CN107643180A - High-speed low temperature turbine pump retainer method for diagnosing faults based on wavelet analysis - Google Patents

High-speed low temperature turbine pump retainer method for diagnosing faults based on wavelet analysis Download PDF

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Publication number
CN107643180A
CN107643180A CN201610579755.0A CN201610579755A CN107643180A CN 107643180 A CN107643180 A CN 107643180A CN 201610579755 A CN201610579755 A CN 201610579755A CN 107643180 A CN107643180 A CN 107643180A
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China
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frequency
turbine pump
retainer
vibration signal
low temperature
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CN201610579755.0A
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Inventor
黄锦殿
王慧
潘亮
何伟锋
袁洁
康红雷
金富贵
孙慧娟
庞红丽
胡坚勇
刘建方
张中洲
郭军
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Beijing Aerospace Propulsion Institute
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Beijing Aerospace Propulsion Institute
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Priority to CN201610579755.0A priority Critical patent/CN107643180A/en
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Pending legal-status Critical Current

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Abstract

The invention belongs to oxyhydrogen engine turbine pump fault diagnosis technology field, and in particular to a kind of high-speed low temperature turbine pump retainer method for diagnosing faults based on wavelet analysis.Comprise the following steps:Step 1:By the structural parameters of bearing and the state that operated at that time, theoretical calculation obtains rolling bearing retainer fault characteristic frequency;Step 2:Fast Fourier analysis are carried out to turbine pump vibration signal, obtain the substantially frequency distribution situation of vibration signal;Step 3:Select wavelet basis function so that the characteristic frequency to be analyzed avoids the occurrence of frequency and mix phenomenon near the centre frequency of appropriate frequency range;Discrete wavelet analysis is carried out to turbine pump vibration signal;Step 4:Short-time Fourier analysis is carried out to the frequency range where retainer fault characteristic frequency.The present invention analyzes and processes with wavelet analysis with the method that Short Time Fourier Analysis is combined to turbine pump vibration signal, realizes and high-speed low temperature turbine pump rolling bearing retainer is monitored.

Description

High-speed low temperature turbine pump retainer method for diagnosing faults based on wavelet analysis
Technical field
The invention belongs to oxyhydrogen engine turbine pump fault diagnosis technology field, and in particular to a kind of based on wavelet analysis High-speed low temperature turbine pump retainer method for diagnosing faults.
Background technology
Turbine pump is operated under extreme physical condition as one of part crucial in hydrogen-oxygen rocket, and with height Speed, high pressure, high flow capacity and high-power feature.In oxyhydrogen engine turbine pump configuration, high-speed low temperature rolling bearing, especially Its retainer, it is one of incident critical piece of failure.High-speed low temperature rolling bearing be in high speed, low temperature, high pressure, sealing Working environment.
Under normal circumstances, the sensor that turbine pump vibration is monitored on oxyhydrogen engine is arranged in turbine pump case, so The background noise environment for causing the vibration signal of collection to include large amount of complex.Moreover, high-speed low temperature rolling bearing retainer, because of it For material using the relatively weak nonmetallic materials of intensity and rigidity, then its fault characteristic frequency vibration level is smaller, compares appearance Easily it is buried under the background noise of complexity.
Using the fault diagnosis technology of routine, the fault characteristic frequency of high-speed low temperature retainer is difficult to be identified Come, and then the effect differentiated to hydrogen turbopump retainer health status can be influenceed.
The content of the invention
It is an object of the invention to provide a kind of high-speed low temperature turbine pump retainer failure based on wavelet analysis to examine Disconnected method, realize that accurately and effectively health status differentiates to high-speed low temperature turbine pump rolling bearing retainer.
To reach above-mentioned purpose, the technical solution used in the present invention is:
A kind of high-speed low temperature turbine pump retainer method for diagnosing faults based on wavelet analysis, comprises the following steps:
Step 1:By the structural parameters of bearing and the state that operated at that time, theoretical calculation obtains rolling bearing retainer Fault characteristic frequency;
In formula:F represents retainer fault characteristic frequency;D represents rolling element diameter;D represents pitch diameter;α represents contact Angle, the angle for the line in common point of contact and the center of circle with vertical line;N represents axle frequency;
Step 2:Fast Fourier analysis are carried out to turbine pump vibration signal, obtain the substantially frequency distribution of vibration signal Situation;
Step 3:Result based on step 1 and step 2, select wavelet basis function so that the characteristic frequency to be analyzed Near the centre frequency of appropriate frequency range, avoid the occurrence of frequency and mix phenomenon;Discrete wavelet analysis is carried out to turbine pump vibration signal;
Step 4:Short-time Fourier analysis is carried out to the frequency range where retainer fault characteristic frequency, extracts it exactly Fault characteristic frequency, realize and the development trend of retainer fault characteristic frequency is effectively monitored, to differentiate high-speed low temperature The health status of turbine pump rolling bearing.
Db16 wavelet basis functions are selected, 7 layer scattering wavelet analysises are carried out to vibration signal, obtain 7 radio-frequency components and 1 It is 625Hz~312Hz that low-frequency component, wherein d6 frequency ranges, which include frequency, and the fault characteristic frequency of retainer is in this frequency range.
Having the beneficial effect that acquired by the present invention:
The present invention divides turbine pump vibration signal with wavelet analysis with the method that Short Time Fourier Analysis is combined Analysis is handled, and realizes and high-speed low temperature turbine pump rolling bearing retainer is monitored.The present invention is applied to more Upper Stages And the health status of high thrust oxyhydrogen engine high-speed low temperature turbine pump rolling bearing retainer differentiates.Certain model Upper Stage, In certain model high thrust oxyhydrogen engine high-speed low temperature turbine pump 6 fracture defect of rolling bearing retainer, using the present invention's Method for diagnosing faults 100% is successfully diagnosed to be.The present invention turns into oxyhydrogen engine high-speed low temperature turbine pump rolling bearing retainer The Main Means that health status differentiates.
Brief description of the drawings
Fig. 1 is the high-speed low temperature turbine pump retainer method for diagnosing faults flow chart based on wavelet analysis;
Fig. 2 is turbine pump vibration signal fast Fourier analysis figure;
Fig. 3 is turbine pump vibration signal discrete wavelet analysis chart;
Fig. 4 is turbine pump vibration signal d6 frequency range Short-time Fourier analysis charts when retainer does not break down;
Turbine pump vibration signal d6 frequency range Short-time Fourier analysis charts when Fig. 5 breaks down for retainer.
Embodiment
The present invention is described in detail with specific embodiment below in conjunction with the accompanying drawings.
As shown in figure 1, the high-speed low temperature turbine pump retainer fault diagnosis side of the present invention based on wavelet analysis Method comprises the following steps:
Step 1:By the structural parameters of bearing and the state that operated at that time, theoretical calculation obtains rolling bearing retainer Fault characteristic frequency;
In formula:F represents retainer fault characteristic frequency;D represents rolling element diameter;D represents pitch diameter;α represents contact Angle, the angle for the line in common point of contact and the center of circle with vertical line;Z represents rolling element number;N represents axle frequency.
Step 2:Fast Fourier analysis are carried out to turbine pump vibration signal, obtain the substantially frequency distribution of vibration signal Situation;
Step 3:Result based on step 1 and step 2, selects suitable wavelet basis function so that the spy to be analyzed Frequency is levied near the centre frequency of appropriate frequency range, frequency is avoided the occurrence of and mixes phenomenon.Turbine pump vibration signal is carried out discrete small Wave analysis;
Step 4:Short-time Fourier analysis is carried out to the frequency range where retainer fault characteristic frequency, extracts it exactly Fault characteristic frequency, realize and the development trend of retainer fault characteristic frequency is effectively monitored, to differentiate high-speed low temperature The health status of turbine pump rolling bearing.
The structural parameters of certain the model oxyhydrogen engine turbine pump high-speed low temperature rolling bearing of table 1
The geometrical structure parameter that rotational frequency with reference to turbine pump work is about n=1100Hz with the bearing of table 1, can be with Obtain table 2.
The high-speed low temperature rolling bearing retainer fault characteristic frequency of table 2
Contact angle α/° 17 18 19 20
Failure-frequency f/Hz 443.3 443.9 444.5 445.2
Turbine pump turbine end vibration signal is analyzed and processed with fast Fourier analysis, obtains vibration signal frequency Substantially distribution situation, see Fig. 2.
With reference to high-speed low temperature turbine pump retainer fault characteristic frequency and vibration signal fast Fourier analysis situation, The present invention selects db16 wavelet basis functions.7 layer scattering wavelet analysises are carried out to this section of vibration signal, obtain 7 radio-frequency components and 1 Individual low-frequency component, is shown in Fig. 3.It is 625Hz~312Hz that wherein d6 frequency ranges, which include frequency, and the fault characteristic frequency of retainer is just herein Frequency range.Fig. 4, Fig. 5 can be obtained by carrying out analysis to this frequency range with Short-time Fourier analysis.

Claims (2)

  1. A kind of 1. high-speed low temperature turbine pump retainer method for diagnosing faults based on wavelet analysis, it is characterised in that:Including Following steps:
    Step 1:By the structural parameters of bearing and the state that operated at that time, theoretical calculation obtains rolling bearing retainer failure Characteristic frequency;
    <mrow> <mi>f</mi> <mo>=</mo> <mfrac> <mi>n</mi> <mn>2</mn> </mfrac> <mrow> <mo>(</mo> <mn>1</mn> <mo>-</mo> <mi>d</mi> <mi> </mi> <mi>c</mi> <mi>o</mi> <mi>s</mi> <mi>&amp;alpha;</mi> <mo>/</mo> <mi>D</mi> <mo>)</mo> </mrow> </mrow>
    In formula:F represents retainer fault characteristic frequency;D represents rolling element diameter;D represents pitch diameter;α represents contact angle, is Angle of the line in point of contact and the center of circle with vertical line altogether;N represents axle frequency;
    Step 2:Fast Fourier analysis are carried out to turbine pump vibration signal, obtain the substantially frequency distribution situation of vibration signal;
    Step 3:Result based on step 1 and step 2, select wavelet basis function so that the characteristic frequency to be analyzed is suitable Near the centre frequency of frequency range, avoid the occurrence of frequency and mix phenomenon;Discrete wavelet analysis is carried out to turbine pump vibration signal;
    Step 4:Short-time Fourier analysis is carried out to the frequency range where retainer fault characteristic frequency, extracts its failure exactly Characteristic frequency, realize and the development trend of retainer fault characteristic frequency is effectively monitored, to differentiate high-speed low temperature turbine The health status of pump rolling bearing.
  2. 2. the high-speed low temperature turbine pump retainer method for diagnosing faults according to claim 1 based on wavelet analysis, It is characterized in that:Select db16 wavelet basis functions, to vibration signal carry out 7 layer scattering wavelet analysises, obtain 7 radio-frequency components with It is 625Hz~312Hz that 1 low-frequency component, wherein d6 frequency ranges, which include frequency, and the fault characteristic frequency of retainer is in this frequency range.
CN201610579755.0A 2016-07-21 2016-07-21 High-speed low temperature turbine pump retainer method for diagnosing faults based on wavelet analysis Pending CN107643180A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109635468A (en) * 2018-12-18 2019-04-16 太原理工大学 A kind of angular contact ball bearing cage stability prediction method
WO2019153388A1 (en) * 2018-02-12 2019-08-15 大连理工大学 Power spectral entropy random forest-based aeroengine rolling bearing fault diagnosis method
WO2019200624A1 (en) * 2018-04-20 2019-10-24 江苏大学 Comprehensive evaluation method for pump flow induced vibration performance

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020186039A1 (en) * 2001-05-01 2002-12-12 Devaney Michael J. Motor bearing damage detection via wavelet analysis of the starting current transient
CN103018043A (en) * 2012-11-16 2013-04-03 东南大学 Fault diagnosis method of variable-speed bearing
CN103424258A (en) * 2013-08-06 2013-12-04 昆明理工大学 Fault diagnosis method for rolling bearing
CN103575535A (en) * 2013-11-26 2014-02-12 南车株洲电力机车研究所有限公司 Method and device for judging fault of wind electricity doubly-fed generator rolling bearing
CN105547698A (en) * 2015-12-31 2016-05-04 新疆金风科技股份有限公司 Fault diagnosis method and apparatus for rolling bearing

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020186039A1 (en) * 2001-05-01 2002-12-12 Devaney Michael J. Motor bearing damage detection via wavelet analysis of the starting current transient
CN103018043A (en) * 2012-11-16 2013-04-03 东南大学 Fault diagnosis method of variable-speed bearing
CN103424258A (en) * 2013-08-06 2013-12-04 昆明理工大学 Fault diagnosis method for rolling bearing
CN103575535A (en) * 2013-11-26 2014-02-12 南车株洲电力机车研究所有限公司 Method and device for judging fault of wind electricity doubly-fed generator rolling bearing
CN105547698A (en) * 2015-12-31 2016-05-04 新疆金风科技股份有限公司 Fault diagnosis method and apparatus for rolling bearing

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
付强 主编: "《水资源系统分析》", 30 June 2012 *
黄锦殿: "基于小波分析的氢涡轮泵低温轴承保持架故障特征辨识", 《火箭推进》 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019153388A1 (en) * 2018-02-12 2019-08-15 大连理工大学 Power spectral entropy random forest-based aeroengine rolling bearing fault diagnosis method
US11333575B2 (en) 2018-02-12 2022-05-17 Dalian University Of Technology Method for fault diagnosis of an aero-engine rolling bearing based on random forest of power spectrum entropy
WO2019200624A1 (en) * 2018-04-20 2019-10-24 江苏大学 Comprehensive evaluation method for pump flow induced vibration performance
GB2586756A (en) * 2018-04-20 2021-03-03 Univ Jiangsu Comprehensive evaluation method for pump flow induced vibration performance
GB2586756B (en) * 2018-04-20 2021-09-08 Univ Jiangsu Comprehensive evaluation method for flow-induced vibration performance of pump
CN109635468A (en) * 2018-12-18 2019-04-16 太原理工大学 A kind of angular contact ball bearing cage stability prediction method
CN109635468B (en) * 2018-12-18 2023-02-03 太原理工大学 Method for predicting stability of angular contact ball bearing retainer

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Application publication date: 20180130