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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    Title :

    NACELLE INLET WITH EXTENDED OUTER BARREL


    Additional title:

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


    Contributors:

    Publication date :

    2021-11-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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