A system is provided for an aircraft. This aircraft system includes a gas turbine engine, a flowpath and an inlet guard. The gas turbine engine includes a compressor section. The flowpath projects longitudinally into the gas turbine engine from an airflow inlet and longitudinally through the compressor section. The inlet guard extends across the flowpath longitudinally upstream of the compressor section. The inlet guard extends circumferentially about an axis. The inlet guard includes a first screen and a second screen. The first screen includes a plurality of first perforations with a first perforation size. The second screen is circumferentially adjacent the first screen about the axis. The second screen includes a plurality of second perforations with a second perforation size that is different than the first perforation size.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    CIRCUMFERENTIALLY TAILORED INLET GUARD FOR AN AIRCRAFT ENGINE INLET


    Beteiligte:
    CUNNINGHAM MARK (Autor:in) / AKCAYOZ ERAY (Autor:in) / MARRANO ROBERTO (Autor:in) / BRETTE CORENTIN (Autor:in)

    Erscheinungsdatum :

    10.04.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Inlet guard screen for an inlet of an aircraft engine

    MARRANO ROBERTO / CUNNINGHAM MARK / AKCAYOZ ERAY et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    VARIABLE INLET GUARD SCREEN FOR AN INLET OF AN AIRCRAFT ENGINE

    MARRANO ROBERTO / CUNNINGHAM MARK / AKCAYOZ ERAY et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    AIRCRAFT ENGINE INLET ASSEMBLY APPARATUS

    BATT EDWARD / SISCO TANNI / SMITH DANIEL et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft engine inlet assembly apparatus

    BATT EDWARD / SISCO TANNI / SMITH DANIEL et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft-engine inlet and exhaust porting

    Young, V.C. | Engineering Index Backfile | 1944