The invention relates to the technical field of electric airplanes, in particular to a heat management system of an electric aircraft, which comprises a heat pump unit and a heat pipe radiator, and the heat pump unit comprises a compressor, a one-way valve, a pipeline, a heat management controller and a valve; the heat pipe radiator comprises a copper heat pipe and aluminum fins. The invention aims to realize effective heat dissipation of heat generated by the electric aircraft by optimizing a heat management system, and meanwhile, the heat is used for heating the interior of an aircraft cabin, so that the comfort of passengers is improved. In addition, the system further has an intelligent heat management function, and it is ensured that the electric aircraft can keep the optimal heat balance state under various flight conditions.

    本发明涉及电动飞机技术领域,特别涉及一种电动飞机的热管理系统,包括热泵单元及热管散热器,其中热泵单元包括压缩器、单向阀、管道、热量管理控制器及阀门;热管散热器包括铜制热管与铝制鳍片。本发明的目的是通过优化热管理系统,实现对电动飞机产生的热量进行有效散热,同时将这部分热量用于飞机机舱内的加热,提升乘客的舒适度。此外,该系统还具备对热量的智能管理功能,确保电动飞机在各种飞行条件下都能保持最佳的热平衡状态。


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    Titel :

    Thermal management system and thermal management method of electric aircraft


    Weitere Titelangaben:

    一种电动飞机的热管理系统及热管理方法


    Beteiligte:
    LI SHUPING (Autor:in) / LI YADI (Autor:in) / CUI HENGJI (Autor:in) / XIONG XUHAI (Autor:in) / HUANG RONG (Autor:in) / WANG SHULI (Autor:in) / FEI YUNZHU (Autor:in) / DAI YUJIAO (Autor:in) / LIU DA (Autor:in)

    Erscheinungsdatum :

    20.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY



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