An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle inlet structure extending axially along and circumferentially about an axis. The nacelle inlet structure includes an inlet lip, an inner barrel, an outer barrel and a plurality of supports. The inlet lip forms a leading edge of the nacelle inlet structure. The inner barrel projects axially aft away from the inlet lip. The outer barrel projects axially aft away from the inlet lip. The outer barrel is radially outboard of and axially overlaps the inner barrel. The supports are arranged circumferentially about the axis in an array. Each of the supports extends longitudinally along the axis. Each of the supports extends radially between and is connected to the inner barrel and the outer barrel.


    Access

    Download


    Export, share and cite



    Title :

    Outer barrel support structure for nacelle inlet structure


    Contributors:

    Publication date :

    2025-04-22


    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



    OUTER BARREL SUPPORT STRUCTURE FOR NACELLE INLET STRUCTURE

    MINER JASEN A | European Patent Office | 2025

    Free access

    OUTER BARREL SUPPORT STRUCTURE FOR NACELLE INLET STRUCTURE

    MINER JASEN A | European Patent Office | 2025

    Free access

    Nacelle inlet with extended outer barrel

    BROWN KEITH T / FOWLER FRANK J / BYRNE STUART J et al. | European Patent Office | 2018

    Free access

    NACELLE INLET WITH EXTENDED OUTER BARREL

    BROWN KEITH T / FOWLER FRANK J / BYRNE STUART J et al. | European Patent Office | 2016

    Free access

    NACELLE INLET WITH EXTENDED OUTER BARREL

    BROWN KEITH T / FOWLER FRANK J / BYRNE STUART J et al. | European Patent Office | 2021

    Free access