PROBLEM TO BE SOLVED: To provide a wireless aircraft engine monitoring system.SOLUTION: The system has a nacelle 110 extending annularly and a sensor 116 positioned radially inward therefrom. The system includes an engine control device 104 coupled communicatively to the sensor and configured to receive engine data from the sensor and receive instruction data from a transmitter device positioned radially outward from a nacelle radially outward surface 111. The system also includes a composite panel including at least a portion of the nacelle and a ground plane positioned radially inward from the nacelle radially outward surface, the composite panel including an antenna coupled communicatively to the engine control device and a radome positioned radially outward from the ground plane. The antenna receives the engine data from the engine control device and transmits the engine data to a receiver device, and receives the instruction data from the transmitter device and transmits the instruction data to the engine control device.SELECTED DRAWING: Figure 1

    【課題】無線航空機エンジン監視システムを提供する。【解決手段】環状に延在するナセル110と、そこから半径方向内側に配置されたセンサ116と、を有する。システムは、センサに通信可能に結合され、センサからエンジンデータを受信し、ナセル半径方向外側表面111から半径方向外側に配置された送信装置からの命令データを受信するように構成されたエンジン制御装置104を含む。システムは、ナセルの少なくとも一部と、ナセルの半径方向外側表面から半径方向内側に配置された接地平面と、を含む複合パネルを含み、複合パネルは、エンジン制御装置に通信可能に結合されたアンテナと、接地平面から半径方向外側に配置されたレードームと、を含む。アンテナは、エンジン制御装置からエンジンデータを受信して、エンジンデータを受信装置に送信すること、および送信装置から命令データを受信して、命令データをエンジン制御装置に送信する。【選択図】図1


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    Title :

    WIRELESS AIRCRAFT ENGINE MONITORING SYSTEM


    Additional title:

    無線航空機エンジン監視システム



    Publication date :

    2018-02-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G08C Übertragungssysteme für Messwerte, Regel-, Steuer- oder ähnliche Signale , TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS



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