An environmental control system (12) for an aircraft according to an example of the present disclosure includes a first turbine (T1) coupled to an engine (10) and a second turbine (T2) coupled to a compressor (C). One or more ducts (16) are configured to provide bleed air from the engine to the first and second turbines and the compressor such that the first and second turbines and the compressor condition the bleed air. A method of conditioning air is also disclosed.


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    Title :

    TWO-TURBINE ENVIRONMENTAL CONTROL SYSTEM


    Additional title:

    ZWEITURBINEN-UMWELTKONTROLLSYSTEM
    SYSTÈME DE COMMANDE ENVIRONNEMENTAL DOTÉ DE DEUX TURBINES


    Contributors:

    Publication date :

    2023-06-14


    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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