The invention discloses a saucer-shaped aircraft. The basic structure of the saucer-shaped aircraft comprises an upper aircraft body, a lower aircraft body and a rotation driving mechanism, wherein an aircraft body space is formed between the upper aircraft body and the lower aircraft body; the rotation driving mechanism is used for driving the upper aircraft body to rotate forwards, and under the condition of no stress, the lower aircraft body can rotate reversely because of conservation of angular kinetic energy; the lower aircraft body is provided with a plurality of air flues; one end of each air flue is communicated with the aircraft body space, and the other end of each air flue is communicated with atmosphere; each air flue is internally provided with a turbofan respectively; an annular magnetic suspension guide rail is arranged between the upper aircraft body and the lower aircraft body; the power source is used for providing required power for the rotation driving mechanism, the turbofans and the magnetic suspension guide rail. Compared with the prior art, the saucer-shaped aircraft is simple in operation principle, and is high in lift force; the lift force of the aircraft and the flight driving force are integrated; the appearance of the aircraft body is a symmetrical streamline type; the aircraft body is good in balance property, can perpendicularly take off and land, hover at random and fly at a high speed; because components, such as a propeller, a turbine engine are omitted, the saucer-shaped aircraft is simple in structure, and is good in controllability.


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    Titel :

    Saucer-shaped aircraft


    Beteiligte:
    LI GUANGCHENG (Autor:in)

    Erscheinungsdatum :

    2015-06-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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