A gas turbine engine has a fan inlet and a fan configured to deliver air to an exhaust nozzle. A core gas turbine engine. including in serial order extending further into the engine, a core turbine section, a combustor and a core compressor section. A core engine inlet duct is spaced from the fan inlet. A method is also described.
Reverse core turbine engine mounted above aircraft wing
12.02.2019
Patent
Elektronische Ressource
Englisch
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