发明名称 Electronic control unit for use in monitoring system in avionics field, has motherboard configured to identify sensor, which is concerned by short circuit in case of short circuit of drive circuit or link beams
摘要 <p>The unit (100) has multiple sensors (C1, C2) generating a detection output. A mother board (200) receives the detection output generated by each sensor through link beams (F1, F2). An interconnection chart (300) separates the common operate current in different ways from excitation paths (V1, V2) toward the sensors. The interconnection chart comprises a series of impedance (Zx1, Zx2) on the excitation paths. The motherboard is configured to identify one sensor, which is concerned by the short circuit in a case of short circuit of a drive circuit or the link beams. An independent claim is also included for a method for identifying a sensor concerned by a short-circuit.</p>
申请公布号 FR2988481(A1) 申请公布日期 2013.09.27
申请号 FR20120052501 申请日期 2012.03.20
申请人 SAGEM DEFENSE SECURITE 发明人 GRIMAUD LOUIS;GENESTE NICOLAS
分类号 G01R31/02 主分类号 G01R31/02
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