The invention provides an aircraft icing detection method and device and an aircraft, and relates to the technical field of icing detection.The method comprises the steps that a first data set of the aircraft at a first time point and a second data set of the aircraft at a second time point are obtained, and meanwhile total temperature data of the second time point are obtained; comparing the second data set with the first data set to detect a change in the aircraft exterior environment or windshield field of view; if the change in the external environment of the aircraft and the view field of the windshield shows visible moisture, and the total temperature data is lower than a preset threshold value, it is judged that the change in the external environment of the aircraft and the view field of the windshield meets a first icing condition. According to the invention, the workload of a pilot in icing judgment can be reduced, and the flight safety performance is further improved.

    本申请提供一种飞行器结冰探测方法、装置及飞行器,涉及结冰探测技术领域,该方法包括:获取飞行器在第一时间点的第一数据集和在第二时间点的第二数据集,同时获取第二时间点的总温数据;比较第二数据集与第一数据集,以检测飞行器外部环境或风挡视野范围内的变化;如果飞行器外部环境及风挡视野范围内的变化显示可见湿气,并且所述总温数据低于预设阈值,则判定飞行器外部环境及风挡视野范围内的变化满足第一结冰条件。本申请能够减轻飞行员在结冰判断方面的工作负担,进一步提升飞行安全性能。


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    Title :

    Aircraft icing detection method and device and aircraft


    Additional title:

    飞行器结冰探测方法、装置及飞行器


    Contributors:
    DONG QIAOTIAN (author) / TAN XUE (author) / KANG YIBO (author) / ZHOU FENG (author) / ZHAO BINBIN (author) / OUYANG YIFANG (author)

    Publication date :

    2025-04-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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