Is a
Patent attributes
Patent Jurisdiction
Patent Number
Date of Patent
May 26, 2015
Patent Application Number
13306413
Date Filed
November 29, 2011
Patent Citations Received
Patent Primary Examiner
Patent abstract
A blade of a gas turbine engine is provided having an airfoil, a platform, a shank, a dovetail, and a skirt. The airfoil may extend distally from the platform, and the shank may extend proximally from the platform. The dovetail may also be provided to extend proximally from the shank. The skirt may be disposed on an aft side of the shank and may extend from the shank in a direction at least partially axially aft from the shank.
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