This AIR provides descriptions of aircraft actuation system failure-detection methods. The methods are those used for ground and in-flight detection of failures in electrohydraulic actuation systems for primary flight control. The AIR concentrates on full Fly-By-Wire (FBW) flight control actuation though it includes one augmented-control system. The background to the subject is discussed in terms of the impact that factors such as the system architecture have on the detection methods chosen for the flight control system. The types of failure covered by each monitoring technique are listed and discussed in general. The way in which these techniques have evolved is illustrated with an historical review of the methods adopted for a series of aircraft, arranged approximately in design chronological order. This document has been reaffirmed to comply with the SAE 5-year Review policy.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Actuation System Failure Detection Methods


    Erscheinungsdatum :

    2007-01-11



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    AUTOMATIC PARKING BRAKE ACTUATION AND FAILURE DETECTION

    LI ZONGZHENG / BI HAIMO / HAN XIAOLING | Europäisches Patentamt | 2024

    Freier Zugriff

    AUTOMATIC PARKING BRAKE ACTUATION AND FAILURE DETECTION

    LI ZONGZHENG / BI HAIMO / HAN XIAOLING | Europäisches Patentamt | 2024

    Freier Zugriff

    ACTUATION CONTROLLER AND ACTUATION SYSTEM

    SHIRAI TOYOTO / SAKAGAWA YUKI / TAKI NORIKAZU et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    INTERNAL-COMBUSTION ENGINE ACTUATION DETECTION SYSTEM

    YOKOYAMA DAIKI / CHIBA HIROYA / KAGEURA YOSHIYUKI et al. | Europäisches Patentamt | 2022

    Freier Zugriff