WING AERIAL REFUELING SYSTEM An aircraft (110) comprises a wing assembly (130), a pod (176), and a pylon (178) attaching the pod (176) to the wing assembly (130), The pylon (178) has a swept pylon flap (410), which is configured to unload the pylon (178) and pod (176) during flight of the aircraft (110), and also to create downward flow that counters a vortex trailing the pod (176). 130, 178 Aq'


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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 :

    25.01.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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