The invention discloses an aircraft information input device. The aircraft information input equipment comprises a key input module and a vernier control module based on a pressure sensor. The key input module is provided with an interface quick switching key input area, an instruction input key input area, a digital input key input area, a latitude and longitude quick input key input area, an X coordinate quick input key and a Y coordinate quick input key. And the vernier control module based on the pressure sensor is used for controlling an indication vernier of the display device. The method has the beneficial effects that the common function modules under the flight condition of the airplane are integrated, a rapid input mode for the function modules is set, and the vernier can be controlled without a stroke on the premise that the space of the airplane is narrow through vernier control based on the pressure sensor, so that the operation is simple and convenient. The problem of instruction interaction between the pilot and the aircraft is well solved.

    本发明公开一种飞机信息输入设备。所述飞机信息输入设备包括:按键输入模块、基于压力传感器的游标控制模块。所述按键输入模块具有界面快速切换按键输入区、指令输入按键输入区、数字输入按键输入区、经纬度快捷输入按键输入区、X坐标快捷输入按键、Y坐标快捷输入按键。所述基于压力传感器的游标控制模块用于控制显示装置的指示游标。本发明的有益效果:综合飞机飞行条件下常用的功能模块,设置针对此类功能模块的快速输入方式,并且通过基于压力传感器的游标控制,满足在飞机空间狭小的前提下,无需行程即可控制游标,较好地解决飞行员与飞机之间的指令交互问题。


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    Title :

    Aircraft information input device


    Additional title:

    一种飞机信息输入设备


    Contributors:
    WANG SHEN (author) / MENG FANCE (author) / ZHANG KE (author) / KANG JINGWEI (author) / TANG YUHUANG (author)

    Publication date :

    2025-03-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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