Is a
Patent attributes
Current Assignee
Patent Jurisdiction
Patent Number
Date of Patent
July 29, 2008
Patent Application Number
11337880
Date Filed
January 21, 2006
Patent Citations Received
Patent Primary Examiner
Patent abstract
An airfoil used in a gas turbine engine exposed to high temperatures, the airfoil having a TBC layer that includes fibers of reinforcing material to add strength to the layer of TBC. The fibers are made from a similar material in which the airfoil is made from to withstand the high temperatures, and have a diameter of about 0.1 mm in order that a thin layer of TBC can completely cover and embed the fibers within the layer.
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