The invention discloses an aircraft data acquisition device and method, and relates to the technical field of aircraft data acquisition, the aircraft data acquisition device comprises an aircraft body, an emergency disengagement assembly is arranged below the aircraft body, the emergency disengagement assembly comprises a butt joint frame and a sleeve plate, and the butt joint frame is fixedly connected below the aircraft body. According to the aircraft data acquisition device and method disclosed by the invention, when a monitor on an aircraft body monitors that the aircraft body is subjected to destructive strike, an electric telescopic rod II drives a butt joint column to be separated from a butt joint sleeve; the gravity of the data collector and other structures outside the data collector drives the suspension air bag to be separated from the butt joint frame, the suspension air bag is filled with hydrogen, the data collector and the aircraft body are separated, the suspension air bag drives the data collector to slowly float to the ground, and emergency separation is achieved. The data collector is prevented from being damaged along with the damage of the aircraft body, and the effect of the data collector is protected.

    本发明公开了一种飞行器数据采集装置及其方法,涉及飞行器数据采集技术领域,包括飞行器本体,所述飞行器本体下方设有紧急脱离组件,且紧急脱离组件包括对接框和套板,对接框固定连接于飞行器本体的下方。本发明公开的一种飞行器数据采集装置及其方法具有在飞行器本体上的监测器监测到飞行器本体正在遭受毁灭性打击时,则电动伸缩杆二带动对接柱从对接套筒中脱离,数据采集器和其外侧其他结构的重力带动悬浮气囊从对接框中分离,悬浮气囊内部填充有氢气,实现数据采集器与飞行器本体之间的分离,悬浮气囊带动数据采集器缓慢的飘向地面,实现紧急脱离,避免数据采集器随着飞行器本体的损坏而损坏,保护数据采集器的效果。


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    Title :

    Aircraft data acquisition device and method thereof


    Additional title:

    一种飞行器数据采集装置及其方法


    Contributors:
    CHEN HAIGUANG (author) / LIU BO (author)

    Publication date :

    2025-03-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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