A vehicle comprising a morphing wing and a body is disclosed. The aircraft is configured to transform from a first configuration into a second configuration for ascent or descent of the aircraft. The drag force and lift force on the aircraft in the second configuration are less than in the first configuration. Transforming from the first to the second configuration comprises: contracting the wing within a geometric plane defined by the wing, and rotating the outer edge of the wing downwards, out of the geometric plane.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft wing control


    Beteiligte:
    NEWSAM MICHAEL (Autor:in)

    Erscheinungsdatum :

    2023-09-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B63G OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS , Angriffs- oder Verteidigungsanordnungen auf Schiffen / B64U



    AIRCRAFT WING CONTROL

    NEWSAM MICHAEL | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT WING CONTROL

    NEWSAM MICHAEL | Europäisches Patentamt | 2020

    Freier Zugriff

    Aircraft wing control

    Europäisches Patentamt | 2019

    Freier Zugriff

    AIRCRAFT WING CONTROL

    NEWSAM MICHAEL | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft wing control

    Europäisches Patentamt | 2019

    Freier Zugriff