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.
REMOVABLE TURBINE GASPATH SENSOR
CAPTEUR DE TRAJET DE GAZ DE TURBINE AMOVIBLE
09.10.2020
Patent
Elektronische Ressource
Englisch
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