A structure for generating lift force comprises a shaft, the shaft is rotatably or fixedly installed on a fuselage, one or more revolution bodies are axially and fixedly installed on the shaft or rotatably installed on the shaft, and a power device drives the revolution bodies to rotate around the shaft; autorotation rotors are mounted on the outer edge of the revolution body, revolve along with the revolution body and rotate windward to generate lift force. The structure for generating the lift force has the advantages of good aerodynamic performance, high lift force generation efficiency, vertical lifting function, forced landing function and structure self-stabilizing function.

    一种产生升力的结构,包括轴,轴可转动或固定安装在机身上,轴上轴向固定或转动安装一个或多个公转体,动力装置驱动公转体绕轴转动;所述公转体外边缘安装有自转旋翼,自转旋翼随公转体公转并迎风自转产生升力。本发明提供的一种产生升力的结构,具备气动性能好、产生升力效率高、垂直升降功能、迫降功能及结构自稳功能。


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    Titel :

    Structure and method for generating lift force


    Weitere Titelangaben:

    一种产生升力的结构及方法


    Beteiligte:
    LONG XIAOBO (Autor:in) / LI YOUPING (Autor:in) / XU BO (Autor:in) / ZHANG CHUNHUI (Autor:in) / XUE BING (Autor:in)

    Erscheinungsdatum :

    09.04.2024


    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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