An aircraft comprises a wing assembly, a pod, and a pylon attaching the pod to the wing assembly. The pylon has a swept pylon flap, which is configured to unload the pylon and pod during flight of the aircraft, and also to create downward flow that counters a vortex trailing the pod.


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    Titel :

    WING AERIAL REFUELING SYSTEM


    Beteiligte:
    FERGUSON STANLEY D (Autor:in) / FIALHO IAN J (Autor:in) / POTTER RICHARD C (Autor:in)

    Erscheinungsdatum :

    26.05.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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