An aircraft engine includes a rotating structure and a casing circumferentially surrounding the rotating structure. The aircraft engine further includes an acoustic panel for noise reduction circumferentially surrounding the rotating structure. The acoustic panel is disposed proximal the casing. Furthermore, the acoustic panel includes a plurality of acoustic panel members. In addition, the acoustic panel is secured to the casing by at least one securement mechanism such that the acoustic panel is substantially circumferentially fixed relative to the casing.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Acoustic panel of turbine engine


    Beteiligte:

    Erscheinungsdatum :

    2019-11-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



    ACOUSTIC PANEL OF TURBINE ENGINE

    HEETER ROBERT WARREN / RIVERS JONATHAN / BURNEY DENNES KYLE | Europäisches Patentamt | 2020

    Freier Zugriff

    ACOUSTIC LINER PANEL AND CONTAINMENT FOR A GAS TURBINE ENGINE

    EVANS DALE E | Europäisches Patentamt | 2020

    Freier Zugriff

    GAS TURBINE ENGINE ACCESS PANEL

    RIVERS JONATHAN M / FULAYTER ROY D | Europäisches Patentamt | 2019

    Freier Zugriff

    Gas turbine engine access panel

    RIVERS JONATHAN M / FULAYTER ROY D | Europäisches Patentamt | 2017

    Freier Zugriff

    Acoustic attenuation on a turbine engine wall

    REGNARD JOSSELIN DAVID FLORIAN / JODET NORMAN BRUNO ANDRÉ | Europäisches Patentamt | 2024

    Freier Zugriff