An aircraft engine includes an air inlet duct and at least one strut having a leading edge and a trailing edge (31B). The at least one strut (30) extends across at least part of the air inlet duct and has a strut passage. The trailing edge (31B) has one or more edge contours (39), each defining a contour edge wall (39W) recessed from a baseline surface (31 BS) of the trailing edge (31B). The one or more edge contours (39) have a recessed tap (38) in fluid communication with the strut passage.


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    Title :

    STRUT FOR AIRCRAFT ENGINE


    Additional title:

    STREBE FÜR EIN FLUGZEUGTRIEBWERK
    ENTRETOISE POUR MOTEUR D'AÉRONEF


    Contributors:

    Publication date :

    2023-10-04


    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



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