The invention discloses a novel rudderless aircraft which comprises an annular spherical shell 1, an aero-engine 2, a directional air deflector 3, a central transmission shaft 4, a lift fan 5, a control system 6, a cabin 7, a rotary flying disc 8, a support slide way 9, a dust cover 10, an undercarriage 11, a fuel cabin 12, a transmission half axle gear 13 and a gear ring 14. An aero-engine is connected with and drives a lift fan to form downward duct airflow wind power, the direction of airflow is controlled through four directional air deflectors, the balance effect of a rotating flying disc is achieved, and up-down, left-right and front-back movement flying is achieved through a unique flying control mode and an innovative design concept. The device is simple to manufacture, low in cost and safe and reliable to use, has novelty and creativity, and can be widely applied to aviation, spaceflight, armies, civil use, commercial use and the like.

    本发明公开了一种新型无舵式飞行器,包括:1圆环球体壳、2航空发动机、3方向导风板、4中心传动轴、5升力风扇、6操控系统、7座舱、8旋转飞盘、9支架滑道、10防尘罩、11起落架、12燃料舱、13传动半轴齿轮、14齿环。主要是利用了由航空发动机连接传动升力风扇,形成向下的涵道气流风力,在通过四块方向导风板控制气流的方向,以及旋转飞盘的平衡作用,其独特的飞行控制模式和创新的设计理念,实现了上、下、左、右、前、后运动飞行,本发明结构设计合理,制造简单,成本低廉,使用安全可靠,具有新颖性和创造性,该发明可广泛应用于航空、航天、军队、民用、商用等。


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    Titel :

    Novel rudderless aircraft


    Weitere Titelangaben:

    一种新型无舵式飞行器


    Beteiligte:
    ZHANG HUIYU (Autor:in) / ZHANG HUI (Autor:in) / ZHANG KUI (Autor:in)

    Erscheinungsdatum :

    22.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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