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Principal components analysis of triaxial vibration data from helicopter transmissions

机译:直升机变速器三轴振动数据的主成分分析

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Research on the nature of the vibration data collected from helicopter transmissions during flight experiments has led to several crucial observations believed to be responsible for the high rates of false alarms and missed detections in aircraft vibration monitoring systems. This work focuses on one such finding, namely, the need to consider additional sources of information about system vibrations. In this light, helicopter transmission vibration data, collected using triaxial accelerometers, were explored in three different directions, analyzed for content, and then combined using Principal Components Analysis (PCA) to analyze changes in directionality. In this paper, the PCA transformation is applied to 176 test conditions/data sets collected from an OH5SC helicopter to derive the overall experiment-wide covariance matrix and its principal eigenvectors. The experiment-wide eigenvectors are then projected onto the individual test conditions to evaluate changes and similarities in their directionality based on the various experimental factors. The paper will present the foundations of the proposed approach, addressing the question of whether experiment-wide eigenvectors accurately model the vibration modes in individual test conditions. The results will further determine the value of using directionality and triaxial accelerometers for vibration monitoring and anomaly detection.
机译:在飞行实验期间从直升机传输中收集的振动数据的性质导致了几个重要的观察,据信对飞机振动监测系统的高误报和错过检测负责。这项工作侧重于一个这样的发现,即,需要考虑有关系统振动的其他信息来源。在这种光线下,使用三轴加速度计收集的直升机传输振动数据,以三种不同的方向探讨,分析含量,然后使用主成分分析(PCA)组合来分析方向性的变化。在本文中,PCA转化应用于从OH5SC直升机收集的176个测试条件/数据集,以导出整体实验范围的协方差基质及其主要特征向量。然后将实验范围的特征向量投射到各个测试条件上,以根据各种实验因素评估其方向性的变化和相似性。本文将介绍所提出的方法的基础,解决了实验范围的特征向量是否准确地模拟各个测试条件中的振动模式的问题。结果将进一步确定使用方向性和三轴加速度计进行振动监测和异常检测的值。

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