An aircraft comprising a wing 10, having a fixed wing 12 and a swing wing tip device 14 pivotably mounted about a pivot 16 at the tip of the fixed wing, wherein the swing wing tip device is configurable between a flight configuration (figure 1); and a ground configuration (figure 2) for ground-based operations, wherein the swing wing tip device is swung rearwardly to reduce the wing span. The swing wing tip device comprises a receiving portion (48, figure 3) located between the upper (30) and lower (32) wing skins. The upper and lower wing skin portions of the fixed wing which are exposed in the flight configuration are at least partially received within the receiving portion of the swing wingtip device in the ground configuration. The front spars of the fixed wing and the swing wing tip device may at least partially overlap and lock together via pins and apertures in the flight configuration. The swing wing tip device may comprise an open box structure.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Swing wing Tip


    Beteiligte:
    STEFAN NAPIER (Autor:in) / ROBERT HART (Autor:in) / MATTHEW HARDING (Autor:in) / NICK LIVINGS (Autor:in)

    Erscheinungsdatum :

    2017-05-31


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Swing wing

    Bird, W. | Tema Archiv | 1973


    Swing wing

    BIRD, W.J. | Emerald Group Publishing | 1973


    Swing wing tip

    NAPIER STEFAN / HART ROBERT / HARDING MATTHEW et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    SWING WING TIP

    NAPIER STEFAN / HART ROBERT / HARDING MATTHEW et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Bionic swing wing aircraft

    QIU HAN / WANG HUIXING | Europäisches Patentamt | 2016

    Freier Zugriff