Is a
Patent attributes
Current Assignee
Patent Jurisdiction
Patent Number
Date of Patent
January 5, 2016
Patent Application Number
13556496
Date Filed
July 24, 2012
Patent Citations Received
Patent Primary Examiner
Patent abstract
A gas turbine engine comprises a fan section including a fan hub supporting a plurality of fan blades for rotation relative to a fan case, a shaft rotatable relative to the fan case about an engine center axis, and a geared architecture driven by the shaft to provide driving output to rotate the fan hub. A compressor is positioned forward of the geared architecture and radially inward of the fan blades, with the compressor being driven by the shaft.
Timeline
No Timeline data yet.
Further Resources
No Further Resources data yet.
