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Aircraft fire detection system - uses three transistor circuit to obviate false alarms in case of detector faults and low voltages

机译:飞机火灾探测系统-在探测器故障和低电压的情况下,使用三个晶体管电路来消除误报

摘要

The electronically controlled fire detection system is designed to operate various warning elements and or protection devices by relays controlled by variable resistance surveillance detection. The system has a first transistor whose base and emitter are connected to the terminals of the detector circuits and which control the conductivity of a second transistor. The second transistor controls the supply of one or several relays controlling the warning and or protection elements. A third transistor controls the supply of a supplementary relay designed to control a fault signalling element when a fault occurs in the circuit of the detectors.
机译:电子控制火灾探测系统设计为通过由可变电阻监视探测控制的继电器来操作各种警告元件和/或保护装置。该系统具有第一晶体管,其基极和发射极连接到检测器电路的端子,并控制第二晶体管的导电性。第二晶体管控制一个或几个继电器的供电,这些继电器控制警告和/或保护元件。第三晶体管控制辅助继电器的电源,该辅助继电器设计成当检测器的电路中发生故障时控制故障信号元件。

著录项

  • 公开/公告号FR2329032B1

    专利类型

  • 公开/公告日1981-08-07

    原文格式PDF

  • 申请/专利权人 L HOTELLIER JACQUES;

    申请/专利号FR19750032279

  • 发明设计人

    申请日1975-10-22

  • 分类号G08B17/00;

  • 国家 FR

  • 入库时间 2022-08-22 15:07:26

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