ABSTRACT The nacelle can have an inlet fluidly connecting a main gas path of a gas turbine engine core, the inlet having an inlet edge connecting an external skin to an internal duct wall, and a step formed in a surface of at least one of the skin and the duct wall, the step delimiting a first portion of the surface from a second portion of the surface, the second portion of the surface being recessed relative to the first portion of the surface, the second portion of the surface extending away from both the step and the inlet edge, whereas the first portion of the surface extends between the inlet edge and the step. Date Recue/Date Received 2020-11-13
GAS TURBINE ENGINE, NACELLE THEREOF, AND ASSOCIATED METHOD OF OPERATING A GAS TURBINE ENGINE
TURBINE A GAZ, NACELLE DE CELLE-CI, ET METHODE D`EXPLOITATION ASSOCIEE D`UNE TURBINE A GAZ
2021-05-28
Patent
Elektronische Ressource
Englisch
GAS TURBINE ENGINE, NACELLE THEREOF, AND ASSOCIATED METHOD OF OPERATING A GAS TURBINE ENGINE
Europäisches Patentamt | 2024
|GAS TURBINE ENGINE, NACELLE THEREOF, AND ASSOCIATED METHOD OF OPERATING A GAS TURBINE ENGINE
Europäisches Patentamt | 2021
|