A pressure relief arrangement for a gas turbine engine comprises a panel and a plurality of pressure relief mechanisms provided in the panel. The mechanisms have a first configuration and a second configuration. In the first configuration the panel is sealed to prevent fluid flow through the panel in a thickness direction and in the second configuration the mechanisms are arranged so that a plurality of holes are provided in the panel so fluid can flow through the panel in a thickness direction.


    Access

    Download


    Export, share and cite



    Title :

    PRESSURE RELIEF ARRANGMENT FOR GAS TURBINE ENGINE


    Additional title:

    DRUCKENTLASTUNGSEINRICHTUNG FÜR GASTURBINENTRIEBWERK
    DISPOSITIF DE LIMITATION DE PRESSION POUR MOTEUR À TURBINE À GAZ


    Contributors:

    Publication date :

    2018-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



    Drive arrangment

    DENYS OPARIN / WILLI RUDER / ISTVAN HORVATH | European Patent Office | 2015

    Free access

    DRIVE ARRANGMENT FOR A BICYCLE

    BRAEDT HENRIK / HANKE JOACHIM | European Patent Office | 2019

    Free access

    BACK-UP MOORING ARRANGMENT

    SMEDAL ARNE / AARSNES JAN VIDAR / SYVERTSEN KÅRE | European Patent Office | 2016

    Free access

    INVERTER DEVICE AND ELECTRIC DRIVE ARRANGMENT

    KÖRNER JULIAN / ENDERLE EDUARD / FU HUAN et al. | European Patent Office | 2024

    Free access

    HOLDING ARRANGMENT AND PROTECTIVE COVER

    FERRERI DOMENICO / MITTIGA FRANCESCO | European Patent Office | 2016

    Free access