A water extractor for an environmental control system of an aircraft includes a water extraction vessel arranged in fluid communication with the separation mechanism. The water extraction vessel includes a first portion for receiving a first airstream and a second portion for receiving a second airstream. A stationary diffuser is mounted within the second portion.


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    Title :

    Vented dynamic pressure recovery module for aircraft ECS


    Contributors:

    Publication date :

    2020-08-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B01D SEPARATION , Trennen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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