The invention discloses a vertical take-off and landing aircraft with a wing body blended with a single duct. The aircraft mainly consists of an aircraft fuselage 3, a front engine 2 and a duct engine 8. The aircraft fuselage 3 is in a blended wing body layout. The front engine 2 is installed on the front part of the fuselage of the aircraft, and the duct 7 is positioned in the middle part of the fuselage 3 of the aircraft. Parts 4 are folding wings positioned on two sides of the fuselage 3. The duct engine 8 is positioned in the middle of the duct 7, and fixedly arranged on the fuselage of the aircraft by a fixing rod 11. Parts 5 and 6 are flaps of the aircraft, and are positioned on the back part of the aircraft and the back parts of the wings. Parts 9 are folding positions of the wings of the aircraft. A front propeller 1 of the aircraft is positioned at the front end of the aircraft. Empennages 12 of the aircraft are positioned at the tail of the aircraft, and are in V-shaped symmetrical distribution. Three undercarriages 13 of the aircraft are distributed on the lower part of the aircraft in a manner that one undercarriage is at the front and two undercarriages are at the back, and the undercarriages 13 can also be supporting rods 14. The vertical take-off and landing aircraft disclosed by the invention is mainly applicable to the field of aviation, and can be applied as small and medium-sized airplanes, unmanned aerial vehicles, model airplanes and aerial photography airplanes.


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    Titel :

    Vertical take-off and landing aircraft with wing body blended with single duct


    Beteiligte:
    ZHANG FEI (Autor:in)

    Erscheinungsdatum :

    2015-11-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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