Heat exchangers include a heat exchanger core defining at least two separate heat exchanger flow streams, a first header configured on the heat exchanger core and fluidly connected to a first of the separate heat exchanger flow streams, a second header configured on the heat exchanger core and fluidly connected to a second of the separate heat exchanger flow streams, and an integrated bypass system configured to directly fluidly connect the first header to the second header with a bypass conduit, the integrated bypass system having a control valve within the bypass conduit and configured to control flow through the bypass conduit.


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    Title :

    Heat Exchanger with Integral Bypass Valve


    Contributors:

    Publication date :

    2017-09-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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