A turbine engine having a nacelle is provided. The nacelle includes, upstream, an air intake fairing and an element for deflecting foreign objects which defines with the fairing an air intake flow path for supplying air to two coaxial flow paths which are a radially inner flow path and a radially outer flow path. The outer flow path being is by a hub housing and scoops, the hub housing and the scoops being installed downstream of the element for deflecting objects. Each scoop includes two independent portions which are an upstream portion borne by the hub housing, and a downstream portion borne by the nacelle.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Turbine engine having an element for deflecting foreign objects


    Beteiligte:

    Erscheinungsdatum :

    29.07.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    System and method for deflecting airborne objects

    DIEHL PETER G / DINGLI ROBERT | Europäisches Patentamt | 2020

    Freier Zugriff

    System and method for deflecting airborne objects

    DIEHL PETER G / DINGLI ROBERT | Europäisches Patentamt | 2020

    Freier Zugriff

    CABLE-DEFLECTING DEVICE AND SEAT LONGITUDINAL ADJUSTMENT APPARATUS HAVING A CABLE DEFLECTING DEVICE

    ROCK ARKADIUS / SUBRAMANIAN KARTHIKEYAN MAHARAJAPURAM / MEDVED ANDREJ et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    Thrust deflecting device and aircraft engine

    KLINGELS HERMANN / KLAEN STEPHAN / SCHERER CHRISTIAN et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    SECURING ELEMENT FOR A DEFLECTING UNIT

    MOSER CHRISTOF | Europäisches Patentamt | 2018

    Freier Zugriff