A nacelle (12) for a gas turbine engine (10) that extends along an engine centerline (CO includes an inner portion (28), an outer portion (30), and a nacelle flow control system (26). The outer portion (30) surrounds the inner portion (28) and connects to the inner portion (28) at a leading edge (32). The nacelle flow control system (26) includes an internal flow control (38) for the inner portion (28) and an external flow control (40) for the outer portion (30).


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    Title :

    NACELLE INTERNAL AND EXTERNAL FLOW CONTROL


    Additional title:

    INTERNE UND EXTERNE FLUSSSTEUERUNG EINER GONDEL
    RÉGULATION DE L'ÉCOULEMENT INTERNE ET EXTERNE D'UNE NACELLE


    Contributors:

    Publication date :

    2016-11-16


    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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