AIRCRAFT CONTROL SURFACE ELEMENT MONITORING SYSTEM
作者： Gerbetz Robert P , Towers Graham K , Venables Neil A , Whitehouse Paul D
DOI:
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摘要: An aircraft moveable element monitoring system is provided. exemplary includes a signal generator (108), transmitter coil (110) electrically connected to the (108); detector (112); receiver (114) and one or more transmission units (115a-c). unit (115) first second coil, being coil. Each configured be installed on respective of an aircraft. The form inductively coupled line. provide electrical detect via further determine condition elements by comparing detected predetermined characteristic.
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