The invention discloses a four-axis gliding aircraft and belongs to the technical field of aircrafts. The four-axis gliding aircraft comprises a fuselage, a left composite wing, a right composite wing, a tail and undercarriages; the left composite wing and the right composite wing are identical in structure, and are symmetrically arranged at the left side and the right side of the fuselage; the tail comprises a horizontal tail and a vertical tail; the left composite wing comprises a support, a small fuselage, an inner electric airscrew, an outer electric airscrew, an inner movable fin and an outer movable fin; the outer electric airscrew and the inner electric airscrew are identical in structure, opposite in direction of rotation and symmetrically arranged at the left side and the right side of the small fuselage; the planes of rotation of the outer electric airscrew and the inner electric airscrew are located at a horizontal position; the outer movable fin and the inner movable fin are identical in structure, symmetrically arranged at the left side and the right side of the small fuselage, and can swing around the small fuselage under the operation of a control system; the outer electric airscrew and the inner electric airscrew are respectively located right below the outer movable fin and the inner movable fin. The aircraft is convenient to adopt zigzag flight mode and a wavy flight mode, can vertically take off and land and hover, is safe, efficient and stable.


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    Title :

    Four-axis gliding aircraft


    Contributors:

    Publication date :

    2016-01-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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