A vertical take-off and landing (VTOL) aircraft is provided and includes a fuselage, inboard wings extending from opposite sides of the fuselage to define a support plane and engine nacelles disposed along the wings. Each of the wings includes ground alighting elements and a variable geometry such that a portion of the ground alighting elements are alignable with the support plane during in-flight conditions and displaceable from the support plane.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH VARIABLE WING GEOMETRY


    Beteiligte:
    ALBER MARK R (Autor:in)

    Erscheinungsdatum :

    08.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Vertical take-off and landing aircraft with variable wing geometry

    ALBER MARK R | Europäisches Patentamt | 2016

    Freier Zugriff

    VARIABLE-GEOMETRY VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT SYSTEM

    SPENCER CAMERON | Europäisches Patentamt | 2020

    Freier Zugriff

    Variable-geometry vertical take-off and landing (VTOL) aircraft system

    SPENCER CAMERON | Europäisches Patentamt | 2022

    Freier Zugriff

    Variable-Geometry Vertical Take-Off and Landing (VTOL) Aircraft System

    SPENCER CAMERON | Europäisches Patentamt | 2021

    Freier Zugriff

    VARIABLE-GEOMETRY VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT SYSTEM

    SPENCER CAMERON | Europäisches Patentamt | 2023

    Freier Zugriff