Is a
Patent attributes
Current Assignee
Patent Jurisdiction
Patent Number
Patent Inventor Names
William P. Allen0
Alan W. Stoner0
Dilip M. Shah0
Alan D. Cetel0
Date of Patent
January 18, 2011
0Patent Application Number
118403300
Date Filed
August 17, 2007
0Patent Citations Received
Patent Primary Examiner
Patent abstract
A high modulus component, such as an aircraft engine turbine blade, is formed from a base metal that has a high modulus crystallographic orientation that is aligned with the primary, i.e. radial, direction of the turbine blade. The base metal is Ni, Fe, Ti, Co, Al, Nb, or Mo based alloy. Alignment of a high modulus direction of the base metal with the primary direction provides enhanced high cycle fatigue life.
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