The invention discloses a distributed type electric ducted fan flap lifting system. The distributed type electric ducted fan flap lifting system is provided with a plurality of ducted fans which are in linear arrangement at the front edge of the upper wing surface of a wing at certain distances, the front edge of a duct stretches to be positioned in front of the front edge of the wing, the rear edge of the duct is located at the maximum thickness position of the wing, and a rear edge flap is arranged at the rear edge of the wing, corresponding to the position of the ducted fan. The distributed type electric ducted fan flap lifting system is safe and has low noise, small vibration, high lifting force and good economical efficiency during working. A hovercar adopting the distributed type electric ducted fan flap lifting system can realize vertical takeoff and landing, high-speed horizontal flight and smooth conversion between the vertical takeoff and landing state and the high-speed horizontal flight state.


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    Titel :

    Distributed type electric ducted fan flap lifting system and hovercar thereof


    Beteiligte:
    LONG CHUAN (Autor:in)

    Erscheinungsdatum :

    30.09.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60F VEHICLES FOR USE BOTH ON RAIL AND ON ROAD , Fahrzeuge für den Verkehr sowohl auf Schienen als auch auf Straßen



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