An apparatus comprises a leading edge (1432) of an inlet (1428). The leading edge (1432) of the inlet (1428) is positioned relative to a direction of air flow such that a total pressure of air along the leading edge (1432) of the inlet (1428) is equalized within selected tolerances.


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    Title :

    Inlet system for a precooler


    Additional title:

    Einlasssystem für einen Vorkühler
    Système d'admission pour un prérefroidisseur


    Contributors:

    Publication date :

    2015-05-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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