A tilting system for a propeller of an aircraft may include a propeller disposed forward of an opening portion of a housing and configured to be selectively tilted relative to the housing; a link assembly disposed in the interior space of the housing, a first end portion thereof being connected to the housing, and a second end portion thereof being connected to the propeller, and the link assembly being configured to tilt the propeller upward or downward when it extends from or retracts into the housing; and an actuator coupled to the link assembly and configured to provide power for extension or retraction to the link assembly.

    一种用于飞行器的螺旋桨的倾斜系统,可以包括:螺旋桨,该螺旋桨设置在壳体的开口部分的前面,并且被配置成选择性地相对于壳体倾斜;连杆组件,该连杆组件设置在壳体的内部空间中,其第一端部部分连接到壳体,并且其第二端部部分连接到螺旋桨,并且连杆组件被配置成当其从壳体伸出或缩回到壳体中时使螺旋桨向上或向下倾斜;以及致动器,该致动器耦接到连杆组件并被配置成向连杆组件提供用于伸出或缩回的动力。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Tilting system for propeller of aircraft


    Weitere Titelangaben:

    用于飞行器的螺旋桨的倾斜系统


    Beteiligte:
    CHOI JAE-YOUNG (Autor:in) / JUNG SANG-HYUN (Autor:in) / IM CHOONG-SIK (Autor:in) / CHO KYU-HOON (Autor:in)

    Erscheinungsdatum :

    21.06.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Hydraulic propeller tilting rotor aircraft

    DU DINGWEN | Europäisches Patentamt | 2015

    Freier Zugriff

    Wing tilting device of multi-propeller tilting wing configuration aircraft and aircraft

    LIU JIFU / MA DONGLIN / LUO JUN et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Tilting coaxial double-propeller multi-power duct manned aircraft

    WU LIAONI / JIANG TANG / GUO FENG | Europäisches Patentamt | 2021

    Freier Zugriff

    Multi-propeller tilting aircraft and flight control method thereof

    LIU ZEFENG | Europäisches Patentamt | 2023

    Freier Zugriff