A method and apparatus for supplying air to a precooler (1417). Air flow is created through a fan duct in an engine system. A first portion of the air flow is directed into a first inlet (1428) of an inlet system (1416) to feed a first half of the precooler (1417). A second portion of the air flow is directed through the fan duct into a second inlet (1441) of the inlet system to feed a second half of the precooler (1417).


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    Title :

    Inlet system having dual inlets


    Additional title:

    Einlasssystem mit zwei Eingängen
    Système d'admission comprenant deux entrées


    Contributors:

    Publication date :

    2018-08-29


    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



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