A system (20) for a gas turbine engine includes a flowpath wall (30, 32) and a deflector (78). The flowpath wall (30, 32) includes a surface (56) and an opening (72) to a blind aperture (68). The surface (56) forms a peripheral boundary of an internal engine flowpath (26). The opening (72) is disposed in the surface (56). The blind aperture (68) extends vertically into the flowpath wall (30, 32) from the opening (72). The deflector (78) projects vertically out from the flowpath wall (32) into the internal engine flowpath (26). The deflector (78) is configured to deflect gas flowing within the internal engine flowpath (26) over the opening (72).


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    Title :

    FLOW DEFLECTOR FOR APERTURE IN GAS TURBINE ENGINE FLOWPATH WALL


    Additional title:

    STRÖMUNGSDEFLEKTOR FÜR ÖFFNUNG IN EINER STRÖMUNGSPFADWANDUNG EINES GASTURBINENMOTORS
    DÉFLECTEUR DE DÉBIT POUR OUVERTURE DANS UNE PAROI DE TRAJET D'ÉCOULEMENT DE MOTEUR À TURBINE À GAZ


    Contributors:

    Publication date :

    2024-01-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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