A pressure relief arrangement for a gas turbine engine comprises a hinged door and a mount spaced from the door. An expandable structure is connected to the door and to the mount such that when the door hinges open the expandable structure expands.


    Access

    Download


    Export, share and cite



    Title :

    Gas turbine engine


    Contributors:

    Publication date :

    2020-10-13


    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 / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    Turbine engine

    European Patent Office | 2019

    Free access

    TURBINE ENGINE

    STRETTON RICHARD G | European Patent Office | 2019

    Free access

    Turbine engine

    European Patent Office | 2019

    Free access

    Turbine for a turbine engine

    SATRE ANTOINE FREDERIC JEAN / COUSSEAU SIMON JEAN-MARIE BERNARD / PERROT ERWAN | European Patent Office | 2021

    Free access

    Engine Avionics Turbine Engine Ignition

    British Library Online Contents | 1996