The invention relates to a helicopter rotor mechanical braking system. Helicopter rotor mechanical braking system comprises braking control lever, brake cover, brake drum, support, two brake shoes, brake lever, roller coupled with brake lever and kinematically connected with brake shoes, a microswitch and a wiring linking the brake control lever to the brake lever. Mechanical system of helicopter rotors braking is equipped with bracket with microswitch, fixed on brake cover by roller, installed on support. Support is equipped with pusher with return spring. Brake cover has a journal and slots for the roller and a pusher. Support is made with possibility of trunnion rotation together with brake drum at its engagement with brake shoes. Wiring is connected with brake lever through spring tip, and brake control lever is made with possibility of its fixation on control panel when brake pads are engaged with brake drum.EFFECT: higher reliability during operation of helicopter and safety of application of braking devices of drive system of helicopter rotors in case of unforeseen situations.4 cl, 9 dwg.

    本发明涉及直升飞机旋翼机械制动系统。直升飞机旋翼的机械制动系统包含制动控制杆、制动器罩、制动鼓、制动钳、两个制动蹄、制动杆、与制动杆连接并在动力学上连接到制动蹄的辊、微动开关和将制动控制杆连接到制动杆的布线。的直升飞机的旋翼的机械制动系统装配有:具有微动开关的支架,该支架安装在制动器罩上;安装在制动钳上的辊;制动钳设置有具有复位弹簧的推杆;制动器罩被制成为具有耳轴和槽,辊和推杆在所述槽中;制动钳被制成为在制动鼓与制动蹄接触时能够与制动鼓一起在耳轴上旋转;布线经由加载弹簧的顶端与制动杆关联;并且制动控制杆被制成为能够将其固定在控制面板上,此时制动蹄与制动鼓接合。


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    Titel :

    Helicopter rotor mechanical braking system


    Weitere Titelangaben:

    直升飞机旋翼机械制动系统



    Erscheinungsdatum :

    08.06.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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