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A system for the analysis of jet engine vibration data

机译:喷气发动机振动数据分析系统

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摘要

A system has been developed to extract diagnostic information from jet engine carcass vibration data. The system consists of a number of modules, each of which focuses on particular subsets of the data known to hold valuable information. Two ofthese modules, based on neural network techniques, are described in detail in this paper. In the first module, novelty detection provides a measure of how unusual the shape of a vibration signature is, by learning a representation of normality basedentirely on normal examples. The low-dimensional vectors which encode vibration signatures are normalised by an appropriate transform before their distribution is modelled by a few kernels, whose placement is optimised by clustering techniques. Novelty is then measured as the local distance from the nearest kernel centre. This method provides good separation between usual and unusual vibration signatures but, given the small number of examples of normal engines, the resulting representation of normalitymay be overfitting the training data. The severity of this effect is investigated for two different normalising transforms. The second module detects sudden transitions in vibration signature curves. A multilayer-perceptron is trained to predict onestep-ahead for curves without these unexpected transitions. Sudden transitions in the test engine data are then reported whenever the prediction error exceeds a predetermined threshold.
机译:已经开发出一种从喷气发动机机体振动数据中提取诊断信息的系统。该系统由许多模块组成,每个模块集中于已知可保存有价值信息的特定数据子集。本文详细介绍了这两个基于神经网络技术的模块。在第一个模块中,新颖性检测通过完全基于正常示例学习正常性的表示,从而提供了一种测量振动信号形状异常的方法。编码振动信号的低维向量通过适当的变换进行归一化,然后通过几个内核对它们的分布进行建模,然后通过聚类技术对其位置进行优化。然后,将新颖性衡量为距最近内核中心的本地距离。这种方法可以很好地区分常规振动信号和异常振动信号,但是,鉴于正常发动机的实例较少,因此,正常性的结果表示可能会过度拟合训练数据。对于两个不同的归一化转换,研究了这种影响的严重性。第二个模块检测振动特征曲线中的突然转变。训练多层感知器可预测曲线的一步一步,而不会出现这些意外的过渡。每当预测误差超过预定阈值时,就会报告测试引擎数据中的突然转变。

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