The invention provides an aircraft capable of rotating in situ and vertically taking off and landing by utilizing the lifting force of the fixed wings; the aircraft is made to rotate by generating torque through the aircraft engines on the wings, the wings generate the lifting force, the gravity of the aircraft is overcome, and the lifting force of the aircraft is close to the gravity; and then the aircraft is pulled or lifted through other aircrafts, or a propeller engine at the top of the aircraft and a jet engine at the bottom of the aircraft are used for displacing the aircraft. Compared with a traditional aircraft, the rotary aircraft can carry out vertical take-off and landing through the vertical pressure difference of the fixed wings; and hovering power and displacement power of the aircraft are provided by different engines separately, and compared with an existing helicopter, the rotary aircraft has higher loading capacity and higher safety, can adapt to complex weather and terrain and is lower in energy consumption.

    本发明提供了一种可在原地自转利用固定翼的升力进行垂直起降的飞行器,本发明通过机翼上的飞机发动机产生扭矩让飞行器进行自转,机翼产生升力,克服飞行器重力,使飞行器升力和重力接近,然后利用其它飞行器牵引或托举本发明,或者使用飞行器顶部的螺旋桨发动机和底部的喷气发动机使本发明进行位移;相比于传统飞行器,本发明可以利用固定翼的上下压力差进行垂直起降,本发明把飞行器的滞空动力和位移动力分开由不同的发动机提供,本发明比现有的直升机具有更大载重力和更高的安全性、能够适应复杂的气候和地形以及更低的能耗。


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    Titel :

    Rotary aircraft


    Weitere Titelangaben:

    一种旋转式飞行器


    Beteiligte:
    ZHU MAOLIN (Autor:in)

    Erscheinungsdatum :

    2021-01-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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