航天推进技术研究院主办
SUN Bai-hong,SONG Shao-wei.Feature extraction for measurement signal of engine rotary inertia moment based on wavelet analysis[J].Journal of Rocket Propulsion,2010,36(06):52-55.
基于小波分析的发动机转动惯量测量信号特征提取
- Title:
- Feature extraction for measurement signal of engine rotary inertia moment based on wavelet analysis
- 文章编号:
- 1672-9374(2010)06-0052-04
- Keywords:
- engine; wavelet analysis; feature extraction
- 分类号:
- V434.12-33
- 文献标志码:
- A
- 摘要:
- 在采用单摆法进行某型号发动机整机转动惯量测量中,发现测量信号含有许多其他信号成分,这给准确提取发动机转动惯量相关参数带来一定的干扰。利用小波多分辨分析特性对测量信号进行处理分析,有效地将实际有用信号和干扰信号分开。通过对有用信号的分析,准确提取到了整个振动系统的振动频率、对数衰减及阻尼系数等参数,并分析了系统阻尼对振动频率的影响;通过对干扰信号的特征分析,弄清了干扰源,发现了实验设备存在的工艺缺陷。将小波分析应用于发动机实际工程测试和分析,能准确提取结构动力学参数、提高测量精度及进行故障分析。
- Abstract:
- Some undesired signals which brought some difficulties for extracting parameters of engine inertia moment were found in a certain engine inertia moment measurement. The useful signals were separated from the undesired signals through the wavelet multi-resolution-analysis. Some engine parameters such as vibrational frequency, logarithmic decrement and the damping ratio were obtained from the useful signals. The impact of the damping on the vibrational frequency of the system was also analyzed. The interference sources and the technique defects were found by the feature analysis of the undesired signals. Results show that the wavelet analysis is a useful tool that may be used to extract the structural dynamic parameters, improve the measurement accuracy and locate the damage in the engine system.
相似文献/References:
[1]胡海峰,高新妮,凌前程,等.火箭发动机喷管分离流动仿真分析[J].火箭推进,2014,40(06):21.
HU Hai-feng,GAO Xin-ni,LING Qian-cheng,et al.Simulation analysis on separation flow in
rocket engine nozzle[J].Journal of Rocket Propulsion,2014,40(06):21.
[2]黄锦殿,柴卫东.基于小波分析的氢涡轮泵低温轴承保持架故障特征辨识[J].火箭推进,2011,37(02):43.
HUANG Jin-dian,CHAI Wei-dong.Fault identification based on wavelet analysis for bearing cage of hydrogen turbopump[J].Journal of Rocket Propulsion,2011,37(06):43.
[3]施先旺.基于DSP/BIOS实现发动机实时在线状态监测[J].火箭推进,2010,36(05):54.
SHI Xian-wang.Real-time on-line state monitoring of an engine based on DSP/BIOS[J].Journal of Rocket Propulsion,2010,36(06):54.
[4]袁晓峰,许化龙,陈淑红,等.基于相似匹配的液体火箭发动机
故障模式挖掘[J].火箭推进,2008,34(04):48.
Yuan Xiaofeng,Xu Hualong,Chen Shuhong,et al.Similarity-search based mining for fault mode
of liquid rocket engine[J].Journal of Rocket Propulsion,2008,34(06):48.
[5]董寻虎,张晓漫.某火箭发动机系统振动特性测试和仿真分析[J].火箭推进,2006,32(01):54.
Dong Xunhu,Zhang Xiaoman.Dynamics test and simulation of a launch vehicle engine system[J].Journal of Rocket Propulsion,2006,32(06):54.
[6]吴汉基,蒋远大,张志远,等.微小卫星的在轨推进技术[J].火箭推进,2006,32(03):40.
Wu Hanji,Jiang Yuanda,Zhang Zhiyuan,et al.On-board propulsion technologies for micro/minisatellites[J].Journal of Rocket Propulsion,2006,32(06):40.
[7]胡伟,李平.双组元轨控发动机声腔技术方案及试验验证[J].火箭推进,2006,32(05):7.
Hu Wei,Li Ping.The acoustic cavity technique options and test validation of the bipropellant orbit control rocket engine[J].Journal of Rocket Propulsion,2006,32(06):7.
[8]靳爱国.蓄压器对发动机试车液路固有频率影响分析[J].火箭推进,2005,31(05):15.
Jin Aiguo.Effect of buffer on frequency of engine flow system in hot tests[J].Journal of Rocket Propulsion,2005,31(06):15.
[9]张赤民.某发动机燃料节流阀特性研究[J].火箭推进,2004,(01):20.
[10]谭松林,张金容.可靠性增长技术在载人航天发动机研制中的应用[J].火箭推进,2004,(04):41.
Tan Songlin,Zhang Jinrong.The Application of Reliability Increasing in the Manned Spaceflight Rocket Engine[J].Journal of Rocket Propulsion,2004,(06):41.
备注/Memo
收稿日期:2010-09-11;修回日期:2010-10-20
基金项目:国家航天技术支撑项目
作者简介: 孙百红(1976—),女,硕士,研究领域为发动机结构强度分析与数据处理