Provided are an aircraft/spacecraft fluid cooling system and an aircraft/spacecraft fluid cooling method in which a fluid in a pipe installed in aircraft or spacecraft can be cooled efficiently so that the amount of fluid required for cooling the fluid can be reduced. A fluid cooling system (1) includes a feed line (6) that feeds a fluid from a storage tank (4) to a pump (8), and a cooling section (26) that expands a propellant having traveled through the pump (8), feeds the propellant to the outer periphery of the feed line (6) so as to cool the propellant in the feed line (6), and discharges the expanded propellant outside.


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    Title :

    AIRCRAFT/SPACECRAFT FLUID COOLING SYSTEM AND AIRCRAFT/SPACECRAFT FLUID COOLING DEVICE


    Additional title:

    FLÜSSIGKEITSKÜHLSYSTEM FÜR FLUGZEUGE/RAUMFAHRZEUGE UND FLÜSSIGKEITSKÜHLVORRICHTUNG FÜR FLUGZEUGE/RAUMFAHRZEUGE
    SYSTÈME DE REFROIDISSEMENT DE FLUIDE D'AÉRONEF/DE VÉHICULE SPATIAL ET DISPOSITIF DE REFROIDISSEMENT DE FLUIDE D'AÉRONEF/DE VÉHICULE SPATIAL


    Contributors:

    Publication date :

    2019-10-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64G Raumfahrt , COSMONAUTICS / F28D Wärmetauscher, soweit in keiner anderen Unterklasse vorgesehen, in denen die Wärmetauschmittel nicht in direkte Berührung miteinander kommen , HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT



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