An apparatus and method for mounting a turbine engine to an aircraft can include an engine core for the turbine engine including a compressor section, a combustor section, and a turbine section in flow arrangement. At least one strut couples to the engine core about a single mount plane. A structural wall at least partially defining a mainstream flow path couples to the at least one strut and passes through the compressor section and the turbine section.
TURBINE ENGINE WITH SINGLE WALL CANTILEVERED ARCHITECTURE
MOTEUR DE TURBINE A ARCHITECTURE EN PORTE-A-FAUX A PAROI SIMPLE
2019-02-22
Patent
Elektronische Ressource
Englisch
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