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Longitudinal cable for transport of data or electric energy in harness of aircraft, has elementary areas having sensor elements, where each sensor element performs measurement of health parameter of cable in respective elementary area

机译:用于在飞机线束中传输数据或电能的纵向电缆具有基本区域,该基本区域具有传感器元件,其中每个传感器元件在相应的基本区域中执行电缆的健康参数的测量

摘要

The cable (10) has an inner functional core (3), an outer protective sheath (2), an elementary area (Zi) having a sensor element (Ci), and another elementary area (Zi plus 1) having another sensor element (Ci plus 1). Each sensor element is intended to perform a measurement of a health parameter e.g. temperature, of the cable in the respective elementary area, where the sensor elements are intended to communicate with each other. The sensor elements are connected by a communication link that extends along the length of the cable. Independent claims are also included for the following: (1) a harness of an aircraft (2) a method for monitoring a longitudinal cable (3) a method for monitoring a harness of an aircraft.
机译:电缆(10)具有内部功能芯(3),外部保护套(2),具有传感器元件(Ci)的基本区域(Zi)和具有另一个传感器元件( Ci加1)。每个传感器元件旨在执行健康参数的测量,例如健康状况。各个基本区域中电缆的温度,在这些基本区域中传感器元件应相互通信。传感器元件通过沿电缆长度延伸的通讯链接连接。还包括以下方面的独立权利要求:(1)飞机的线束(2)一种用于监视纵向电缆的方法(3)一种用于监视飞机的线束的方法。

著录项

  • 公开/公告号FR2997508A1

    专利类型

  • 公开/公告日2014-05-02

    原文格式PDF

  • 申请/专利权人 LABINAL;

    申请/专利号FR20120060292

  • 申请日2012-10-29

  • 分类号G01R31;

  • 国家 FR

  • 入库时间 2022-08-21 15:36:29

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