The invention relates to a high lift aircraft, which belongs to the technical field of aircrafts. The high lift aircraft comprises a left wing, a right wing, a left rotor wing, a right rotor wing, a left engine, a right engine, a thrust propeller, a front engine, a tail wing, a landing gear and an aircraft body. An operation system and airbore equipment are mounted in the aircraft body. The front engine supplies power to the thrust propeller. The landing gear uses a wheel type structure. The tail wing comprises a horizontal tail wing and a vertical tail wing. The left wing and the right wing have same structures and are symmetrically mounted on the left side and the right side of the aircraft body. The left wing and the right wing are horizontally placed. The left rotor wing and the right rotor wing have same parameters and rotate in reverse directions; and the left rotor wing and the right rotor wing are respectively mounted in back positions under the left wing and the right wing. Rotating planes of the left rotor wing and the right rotor wing share a plane. The rotating plane of the left rotor wing is inclined towards the rear bottom. The left engine and the right engine supply power to the left rotor wing and the right rotor wing, respectively. The front edge of the left wing is at the front and the wing point of the left rotor wing rotates to the front end of a circumference. The aircraft can generate greater lift force and is stable and safe.


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    Titel :

    High lift aircraft


    Beteiligte:
    WANG ZHICHENG (Autor:in)

    Erscheinungsdatum :

    2016-01-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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