An environmental control system (20) of an aircraft includes a compressing device (40) having a compressor (42) configured to receive a flow of a first medium and a turbine (44) configured to receive the flow of the first medium from the compressor and a flow of a second medium. The turbine (44) is arranged downstream from the compressor along a flow path of the first medium. A dehumidification system is arranged in fluid communication with the turbine and a bypass valve is operable configured to divert the flow of the first medium around the turbine and at least a portion of the dehumidification system.


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    Title :

    SHOESTRING ENVIRONMENTAL CONTROL SYSTEM FOR AN AIRCRAFT


    Additional title:

    SHOESTRING-UMWELTSTEUERSYSTEM FÜR EIN FLUGZEUG
    SYSTÈME DE CONTRÔLE ENVIRONNEMENTAL RESTREINT POUR AÉRONEF


    Contributors:

    Publication date :

    2024-04-03


    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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