The invention relates to an airspeed tube heating control method and device and an aircraft. The method comprises the following steps: acquiring first flight data of an aircraft; when the first flight data reach a preset heating condition, controlling the airspeed tube to start heating; after the airspeed tube begins to heat, monitoring the flight mode of the aircraft; acquiring second flight data of the aircraft corresponding to the flight mode according to the flight mode of the aircraft; and when the second flight data reaches a preset heating stopping condition, controlling the airspeed tube to stop heating. According to the scheme provided by the invention, the heating control of the airspeed tube can be carried out by utilizing the existing signals of the aircraft in various flight modes of the aircraft, and no additional sensor is needed.

    本申请涉及一种空速管加热控制方法、装置及飞行器。该方法包括:获取飞行器的第一飞行数据;当第一飞行数据达到预设加热条件时,控制空速管开始加热;待空速管开始加热后,监控飞行器的飞行模式;根据飞行器的飞行模式,获取飞行模式对应的飞行器的第二飞行数据;当第二飞行数据达到预设停止加热条件时,控制空速管停止加热。本申请提供的方案,能够在飞行器的各种飞行模式下,利用飞行器已有的信号,进行空速管的加热控制,无需额外增加传感器。


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    Title :

    Airspeed tube heating control method and device and aircraft


    Additional title:

    空速管加热控制方法、装置及飞行器


    Contributors:
    LUO RIXING (author) / TAO YONGKANG (author) / GU YU (author) / XU MINGGUI (author)

    Publication date :

    2024-08-13


    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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