A method for controlling a pressure control mechanism in a turbofan engine having a precooler permitting heat exchange between ambient air and bleed air includes detecting at least one of an engine failure or a bleed system failure, detecting at least one of an ice condition or an activation of an anti-ice system, and actuating the pressure control mechanism, thereby altering the heat exchange between the ambient air and the bleed air.


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    Title :

    CONTROL SYSTEM AND METHOD FOR OPERATING A PRECOOLER IN AN AIRCRAFT


    Additional title:

    REGELSYSTEM UND VERFAHREN ZUM BETRIEB EINES VORKÜHLERS IN EINEM FLUGZEUG
    SYSTÈME DE COMMANDE ET PROCÉDÉ POUR UTILISER UN PRÉREFROIDISSEUR DANS UN AÉRONEF


    Contributors:

    Publication date :

    2018-10-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / 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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