An aircraft assembly 1 with an aircraft structure includes a flight control surface, 3a, 3b that is moveable relative to the aircraft structure between a retracted configuration and a deployed configuration. A rigid chain actuator 50a is connected between the aircraft structure and the flight control surface. The rigid chain actuator includes a drive assembly 56a and a chain 54a and the chain extends through the drive assembly towards the flight control surface 22. The drive assembly is arranged to drive the chain to move the flight control surface between the retracted and deployed configurations.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Flight control surface deployment


    Beteiligte:
    JAMES SAUVEN (Autor:in)

    Erscheinungsdatum :

    05.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Flight control surface deployment

    Europäisches Patentamt | 2023

    Freier Zugriff

    Flight recorder deployment mechanism

    VAN DEN HEUVEL BLAKE / KAUFMANN ARI / WOOZLEY MARK et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    FLIGHT RECORDER DEPLOYMENT MECHANISM

    VAN DEN HEUVEL BLAKE / KAUFMANN ARI / WOOZLEY MARK et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    ADVANCED MOBILE FLIGHT CONTROL DEVELOPMENT AND DEPLOYMENT CENTER

    Harris, W. J. / Krainski, J. / American Helicopter Society | British Library Conference Proceedings | 2001