The invention belongs to the technical field of aviation, and particularly relates to a liquid cooling and anti-icing integrated heat energy management system which comprises a booster pump, the booster pump is provided with an inlet and an outlet in the liquid flowing direction, and the outlet is sequentially connected with an electric heater, an electronic equipment cold plate, a double-skin anti-icing structure and the inlet through a pipeline; the liquid storage tank is connected with the inlet; according to the liquid cooling system, the liquid cooling agent in the liquid cooling system is cooled, the anti-icing problem of wings or empennages of airplanes is solved, and the compensation loss caused by using the air-liquid heat exchanger cooling liquid refrigerant is reduced.

    本申请属于本申请属于航空技术领域,特别涉及一种综合液冷与防冰的热能管理系统,本申请包括增压泵,增压泵具有沿液体流动方向的进口与出口,所述出口通过管道依次连接有电加温器,电子设备冷板,双蒙皮防冰结构与所述进口;储液箱,储液箱连接所述进口;本申请既冷却了液冷系统中的液冷剂,又解决了飞机机翼或尾翼的防冰问题,且减少因使用空‑液热交换器冷却液冷剂带来的代偿损失。


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    Titel :

    Heat energy management system integrating liquid cooling and anti-icing


    Weitere Titelangaben:

    一种综合液冷与防冰的热能管理系统


    Beteiligte:
    CHEN RUOBING (Autor:in) / DANG XIAOMIN (Autor:in) / BAI RU (Autor:in) / HE ZHOUDONG (Autor:in)

    Erscheinungsdatum :

    2022-07-05


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    H05K PRINTED CIRCUITS , Gedruckte Schaltungen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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