A method and apparatus for separating particles from an inlet airflow of a turbine engine has a centerbody with at least one radially outward scavenge conduit. The inlet airflow has entrained particulate matter, which can impact an impact surface defining part of the centerbody. The particulate matter is radially diverted outward through at least one inlet to a scavenge conduit, unable to make a turn defined by the shape of the centerbody.


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    Titel :

    Inlet particle separator for a turbine engine


    Beteiligte:

    Erscheinungsdatum :

    03.09.2019


    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 / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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