rotating machinery vibration analysis method of end motion track can effectively solve the uneven pattern on analysis rotor, improve dynamic balancing Efficiency the problem of.
The technical solution that the present invention solves is:
A kind of rotating machinery vibration analysis method based on two ends of rotor motion profile, comprising the following steps:
(1) reflective marker is set in shaft, photoelectric sensor is directed at reflective marker, or open one in shaft Eddy current sensor is directed at keyway by keyway, and the method for reflective strip or key phase fit keyway is cooperated with photoelectric sensor, is surveyed Key phase pulse signal is taken, shaft often rotates a circle, and generates such pulse signal, remembers the time between two neighboring pulse Between be divided into T, then real-time rotational frequency f=1/T;
(2) one group of vibrating sensor is vertically and horizontally respectively arranged in two ends of rotor detected part, with key phase pulse Signal is triggering benchmark, and synchronous acquisition two ends of rotor vertically and horizontally vibration signal is denoted as x1(t),x2(t),y1(t),y2 (t);
(3) Fast Fourier Transform (FFT) is carried out to collected vibration signal, obtains industrial frequency harmonic identical with rotational frequency The amplitude and phase of component, are denoted as: A respectivelyx1,Ax2,Ay1,Ay2With
(4) it according to the amplitude and phase of a multiplied frequency harmonic component, reconstructs and two ends of rotor vertically and horizontally vibration signal Corresponding multiplied frequency harmonic component signal:
(5) remember that the period corresponding with rotational frequency f is T, then have: T=1/f;It will be divided into 1000 sections between [0, T], obtains Each point vibration values under different moments in by rotation one week: x1'(ti),y1'(ti),x'2(ti),y'2(ti);
(7) it defines different moments lower rotor part and vibrates radius ri
(8) oscillating curve that two ends of rotor is made of under different moments vibration radius is drawn out;
(9) when finding after the t=0 moment on two ends of rotor vibration radius curve corresponding to the 1st vibration radius peak point Between put and its amplitude, be denoted as respectively: t1,A1And t2,A2
(10) phase angle ψ corresponding with vibration radius peak point is calculated12
(11) to vibrate radius A1∠ψ1,A2∠ψ2It is vibrated as two ends of rotor, is vibrated, decomposed according to two ends of rotor To vibrate A in the same directiontAnd reversal of vibrations Af
(12) according to obtained in the same direction and reversal of vibrations component value, judge out-of-balance force pattern on rotor:
If AtGreater than outstanding value specified in rotating machinery vibrating standard, out-of-balance force in the same direction is big on rotor;
If AfGreater than outstanding value specified in rotating machinery vibrating standard, reversed out-of-balance force is big on rotor;
If AtAnd AfBoth greater than outstanding value specified in rotating machinery vibrating standard mixes the out-of-balance force of pattern on rotor Greatly.
The method of the present invention is simple, it is believed that two ends of rotor vibration is carried out in the plane perpendicular to axis, is needed with vertical Vibration in straight and horizontal both direction carrys out integrating representation, accordingly, propose according to two ends of rotor vertically and horizontally on vibration Dynamic signal, acquires motion profile of the two ends of rotor in vertical axis plane, and defining the vibration radius under different moments is track The upper moment point is to the distance in the center of circle, after acquiring two ends of rotor vibration radius change curve, with the 1st vibration half after the t=0 moment The phase angle of diameter peak value point is the end phase angle, is vibrated using vibrating radius peak value as the end.On this basis, to rotor Both ends vibration information is analyzed, and judges uneven pattern on rotor.Rotor oscillation is regarded as in the plane perpendicular to axis Interior planar obit simulation movement, when vibration analysis and out-of-balance force pattern analysis, which has comprehensively considered, vertically and horizontally to be vibrated, and It is not only to be vibrated only in accordance with single direction, obtained analysis conclusion is in rotating machinery vibration analysis method comprehensively, reliably Innovation.
Detailed description of the invention
Fig. 1 is vibration of rotor system test simplified schematic diagram.
Each appended drawing reference respectively indicates in figure: 1 bearing, 2 rotors, 3 vibrating sensors, 4 key phases, 5 vibration numbers According to Acquisition Instrument, 6 wheel discs
Fig. 2 is 4, the both ends vibration measuring point original waveform that rotor test obtains.
Wherein: x1 and y1 is that a bearing side both horizontally and vertically vibrates, and x2 and y2 are that another bearing side is horizontal and vertical Direction vibration;
Fig. 3 is the key phase pulse signal figure that test obtains.
Fig. 4 is the original rumble spectrum figure of 4 measuring points of two ends of rotor that test obtains, and is labelled with a multiplied frequency harmonic component on figure Amplitude and phase.
Fig. 5 be using this method by test signal reconstruction after obtain with 4 measuring points of two ends of rotor, one multiplied frequency harmonic component Corresponding waveform diagram.
Fig. 6 is the two ends of rotor vibration radius waveform diagram obtained using this method.
The flow chart of Fig. 7 the method for the present invention
Specific embodiment
Below in conjunction with attached drawing, specific embodiments of the present invention will be described in further detail.
It is provided by Fig. 1-7, a kind of rotating machinery vibration analysis method based on two ends of rotor motion profile of the present invention, including Following steps:
(1) reflective marker is set in shaft, photoelectric sensor is directed at reflective marker, or open one in shaft Eddy current sensor is directed at keyway by keyway, and the method for reflective strip or key phase fit keyway is cooperated with photoelectric sensor, is surveyed Key phase pulse signal is taken, shaft often rotates a circle, and generates such pulse signal, remembers the time between two neighboring pulse Between be divided into T, then real-time rotational frequency f=1/T;
(2) one group of vibrating sensor is vertically and horizontally respectively arranged in two ends of rotor detected part, with key phase pulse Signal is triggering benchmark, and synchronous acquisition two ends of rotor vertically and horizontally vibration signal is denoted as x1(t),x2(t),y1(t),y2 (t);
(3) Fast Fourier Transform (FFT) is carried out to collected vibration signal, obtains industrial frequency harmonic identical with rotational frequency The amplitude and phase of component, are denoted as: A respectivelyx1,Ax2,Ay1,Ay2With
(4) it according to the amplitude and phase of a multiplied frequency harmonic component, reconstructs and two ends of rotor vertically and horizontally vibration signal Corresponding multiplied frequency harmonic component signal:
(5) remember that the period corresponding with rotational frequency f is T, then have: T=1/f;It will be divided into 1000 sections between [0, T], obtains Each point vibration values under different moments in by rotation one week: x1'(ti),y1'(ti),x'2(ti),y'2(ti);
(7) it defines different moments lower rotor part and vibrates radius ri
(8) oscillating curve that two ends of rotor is made of under different moments vibration radius is drawn out;
(9) when finding after the t=0 moment on two ends of rotor vibration radius curve corresponding to the 1st vibration radius peak point Between put and its amplitude, be denoted as respectively: t1,A1And t2,A2
(10) phase angle ψ corresponding with vibration radius peak point is calculated12
(11) to vibrate radius A1∠ψ1,A2∠ψ2It is vibrated as two ends of rotor, is vibrated, decomposed according to two ends of rotor To vibrate A in the same directiontAnd reversal of vibrations Af
(12) according to obtained in the same direction and reversal of vibrations component value, judge out-of-balance force pattern on rotor:
If AtGreater than outstanding value specified in rotating machinery vibrating standard, out-of-balance force in the same direction is big on rotor;
If AfGreater than outstanding value specified in rotating machinery vibrating standard, reversed out-of-balance force is big on rotor;
If AtAnd AfBoth greater than outstanding value specified in rotating machinery vibrating standard mixes the out-of-balance force of pattern on rotor Greatly.
The key phase, vibrating sensor and data collecting instrument are the prior art, as ROS-W type photoelectricity key passes on from one to another Sensor, ZXP type vibrating sensor, EVM-8 type vibrating data collection instrument.
It is acted in the plane perpendicular to axis by rotor oscillation it can be seen from above situation and bear vibration, this is one A plane motion problem, rely solely on the vibration on single direction carry out analysis be it is incomplete, a kind of development trend is exactly By the vibration integrated analysis on vertically and horizontally.For example, traditional spectrum analysis technique be for single signal into Capable, and full spectral analysis technology is grown up on the basis of traditional spectrum analysis technique, and vertical and water is fully utilized Vibration signal in flat both direction can further obtain the profound letter such as positive precession and backward whirl on the basis of traditional frequency spectrum Breath and feature.It is considered herein that two ends of rotor vibration is carried out in the plane perpendicular to axis, need with vertically and horizontally Vibration in both direction carrys out integrating representation.Accordingly, propose according to two ends of rotor vertically and horizontally on vibration signal, ask Motion profile of the two ends of rotor in vertical axis plane is obtained, defining the vibration radius under different moments is the moment point on track To the distance in the center of circle, after acquiring two ends of rotor vibration radius change curve, where the 1st vibration radius peak value after the t=0 moment The phase angle of point is the end phase angle, is vibrated using vibrating radius peak value as the end.On this basis, two ends of rotor is vibrated and is believed Breath is analyzed, and judges uneven pattern on rotor.Its method is simple, and rotor oscillation is regarded as in the plane perpendicular to axis Interior planar obit simulation movement, when vibration analysis and out-of-balance force pattern analysis, which has comprehensively considered, vertically and horizontally to be vibrated, and It is not only to be vibrated only in accordance with single direction, obtained analysis conclusion is in rotating machinery vibration analysis method comprehensively, reliably Innovation achieves good technical effect through practical application:
As shown in the table, be the two ends of rotor vibration radius amplitude and phase obtained using this method, with x to vibration for according to According to component amplitude in the same direction is small, and reversed component amplitude is big, and there are cone out-of-balance forces for rotor.Using Y-direction vibration as foundation, together Big to component amplitude, reversed component amplitude is small, and there are pattern out-of-balance forces in the same direction for rotor.According to x and y to vibration to unbalanced type The judgement conclusion of formula is different, and there are contradictions.For the vibration radius obtained using this method as foundation, component amplitude in the same direction is greater than whirler Outstanding value specified in tool vibration standard, reversed component amplitude are less than outstanding value specified in rotating machinery vibrating standard, rotor There are pattern out-of-balance forces in the same direction.This method has comprehensively considered the vibration in x and y both direction, rather than only only in accordance with single Direction vibration, obtained analysis conclusion are the innovations in rotating machinery vibration analysis method through practical application comprehensively, reliably.

Claims (1)

1. a kind of rotating machinery vibration analysis method based on two ends of rotor motion profile, which comprises the following steps:
(1) reflective marker is set in shaft, photoelectric sensor is directed at reflective marker, or open a key in shaft Eddy current sensor is directed at keyway by slot, and the method for reflective strip or key phase fit keyway is cooperated with photoelectric sensor, is measured Key phase pulse signal, shaft often rotate a circle, and generate such pulse signal, remember between the time between two neighboring pulse It is divided into T, then real-time rotational frequency f=1/T;
(2) one group of vibrating sensor is vertically and horizontally respectively arranged in two ends of rotor detected part, with key phase pulse signal To trigger benchmark, synchronous acquisition two ends of rotor vertically and horizontally vibration signal is denoted as x1(t),x2(t),y1(t),y2(t);
(3) Fast Fourier Transform (FFT) is carried out to collected vibration signal, obtains power frequency harmonic component identical with rotational frequency Amplitude and phase, be denoted as respectively: Ax1,Ax2,Ay1,Ay2With
(4) according to the amplitude and phase of a multiplied frequency harmonic component, reconstruct that vertically and horizontally vibration signal is opposite with two ends of rotor The multiplied frequency harmonic component signal answered:
(5) remember that the period corresponding with rotational frequency f is T, then have: T=1/f;It will be divided into 1000 sections between [0, T], is turned Each point vibration values under different moments in one week dynamic: x '1(ti),y′1(ti),x'2(ti),y'2(ti);
(7) it defines different moments lower rotor part and vibrates radius ri
(8) oscillating curve that two ends of rotor is made of under different moments vibration radius is drawn out;
(9) two ends of rotor vibrates time point corresponding to the 1st vibration radius peak point on radius curve after finding the t=0 moment And its amplitude, it is denoted as respectively: t1,A1And t2,A2
(10) phase angle ψ corresponding with vibration radius peak point is calculated12
(11) to vibrate radius A1∠ψ1,A2∠ψ2It vibrates as two ends of rotor, is vibrated according to two ends of rotor, is broken down into the same direction Vibrate AtAnd reversal of vibrations Af
(12) according to obtained in the same direction and reversal of vibrations component value, judge out-of-balance force pattern on rotor:
If AtGreater than outstanding value specified in rotating machinery vibrating standard, out-of-balance force in the same direction is big on rotor;
If AfGreater than outstanding value specified in rotating machinery vibrating standard, reversed out-of-balance force is big on rotor;
If AtAnd AfBoth greater than outstanding value specified in rotating machinery vibrating standard, the out-of-balance force that pattern is mixed on rotor are big.
CN201810893544.3A 2018-08-08 2018-08-08 Rotary mechanical vibration analysis method based on movement tracks of two ends of rotor Active CN109029689B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810893544.3A CN109029689B (en) 2018-08-08 2018-08-08 Rotary mechanical vibration analysis method based on movement tracks of two ends of rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810893544.3A CN109029689B (en) 2018-08-08 2018-08-08 Rotary mechanical vibration analysis method based on movement tracks of two ends of rotor

Publications (2)

Publication Number Publication Date
CN109029689A true CN109029689A (en) 2018-12-18
CN109029689B CN109029689B (en) 2020-05-22

Family

ID=64650071

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810893544.3A Active CN109029689B (en) 2018-08-08 2018-08-08 Rotary mechanical vibration analysis method based on movement tracks of two ends of rotor

Country Status (1)

Country Link
CN (1) CN109029689B (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110779438A (en) * 2019-10-29 2020-02-11 润电能源科学技术有限公司 Rotor bending value measuring method, steam turbine generator and computer readable storage medium
CN110849414A (en) * 2019-10-29 2020-02-28 润电能源科学技术有限公司 Method, device and equipment for identifying bending direction of rotor and storage medium
CN111473933A (en) * 2020-04-27 2020-07-31 上海海事大学 Multifunctional blade and rotor test bed
CN111550429A (en) * 2020-05-14 2020-08-18 北京化工大学 Centrifugal compressor rotor system stability comprehensive control method and device
CN113191057A (en) * 2021-05-12 2021-07-30 四川长虹空调有限公司 Method and device for determining direction of unbalanced force
CN113358203A (en) * 2021-06-02 2021-09-07 中国大唐集团科学技术研究院有限公司华东电力试验研究院 Rotor natural frequency identification method and system based on harmonic component decomposition

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1269504A (en) * 1999-04-06 2000-10-11 黄震西 Two-point measuring method of rotor unbalance
CN101487756A (en) * 2009-01-13 2009-07-22 东南大学 Harmonic component rotational speed balancing method in rotating machinery vibration analysis
US20150290772A1 (en) * 2014-04-09 2015-10-15 Balance Systems S.R.L. Dynamic balancing process and device for a rotating body
CN107255549A (en) * 2017-06-14 2017-10-17 西安交通大学 A kind of rotor multiple spot amount of unbalance recognition methods

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1269504A (en) * 1999-04-06 2000-10-11 黄震西 Two-point measuring method of rotor unbalance
CN101487756A (en) * 2009-01-13 2009-07-22 东南大学 Harmonic component rotational speed balancing method in rotating machinery vibration analysis
US20150290772A1 (en) * 2014-04-09 2015-10-15 Balance Systems S.R.L. Dynamic balancing process and device for a rotating body
CN107255549A (en) * 2017-06-14 2017-10-17 西安交通大学 A kind of rotor multiple spot amount of unbalance recognition methods

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
夏亚磊: "柔性转子转轴弯曲与不平衡耦合振动分析", 《动力工程学报》 *

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110779438A (en) * 2019-10-29 2020-02-11 润电能源科学技术有限公司 Rotor bending value measuring method, steam turbine generator and computer readable storage medium
CN110849414A (en) * 2019-10-29 2020-02-28 润电能源科学技术有限公司 Method, device and equipment for identifying bending direction of rotor and storage medium
CN110849414B (en) * 2019-10-29 2021-05-04 润电能源科学技术有限公司 Method, device and equipment for identifying bending direction of rotor and storage medium
CN111473933A (en) * 2020-04-27 2020-07-31 上海海事大学 Multifunctional blade and rotor test bed
CN111473933B (en) * 2020-04-27 2021-11-02 上海海事大学 Multifunctional blade and rotor test bed
CN111550429A (en) * 2020-05-14 2020-08-18 北京化工大学 Centrifugal compressor rotor system stability comprehensive control method and device
CN111550429B (en) * 2020-05-14 2021-07-20 北京化工大学 Centrifugal compressor rotor system stability comprehensive control method and device
WO2021227251A1 (en) * 2020-05-14 2021-11-18 北京化工大学 Comprehensive control method and device for stability of rotor system of centrifugal compressor
CN113191057A (en) * 2021-05-12 2021-07-30 四川长虹空调有限公司 Method and device for determining direction of unbalanced force
CN113191057B (en) * 2021-05-12 2022-04-12 四川长虹空调有限公司 Method and device for determining direction of unbalanced force
CN113358203A (en) * 2021-06-02 2021-09-07 中国大唐集团科学技术研究院有限公司华东电力试验研究院 Rotor natural frequency identification method and system based on harmonic component decomposition

Also Published As

Publication number Publication date
CN109029689B (en) 2020-05-22

Similar Documents

Publication Publication Date Title
CN109029689A (en) A kind of rotating machinery vibration analysis method based on two ends of rotor motion profile
US8272265B2 (en) System and method for active detection of asymmetry in rotating structures
CN101556200A (en) Vector spectrum based dynamic balance method for flexible rotor
CN100434890C (en) Flexible rotor holographic dynamic balancing method based on empirical mode decomposition
CN101487756B (en) Harmonic component rotational speed balancing method in rotating machinery vibration analysis
CN102087138A (en) System and method for vibration analysis and phase analysis of vibration waveforms using dynamic statistical averaging of tachometer data to accurately calculate rotational speed
CN101907089A (en) Fault diagnosis method of compressor shafting based on three-dimensional space axle center orbit
CN106523299A (en) Stator current data driving based unbalance detecting method for blades of doubly-fed induction generator
Saadaoui et al. Induction motor bearing damage detection using stator current analysis
Ahmed et al. Detection of eccentricity faults in machine usingfrequency spectrum technique
Pedotti et al. Fault diagnostics in rotary machines through spectral vibration analysis using low-cost MEMS devices
CN110579312A (en) dynamic balance fault detection method for multi-wheel-disc shafting of non-trial-weight rotating machinery
CN106441840A (en) Rotary machine pseudo-subsynchronous fault holographic diagnosis method based on model
KR100905397B1 (en) Dynamic balancing apparatus and methods using periodic angular motion
CN105651515A (en) Fault detection method and device for aircraft engine intermediate bearing
KR100941467B1 (en) Dynamic Balancing Apparatus and Methods using a Linear Time-varying Angular Velocity Model
Ewert et al. Application of selected higher-order methods to detect rotor unbalance of drive system with PMSM
CN1186600C (en) Extraction and monitoring method of half-speed vortex on-line stability characteristics of high-speed rotating machine
CN106053034A (en) Rotary machine holographic diagnostics method based on frequency modulation information reconstruction
US4608867A (en) Method for the dynamic balancing of rotating machines in assembled condition
Luwei et al. Data fusion of acceleration and velocity features (dFAVF) approach for fault diagnosis in rotating machines
RU2356021C2 (en) Method of rotor system vibration diagnostics
CN114235318A (en) Multifunctional vibration test bench
CN101464202A (en) Dynamic balancing method for dual-rotor rotating machine with little speed difference
Otuyemi et al. Modulation signal bispectrum analysis of motor current signals for condition monitoring of electromechanical systems

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