Systems and methods are provided for an aircraft propulsor with a fan cowl with one or more tangential restraints. The tangential restraints may be configured to enter respective tangential receiving portions of a fixed portion of the aircraft propulsor. The fan cowl may receive a load that may include a bending load. The tangential restraints may be configured to convert the bending load to membrane tension and thus decrease deflection of the fan cowl. The fan cowl may be a translating sleeve used for a reverse thrust.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    NACELLE WITH TANGENTIAL RESTRAINT


    Beteiligte:
    JOEL JASON F (Autor:in)

    Erscheinungsdatum :

    2020-09-10


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Nacelle with tangential restraint

    JOEL JASON F | Europäisches Patentamt | 2022

    Freier Zugriff

    Nacelle cowl tangential restraint

    JOEL JASON F | Europäisches Patentamt | 2020

    Freier Zugriff

    NACELLE FAN COWL TANGENTIAL RESTRAINT

    JOEL JASON F | Europäisches Patentamt | 2019

    Freier Zugriff

    NACELLE FAN COWL TANGENTIAL RESTRAINT

    JOEL JASON F | Europäisches Patentamt | 2018

    Freier Zugriff

    Nacelle for aircraft propulsion unit comprising access space closed by tangential clamping shroud

    CARURE PIERRE CHARLES | Europäisches Patentamt | 2024

    Freier Zugriff