A system for an aircraft (100) includes an engine bleed source (251) of a gas turbine engine (20). The system also includes a means for chilling an engine bleed air flow (252) from the engine bleed source (251) to produce a chilled working fluid. The system further includes a means for providing the chilled working fluid for an aircraft use.


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    Title :

    CHILLED WORKING FLUID GENERATION AND SEPARATION FOR AN AIRCRAFT


    Additional title:

    ERZEUGUNG UND TRENNUNG GEKÜHLTER ARBEITSFLUIDE FÜR EIN FLUGZEUG
    GÉNÉRATION ET SÉPARATION DE FLUIDE DE TRAVAIL RÉFRIGÉRÉ POUR UN AÉRONEF


    Contributors:

    Publication date :

    2023-02-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F25J LIQUEFACTION, SOLIDIFICATION, OR SEPARATION OF GASES OR GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT , Verflüssigen, Verfestigen oder Trennen von Gasen oder Gasgemischen durch Druck- und Kältebehandlung



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