A heat exchanging arrangement includes a first flow circuit (102) for a first fluid to be cooled, which has a first inlet (109), a first outlet (110), and a second outlet (112). The heat exchanging arrangement includes a second flow circuit (104) for a second fluid, which is in thermal communication with the first flow circuit. The heat exchanging arrangement includes a third flow circuit configured to port a portion of the first fluid from a first location of the first flow circuit (102) to a second location of the first flow circuit (102), the first location being downstream of the second location.


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    Title :

    HEAT EXCHANGER THERMAL SHOCK REDUCER


    Additional title:

    THERMOSCHOCKREDUZIERER FÜR WÄRMETAUSCHER
    RÉDUCTEUR DE CHOC THERMIQUE D'ÉCHANGEUR DE CHALEUR


    Contributors:

    Publication date :

    2020-10-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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