An aircraft (100) including a fuselage (102) having a longitudinal axis (20) extending through the fuselage front end (104) and the fuselage rear end (106); a foldable wing (120) located on the fuselage (102) and being movable between a flight position wherein the wing (102) is generally perpendicular to the longitudinal axis (20), and a stowed position wherein the wing (102) is generally parallel to the longitudinal axis (20); and a pair of stabilizing wings (140, 142) having an anhedral orientation disposed on the fuselage (102).


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    Title :

    FOLDABLE AIRCRAFT WITH ANHEDRAL STABILIZING WINGS


    Additional title:

    FALTBARES FLUGZEUG MIT ABWÄRTSGERICHTETEN STABILISIERUNGSFLÜGELN
    AÉRONEF PLIABLE COMPORTANT DES AILES DE STABILISATION À DIÈDRE NÉGATIF


    Contributors:

    Publication date :

    2020-08-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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