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Leak Detection in Spacecraft Using a 64-Element Multiplexed Passive Array to Monitor Structure-Borne Noise

机译:使用64元件复用无源阵列在航天器中泄漏检测,以监测结构传承的噪声

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We demonstrate an array sensor method intended to locate leaks in manned spacecraft using leak-generated, structure-borne ultrasonic noise. We have developed and tested a method for sensing and processing leak noise to reveal the leak location involving the use of a 64-element phased-array. Cross-correlations of ultrasonic noise waveforms from a leak into vacuum have been used with a phased-array analysis to find the direction from the sensor to the leak. This method measures the propagation of guided ultrasonic Lamb waves passing under the PZT array sensor in the spacecraft skin structure. This paper will describe the custom-designed array with integrated electronics, as well as the performance of the array in prototype applications. We show that this method can be used to successfully locate leaks to within a few millimeters on a 0.6-m square aluminum plate.
机译:我们展示了一种阵列传感器方法,用于使用泄漏产生的结构传播的超声波噪声定位载人航天器中的泄漏。我们已经开发并测试了一种用于传感和处理泄漏噪声的方法,以显示涉及使用64元件相控阵的泄漏位置。从泄漏到真空中的超声噪声波形的互相关已经用于分阶段阵列分析,以找到从传感器到泄漏的方向。该方法测量在航天器皮肤结构中通过PZT阵列传感器下方的引导超声羔羊波的传播。本文将描述具有集成电子设备的定制设计阵列,以及原型应用中的数组的性能。我们表明该方法可用于成功定位泄漏到0.6米方铝板上的几毫米​​内。

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