Various implementations described herein are directed to a lubrication system for a gearbox of an aircraft. A lubrication line is coupled to a plurality of jets and/or orifices to provide lubrication to one or more components of the gearbox. A check valve is placed within the lubrication line in a location upstream from the plurality of jets and/or orifices.


    Access

    Download


    Export, share and cite



    Title :

    Lubrication system


    Contributors:

    Publication date :

    2021-11-30


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge / F16K VALVES , Ventile



    Lubrication system

    BALDWIN TYLER WAYNE / CRAVENER KYLE THOMAS / HENRY TYSON | European Patent Office | 2022

    Free access

    Lubrication system

    GEHMAN K MARLIN | European Patent Office | 2025

    Free access

    LUBRICATION SYSTEM

    GMIRYA YURIY | European Patent Office | 2024

    Free access

    LUBRICATION SYSTEM

    BALDWIN TYLER WAYNE / CRAVENER KYLE THOMAS / HENRY TYSON | European Patent Office | 2022

    Free access

    LUBRICATION SYSTEM

    BALDWIN TYLER WAYNE / CRAVENER KYLE THOMAS / HENRY TYSON | European Patent Office | 2020

    Free access