A vertical take-off and landing aircraft is shown. The VTOL aircraft has a main wing comprising a left wing and a right wing configured as folding wings, and one or more of a foreplane, comprising a left canard and a right canard configured as folding wings, and/or a tailplane, comprising 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.


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    Title :

    VTOL AIRCRAFT


    Additional title:

    SENKRECHTSTART- UND -LANDEFLUGZEUG
    AÉRONEF ADAV


    Contributors:

    Publication date :

    2021-01-27


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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