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Leak detection in spacecraft using structure-borne noise with distributed sensors

机译:使用结构噪声和分布式传感器在航天器中进行泄漏检测

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摘要

We have developed and tested in the laboratory a method for in-orbit detection and location of air leaks in manned spacecraft that uses only a small number of sensors distributed arbitrarily on the inner surface of the spacecraft skin. Then, structure-borne ultrasound in the range of 300–600 kHz is monitored from each of the sensors. When cross correlations between measured sensor waveforms indicate the presence of a leak, these correlations are compared with a large dynamically generated database of simulated correlations to locate the leak on the pressure vessel. A series of experimental tests were performed and at worst the method identified some false locations, but the true location of the leak always appeared.
机译:我们已经在实验室开发并测试了一种用于载人航天器在轨探测和漏气定位的方法,该方法仅使用少量在航天器蒙皮内表面上任意分布的传感器。然后,从每个传感器监视300-600 kHz范围内的结构声超声波。当测得的传感器波形之间的互相关表明存在泄漏时,会将这些相关与大型动态生成的模拟相关数据库进行比较,以将泄漏定位在压力容器上。进行了一系列实验测试,在最坏的情况下,该方法识别出一些错误的位置,但始终会出现泄漏的真实位置。

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