The invention discloses a compound type delta wing aircraft, which belongs to the technical field of aircrafts. The compound type delta wing aircraft comprises a delta wing, an undercarriage, a left aileron, a right aileron as well as two, four, six or eight propellers and engines thereof, wherein the propellers are symmetrically distributed below the delta wing; the engines are arranged on the lower surface of the delta wing or in the body of the delta wing; rotating planes of the propellers are positioned at horizontal positions or are inclined towards the front-lower direction; included angles between the rotating planes of the propellers at the front part and the bottom surface of the delta wing are 5 to 30 degrees; when the propellers rotate, the minimum space between propeller tips and the bottom surface of the delta wing is greater than 5mm; the engines drive the corresponding propellers to rotate; a combined action of the propellers and the delta wing generates a forward push force and an upward lift force; by adjusting the deflection amplitudes and the directions of the two ailerons as well as the rotating speed of the propellers, the aircraft can realize multiple flying attitudes such as pitching, side rolling and elevating; the compound type delta wing aircraft is flexible and is suitable for flying at low speed.


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    Titel :

    Compound type delta wing aircraft


    Beteiligte:
    WANG ZHICHENG (Autor:in)

    Erscheinungsdatum :

    2016-01-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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