The invention provides an aircraft heat dissipation system and an aircraft. The aircraft heat dissipation system comprises an equipment compartment and an air cooling channel. The equipment cabin is arranged in a body of the aircraft and used for mounting heating equipment; the air cooling channel is arranged in the machine body in a penetrating manner; wherein the machine body is provided with an air inlet communicated with the air cooling channel, cooling airflow enters the air cooling channel from the air inlet in the flying process of the aircraft, and cooling is directly or indirectly provided for the heating equipment in the equipment compartment. The problems that in the prior art, a fuselage of an aircraft is poor in heat dissipation, and the weight of the fuselage of the aircraft is large when a liquid cooling system is completely adopted for cooling can be solved.

    本发明提供一种飞行器散热系统和飞行器,该飞行器散热系统包括:设备舱和风冷通道。设备舱设置于飞行器的机体内,用于安装发热设备;风冷通道贯通设置在所述机体内;其中,所述机体上具有与所述风冷通道相连通的进风口,冷却气流在所述飞行器飞行的过程中,自所述进风口进入所述风冷通道,直接或间接的为所述设备舱内的所述发热设备提供冷却。本发明可以改善现有技术中飞行器的机身散热较差,完全采用液冷系统冷却飞行器机身重量较大的问题。


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    Title :

    Aircraft heat dissipation system and aircraft


    Additional title:

    一种飞行器散热系统和飞行器


    Contributors:
    XUE SONGBAI (author) / XIAO RENCHAO (author) / XIE SHAIMING (author) / LI QING (author) / LIAO ZHIQIAO (author)

    Publication date :

    2023-01-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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