An engine monitoring system (100) for an aircraft engine (102) having a nacelle (110) extending annularly thereabout 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/or receive instruction data from a transmitter device (512) positioned radially outward from a nacelle radially outward surface (111). The system also includes a composite panel (208,702,802,902) including at least a portion of the nacelle and a ground plane (602) positioned radially inward from the nacelle radially outward surface, the composite panel including an antenna (502) coupled communicatively to engine control device and a radome (405,504) positioned radially outward from ground plane. The antenna is configured to at least one of receive engine data from the engine control device and transmit engine data to a receiver device (510), and receive instruction data from the transmitter device and transmit instruction data to the engine control device.


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    Title :

    WIRELESS AIRCRAFT ENGINE MONITORING SYSTEM


    Additional title:

    DRAHTLOSES FLUGZEUGMOTORÜBERWACHUNGSSYSTEM
    SYSTÈME DE SURVEILLANCE DE MOTEUR D'AÉRONEF SANS FIL



    Publication date :

    2020-02-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



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