A nacelle inlet may comprise a lip skin and a bulkhead mounted to the lip skin. The lip skin may define an orifice. The bulkhead may comprise a forward face, a first flange extending axially from an outer circumference of the forward face, and a ventilation groove formed in the forward face. The ventilation groove may be circumferentially aligned with the orifice.


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    Title :

    INLET BULKHEAD WITH VENTILATION GROOVE


    Contributors:

    Publication date :

    2020-11-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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