A gas turbine engine exhaust system comprises an instrumented exhaust duct including a set of exhaust temperature probes installed at the exhaust end of the duct in an air space between the engine outer case and a surrounding engine nacelle. A shield is removably installed at the end of the exhaust duct to protect the probes and associated wiring in the air space.
INSTRUMENTED TURBINE EXHAUST DUCT
CONDUIT D'EVACUATION DE TURBINE PAR INSTRUMENT
2022-08-18
Patent
Elektronische Ressource
Englisch
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