A method for recovering air in an aircraft includes bleeding bypass air (122;196) from an engine bypass (76;152), bleeding core air (120;194) from an engine core (74;150), and placing the bypass air and the core air in a heat exchange relationship to produce heated bypass air (126;200) and cooled core air (124;198). The method further includes directing the heated bypass air to one or more of: the engine bypass (76), a cowl (149) de-icing system, and a wing (206) anti-ice system.


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    Title :

    AIR RECOVERY SYSTEM FOR PRECOOLER HEAT-EXCHANGER AND CORRESPONDING METHOD


    Additional title:

    LUFTRÜCKGEWINNUNGSSYSTEM FÜR EINEN VORKÜHLERWÄRMETAUSCHER SOWIE DAZUGEHÖRIGES VERFAHREN
    SYSTÈME DE RÉCUPÉRATION D'AIR POUR ÉCHANGEUR THERMIQUE DE PRÉREFROIDISSEUR ET PROCÉDÉ CORRESPONDANT


    Contributors:

    Publication date :

    2020-04-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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