The invention relates to an external cooling system of a water-cooled engine. The system involves an unmanned aerial vehicle body, an unmanned aerial vehicle engine and the external cooling system arranged on the unmanned aerial vehicle body, wherein the external cooling system involves a plurality of condensation pipes, the condensation pipes are hollow to form cooling cavities, the cooling cavities are filled with liquid condensing agents, the plurality of cooling cavities communicate, the condensation pipes are hollow pipes and form air cavities, the cooling cavities are annular, and a plurality of cooling fins are arranged on the inner walls of the air cavities. The external cooling system is arranged in the unmanned aerial vehicle body and is used for reducing heat generated by the unmanned aerial vehicle engine; and the condensation pipes in the external cooling system are arranged in the unmanned aerial vehicle body, heat generated by an unmanned aerial vehicle is transmitted to the condensation pipes and the liquid condensing agents in the condensation pipes, opposite wind generated in the flying process of the unmanned aerial vehicle takes away the heat of the condensation pipes, and therefore the effect of reducing the temperature of the unmanned aerial vehicle is achieved.

    本发明涉及到一种水冷发动机的外置冷却系统,包括无人机机身、无人机发动机,还包括设置在无人机机身上的外置冷却系统,所述外置冷却系统包括若干冷凝管,所述冷凝管内部中空形成冷却空腔,所述冷却空腔中填充设置有液态冷凝剂,若干所述冷却空腔连通,所述冷凝管为空心管形成气腔,所述冷却空腔为环形,所述气腔内壁设置有若干散热翅。外置冷却系统设置在无人机机身中,是用于降低因无人机发动机产生的热量;外置冷却系统中的冷凝管分别在无人机机身中,无人机产生的热量传递至冷凝管以及冷凝管中的液态冷凝剂中,无人机飞行的过程中所产生相向的风带走冷凝管的热量,以此起到降低无人机温度的作用。


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    Titel :

    External cooling system of water-cooled engine


    Weitere Titelangaben:

    一种水冷发动机的外置冷却系统


    Beteiligte:
    ZHOU ZHENFEI (Autor:in)

    Erscheinungsdatum :

    2021-06-04


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F01P Kühlung von Kraft- und Arbeitsmaschinen oder Kraftmaschinen allgemein , COOLING OF MACHINES OR ENGINES IN GENERAL / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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