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    • 3. 发明授权
    • System for detecting the first signs of a malfunction of an aircraft engine valve
    • 用于检测飞机发动机气门故障的第一迹象的系统
    • US08825278B2
    • 2014-09-02
    • US13774065
    • 2013-02-22
    • SNECMA
    • William BenseJean-Yves Picart
    • G01M17/00
    • B64D45/00F01D17/08F01D21/003F02C7/047F05D2260/80F05D2260/81F05D2270/3013F16K37/0083F16K37/0091
    • A method and a system for detecting the first signs of malfunction of an aircraft engine valve, including an acquisition device to acquire the output pressure measurements of the valve, and contextual and command data of the valve, a processor to define a set of indicators of the first signs of malfunction, according to the output pressure measurements and the contextual and command data. A set of estimators corresponding to the set of indicators of the first signs of a malfunction, is determined using a previously produced regression model. At least one distance between the set of indicators and the set of estimators is computed. The distance is compared to a threshold of the first signs of a malfunction, in order to detect the first signs of malfunction of the said valve.
    • 一种用于检测飞机发动机气门的故障的第一迹象的方法和系统,包括用于获取阀的输出压力测量值的采集装置,以及阀门的上下文和指令数据,处理器,用于定义一组指示器 根据输出压力测量和上下文和命令数据,出现故障的第一个迹象。 使用先前产生的回归模型来确定对应于故障的第一迹象的一组指示符的一组估计器。 计算指标集和估计量集之间的至少一个距离。 该距离与故障的第一迹象的阈值进行比较,以便检测所述阀的故障的第一迹象。