An aircraft engine, comprising a thermal engine, an axial turbine having a turbine inlet, and an exhaust assembly fluidly connecting the thermal engine to the axial turbine. The exhaust assembly includes a housing and a deflector removably mounted within the housing. The deflector has circumferentially distributed vanes. The deflector is a first deflector, having a first set of geometric characteristics, that is removable from the housing and replaceable by a second deflector having a second set of geometric characteristics different from the first set of geometric characteristics. The first deflector is one of a first class of deflectors and the second deflector is one of a second class of deflectors, the first and second class of deflectors respectively defining first and second exhaust flow profiles that differ from each other.
AIRCRAFT ENGINE WITH EXHAUST HAVING REOVABLE DEFLECTOR
MOTEUR D'AERONEF COMPRENANT UN ECHAPPEMENT A DEFLECTEUR AMOVIBLE
2024-06-01
Patent
Elektronische Ressource
Englisch
AIRCRAFT ENGINE WITH EXHAUST HAVING REMOVABLE DEFLECTOR
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