The invention discloses a Hall slat inclination sensor of a high-lift system, an airplane and a detection method. The Hall slat inclination sensor comprises a probe shell, a shell and a piston, the probe shell extends into the shell, the rear end of the probe shell is located at the position close to the middle of the probe shell, the front end of the probe shell is connected with the front end of the probe shell, and a Hall chip is arranged at the rear end of the probe shell; the piston is axially and slidably connected between the probe shell and the shell, a magnetic target is arranged on the piston, and the rear end of the piston extends out of the rear end of the shell. The slat inclination detection is realized, the size and weight of the slat inclination sensor are greatly reduced, the installation is simple and convenient, the maintainability is good, the output signal reliability and stability are high, and the comprehensive performance of the product is improved.

    本发明公开了一种高升力系统霍尔式缝翼倾斜传感器、飞机及检测方法,包括探头壳体、外壳和活塞;探头壳体伸入外壳内部,探头壳体后端位于探头壳体靠近中间位置,前端与探头壳体前端连接,探头壳体后端设置有霍尔芯片;活塞轴向滑动连接在探头壳体与外壳之间,活塞上设置有磁靶,活塞后端伸出外壳后端。实现缝翼倾斜检测,大大减小了缝翼倾斜传感器的尺寸和重量,安装简便、维修性好,输出信号可靠性、稳定性高,产品综合性能得到提高。


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    Titel :

    Hall slat inclination sensor of high-lift system, airplane and detection method


    Weitere Titelangaben:

    一种高升力系统霍尔式缝翼倾斜传感器、飞机及检测方法


    Beteiligte:
    YANG KAI (Autor:in) / WANG SHICHAO (Autor:in) / YANG LUN (Autor:in) / BAI XINYU (Autor:in) / LI SHAOLONG (Autor:in) / SHI RONGWU (Autor:in)

    Erscheinungsdatum :

    10.05.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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