A vertical take-off and landing aircraft is shown. The VTOL aircraft has a main wing having a left wing and a right wing configured as folding wings, and one or more of a foreplane, having a left canard and a right canard configured as folding wings, and/or a tailplane, having a left stabiliser and a right stabiliser configured as folding wings. Each one of the folding wings has a fixed inboard section and a folding outboard section. The folding outboard section is downwardly foldable to a landing condition to support the aircraft on a surface.


    Access

    Download


    Export, share and cite



    Title :

    VTOL AIRCRAFT


    Contributors:

    Publication date :

    2020-01-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    VTOL AIRCRAFT

    STOBBE MARTIN / RAJPUT KRISHNA PAL / MORES SEBASTIAN | European Patent Office | 2025

    Free access

    VTOL Aircraft

    European Patent Office | 2020

    Free access

    VTOL AIRCRAFT

    BRODY DAVID E / OLCOTT DENNIS D | European Patent Office | 2016

    Free access

    VTOL AIRCRAFT

    FÜRLINGER ANDREAS | European Patent Office | 2023

    Free access

    VTOL AIRCRAFT

    BRODY DAVID E / OLCOTT DENNIS D | European Patent Office | 2020

    Free access