An aeronautical apparatus is disclosed that has two pairs of wings: an aft pair and a fore pair. Each wing has a thrust-angle motor. An assembly is coupled to each thrust-angle motor. Assemblies coupled to the wings have a propeller motor with a propeller and a control surface. The control surface provides lift when in forward flight. In vertical flight or hovering, the control surface, if it remains fixed with respect to the fuselage, i.e., in the position which provides lift in forward flight, produces significant drag. However, by rotating the control surfaces with the propeller motor, the drag from the control surfaces is significantly reduced. The control surfaces are outboard the propellers in some embodiments and inboard in others. In the latter case, the control surface is part of the trailing edge of the wing.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aeronautical Apparatus


    Beteiligte:
    BURNS KEVIN (Autor:in) / BREHOB DIANA (Autor:in)

    Erscheinungsdatum :

    2021-12-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aeronautical apparatus

    BURNS KEVIN | Europäisches Patentamt | 2024

    Freier Zugriff

    Aeronautical apparatus

    BURNS KEVIN / BREHOB DIANA | Europäisches Patentamt | 2021

    Freier Zugriff

    Aeronautical Apparatus

    BURNS KEVIN | Europäisches Patentamt | 2021

    Freier Zugriff

    AERONAUTICAL APPARATUS

    PAVLUSHCHENKO ALEKSEJ NIKOLAEVICH / SOLTUS ANDREJ SERGEEVICH | Europäisches Patentamt | 2017

    Freier Zugriff

    Aeronautical Apparatus

    BURNS KEVIN / BREHOB DIANA | Europäisches Patentamt | 2019

    Freier Zugriff