The invention is applicable to the technical field of aerospace, and provides a flight device. The flight device comprises a fuselage, front wings, rear wings and rotor wings, wherein the fuselage isused for supporting and mounting; the front wings are mounted on two sides of the front end of the fuselage in a forward-swept and downward-inverted-angle mode; the rear wings are mounted on two sidesof the rear end of the fuselage in a backward-swept and upward-inverted-angle mode; the rotor wings are mounted at the ends of the front wings and the rear wings and used for providing lifting power;the front wings and the rear wings are provided with tilting mechanisms for adjusting the tilting angles of the rotor wings through wing connecting platforms; and the front end and the rear end of the interior of the fuselage are connected with transmission shafts in the front wings and the rear wings through left-right power distribution structures for driving the rotor wings to rotate. Comparedwith a helicopter, a tilting rotor aircraft has the advantages of being long in voyage, high in navigational speed and low in transportation cost; and compared with a fixed-wing aircraft, the tiltingrotor aircraft has the advantages that vertical take-off and landing can be achieved, stable hovering in the air is achieved, and the loading capacity and the flight speed in a front flight mode areimproved through the four tilting rotor wings. The flight device has the advantages of being simple in structure, stable in flight, long in endurance voyage and convenient to adjust.

    本发明适用于航空航天技术领域,提供了一种飞行装置,所述飞行装置包括:机身,用于支撑和安装;前机翼,前掠且下反角安装在机身的前端两侧;后机翼,后掠且上反角安装在机身的后端两侧;旋翼,安装在前机翼和后机翼的端部,用于提供抬升动力;其中,前机翼、后机翼通过机翼连接平台设置有调节旋翼倾斜角度的倾转机构;机身的内部前后端通过左右动力分配结构与前机翼、后机翼内传动轴连接,用于驱动旋翼转动。可倾转旋翼飞行器与直升机相比,具有航程远,航速高,运输成本低的优点;与固定翼飞机相比,可实现垂直起降,空中平稳悬停,可倾转四旋翼提高了载重能力和前飞模式下的飞行速度。本发明优点:结构简单,飞行稳定,航时航程长,调节方便。


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    Title :

    Flight device and manned aircraft


    Additional title:

    一种飞行装置及载人飞行器


    Contributors:

    Publication date :

    2020-12-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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