The invention discloses an anti-falling remote control helicopter with a propeller and fuselage self-separation function in the technical field of remote control helicopters. The structure comprises a fuselage main body, a transmission assembly, a mechanical gripper fixing assembly, a fixed mounting assembly, an undercarriage buffer assembly and a parachute bag, and the mechanical gripper fixing assembly is installed on the top of the transmission assembly; and the fixed installation assembly is installed on the top of the machine body. The device is reasonable in structural design; when the operation is improper, the hydraulic rod is turned on to work through the remote controller switch, the hydraulic rod drives the gripper to move left and right, and the gripper is separated from the connecting column; then the mechanical gripper fixing assembly is separated from the connecting column; and after separation, the fixing plate is far away from the connecting shell, so that the fuselage is conveniently separated from the propeller blades. When the aircraft body falls to a certain height, an operator opens the parachute bag through the remote controller, and the parachute bag opens the parachute to buffer the force generated by falling.

    本发明公开了遥控直升机技术领域的一种具有螺旋桨、机身自分离功能的防摔型遥控直升机,包括机身主体、传动组件、机械抓手固定组件、固定安装组件、起落架缓冲组件和降落伞包,机械抓手固定组件安装于传动组件的顶部,固定安装组件安装于机身主体的顶部;本发明结构设计合理,在操作不当时,通过遥控器开关打开液压杆工作,液压杆带动抓手左右移动,将抓手与连接柱进行分离,再将机械抓手固定组件与连接柱分离,分离后固定板与连接壳体远离,从而便于将机身与螺旋桨叶进行分离,机身进行下坠,当下坠一定高度时,操作者通过遥控器打开降落伞包,降落伞包将降落伞打开,使其缓冲下坠产生的力度。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Anti-falling remote control helicopter with propeller and fuselage self-separation function


    Weitere Titelangaben:

    一种具有螺旋桨、机身自分离功能的防摔型遥控直升机


    Beteiligte:
    CHEN SHUPING (Autor:in)

    Erscheinungsdatum :

    2021-07-30


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    Analysis of Rotor/Propeller/Fuselage Interaction Characteristics of High-speed Helicopter

    SHEN Suiyuan / ZHU Qinghua / ZHU Zhenhua et al. | DOAJ | 2020

    Freier Zugriff

    Light helicopter fuselage

    SUN ZHIWU | Europäisches Patentamt | 2022

    Freier Zugriff

    Helicopter Anti-Torque System Using Fuselage Strakes

    H. L. Kelley / J. C. Wilson | NTIS | 1987


    Helicopter anti-torque system using fuselage strakes

    Kelley, Henry L. / Wilson, John C. | NTRS | 1987


    Unmanned helicopter fuselage structure

    LIU MINSHENG / BO XIAOMING | Europäisches Patentamt | 2021

    Freier Zugriff