Is a
Patent attributes
Current Assignee
Patent Jurisdiction
Patent Number
Date of Patent
April 7, 2015
Patent Application Number
12915208
Date Filed
October 29, 2010
Patent Citations Received
Patent Primary Examiner
Patent abstract
A bypass gas turbine engine includes a variable area fan nozzle with a second fan nacelle section axially movable relative to a first fan nacelle section to define an auxiliary port to vary a fan nozzle exit area and adjust fan bypass airflow. The second fan nacelle section includes a leading edge region that defines a concave external contour and the first fan nacelle section includes a trailing edge region that defines a convex internal contour.
Timeline
No Timeline data yet.
Further Resources
No Further Resources data yet.
