The invention relates to an anti-icing system of an aircraft wing, a control method of the anti-icing system and an aircraft. The anti-icing system of the aircraft wing comprises an air source, an anti-icing pipeline, an anti-icing valve, an electric heating device and an anti-icing controller, wherein the anti-icing valve and the electric heating device are arranged on the anti-icing pipeline. The gas source is used for supplying gas with a first preset temperature, and the anti-icing pipeline is connected between the gas source and a pipeline in an aircraft wing. And the anti-icing controller is electrically connected with the anti-icing valve and the electric heating device. When the weather condition is converted from the non-icing weather to the first icing weather, the anti-icing controller controls the anti-icing valve to be opened, so that the gas with the first preset temperature is transmitted into the pipeline of the aircraft wing through the anti-icing pipeline; and when the meteorological condition is converted from the first icing weather to the second icing weather, the anti-icing controller controls the anti-icing valve and the electric heating device to be started at the same time, so that the gas is heated from the first preset temperature to the second preset temperature when passing through the electric heating device, and then the gas is transmitted to the pipeline in the aircraft wing.

    本申请涉及一种飞机机翼的防冰系统、其控制方法及飞机,其中飞机机翼的防冰系统包括:气源、防冰管路、设于防冰管路上的防冰活门和电加热装置以及防冰控制器。气源用于供给具有第一预设温度的气体,防冰管路连接于气源和飞机机翼中的管路之间。防冰控制器与防冰活门、电加热装置电连接。当气象条件由非结冰气象转换为第一结冰气象时,防冰控制器控制防冰活门开启,以使具有第一预设温度的气体通过防冰管路传输至飞机机翼的管路中;当气象条件由第一结冰气象转换为第二结冰气象时,防冰控制器控制防冰活门和电加热装置同时开启,以使气体在经过电加热装置时由第一预设温度加热至第二预设温度,再传输至飞机机翼中的管路。


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    Titel :

    Anti-icing system of aircraft wing, control method of anti-icing system and aircraft


    Weitere Titelangaben:

    一种飞机机翼的防冰系统、其控制方法及飞机


    Beteiligte:
    WU DONGWEN (Autor:in) / ZHANG WEIHAO (Autor:in) / JIAO SHUHUI (Autor:in) / WANG HAOYU (Autor:in) / ZHANG YUQING (Autor:in) / CHANG YUXIN (Autor:in)

    Erscheinungsdatum :

    30.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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