A bifurcated inlet scoop frame for a gas turbine engine and method of using such frame for a gas turbine engine are disclosed. The bifurcated inlet scoop frame having a nose, a first side panel, and a second side panel. The first side panel and the nose defining a first inlet port. The second side panel and the nose defining a second inlet port. The method including the steps of providing a bifurcated inlet scoop frame, splitting the fan air flow, and receiving fan air through the bifurcated inlet scoop frame.


    Access

    Download


    Export, share and cite



    Title :

    BIFURCATED INLET SCOOP FOR GAS TURBINE ENGINE


    Additional title:

    VERZWEIGTE EINLASSHUTZE FÜR GASTURBINENMOTOR
    PRISE D'AIR À ENTRÉE BIFURQUÉE POUR MOTEUR À TURBINE À GAZ


    Contributors:

    Publication date :

    2020-02-26


    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



    Bifurcated inlet scoop for gas turbine engine

    JEN HSIANMIN / LOSYEV SERGEY | European Patent Office | 2019

    Free access

    GAS TURBINE ENGINE HAVING A BIFURCATED AIR INLET HOUSING

    JONES ANTHONY C / LYDON PATRICK M / THAYALAKHANDAN NAGAMANY et al. | European Patent Office | 2019

    Free access

    Bifurcated air inlet housing for a miniature gas turbine engine

    JONES ANTHONY C / LYDON PATRICK M / THAYALAKHANDAN NAGAMANY et al. | European Patent Office | 2020

    Free access

    Nacelle scoop inlet

    ZYSMAN STEVEN H | European Patent Office | 2015

    Free access

    Deployable inlet scoop for an inboard ram air turbine

    RIORDAN CONOR | European Patent Office | 2018

    Free access