An aircraft wing with a wing structure and a spoiler movable between a stowed configuration and a deployed configuration are disclosed. The spoiler includes an actuator configurable between an engaged mode and a disengaged mode. When the actuator is in the engaged mode, the actuator can restrict movement of the spoiler and move the spoiler between the stowed configuration and deployed configuration. In the disengaged mode, the actuator allows free movement of the spoiler, such that the spoiler may pop up due to reduced air pressure on the aircraft wing.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft spoiler and actuation apparatus


    Beteiligte:
    BISHOP BENJAMIN (Autor:in) / BRYANT ANTHONY (Autor:in)

    Erscheinungsdatum :

    2023-09-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    AIRCRAFT SPOILER AND ACTUATION APPARATUS

    BRYANT ANTHONY / BISHOP BEN | Europäisches Patentamt | 2024

    Freier Zugriff

    AIRCRAFT SPOILER AND ACTUATION APPARATUS

    BISHOP BENJAMIN / BRYANT ANTHONY | Europäisches Patentamt | 2022

    Freier Zugriff

    SPOILER ACTUATION APPARATUS FOR MOVING AN AIRCRAFT SPOILER

    BISHOP BENJAMIN | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft spoiler and actuation apparatus

    ANTHONY BRYANT / BEN BISHOP | Europäisches Patentamt | 2023

    Freier Zugriff

    SPOILER ACTUATION APPARATUS FOR MOVING AN AIRCRAFT SPOILER

    BISHOP BENJAMIN | Europäisches Patentamt | 2022

    Freier Zugriff