A distributed electronic control system (100) for an aircraft includes an engine data controller (103) arranged on an airframe of the aircraft and a plurality of engine data concentrators (104-106) arranged proximate an engine of the aircraft in signal communication with the engine data controller. The engine data controller (103) is configured to process information related to the engine of the aircraft, the plurality of engine data concentrators (104-106) are configured to receive engine sensor information from a plurality of engine sensors (141-161), and the plurality of engine data concentrators (104-106) are further configured to transmit the engine sensor information to the engine data controller (103).


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    Title :

    Distributed electronic engine control architecture


    Additional title:

    Verteilte elektronische Triebwerkssteuerungsarchitektur
    Architecture réparti de commande électronique de turboréacteur


    Contributors:

    Publication date :

    2017-05-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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