The invention provides a tandem wing tilting rotor aircraft and an aircraft manufacturing method, and relates to the technical field of aircrafts. The tandem wing tilting rotor aircraft provided by the invention comprises an aircraft body, wing assemblies and rotor assemblies; the rotor assemblies are mounted on the wing assemblies; the wing assemblies are rotationally connected to the aircraft body and have a first working state and a second working state; in the first working state, the rotor assemblies drive gas to flow from front to back, and the wing assemblies are used for generating lift force in the gas flowing process; and in the second working state, the rotor assemblies are used for driving gas to flow from top to bottom to generate the lift force. According to the tandem wing tilting rotor aircraft provided by the invention, the working states of rotors can be adjusted through tilting of the wing assemblies, the gravity center setting range of the aircraft is enlarged, andthe layout and assembly difficulty of the aircraft is reduced.

    本发明提供了一种串列式机翼倾转旋翼飞行器及飞行器制造方法,涉及飞行器技术领域,本发明提供的串列式机翼倾转旋翼飞行器,包括:机身、机翼组件和旋翼组件;旋翼组件安装于机翼组件;机翼组件转动连接于机身,且机翼组件具有第一工作状态和第二工作状态;在第一工作状态下,旋翼组件驱动气体自前向后流动,机翼组件用于在气体流动过程中产生升力;在第二工作状态下,旋翼组件用于驱动气体自上向下流动以产生升力。本发明提供的串列式机翼倾转旋翼飞行器,可通过机翼组件倾转调节旋翼工作状态,增大了飞行器重心设置的范围,降低了飞行器布局和装配难度。


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    Titel :

    Tandem wing tilting rotor aircraft and aircraft manufacturing method


    Weitere Titelangaben:

    串列式机翼倾转旋翼飞行器及飞行器制造方法


    Beteiligte:
    CHEN FANGPING (Autor:in) / MENG ZHAOJUN (Autor:in) / ZHANG XIAOQI (Autor:in) / LI MING (Autor:in)

    Erscheinungsdatum :

    2020-12-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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