Various implementations described herein are directed to an emergency lubrication system for an aircraft. The emergency lubrication system includes a lubrication chamber, a bladder, a gearbox, and a valve. The bladder is coupled to the lubrication chamber and includes one or more chemicals that pressurize the lubrication in the lubrication chamber when activated. The valve is coupled between the lubrication chamber and the gearbox and provides the lubrication to one or more components within the gearbox.


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    Titel :

    Chemically Pressurized Emergency Lubrication System


    Beteiligte:
    HENRY TYSON (Autor:in)

    Erscheinungsdatum :

    2020-05-28


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16H Getriebe , GEARING / B64C AEROPLANES , Flugzeuge



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