The present invention discloses an aircraft using a distributed electric ducted fan flap lift-rising system. The aircraft symmetrically arranges two distributed electric ducted fan flap lift-rising systems on both sides of the front middle part of the fuselage; the distributed electric ducted fan wing flap lift system has relatively large wingspan and aspect ratio; the number of electric ducted fans arranged on the leading edge is relatively large; the rear middle part of the fuselage is provided with a lift fan; rear wings are symmetrically disposed both sides of the rear middle part of the fuselage; the center of gravity of the aircraft is located in the middle of the fuselage; and the aircraft has a tandem wing layout. The aircraft of the present invention has the advantages of small friction, and no pollution and low noise of the electric ducted fan.


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    Title :

    Aircraft using distributed electric ducted fan flap lift-rising system


    Contributors:
    LONG CHUAN (author)

    Publication date :

    2015-10-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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