A deployable drains mast for draining fluids from a propulsion system is provided. The deployable drains mast includes a bordered structure. The bordered structure includes a plurality of exterior walls forming a cavity. The bordered structure further includes at least one drain opening to the cavity located at a first end of the bordered structure. The at least one drain opening configured to receive a drain line from a component of a core compartment of the propulsion system. The bordered structure further includes at least one drain exit from the cavity located at a second end of the bordered structure opposite the first end. The drain exit configured to expel the fluid.


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    Title :

    DEPLOYABLE DRAINS MAST


    Contributors:

    Publication date :

    2025-06-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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