An aircraft cooling system (4500) comprises an evaporator (4500, 5004), condenser (4512, 4806), an accumulator, and a pump system (4514). The evaporator (4500, 5004) is configured to cool a set of heat loads (4501, 4805, 5011) in an aircraft (199, 400, 3127, 3855, 4502) using a liquid (4516, 5032). The liquid (4516, 5032) forms a vapor (4519, 5031) in response to cooling the set of heat loads (4501, 4805, 5011). The condenser (4512, 4806) is configured to receive the vapor (4519, 5031) from the evaporator (4500, 5004) and cool the vapor (4519, 5031) in which cooling the vapor (4519, 5031) forms the liquid (4516, 5032). The accumulator (4513, 4808, 5008)is configured to receive the liquid (4516, 5032) from the condenser (4512, 4806) and store the liquid (4516, 5032). The pump system (4514) is configured to pump the liquid (4516, 5032) stored in the accumulator (4513, 4808, 5008) to the evaporator (4500, 5004).


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    Titel :

    PUMPED TWO-PHASE COOLING OF AIRCRAFT ELECTRONICS


    Weitere Titelangaben:

    GEPUMPTE ZWEIPHASENKÜHLUNG VON FLUGZEUGELEKTRONIK
    REFROIDISSEMENT À DEUX PHASES POMPÉ DE L'ÉLECTRONIQUE D'UN AÉRONEF


    Beteiligte:
    STOIA MICHAEL F (Autor:in) / TU JIANPING (Autor:in) / MULEY ARUN (Autor:in) / SMITH RICHARD C III (Autor:in) / JUI KEVIN JAVIER (Autor:in)

    Erscheinungsdatum :

    19.02.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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