A cryogenic cooling system for an aircraft includes a first air cycle machine, a second air cycle machine, and a means for collecting liquid air. The first air cycle machine is operable to output a cooling air stream based on a first air source. The second air cycle machine is operable to output a chilled air stream at a cryogenic temperature based on a second air source cooled by the cooling air stream of the first air cycle machine. An output of the second air cycle machine is provided to the means for collecting liquid air.


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    Titel :

    CRYOGENIC COOLING SYSTEM FOR AN AIRCRAFT


    Beteiligte:
    SCHWARZ FREDERICK M (Autor:in) / WINTER MICHAEL (Autor:in) / LENTS CHARLES E (Autor:in) / SNAPE NATHAN (Autor:in) / EPSTEIN ALAN H (Autor:in)

    Erscheinungsdatum :

    26.09.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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