A gas turbine engine has a first shaft including a first turbine rotor, and a second shaft including a second turbine rotor disposed downstream of the first turbine rotor. A third shaft includes a propulsor turbine positioned downstream of the second turbine rotor for driving a propeller. A mount ring is secured between the second turbine rotor and the propeller.


    Access

    Download


    Export, share and cite



    Title :

    TWO SPOOL GAS GENERATOR WITH MOUNT RING


    Additional title:

    ZWEISPULENGASGENERATOR MIT HALTERING
    GÉNÉRATEUR DE GAZ DOUBLE CORPS AVEC ANNEAU DE MONTAGE


    Contributors:

    Publication date :

    2020-01-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    DUAL VOLTAGE LOW SPOOL GENERATOR

    KRENZ MICHAEL | European Patent Office | 2021

    Free access

    DUAL VOLTAGE LOW SPOOL GENERATOR

    KRENZ MICHAEL | European Patent Office | 2021

    Free access

    Aircraft with low pressure spool emergency generator

    FINNEY ADAM M / KRENZ MICHAEL / WAGNER CARL A et al. | European Patent Office | 2021

    Free access

    COMBINATION LOW SPOOL GENERATOR AND RAM AIR TURBINE GENERATOR

    DOOLEY KEVIN ALLAN / CHENG AUDREY / MAKUSZEWSKI JERZY | European Patent Office | 2019

    Free access

    FLUID PRESSURE GENERATOR AND SPOOL POSITION ESTIMATION DEVICE

    NINOYU MASAKI / OKANO TAKAHIRO / MASUDA YOSHIO | European Patent Office | 2017

    Free access