A nacelle inlet (42) is provided for an aircraft propulsion system (20). This nacelle inlet (42) includes an outer barrel (54), a bulkhead (58,60) and a plurality of supports (62). The outer barrel (54) extends around an axis (36) and along the axis (36) to an aft end (74). The bulkhead (58, 60) is within and connected to the outer barrel (54). An aft portion (86) of the outer barrel (54) projects axially aftward from the bulkhead (58, 60) to the aft end (74). The supports (62) are disposed around the axis (36) and next to the bulkhead (58, 60). The supports (62) are configured to support the aft portion (86) of the outer barrel (54).


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    Titel :

    NACELLE INLET WITH EXTENDED OUTER BARREL


    Weitere Titelangaben:

    GONDELEINLASS MIT ERWEITERTEM AUSSENGEHÄUSE
    ENTRÉE DE NACELLE PRÉSENTANT UNE EXTENSION DE CYLINDRE EXTERNE


    Beteiligte:
    BROWN KEITH T (Autor:in) / FOWLER FRANK J (Autor:in) / BYRNE STUART J (Autor:in) / STEIN ADAM (Autor:in)

    Erscheinungsdatum :

    24.11.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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