A cooling system (2) for an interior space of a vehicle comprises a main cooling system (4) coupled with an air inlet (6) for receiving air (10) and coupled with the interior space (12, 14, 16, 18, 20) for providing cooled air to the interior space (12, 14, 16, 18, 20), at least one air (8, 22, 24, 26) duct arranged between the air inlet (6) and the interior space (12, 14, 16, 18, 20), a reservoir (30) for liquid nitrogen having a nitrogen outlet (34) and a valve (36) arranged between the outlet (34) and an injection port (38) of the at least one air duct (8, 22, 24, 26). The reservoir (30) is couplable with the injection port (38) of the at least one air duct (8, 22, 24, 26) via the valve (36) on demand for evaporating nitrogen in the at least one air duct (8, 22, 24, 26). With the injection of liquid nitrogen the main cooling system (4) is supported in case it is not able to provide a sufficient cooling power.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft supplementary cooling system by evaporating liquid nitrogen


    Weitere Titelangaben:

    Flugzeug-Zusatzkühlanlage durch Verdampfen flüssigen Stickstoffs
    Système de refroidissement supplémentaire d'aéronef par évaporation d'azote liquide


    Beteiligte:
    THIELE CHRISTIAN (Autor:in) / CERNKO EMIL (Autor:in)

    Erscheinungsdatum :

    13.03.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aircraft supplementary cooling system by evaporating liquid nitrogen

    THIELE CHRISTIAN / CERNKO EMIL | Europäisches Patentamt | 2018

    Freier Zugriff

    AIRCRAFT SUPPLEMENTARY COOLING SYSTEM BY EVAPORATING LIQUID NITROGEN

    THIELE CHRISTIAN / CERNKO EMIL | Europäisches Patentamt | 2016

    Freier Zugriff


    TRANSIENT SIMULATION OF A DIRECT-EVAPORATING CO2 COOLING SYSTEM FOR AN AIRCRAFT

    Vasel, J. / Schmitz, G. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2006


    Skin thermal response for an aircraft with supplementary skin cooling system

    Hashemi, Ab / Wong, Hubert / Schneider, Julie et al. | AIAA | 1998