A nacelle assembly includes a fixed inlet segment (56) and a translating inlet segment (58). The translating inlet segment (58) includes a slider beam (86) laterally between a pair of tracks (68;70) of the fixed inlet segment (56). The slider beam (86) is mated with and slidable longitudinally along the pair of tracks (68;70). The translating inlet segment (58) is configured to translate longitudinally between a retracted position and an extended position. An aft end (78) of the translating inlet segment (58) is abutted against a forward end (60) of the fixed inlet segment (56) when the translating inlet segment (58) is in the retracted position. An airflow inlet (46) into an inlet passage of the nacelle assembly is opened longitudinally between the aft end (78) and the forward end (60) when the translating inlet segment (58) is in the extended position.


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    Title :

    NACELLE WITH A TRANSLATABLE INLET FOR AN AIRCRAFT PROPULSION SYSTEM


    Additional title:

    GONDEL MIT EINEM VERSCHIEBBAREN EINLASS FÜR EIN FLUGZEUGANTRIEBSSYSTEM
    NACELLE AYANT UNE ENTRÉE DÉPLAÇABLE POUR SYSTÈME DE PROPULSION D'AÉRONEF


    Contributors:

    Publication date :

    2022-10-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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