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Helicopter Transmission Diagnostics using Constrained Adaptive Lifting

机译:直升机传输诊断使用约束自适应提升

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This paper presents a methodology for detecting and diagnosing gear faults in the planetary stage of a helicopter transmission. This diagnostic technique is based on the constrained adaptive lifting algorithm. The lifting scheme, developed by Wim Sweldens of Bell Labs, is a time domain, prediction-error realization of the wavelet transform that allows for greater flexibility in the construction of wavelet bases. Classic lifting analyzes a given signal using wavelets derived from a single fundamental basis function. A number of researchers have proposed techniques for adding adaptivity to the lifting scheme, allowing the transform to choose from a set of fundamental bases the basis that best fits the signal. This characteristic is desirable for gear diagnostics as it allows the technique to tailor itself to a specific transmission by selecting a set of wavelets that best represent vibration signals obtained while the gearbox is operating under healthy-state conditions. However, constraints on certain basis characteristics are necessary to enhance the detection of local wave-form changes caused by certain types of gear damage. The proposed methodology analyzes individual tooth-mesh waveforms from a healthy-state gearbox vibration signal that was generated using the vibration separation (synchronous signal-averaging) algorithm. Each waveform is separated into analysis domains using zeros of its slope and curvature. The bases selected in each analysis domain are chosen to minimize the prediction error, and constrained to have the same-sign local slope and curvature as the original signal. The resulting set of bases is used to analyze future-state vibration signals and the lifting prediction error is inspected. The constraints allow the transform to effectively adapt to global amplitude changes, yielding small prediction errors. However, local wave-form changes associated with certain types of gear damage are poorly adapted, causing a significant change in the prediction error. The constrained adaptive lifting diagnostic algorithm is validated using data collected from the University of Maryland Transmission Test Rig and the results are discussed.
机译:本文介绍了用于检测和诊断直升机传输的行星级的齿轮故障的方法。该诊断技术基于受约束的自适应提升算法。由WIM开发的贝尔实验室开发的提升方案是一个时域,预测误差实现了小波变换,允许在小波底座的构造中具有更大的灵活性。经典提升使用从单个基础函数的小波获得的给定信号。许多研究人员已经提出了用于向提升方案增加适应性的技术,允许转换从一组基础基础上选择最能拟拟合信号的基础。这个特性是理想的齿轮诊断,因为它允许技术裁缝本身的特定的发送通过选择一组最能代表获得的振动信号,而变速箱健康状态条件下操作的子波。然而,在某些基础特征上的约束是为了增强由某些类型的齿轮损坏引起的局部波形变化的检测是必要的。所提出的方法从使用振动分离(同步信号平均)算法产生的健康状态齿轮箱振动信号中分析各个齿网波形。每个波形都使用斜率和曲率的零分离成分析域。选择在每个分析域中选择的基础以最小化预测误差,并约束为具有与原始信号的相同符号局部斜率和曲率。得到的一组碱基用于分析未来状态振动信号,并检查提升预测误差。约束允许变换有效地适应全局幅度变化,产生小的预测误差。然而,与某些类型的齿轮损伤相关联的局部波形变化适应很差,导致预测误差的显着变化。使用从马里兰州传输试验台收集的数据进行验证约束的自适应提升诊断算法,并讨论了结果。

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