A gas turbine engine comprises a turbine within a turbine case defining a hot combustion gas path. The turbine case has an inner port. An outer case is disposed radially outward from the turbine case. The outer case has an outer port. A sleeve releasably engages the outer port and the inner port. A sensor is mounted to a distal end of the sleeve. The sensor has a probe extending through the inner port into the hot combustion gas path.


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    Titel :

    REMOVABLE TURBINE GASPATH SENSOR


    Weitere Titelangaben:

    CAPTEUR DE TRAJET DE GAZ DE TURBINE AMOVIBLE


    Beteiligte:
    SMITH SCOTT (Autor:in)

    Erscheinungsdatum :

    09.10.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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