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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    Titel :

    TWO-TURBINE ENVIRONMENTAL CONTROL SYSTEM


    Weitere Titelangaben:

    ZWEITURBINEN-UMWELTKONTROLLSYSTEM
    SYSTÈME DE COMMANDE ENVIRONNEMENTAL DOTÉ DE DEUX TURBINES


    Beteiligte:

    Erscheinungsdatum :

    14.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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