The invention belongs to the technical field of aircraft thermal management, and discloses an aircraft thermal management system and a control method, the system comprises an evaporation circulation refrigeration loop, a liquid cooling circulation loop, a power battery, a motor control box and a motor; an in-cabin evaporator of the evaporation circulation refrigeration loop and an in-cabin radiator of the liquid cooling circulation loop are arranged in the same air duct, and the liquid cooling circulation loop flows through the power battery, the motor control box and the motor and dissipates heat for the power battery, the motor control box and the motor; an evaporation fan is arranged in the air duct.

    本发明属于飞行器热管理技术领域,公开了一种飞行器热管理系统及控制方法,系统包括:蒸发循环制冷回路、液冷循环回路、动力电池、电机控制盒及电机;蒸发循环制冷回路的舱内蒸发器和液冷循环回路的舱内散热器设置在同一风道内,液冷循环回路流经动力电池、电机控制盒及电机并为其散热;风道内设置蒸发风机。


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    Titel :

    Aircraft thermal management system and control method


    Weitere Titelangaben:

    一种飞行器热管理系统及控制方法


    Beteiligte:
    ZHANG YANG (Autor:in) / SUN DONGHONG (Autor:in) / LAI YAOZU (Autor:in) / WANG ZHIHUI (Autor:in) / HUANG HEMING (Autor:in)

    Erscheinungsdatum :

    03.01.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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