The invention discloses an aircraft environment control system which comprises a hot air conveying pipeline arranged between the position of an engine and the position of an air inlet lip of a fuselage, a control switch is arranged on the hot air conveying pipeline, and the hot air conveying pipeline is used for introducing hot air of the engine into the position of the air inlet lip. The control center is connected with the control switch, and is also connected with a first temperature sensing part arranged at the lip position of the air inlet channel; the control center is used for turning on the control switch when the temperature detected by the first temperature sensing component is lower than a preset temperature threshold value so as to convey heat of the engine to the lip position of the air inlet channel. According to the aircraft environment control system, anti-icing and deicing can be conducted on the engine air inlet lip, the situation that the local temperature of the aircraft is too low is avoided, and the overall flight safety of the aircraft is guaranteed.

    本申请公开了一种飞行器环控系统,包括设置于发动机位置和机身进气道唇口位置之间的热气输送管路,所述热气输送管路上设置有控制开关,所述热气输送管路用于将发动机的热气引入所述进气道唇口位置,还包括与所述控制开关连接的控制中心,所述控制中心还连接有设置于所述进气道唇口位置的第一温度传感部件,所述控制中心用于当所述第一温度传感部件检测到的温度低于预设温度阈值时开启所述控制开关以将发动机的热量输送到进气道唇口位置。上述飞行器环控系统,能够对发动机进气道唇口进行防冰除冰,避免飞行器局部温度过低,保证飞行器整体的飞行安全。


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    Titel :

    Aircraft environment control system


    Weitere Titelangaben:

    一种飞行器环控系统


    Beteiligte:
    LI YIDONG (Autor:in) / ZHENG YONGFENG (Autor:in) / CHOI JE-DA (Autor:in) / WANG YUEXING (Autor:in) / MIAO WEIXING (Autor:in) / GAO JIANLI (Autor:in) / TIAN HAO (Autor:in)

    Erscheinungsdatum :

    2022-04-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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