An environmental control system (20) of an aircraft includes a ram air circuit (30) including a ram air shell (32) having at least one heat exchanger (34) positioned therein, a dehumidification system (60) arranged in fluid communication with the ram air circuit, and a compressing device (40) arranged in fluid communication with the ram air circuit and the dehumidification system. The compression device includes a compressor (42) and a first turbine (44) coupled to one another via a shaft (50). During operation of the first turbine, work is extracted from a first medium within the first turbine to power the compressor. At an outlet of the first turbine, a temperature of the first medium is above freezing and at least a portion of the moisture within the first medium is condensed.


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    Title :

    AIRCRAFT ENVIRONMENTAL CONTROL SYSTEM


    Additional title:

    UMWELTKONTROLLSYSTEM FÜR FLUGZEUG
    SYSTÈME DE CONTRÔLE ENVIRONNEMENTAL D'UN AÉRONEF


    Contributors:

    Publication date :

    2019-07-24


    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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