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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    Title :

    PUMPED TWO-PHASE COOLING OF AIRCRAFT ELECTRONICS


    Additional title:

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


    Contributors:

    Publication date :

    2025-02-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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