An inertial particle separator (IPS) for a gas turbine engine, has: a plenum circumferentially extending about a central axis and defined between an outer wall and an inner wall, the plenum having an inlet facing a circumferential direction relative to the central axis, a radius of the outer wall decreasing in an axial direction relative to the central axis between the inlet and an annular splitter extending circumferentially around the central axis and located downstream of the inlet radially between the outer wall and the inner wall, a particle outlet including an annulus radially between the outer wall and the splitter, an air outlet fluidly connectable to a compressor of the gas turbine engine and defined radially between the splitter and the inner wall.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Inertial particle separator for turbine engine


    Beteiligte:
    MENHEERE DAVID (Autor:in) / CHIAPPETTA SANTO (Autor:in) / REDFORD TIM (Autor:in) / VAN DEN ENDE DANIEL (Autor:in)

    Erscheinungsdatum :

    2022-03-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B01D SEPARATION , Trennen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    INERTIAL PARTICLE SEPARATOR FOR TURBINE ENGINE

    MENHEERE DAVID / CHIAPPETTA SANTO / REDFORD TIM et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Axial inertial particle separator for turbine engine

    MENHEERE DAVID / CHIAPPETTA SANTO / REDFORD TIM et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    GAS TURBINE ENGINE WITH INERTIAL PARTICLE SEPARATOR

    MARRANO ROBERTO / BISSON FRANCOIS | Europäisches Patentamt | 2019

    Freier Zugriff

    ADAPTABLE INERTIAL PARTICLE SEPARATOR FOR A GAS TURBINE ENGINE INTAKE

    SNYDER PHILIP HAROLD | Europäisches Patentamt | 2020

    Freier Zugriff

    Inertial particle separator for engine inlet

    BISSON FRANCOIS / CUNNINGHAM MARK | Europäisches Patentamt | 2019

    Freier Zugriff