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Method for detecting a failure of a vibration sensor for an engine part

机译:用于检测发动机部件的振动传感器的故障的方法

摘要

The invention relates to a method for detecting (S) a failure of a sensor (1), said sensor (1) being configured to detect at least one vibration of a part of an engine, in particular of a aircraft engine, and to supply an electrical voltage representative of the detected vibration, the detection method comprising the following steps: S1: measure a voltage supplied by the sensor (1), S2: compare the voltage thus measured with a first threshold predefined, S3: when the voltage is greater than the first predefined threshold, determine at least one shape parameter from the measurements of the voltage supplied by the sensor (1), S4: compare the shape parameter thus determined with a second predefined threshold and S5: generate a failure signal when the shape parameter exceeds the second predefined threshold.
机译:用于检测(S)传感器(1)故障的方法技术领域本发明涉及一种用于检测(S)传感器(1)故障的方法,所述传感器(1)被配置为检测发动机,尤其是飞机发动机的一部分的至少一个振动并提供代表检测到的振动的电压,该检测方法包括以下步骤:S1:测量由传感器(1)提供的电压,S2:将如此测量的电压与预定的第一阈值进行比较,S3:当电压大于从传感器(1)提供的电压的测量值中确定至少一个形状参数,S4:将由此确定的形状参数与第二预定义阈值进行比较,S5:当形状参数时,生成故障信号超过第二预定义阈值。

著录项

  • 公开/公告号FR3089636A1

    专利类型

  • 公开/公告日2020-06-12

    原文格式PDF

  • 申请/专利权人 SAFRAN AIRCRAFT ENGINES;

    申请/专利号FR1872690

  • 发明设计人 QUENTIN PHILIPPE GROELLY;

    申请日2018-12-11

  • 分类号G01R31/02;G05B23/02;G01P21;

  • 国家 FR

  • 入库时间 2022-08-21 11:00:26

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