发明名称 Aircraft temperature monitoring system
摘要 The system includes an electrical supply unit, a number of temperature-responsive switches (11-20). The switches are connected at one terminal to a line connected with the supply unit and at another terminal to a location at a potential different from the supply line such that closing of a switch causes current flow through the switch. Each switch is associated with a respective resistor (25-36) such that closing each switch causes a different voltage to be applied to a monitor (45-54) allowing the monitor to determine the identity of the closed switch. The supply line can be formed in a first loop (22) where the resistors are connected in series. Each end of the loop can be connected to a respective source of constant current. The monitor device receives the voltage at opposite ends of the loop.
申请公布号 DE19717767(A1) 申请公布日期 1997.11.06
申请号 DE19971017767 申请日期 1997.04.26
申请人 SMITHS INDUSTRIES PLC, LONDON, GB 发明人 WILLIAMS, BRIAN, CHELTENHAM, GLOUCESTERSHIRE, GB
分类号 G08B25/01;(IPC1-7):B64D15/02;B64D47/00 主分类号 G08B25/01
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