Vertical take-off and landing (VTOL) aircraft and nacelle devices for VTOL aircraft are disclosed. The nacelle device is connected via a pylon device to a wing of the vertical take-off and landing aircraft and is pivotable relative to the pylon device by a pivoting device about an axis of rotation between a first position, (e.g., a propulsion position), and a second position, (e.g., a lift position). The axis of rotation is arranged within the pylon device and/or the nacelle device, in particular on an axial center plane of the pylon device.


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    Titel :

    NACELLE DEVICE AND VTOL AIRCRAFT


    Beteiligte:
    FRÖDE ANDREAS (Autor:in)

    Erscheinungsdatum :

    30.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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    M. A. Boles / R. W. Luidens / N. O. Stockman | NTIS | 1978


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    Boles, Michael A. / Luidens, Roger W. / Stockman, Norbert O. | TIBKAT | 1978


    Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft

    Boles, M. A. / Luidens, R. W. / Stockman, N. O. | NTRS | 1978


    Theoretical study of VTOL tilt-nacelle axisymmetric inlet geometries

    Hawk, J. Dennis / Stockman, Norbert O. | TIBKAT | 1979


    Aircraft nacelle section and aircraft having aircraft nacelle section

    WEN AMY / KIRSTEIN HENNING / TEICHMANN SIEGFRIED et al. | Europäisches Patentamt | 2022

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