CN109101769A - Leaf end timing sensor number determination method based on compressed sensing - Google Patents

Leaf end timing sensor number determination method based on compressed sensing Download PDF

Info

Publication number
CN109101769A
CN109101769A CN201811103282.2A CN201811103282A CN109101769A CN 109101769 A CN109101769 A CN 109101769A CN 201811103282 A CN201811103282 A CN 201811103282A CN 109101769 A CN109101769 A CN 109101769A
Authority
CN
China
Prior art keywords
blade
tip
timing
compressed sensing
timing sensor
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
CN201811103282.2A
Other languages
Chinese (zh)
Other versions
CN109101769B (en
Inventor
杨拥民
潘明昊
官凤娇
胡海峰
陈仲生
徐海龙
周畅祎
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.)
National University of Defense Technology
Original Assignee
National University of Defense 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 National University of Defense Technology filed Critical National University of Defense Technology
Priority to CN201811103282.2A priority Critical patent/CN109101769B/en
Publication of CN109101769A publication Critical patent/CN109101769A/en
Application granted granted Critical
Publication of CN109101769B publication Critical patent/CN109101769B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • Geometry (AREA)
  • General Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Abstract

The application discloses a method for determining the number of leaf end timing sensors based on compressed sensing, which comprises the following steps: step 10, calculating a time difference sequence of the blade passing through a blade end timing sensor, and constructing a blade end timing vibration measurement equivalent model according to the time difference sequence; step 20, constructing a compressed sensing model according to the leaf end timing vibration measurement equivalent model; and step 30, calculating the optimal solution of the leaf end timing sensor number according with the compressed sensing model according to the preset sensor number. Through the technical scheme in this application, improved the accuracy of confirming tip timing sensor quantity, be favorable to improving blade vibration real-time detection's reliability, reduced because of the blade vibration leads to the possibility of rotating vane trouble.

Description

A kind of compressed sensing based tip-timing sensor number determines method
Technical field
This application involves the technical fields of blade vibration non-contact detecting, are based on compressed sensing in particular to one kind Tip-timing sensor number determine method.
Background technique
Rotating vane is the key that dynamic component in aero-engine, and rotating vane is under extreme Service Environment in operational process Often transformation operating condition, rotating vane is easy to produce vibration, and then induces rotating vane failure.Apparatus for rotating vane vibration is carried out online Precise measurement can effectively grasp the Vibration Condition of blade, so that providing for engine blade safety monitoring and fault diagnosis can By foundation, for guaranteeing that the safe and stable operation of rotating machinery, prevention significant trouble are of great significance.
Contactless tip-timing measurement passes through the one group of Tip-Timing sensing being along the circumferential direction mounted on casing and passes Sensor records time of the blade by sensor.When blade there is no vibration when, reach sensor fiducial time only with Revolving speed, blade radius and sensing installation angle are related;And when blade vibrates, reach the real time meeting of sensor In advance or this fiducial time is lagged behind, generates a time difference.Carrying out processing to the time difference signal sequence can be obtained by The vibration displacement sequence of rotating vane end of blade, so as to extract every vibration characteristics of blade.
And in actual condition, due to the restriction of the factors such as aero-engine space structure and service requirement, blade tip-timing is passed Sensor number is generally less, and sample frequency is generally significantly less than the intrinsic frequency of high speed blade, causes measuring signal to belong to and owes to adopt Sample signal.It is that apparatus for rotating vane vibration blade tip-timing is surveyed that multifrequency vibratory response is obtained by the lack sampling data of Tip-Timing Measurement The key problem of amount.Therefore, apparatus for rotating vane vibration measurement problem is often closely bound up with Tip-Timing Measurement number of sensors.
And in the prior art, usually assume that blade vibration response is that single-frequency responds, and must accurately obtain blade vibration Under the premise of prior information, the quantity of Tip-Timing Measurement sensor can be determined.But actual vibration measurement process In high speed rotational blade vibratory response be closely related with blade state itself and its working condition, on the one hand, due to pivoting leaf Piece running environment is complicated, causes the factor of blade vibration there are diversity, and single-frequency responds the reality that can not reflect blade vibration Border situation, leading to the mathematical model of determining Tip-Timing Measurement number of sensors, there are inevitable errors, and then influence passes The accuracy that sensor quantity determines.On the other hand, rotating vane usually can not accurately be obtained in different shapes during vibration measurement Vibration prior information under state and running environment.
Summary of the invention
The purpose of the application is at least to solve in the prior art or one of technical problem present in the relevant technologies, to improve The accuracy of determining tip-timing sensor quantity is conducive to the reliability for improving blade vibration real-time detection, reduce because Blade vibration leads to a possibility that rotating vane failure.
The technical solution of the application is: providing a kind of compressed sensing based tip-timing sensor number determination side Method, this method comprises: step 10, calculates the time difference sequence that blade passes through tip-timing sensor, according to time difference sequence, structure Build blade tip-timing vibration measurement equivalent model;Step 20, according to blade tip-timing vibration measurement equivalent model, compressed sensing mould is constructed Type;Step 30, according to default number of sensors, the tip-timing sensor quantity optimal solution for meeting compressed sensing model is calculated, Wherein, in step 30, it specifically includes:
Step 31, the order of the matrix equation of end of blade timing sampling signal spectrum in compressed sensing model is calculated;
Step 32, it according to the relevant sensing matrix of tip-timing sensor quantity in compressed sensing model and position, calculates Cross-correlation coefficient;
Step 33, according to sum of ranks cross-correlation coefficient, meeting the maximum of default number of sensors just according to preset formula calculating Integer is denoted as tip-timing sensor quantity optimal solution, wherein default calculation formula are as follows:
In formula, | | Xl(f)||0For multifrequency blade vibration signal spectrum vector Xl(f) number of the non-zero row vector in, W are Cross-correlation coefficient, Rank (Y (f)) are the order of matrix equation Y (f),Indicate the maximum positive integer smaller than b, giRepresenting matrix Φ I-th column, gjThe jth of representing matrix Φ arranges.
In any of the above-described technical solution, further, in step 10, specifically includes: step 11, being reached according to blade The theoretical arrival time of tip-timing sensor and actual time of arrival calculate time difference sequence;Step 12, according to time difference sequence Column and lack sampling principle construct blade tip-timing vibration measurement equivalent model.
In any of the above-described technical solution, further, in step 20, specifically include: step 21, according to blade tip-timing Vibration measurement equivalent model calculates corresponding matrix equation;Step 22, it is shown in a frequency domain according to blade vibration signal dilute Characteristic is dredged, calculating matrix non trivial solution is denoted as compressed sensing model.
The beneficial effect of the application is: by constructing compressed sensing model, determining the quantity of tip-timing sensor, improves The accuracy and reliability of determining tip-timing sensor quantity improves identification and reconstruct multifrequency end of blade combination of vibrations signal Frequency accuracy, be conducive to improve blade vibration real-time detection measurement accuracy, reduce because blade vibration causes to rotate A possibility that blade fault.
Detailed description of the invention
The advantages of above-mentioned and/or additional aspect of the application, will become bright in combining description of the following accompanying drawings to embodiment It shows and is readily appreciated that, in which:
Fig. 1 is to determine method according to the compressed sensing based tip-timing sensor number of one embodiment of the application Schematic flow diagram;
Fig. 2 is the tip-timing sensor schematic view of the mounting position according to one embodiment of the application.
Specific embodiment
It is with reference to the accompanying drawing and specific real in order to be more clearly understood that the above objects, features, and advantages of the application Mode is applied the application is further described in detail.It should be noted that in the absence of conflict, the implementation of the application Feature in example and embodiment can be combined with each other.
In the following description, many details are elaborated in order to fully understand the application, still, the application may be used also To be implemented using other than the one described here other modes, therefore, the protection scope of the application is not by described below Specific embodiment limitation.
Presently filed embodiment is illustrated hereinafter with reference to Fig. 1-2.
As shown in Figure 1, compressed sensing based tip-timing sensor number determines that method includes the following steps:
Step 10, the time difference sequence that blade passes through tip-timing sensor is calculated, according to time difference sequence construct end of blade Timing vibration measures equivalent model;
In the step 10, specifically include:
Step 11, the theoretical arrival time and actual time of arrival that tip-timing sensor is reached according to blade, when calculating Between difference sequence;
Specifically, it as shown in Fig. 2, I tip-timing sensor 22 is installed on the surrounding of machine circle 21, is equipped in rotor leaf dish M rotating vane 23, the vibration displacement d (t) of each rotating vane can be measured by I tip-timing sensor 22, Setting refers to tip-timing sensor r0The surface of installation and shaft middle line, and a reflective position is set in shaft, with Just a rotary speed reference signal is obtained in each swing circle, wherein tip-timing sensor 22 is circumferentially relative to reference Sensor r0Angle be αi, i=1,2 ..., I, the relative angle of blade in rotational direction is θkK=1,2 ..., M, time Difference sequenceCorresponding calculation formula are as follows:
In formula, R is vane pivot radius, and n is the rotating cycle of blade, frFor the constant speed of blade,It is K blade passes through the actual time of arrival of i-th of tip-timing sensor in the n-th circle,Sample bits are vibrated for end of blade It moves,Pass through the theoretical arrival time of i-th of tip-timing sensor in the n-th circle for k-th of blade.
Step 12, according to time difference sequence and lack sampling principle, blade tip-timing vibration measurement equivalent model is constructed.
Specifically, according to time difference sequence, end of blade vibration sample shift is obtainedCalculation formula, corresponding calculating Formula are as follows:
Since blade tip-timing vibration measuring signal is typical undersampled signal, sets L and put as machine circle is circumferentially distributed The quantity of tip-timing sensor position 24 is set, I is the number of tip-timing sensor 22, and C indicates I tip-timing sensor 22 layout on casing 21.I position installation blade tip-timing is chosen in L mountable tip-timing sensor positions 24 to pass Sensor 22, therefore, the road I sample sequence C={ ci: 1≤i≤I }, wherein 1≤c1< c2... < cI≤ L, ciIt is fixed for i-th of end of blade When sensor position, so the sampling of practical blade tip-timing may be defined as (L, I, C) sampling configuration, for example, mountable end of blade is fixed When sensor position quantity L=20, the number of sensors I of actual installation is 4, selected position C=1,5,11, 17 }, i.e., tip-timing sensor is placed at the 1st, the 5th, the 11st and the 17th 4 position.Therefore, actual sampling sequence number is n × L+C, i.e., as n=0, the sampling sequence number of first lap is C(0)={ 1,5,11,17 }, as n=1, the sampling sequence number of the second circle For C(1)={ 1+20,5+20,11+20,17+20 }, that is to say, that the sampling of tip-timing sensor can be equivalent to adopts from the road L The resampling on the road I is carried out in sample data.
Therefore, k-th of blade passes through the theoretical arrival time of i-th of tip-timing sensor in the n-th circleAnd the setting angle of tip-timing sensor i is αi, therefore, k-th of blade passes through in the n-th circle The theoretical arrival time of i-th of tip-timing sensor are as follows:
The vibration signal of blade k is set as x (t), obtains blade tip-timing vibration measurement equivalent model yi(n), corresponding meter Calculate formula are as follows:
In formula, i=1,2 ..., I, n ∈ Z, δ are dirichlet functions.
Step 20, according to blade tip-timing vibration measurement equivalent model, compressed sensing model is constructed;
In the step 20, specifically include:
Step 21, according to blade tip-timing vibration measurement equivalent model, corresponding matrix equation is calculated;
Specifically, compressed sensing model is set as P0, to blade tip-timing vibration measurement equivalent model yi(n) Fourier is carried out Transformation, corresponding calculation formula are as follows:
In formula, fRFor fundamental frequency section [- fr/ 2, fr/ 2], the frequency separation of blade vibration signal spectrum X (f) is [- fmin, fmax], and according to tip-timing sensor position L can be placed, the entire frequency separation of X (f) is averaged and is divided into L son frequency Band, the frequency bandwidth of sub-band are fr, the definition of first of sub-band is Xl(f)=X (fR+(l-(L+1)/2)fr), l=1, 2 ..., L.
According to compressed sensing basic theory, by the blade tip-timing vibration measurement equivalent model Y after Fourier transformi(f), turn It is changed to matrix equation, corresponding matrix equation Y (f) are as follows:
Y (f)=Φ Xl(f),
In formula, Y (f)=[Y1(f), Y2(f) ..., YI(f)]T, Y (f) is the matrix side of blade tip-timing sampled signal frequency spectrum Journey,Xl(f) be multifrequency blade vibration signal spectrum vector, Φ be with The relevant sensing matrix of tip-timing sensor quantity and position, corresponding formula are as follows:
Step 22, the sparse characteristic shown in a frequency domain according to blade vibration signal, calculating matrix non trivial solution, is denoted as Compressed sensing model;
Specifically, according to sparse characteristic, signal spectrum X (f) just has spectrum only in frequency range, is felt according to compression Know theory, the solution X of calculating matrix equation Y (f)l(f)。
According to the basic theories and formula of compressed sensing, the specific observation expression formula of compressive sensing theory is y=Θ x=Θ Ψ θ=Φ θ, signal accuracy, which restores problem, can be expressed as l0Norm minimum problem,Wherein, Θ For observing matrix, Ψ is the rarefaction representation matrix of signal, and θ is sparse vector of the original signal x in sparse transform-domain, and Φ is to pass Feel matrix.Xl(f) be matrix equation Y (f) most sparse solution, the minimum model that solution matrix equation Y (f) can be expressed as Number l0Vibration measurement process based on blade tip-timing is converted to the sparse Solve problems of compressed sensing model P0 by problem, compression The corresponding calculation formula of sensor model P0 are as follows:
Step 30, according to default number of sensors, calculating meets the tip-timing sensor quantity of compressed sensing model most Excellent solution,
Wherein, in step 30, it specifically includes:
Step 31, the order of the matrix equation of end of blade timing sampling signal spectrum in compressed sensing model is calculated;
Step 32, it according to the relevant sensing matrix of tip-timing sensor quantity in compressed sensing model and position, calculates Cross-correlation coefficient;
Step 33, according to the sum of ranks cross-correlation coefficient of matrix equation, meet default sensor number according to preset formula calculating The maximum positive integer of amount is denoted as tip-timing sensor quantity optimal solution, wherein default calculation formula are as follows:
In formula, | | Xl(f)||0For multifrequency blade vibration signal spectrum vector Xl(f) number of the non-zero row vector in, W are Cross-correlation coefficient, Rank (Y (f)) are the order of matrix equation Y (f),Indicate the maximum positive integer smaller than b, giRepresenting matrix Φ I-th column, gjThe jth of representing matrix Φ arranges.
Specifically, it is assumed that multifrequency blade vibration signal spectrum vector Xl(f) be compressed sensing model P0 solution, work as Xl(f) full Foot | | Xl(f)||0When < spark (Φ)/2, then Xl(f) be compressed sensing model P0 most sparse solution, wherein | | Xl(f)||0For Multifrequency blade vibration signal spectrum vector Xl(f) number of the non-zero row vector in, i.e. the frequency-domain sparse degree of blade vibration signal, Linear relevant minimum column vector number in spark (Φ) representing matrix Φ.
Xl(f) non-zero row only a small number of in, extracts Xl(f) the non-zero row in, is denoted as supported collection IM, multifrequency blade is shaken Dynamic spectral matrix Xl(f) supported collection IMGesture be denoted as p, that is to say, that as supported collection IMGesture p be less than spark (Φ)/2 when, The most sparse solution of compressed sensing model P0 can then be found out.
Further, according to the property Rank (Y (f))≤1 of rank of matrix, therefore, if XlIt (f) is compressed sensing mould Unique sparse solution of type P0, then meet:
In view of being difficult to determination when spark (Φ), therefore, spark (Φ) is replaced to be counted by cross-correlation coefficient W It calculates.The calculation formula of cross-correlation coefficient W are as follows:
In formula, Φ is sensing matrix, giThe i-th column of representing matrix Φ, gjThe jth of representing matrix Φ arranges.
Therefore, it in conjunction with default number of sensors, can use preset formula, show that tip-timing sensor quantity is optimal Solution, the i.e. number of tip-timing sensor, preset formula are as follows:
In formula, operationExpression takes the maximum positive integer smaller than b.
In the present embodiment, the Parameter Conditions of blade vibration signal x (t): maximum frequency f are setmax=790Hz, blade turn Speed is 5000r/min, and sensor position is installed in Tip-Timing Measurement and meets Lfr≥2fmax, mountable blade tip-timing sensing The quantity L=19 of device position can be calculated under multiple-frequency signal vibration blade difference degree of rarefication, blade tip-timing by the above method Tip-timing sensor number required for measuring, as shown in table 1.
Table 1
From table 1 it follows that setting end of blade when the spectrum sparse degree value for choosing multifrequency blade vibration signal is 6 Time Pick-off Units number is 9, be may be implemented to apparatus for rotating vane vibration blade tip-timing precise measurement.
The technical solution for having been described in detail above with reference to the accompanying drawings the application, present applicant proposes a kind of compressed sensing based Tip-timing sensor number determines method, this method comprises: step 10, calculates time of the blade by tip-timing sensor Difference sequence constructs blade tip-timing vibration measurement equivalent model according to time difference sequence;Step 20, it is vibrated and is surveyed according to blade tip-timing Equivalent model is measured, compressed sensing model is constructed;Step 30, according to default number of sensors, calculating meets compressed sensing model Tip-timing sensor quantity optimal solution.The accuracy for improving determining tip-timing sensor quantity is conducive to improve blade The reliability for vibrating real-time detection, reduces a possibility that leading to rotating vane failure because of blade vibration.
Step in the application can be sequentially adjusted, combined, and deleted according to actual needs.
Unit in the application device can be combined, divided and deleted according to actual needs.
Although disclosing the application in detail with reference to attached drawing, it will be appreciated that, these descriptions are only exemplary, not For limiting the application of the application.The protection scope of the application may include not departing from this Shen by appended claims It please be in the case where protection scope and spirit for various modifications, remodeling and equivalent scheme made by inventing.

Claims (3)

1. a kind of compressed sensing based tip-timing sensor number determines method, which is characterized in that this method comprises:
Step 10, the time difference sequence that blade passes through tip-timing sensor is calculated, according to the time difference sequence, building Blade tip-timing vibration measurement equivalent model;
Step 20, according to the blade tip-timing vibration measurement equivalent model, compressed sensing model is constructed;
Step 30, according to default number of sensors, calculating meets the tip-timing sensor quantity of the compressed sensing model most Excellent solution,
Wherein, in step 30, it specifically includes:
Step 31, the order of the matrix equation of end of blade timing sampling signal spectrum in the compressed sensing model is calculated;
Step 32, it according to the relevant sensing matrix of tip-timing sensor quantity and position in the compressed sensing model, calculates Cross-correlation coefficient;
Step 33, the cross-correlation coefficient according to the sum of ranks, according to preset formula, calculating meets the default number of sensors Maximum positive integer, be denoted as the tip-timing sensor quantity optimal solution, wherein default calculation formula are as follows:
In formula, ‖ Xl(f)‖0For multifrequency blade vibration signal spectrum vector Xl(f) number of the non-zero row vector in, W are described mutual Related coefficient, Rank (Y (f)) are the order of the matrix equation Y (f),Indicate the maximum positive integer smaller than b, giIt indicates The i-th column of matrix Φ, gjThe jth of representing matrix Φ arranges.
2. compressed sensing based tip-timing sensor number as described in claim 1 determines method, which is characterized in that its It is characterized in that, in step 10, specifically includes:
Step 11, the theoretical arrival time and actual time of arrival of the tip-timing sensor are reached according to the blade, are counted Evaluation time difference sequence;
Step 12, according to the time difference sequence and lack sampling principle, the blade tip-timing vibration measurement equivalent model is constructed.
3. compressed sensing based tip-timing sensor number as described in claim 1 determines method, which is characterized in that In step 20, specifically include:
Step 21, according to the blade tip-timing vibration measurement equivalent model, corresponding matrix equation is calculated;
Step 22, the sparse characteristic shown in a frequency domain according to blade vibration signal calculates the solution of the matrix equation, is denoted as The compressed sensing model.
CN201811103282.2A 2018-09-20 2018-09-20 Leaf end timing sensor number determination method based on compressed sensing Active CN109101769B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811103282.2A CN109101769B (en) 2018-09-20 2018-09-20 Leaf end timing sensor number determination method based on compressed sensing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811103282.2A CN109101769B (en) 2018-09-20 2018-09-20 Leaf end timing sensor number determination method based on compressed sensing

Publications (2)

Publication Number Publication Date
CN109101769A true CN109101769A (en) 2018-12-28
CN109101769B CN109101769B (en) 2021-09-03

Family

ID=64866950

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811103282.2A Active CN109101769B (en) 2018-09-20 2018-09-20 Leaf end timing sensor number determination method based on compressed sensing

Country Status (1)

Country Link
CN (1) CN109101769B (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109870282A (en) * 2019-03-26 2019-06-11 西安交通大学 Compressed sensing based blade vibration feature identification method and system
CN109883380A (en) * 2019-03-22 2019-06-14 西安交通大学 A kind of rotor blade displacement field measurement method and its system based on blade tip-timing
CN109883379A (en) * 2019-03-22 2019-06-14 西安交通大学 Blade displacement strain measurement method based on Mode Shape
CN109883389A (en) * 2019-03-22 2019-06-14 西安交通大学 A kind of rotating vane dynamic strain field measurement method and its system
CN110896308A (en) * 2019-10-31 2020-03-20 中国工程物理研究院电子工程研究所 Single tone signal reconstruction method
CN111353129A (en) * 2020-02-10 2020-06-30 西安交通大学 Leaf-end timing data storage matrixing processing method
CN112362275A (en) * 2020-10-27 2021-02-12 湖南工业大学 Method and device for reducing timing measurement deviation of blade vibration blade end under variable rotating speed
CN113340244A (en) * 2021-03-04 2021-09-03 北京化工大学 Non-contact type turbine machinery blade vibration displacement monitoring method and device

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101625260A (en) * 2009-07-31 2010-01-13 天津大学 Method for detecting high speed rotating blade synchronous vibration parameters under speed change
EP2199764A2 (en) * 2008-12-16 2010-06-23 Rolls-Royce plc Timing analysis
EP2631617A2 (en) * 2012-02-24 2013-08-28 Rolls-Royce plc Blade Tip Timing Uncertainty
CN105466550A (en) * 2015-12-04 2016-04-06 中国人民解放军国防科学技术大学 Inhomogeneous undersampled blade end timing vibration signal reconstruction method and device
CN105509876A (en) * 2015-12-04 2016-04-20 中国人民解放军国防科学技术大学 Undersampled leaf apex timing vibration signal reconstruction method and device thereof
CN105973448A (en) * 2016-02-02 2016-09-28 南京航空航天大学 Rotating blade vibration measuring method and system
CN107843333A (en) * 2017-07-17 2018-03-27 北京大学 A kind of pipeline radial direction glottis neoplasms detecting system and method based on compressive sensing theory
CN108051078A (en) * 2017-12-12 2018-05-18 湖南工业大学 Blade vibration blade tip-timing on-line monitoring method and device when a kind of rotating speed is non-constant

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2199764A2 (en) * 2008-12-16 2010-06-23 Rolls-Royce plc Timing analysis
CN101625260A (en) * 2009-07-31 2010-01-13 天津大学 Method for detecting high speed rotating blade synchronous vibration parameters under speed change
EP2631617A2 (en) * 2012-02-24 2013-08-28 Rolls-Royce plc Blade Tip Timing Uncertainty
CN105466550A (en) * 2015-12-04 2016-04-06 中国人民解放军国防科学技术大学 Inhomogeneous undersampled blade end timing vibration signal reconstruction method and device
CN105509876A (en) * 2015-12-04 2016-04-20 中国人民解放军国防科学技术大学 Undersampled leaf apex timing vibration signal reconstruction method and device thereof
CN105973448A (en) * 2016-02-02 2016-09-28 南京航空航天大学 Rotating blade vibration measuring method and system
CN107843333A (en) * 2017-07-17 2018-03-27 北京大学 A kind of pipeline radial direction glottis neoplasms detecting system and method based on compressive sensing theory
CN108051078A (en) * 2017-12-12 2018-05-18 湖南工业大学 Blade vibration blade tip-timing on-line monitoring method and device when a kind of rotating speed is non-constant

Non-Patent Citations (3)

* Cited by examiner, † Cited by third party
Title
MINGHAO PAN,ET AL: "Sparse Representation Based Frequency Detection", 《SENSORS》 *
谢勇: "高速旋转叶片异常振动非接触在线检测与诊断技术研究", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 *
陈仲生 等: "基于余数定理的叶端定时欠采样信号处理方法", 《振动、测试与诊断》 *

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109883389B (en) * 2019-03-22 2020-08-25 西安交通大学 Method and system for measuring dynamic strain field of rotating blade
CN109883380A (en) * 2019-03-22 2019-06-14 西安交通大学 A kind of rotor blade displacement field measurement method and its system based on blade tip-timing
CN109883379A (en) * 2019-03-22 2019-06-14 西安交通大学 Blade displacement strain measurement method based on Mode Shape
CN109883389A (en) * 2019-03-22 2019-06-14 西安交通大学 A kind of rotating vane dynamic strain field measurement method and its system
CN109870282A (en) * 2019-03-26 2019-06-11 西安交通大学 Compressed sensing based blade vibration feature identification method and system
CN110896308A (en) * 2019-10-31 2020-03-20 中国工程物理研究院电子工程研究所 Single tone signal reconstruction method
CN110896308B (en) * 2019-10-31 2023-09-12 中国工程物理研究院电子工程研究所 Single-tone signal reconstruction method
CN111353129A (en) * 2020-02-10 2020-06-30 西安交通大学 Leaf-end timing data storage matrixing processing method
CN111353129B (en) * 2020-02-10 2021-12-28 西安交通大学 Leaf-end timing data storage matrixing processing method
CN112362275A (en) * 2020-10-27 2021-02-12 湖南工业大学 Method and device for reducing timing measurement deviation of blade vibration blade end under variable rotating speed
CN112362275B (en) * 2020-10-27 2021-08-13 湖南工业大学 Method and device for reducing timing measurement deviation of blade vibration blade end under variable rotating speed
CN113340244A (en) * 2021-03-04 2021-09-03 北京化工大学 Non-contact type turbine machinery blade vibration displacement monitoring method and device
CN113340244B (en) * 2021-03-04 2023-06-13 北京化工大学 Non-contact turbine mechanical blade vibration displacement monitoring method and device

Also Published As

Publication number Publication date
CN109101769B (en) 2021-09-03

Similar Documents

Publication Publication Date Title
CN109101769A (en) Leaf end timing sensor number determination method based on compressed sensing
CN109101768A (en) Leaf end timing sensor layout optimization design method based on compressed sensing
CN105424160B (en) The method for realizing the identification of blade synchronization vibration parameters
CN110567574B (en) Method and system for identifying timing vibration parameters of blade end of rotating blade
US6584849B2 (en) Analyzing vibration of rotating blades
CN105509876B (en) Lack sampling blade tip-timing vibration signal reconstruction method and its device
CN103363921B (en) A kind of modified three point method turn error, deviation from circular from computing method
US20100179775A1 (en) Determination of blade vibration frequencies and/or amplitudes
CN105466550B (en) Non-homogeneous lack sampling blade tip-timing vibration signal reconstruction method and its device
CN109716077A (en) Use the method and system of Tip-Timing (BTT) monitoring turbine rotor blade
CN108051078A (en) Blade vibration blade tip-timing on-line monitoring method and device when a kind of rotating speed is non-constant
CN103575523A (en) Rotating machine fault diagnosis method based on Fast ICA-spectrum kurtosis-envelope spectrum analysis
CN106382882A (en) Test system and test method of rotating machinery rotor-stator rim field
CN110285879A (en) Based on the contactless vibration detection device of current vortex sensor shrouded blade and method
CN108731896A (en) A kind of vibration monitoring device for gas turbine compressor blade and blade
CN110108467A (en) Active sounding speed-measuring method based on portable mobile apparatus
CN108021064A (en) A kind of power-equipment health status inline diagnosis method
CN101368870B (en) Preparation method of amplitude frequency spectrum used for mechanical rotor single cross section shaft vibration analysis
CN103760376A (en) Engine rotating speed measuring instrument based on vibration principle and test method thereof
Al-Badour et al. Non-stationary vibration signal analysis of rotating machinery via time-frequency and wavelet techniques
CN106092534A (en) Blade modal damping assay method
CN101451882B (en) Short time amplitude frequency spectrum array for single section shaft vibration analysis for mechanical rotor
CN115081271B (en) Leaf end timing system checking method and checking system based on digital simulator
CN105954353A (en) Test method and device of comprehensive acoustic attenuation coefficient
CN109342057A (en) A kind of transmission parts test macro with high-speed data acquisition function

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