An environmental control system of an aircraft includes a ram air circuit including a ram air shell having at least one heat exchanger positioned therein, a dehumidification system arranged in fluid communication with the ram air circuit, and a compression device arranged in fluid communication with the ram air circuit and the dehumidification system. The compression device includes a compressor, a turbine, and a fan coupled by a shaft, wherein the fan is operable to move ram air through the ram air circuit and the turbine includes a first inlet for receiving a first flow of medium and a second inlet for receiving a second flow of medium.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM


    Contributors:

    Publication date :

    2019-12-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B01D SEPARATION , Trennen / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS



    Aircraft environmental control system

    BRUNO LOUIS J / HO TONY / COUTIN AIDEN | European Patent Office | 2023

    Free access

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

    BRUNO LOUIS J / HO TONY / COUTIN AIDEN | European Patent Office | 2022

    Free access

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

    BRUNO LOUIS J / HO TONY / COUTIN AIDEN | European Patent Office | 2022

    Free access

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

    BRUNO LOUIS J / HO TONY / COUTIN AIDEN | European Patent Office | 2022

    Free access

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM

    BRUNO LOUIS J / ZYWIAK THOMAS M | European Patent Office | 2019

    Free access