According to the propeller aircraft lubricating oil cooling system and cooling method, an engine lubricating oil radiator and a generator lubricating oil radiator are integrated into an integrated lubricating oil radiator, the integrated lubricating oil radiator is located between an air inlet channel and an exhaust channel to form the lubricating oil cooling system, and the lubricating oil cooling system is installed on the lower portion of an aircraft nacelle. The air inlet channel, the integrated lubricating oil radiator and the exhaust channel form an air circulation channel; the two ends of an aircraft generator lubricating oil cooling pipeline are connected with a generator lubricating oil inlet connector and a generator lubricating oil outlet connector of the integrated lubricating oil radiator respectively; the two ends of the aircraft engine lubricating oil cooling pipeline are connected with the engine lubricating oil inlet connector and the engine lubricating oil outlet connector of the integrated lubricating oil radiator respectively.

    一种螺旋桨飞机滑油散热系统及散热方法,将发动机滑油散热器和发电机滑油散热器集成为一个集成滑油散热器,该集成滑油散热器位于进气道和排气道之间,形成滑油散热系统,该滑油散热系统安装在飞机短舱下部,使进气道、集成滑油散热器和排气道形成一个空气流通通道;将飞机发电机滑油冷却管路的两端分别与集成滑油散热器的发电机滑油入口接头和发电机滑油出口接头连接;将飞机发动机滑油冷却管路的两端分别与集成滑油散热器的发动机滑油入口接头和发动机滑油出口接头连接。


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    Titel :

    Propeller aircraft lubricating oil heat dissipation system and heat dissipation method


    Weitere Titelangaben:

    一种螺旋桨飞机滑油散热系统及散热方法


    Beteiligte:
    ZHANG MIAO (Autor:in) / YANG SONGTAO (Autor:in) / WANG BIN (Autor:in)

    Erscheinungsdatum :

    14.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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