An environmental control system of an aircraft includes a heat exchanger (58) configured to cool an airstream and a water extractor (60) arranged in fluid communication with an outlet of the heat exchanger. The water extractor includes a separation mechanism (70) for separating the airstream into a first airstream and a second airstream. The first airstream has water droplets entrained therein. A flow path of the airstream within the separation mechanism includes an angle. The separation mechanism includes a water extractor vessel (72) axially aligned and in fluid communication with the separation mechanism. The water extractor vessel includes a first portion for receiving the first airstream and a second portion for receiving the second airstream. The first portion is configured to collect and remove water droplets from the first airstream.


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    Titel :

    TANGENTIAL ENTRY WATER SEPARATOR FOR AIRCRAFT ECS


    Weitere Titelangaben:

    WASSERABSCHEIDER MIT TANGENTIALEM EINTRITT FÜR FLUGZEUG-ECS
    SÉPARATEUR D'EAU D'ENTRÉE TANGENTIELLE POUR SYSTÈMES DE CONTRÔLE DE L'ENVIRONNEMENT (ECS) D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    24.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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