PDF下载 分享
[1]臧东情,秦雷,何伟锋,等.基于EMD-Hilbert包络谱分析的涡轮泵轴承故障特征识别[J].火箭推进,2023,49(05):59-65.
 ZANG Dongqing,QIN Lei,HE Weifeng,et al.Fault feature identification of turbopump bearings based on EMD-Hilbert envelope spectrum analysis[J].Journal of Rocket Propulsion,2023,49(05):59-65.
点击复制

基于EMD-Hilbert包络谱分析的涡轮泵轴承故障特征识别

参考文献/References:

[1] 刘子俊,冯勇,陈景龙,等.基于多源数据的液体火箭发动机智能异常检测[J].火箭推进,2022,48(3):79-86.
LIU Z J,FENG Y,CHEN J L,et al.Intelligent anomaly detection of liquid rocket engine with multi-source data[J].Journal of Rocket Propulsion,2022,48(3):79-86.
[2] 郭霄峰.液体火箭发动机试验[M].北京:中国宇航出版社,1991.
[3] 宋征宇.运载火箭远程故障诊断技术综述[J].宇航学报,2016,37(2):135-144.
[4] 戴屹梅,张和生,方柯.基于导航定位原理的火箭涡轮泵轴承故障诊断[J].宇航学报,2019,40(3):286-294.
[5] 王奉涛,苏文胜.滚动轴承故障诊断与寿命预测[M].北京:科学出版社,2018.
[6] BOUDIAF A,MOUSSAOUI A,DAHANE A,et al.A comparative study of various methods of bearing faults diagnosis using the case western reserve university data[J].Journal of Failure Analysis and Prevention,2016,16(2):271-284.
[7] SMITH W A,RANDALL R B.Rolling element bearing diagnostics using the Case Western Reserve University data:A benchmark study[J].Mechanical Systems and Signal Processing,2015,64/65:100-131.
[8] 栾孝驰,沙云东,柳贡民,等.基于WPD-KVI-Hilbert变换相结合的滚动轴承早期故障特征精准识别[J].推进技术,2022,43(2):362-373.
[9] YUAN S F,CHU F L.Support vector machines-based fault diagnosis for turbo-pump rotor[J].Mechanical Systems and Signal Processing,2006,20(4):939-952.
[10] WIDODO A,YANG B S,HAN T.Combination of independent component analysis and support vector machines for intelligent faults diagnosis of induction motors[J].Expert Systems with Applications,2007,32(2):299-312.
[11] WANG J H,QIAO L Y,YE Y Q.Fractional envelope analysis for rolling element bearing weak fault feature extraction[J].IEEE/CAA Journal of Automatica Sinica,2017,4(2):353-360.
[12] CHEN J L,LI Z P,PAN J,et al.Wavelet transform based on inner product in fault diagnosis of rotating machinery:A review[J].Mechanical Systems and Signal Processing,2016,70/71:1-35.
[13] HUANG N E,SHEN Z,LONG S R,et al.The empirical mode decomposition and the Hilbert spectrum for nonlinear and non-stationary time series analysis[J].Proceedings of the Royal Society A:Mathematical,Physical and Engineering Sciences,1998,454(1971):903-995.
[14] LEI Y G,LIN J,HE Z J,et al.A review on empirical mode decomposition in fault diagnosis of rotating machinery[J].Mechanical Systems and Signal Processing,2013,35(1/2):108-126.
[15] 李思琦,蒋志坚.基于EEMD-CNN的滚动轴承故障诊断方法[J].机械强度,2020,42(5):1033-1038.
[16] KING F W.Hilbert transforms[M].Cambridge:Cambridge University Press,2009.
[17] 何正嘉,訾艳阳,张西宁.现代信号处理及工程应用[M].西安:西安交通大学出版社,2007.
[18] RAI A,UPADHYAY S H.A review on signal processing techniques utilized in the fault diagnosis of rolling element bearings[J].Tribology International,2016,96:289-306.

相似文献/References:

[1]霍世慧,袁军社,徐学军,等.双推力室机架快速优化设计方法研究[J].火箭推进,2015,41(04):55.
 HUO Shihui,YUAN Junshe,XU Xuejun,et al.A rapid optimization design method for frame structure of double thrust chambers[J].Journal of Rocket Propulsion,2015,41(05):55.
[2]沈传兵,苏 杭,朱子勇.基于PLC和WinCC的火箭发动机热真空试验控制系统[J].火箭推进,2015,41(03):93.
 SHEN Chuan-bing,SU Hang,ZHU Zi-yong.Control system for liquid rocket engine heat-vacuum test based on PLC and WinCC[J].Journal of Rocket Propulsion,2015,41(05):93.
[3]刘万龙,牛向楠,李全令,等.一种姿轨控发动机地面试验控制系统设计[J].火箭推进,2015,41(02):114.
 LIU Wan-long,NIU Xiang-nan,LI Quan-ling,et al.Design of a ground test control system for attitude and orbital control engine[J].Journal of Rocket Propulsion,2015,41(05):114.
[4]段文浩,于 涛,杨 莹.辐射式热流测量系统及其应用[J].火箭推进,2014,40(01):85.
 DUAN Wen-hao,YU Tao,YANG Ying.Radiant heat flux measuring system and its application[J].Journal of Rocket Propulsion,2014,40(05):85.
[5]朱子环,耿卫国,管 理,等.某型号大推力火箭发动机试验推力测量不确定度评定[J].火箭推进,2012,38(05):81.
 ZHU Zi-huan,GENG Wei-guo,GUAN Li,et al.Assessment of thrust measurement uncertainty for test of large thrust rocket engine[J].Journal of Rocket Propulsion,2012,38(05):81.
[6]周奎,吴伟亮,张玫宝.火箭发动机喷雾均匀性数值分析[J].火箭推进,2010,36(02):26.
 Zhou Kui,Wu Weiliang,Zhang Meibao.Numerical analysis on uniformity of spray in rocket engines[J].Journal of Rocket Propulsion,2010,36(05):26.
[7]张涛,唐虎,周江平,等.可贮存推进剂泵压式液体火箭发动机多次起动系统研究[J].火箭推进,2010,36(03):15.
 Study on the multi-start system of turbopump-fed rocket engine with storable propellants[J].Journal of Rocket Propulsion,2010,36(05):15.
[8]刘小勇,李君,周云端.液体火箭发动机声振环境试验及统计能量分析研究[J].火箭推进,2010,36(03):49.
 Liu Xiaoyong,Li Jun,Zhou Yunduan.Measurement and analysis of noise field of rocket engine based on statistical energy analysis[J].Journal of Rocket Propulsion,2010,36(05):49.
[9]刘永兴,王 魁,曹再勇.RBCC推进系统主火箭发动机气氧/煤油推力室研究[J].火箭推进,2009,35(06):23.
 Liu Yongxing,Wang Kui,Cao Zaiyong.Investigation of GO2/kerosene thrust chamber of the main rocket engine for the RBCC propulsion system[J].Journal of Rocket Propulsion,2009,35(05):23.
[10]袁晓峰,许化龙,徐志高.液体火箭发动机诊断知识挖掘系统设计[J].火箭推进,2008,34(03):44.
 Yuan Xiaofeng,Xu Hualong,Xu Zhigao.Design of diagnostic knowledge mining system for liquid propellant rocket engine[J].Journal of Rocket Propulsion,2008,34(05):44.

备注/Memo

收稿日期:2022-08-03; 修回日期:2022-09-26
作者简介:臧东情(1994—),女,硕士,研究领域为液体火箭发动机冷态试验测控技术。

更新日期/Last Update: 1900-01-01