An air inlet for an aircraft propulsion system nacelle includes an outer skin, an inner skin, a lip skin, and a forward bulkhead. The lip skin extends between and to an outer end and an inner end. The outer end is disposed at the outer skin. The inner end is disposed at the inner skin. The forward bulkhead includes a first bulkhead portion and a second bulkhead portion. The first bulkhead portion and the second bulkhead portion are mounted to the outer skin. The first bulkhead portion and the second bulkhead portion are mounted to the inner skin. The first bulkhead portion includes a rigid body material and the second bulkhead portion includes a flexible body material.


    Access

    Download


    Export, share and cite



    Title :

    AIR INLET BULKHEAD ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM


    Contributors:

    Publication date :

    2024-08-01


    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



    AIR INLET BULKHEAD ASSEMBLY FOR AN AIRCRAFT PROPULSION SYSTEM

    SCHRELL JOHANN / SHERMAN BRIAN A | European Patent Office | 2024

    Free access

    INLET BULKHEAD FOR LARGE DIAMETER AIRCRAFT ENGINES

    WIJESINGHE JANAKA / ROCHA ANDREW G / ZIMNEY ERIC J | European Patent Office | 2021

    Free access

    AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET ASSEMBLY

    GORMLEY TIMOTHY | European Patent Office | 2025

    Free access

    Inlet bulkhead with ventilation groove

    KROEGER DANIEL / HERMOSURA DELBERT N | European Patent Office | 2022

    Free access

    AIRCRAFT PROPULSION SYSTEM WITH VARIABLE AREA INLET ASSEMBLY

    GORMLEY TIMOTHY | European Patent Office | 2025

    Free access