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液体火箭发动机高速涡轮泵的振动故障检测
引用本文:朱恒伟,黄卫东,王克昌,陈启智.液体火箭发动机高速涡轮泵的振动故障检测[J].推进技术,1997,18(5):13-16.
作者姓名:朱恒伟  黄卫东  王克昌  陈启智
作者单位:国防科技大学航天技术系!长沙,410073
摘    要:讨论了涡轮泵故障的几个主要原因,据此提取涡轮泵振动数据的特征,用BP神经网络的方法进行故障检测。BP神经网络的训练样本集由一个具有无监督聚类功能的神经网络从原始的特征向量集获取。

关 键 词:液体推进剂火箭发动机  涡轮泵  振动分析  人工神经元网络  故障分析

FAULT DETECTION OF HIGH SPEED TURBOPUMP VIBRATION IN LIQUID PROPELLANT ROCKET ENGINE
Zhu Hengwei,Huang Weidong,Wang Kechang and Chen Qizhi.FAULT DETECTION OF HIGH SPEED TURBOPUMP VIBRATION IN LIQUID PROPELLANT ROCKET ENGINE[J].Journal of Propulsion Technology,1997,18(5):13-16.
Authors:Zhu Hengwei  Huang Weidong  Wang Kechang and Chen Qizhi
Institution:Dept. of Aerospace Technology, National Univ. of Defence Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ. of Defence Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ. of Defence Technology, Changsha, 410073;Dept. of Aerospace Technology, National Univ. of Defence Technology, Changsha, 410073
Abstract:Some main causes of occurred faults in the fuel trubopump of a rocket engine arediscussed. According to these faults, some features for fault detection are summarized from the powerspectrum density of a channel of vibration acceleration signal measured from the turbopump case.Neural networks are used to detect faults. With a BP neural network acting as fault detector, anunsupervised clustering neural network is used to obtain patterns required for training the faultdetector from the original test data characteristic vectors. The validation of the vibration signal inengine ground firing test shows the feasibility and effectiveness of this method.
Keywords:Liquid propellant rocket engine  Turbine pump  Vibration analysis  Artificial neural network  Fault analysis
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