A gas turbine engine according to an exemplary embodiment of this disclosure includes, among other possible things, a fan including a plurality of fan blades rotatable about an axis, a plurality of inlet guide vanes mounted forward of the plurality of fan blades, the plurality of inlet guide vanes selectively rotatable about the axis independent of the plurality of fan blades; and a motor for controlling rotation of the plurality of inlet guide vanes about the axis.
Turbofan with motorized rotating inlet guide vane
2020-08-11
Patent
Electronic Resource
English
The Use of Cyclic Outlet Guide Vane in Turbofan
British Library Conference Proceedings | 1999
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