A propulsion system for an aircraft includes a gas generating core engine, a propulsor that is driven by an exhaust gas flow that is generated by the core engine, and an inlet assembly where an inlet airflow is communicated to the core engine. The inlet assembly is disposed aft of the core engine and includes a turning duct that directs inlet air into the core engine, and a particle exhaust outlet that directs particulates away from the core engine.


    Access

    Download


    Export, share and cite



    Title :

    AFT AIR INLET PARTICLE SEPARATOR FOR TURBINE ENGINE


    Contributors:

    Publication date :

    2024-08-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Inlet particle separator for a turbine engine

    KISZEWSKI COURTNEY ANN | European Patent Office | 2019

    Free access

    Inertial particle separator for engine inlet

    BISSON FRANCOIS / CUNNINGHAM MARK | European Patent Office | 2019

    Free access

    Engine inlet with deployable particle separator

    GIANOPULOS ELIA N | European Patent Office | 2022

    Free access

    ENGINE INLET WITH DEPLOYABLE PARTICLE SEPARATOR

    GIANOPULOS ELIA N | European Patent Office | 2020

    Free access

    Inertial particle separator for engine inlet

    BISSON FRANCOIS / CUNNINGHAM MARK | European Patent Office | 2020

    Free access