A turbine engine system includes an inlet particle separator (36) receiving an inlet fluid flow and having a clean outlet (52) for a first flow of substantially clean fluid, and a scavenge outlet (54) for a second flow of scavenge fluid. A fluid pump (64) communicates with the scavenge outlet (54). The flow of scavenge fluid through the fluid pump (64) is selectively regulated.


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    Title :

    SYSTEM AND METHOD WITH INLET PARTICLE SEPARATOR


    Additional title:

    SYSTEM UND VERFAHREN MIT EINLASSTEILCHENABSCHEIDER
    SYSTÈME ET PROCÉDÉ À FILTRE SÉPARATEUR DE PARTICULES


    Contributors:

    Publication date :

    2016-06-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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