A system includes an inlet line (102) configured to receive a medium flowing from a low-pressure location of an engine to a chamber (104), a plurality of heat exchangers (110,120) configured to receive the medium from the inlet line (102), and a valve (106) located upstream from the plurality of heat exchangers (110,120). The valve (106) is configured to divide in parallel the medium across at least a first heat exchanger (110) and a second heat exchanger (120) of the plurality of heat exchangers. A recirculation air system (400) is configured to supply a recirculation air from the chamber (104) to the inlet line (102) upstream of the heat exchangers (110,120).


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    Title :

    RECIRCULATION SYSTEM FOR PARALLEL RAM HEAT EXCHANGERS


    Additional title:

    RÜCKFÜHRUNGSSYSTEM FÜR PARALLELE RAM-WÄRMETAUSCHER
    SYSTÈME DE RECIRCULATION POUR ÉCHANGEURS DE CHALEUR DE RAM PARALLÈLES


    Contributors:

    Publication date :

    2021-01-20


    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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