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Turbopump fault detection algorithm based on protruding frequency components RMS and SVM

机译:基于突出频率分量RMS和SVM的涡轮泵故障检测算法

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A fault detection algorithm based on protruding frequency components RMS (Root Mean Square) and SVM (Support Vector Machine) was proposed for LRE (Liquid Rocket Engine) turbopump real-time fault detection. In the algorithm, contribution coefficient and contribution limit were proposed to find protruding frequency components which have greater contribution to the frequency spectrum changes than other frequency components. The algorithm firstly divides the signal frequency spectrum into several bands. Secondly, in every frequency band the algorithm selects all the protruding frequency components and computes their RMS value. Thirdly the algorithm combines the RMS values of all frequency bands to construct a multi-dimensional vector as a fault feature. At last the algorithm uses the fault feature vectors got from historical signals to construct the SVM training sample set, and obtains SVM classifier which can be used in turbopump real-time fault detection. We used some historical vibration acceleration signals of a certain type of turbopump to validate the algorithm. The test results showed that the algorithm met the demands of accuracy and real-time ability.
机译:提出了一种基于凸频分量RMS(均方根)和SVM(支持向量机)的故障检测算法,用于LRE(液体火箭发动机)涡轮泵实时故障检测。在该算法中,提出了贡献系数和贡献极限,以找到比其他频率分量对频谱变化的贡献更大的突出频率分量。该算法首先将信号频谱划分为几个频带。其次,在每个频带中,算法都会选择所有突出的频率分量并计算其RMS值。第三,该算法结合了所有频段的RMS值,以构建多维矢量作为故障特征。最后,该算法利用从历史信号中得到的故障特征向量来构造SVM训练样本集,并获得了可用于Turbopump实时故障检测的SVM分类器。我们使用某些类型的涡轮泵的历史振动加速度信号来验证算法。测试结果表明,该算法满足了精度和实时性的要求。

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