The invention discloses an aircraft control handle lifting and rotating mechanism with a damping hand feeling. The airplane control handle lifting and rotating mechanism comprises a main shaft part, a rod part and a damping part. The main shaft component is provided with a transverse main shaft which is driven by the rod component to rotate. The damping component is provided with an adjusting nut, a compression reed, a damping friction plate and a damping fixing plate. The transverse main shaft sequentially penetrates through the adjusting nut, the compression reed, the damping friction plate and the damping fixing plate. The aircraft control handle has the beneficial effects that the damping part is additionally arranged, relative friction is generated between the damping friction plate and the damping fixing plate, rotation damping force on the transverse main shaft is formed, and the aircraft control handle has the damping hand feeling.

    本发明公开一种具备阻尼手感的飞机操纵手柄提拉旋转机构。所述飞机操纵手柄提拉旋转机构包括:主轴部件、杆部件、阻尼部件。所述主轴部件具有横向主轴,所述横向主轴由所述杆部件带动旋转。所述阻尼部件具有调节螺母、压缩簧片、阻尼摩擦片、阻尼固定片。所述横向主轴依序穿过所述调节螺母、所述压缩簧片、所述阻尼摩擦片、所述阻尼固定片。本发明的有益效果在于:增加所述阻尼部件,所述阻尼摩擦片与所述阻尼固定片产生相对摩擦,形成对所述横向主轴的旋转阻尼力,使得所述飞机操纵手柄具备阻尼手感。


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    Title :

    Aircraft control handle lifting and rotating mechanism with damping hand feeling


    Additional title:

    一种具备阻尼手感的飞机操纵手柄提拉旋转机构


    Contributors:
    XU YONGPAN (author) / CHEN AOJIE (author) / XU CONG (author)

    Publication date :

    2025-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / F16C SHAFTS , Wellen



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