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 :

    CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT


    Additional title:

    KRYOGENES KÜHLSYSTEM FÜR EIN FLUGZEUG
    SYSTÈME DE REFROIDISSEMENT CRYOGÉNIQUE POUR AÉRONEF


    Contributors:

    Publication date :

    2024-04-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    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 / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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