The invention provides a distributed large airplane flap control computer system. The system includes a flap and slat control computer, an actuator control electronic unit, a power drive device, a flap and slat control handle sensor, a flap position sensor, a slat position sensor, a flap inclination sensor and a slat inclination sensor; and the flap and slat computer acquires the instruction of the flap and slat control handle sensor and information of the slat inclination sensor, the actuator control electronic unit acquires the position information of a controlled slat surface, and the flap and slat control computer is in data communication with the actuator control electronic unit via a high integrity data bus. The distributed large airplane flap fly-by-wire control fault-tolerant computer system meets different large airplanes' needs of control calculation and execution mechanism configurable management, and has the advantages of high reliability, configurability and upgradability.


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    Titel :

    Distributed large airplane flap control computer system


    Beteiligte:
    XU AO (Autor:in) / LIN JIAN (Autor:in) / XIA DETIAN (Autor:in) / XIE WENTAO (Autor:in) / ZHENG JIUSHOU (Autor:in) / KANG XIAODONG (Autor:in)

    Erscheinungsdatum :

    22.04.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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