A gas turbine engine exhaust system comprises an instrumented exhaust duct including a set of exhaust temperature probes installed at the exhaust end of the duct in an air space between the engine outer case and a surrounding engine nacelle. A shield is removably installed at the end of the exhaust duct to protect the probes and associated wiring in the air space.


    Access

    Download


    Export, share and cite



    Title :

    INSTRUMENTED TURBINE EXHAUST DUCT


    Additional title:

    CONDUIT D'EVACUATION DE TURBINE PAR INSTRUMENT


    Contributors:

    Publication date :

    2022-08-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    EXHAUST DUCT FOR TURBINE FORWARD OF FAN

    LORD WESLEY K / CHANDLER JESSE M / SUCIU GABRIEL L | European Patent Office | 2020

    Free access

    Exhaust duct for turbine forward of fan

    LORD WESLEY K / CHANDLER JESSE M / SUCIU GABRIEL L | European Patent Office | 2019

    Free access

    EXHAUST DUCT FOR TURBINE FORWARD OF FAN

    LORD WESLEY K / CHANDLER JESSE M / SUCIU GABRIEL L | European Patent Office | 2018

    Free access

    EXHAUST DUCT AND EXHAUST DUCT ASSEMBLY AND AIRCRAFT USING THE EXHAUST DUCT

    JOO YOUNG JUNG / CHUNG HEE YOON | European Patent Office | 2021

    Free access

    GAS GENERATOR BIFURCATING EXHAUST DUCT TO FREE TURBINE

    CHANDLER JESSE M / SUCIU GABRIEL L | European Patent Office | 2018

    Free access