The invention provides a helicopter equipment compartment heat dissipation system and a heat dissipation control method, and the helicopter equipment compartment heat dissipation system comprises a control device, a temperature sensor, an upper air port, an equipment frame, a heat dissipation fan, a lower air port and other components. The air direction, the air volume and the hot air flow direction of the cooling fan can be adjusted according to the environment temperature and the flight state of the helicopter, in the using process, power consumption can be reduced, noise can be lowered, in the low-temperature environment, hot air can be exhausted into a cabin to heat the cabin, and comprehensive utilization of heat of the helicopter is achieved.

    本发明提供一种直升机设备舱散热系统及散热控制方法,所述一种直升机设备舱散热系统包括:控制装置、温度传感器、上部风口、设备架、散热风扇和下部风口等零组件,可以根据环境温度、直升机飞行状态调整散热风扇的风向、风量和热空气流向,使用过程中,能够减少功耗,降低噪音,在低温环境中,还能将热空气排到座舱中,对座舱进行加温,实现直升机热量的综合利用。


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    Title :

    Helicopter equipment compartment heat dissipation system and heat dissipation control method


    Additional title:

    一种直升机设备舱散热系统及散热控制方法


    Contributors:
    CHEN JIAPENG (author) / XU CHAOLIANG (author) / ZHOU LE'E (author) / XIE DINGXIANG (author) / SHI JIN (author)

    Publication date :

    2023-08-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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




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