A turbofan engine defining a circumferential direction is provided. The turbofan engine includes a turbomachine; an unducted rotor assembly drivingly coupled to the turbomachine, the unducted rotor assembly including a plurality of unducted rotor blades; and a plurality of outlet guide vanes positioned downstream of the plurality of unducted rotor blades, the plurality of outlet guide vanes each defining a span, the spans of the plurality of outlet guide vanes being nonuniform along the circumferential direction.
OUTLET GUIDE VANE ASSEMBLY FOR A TURBOFAN ENGINE
2024-06-27
Patent
Electronic Resource
English
The Use of Cyclic Outlet Guide Vane in Turbofan
British Library Conference Proceedings | 1999
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