07338259 is referenced by 9 patents and cites 24 patents.

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.

Application Number
10/791421
Publication Number
7338259 (B2)
Application Date
March 2, 2004
Publication Date
March 4, 2008
Inventor
William P Allen
Plainfield
IL, US
Alan W Stoner
Tullahoma
TN, US
Alan D Cetel
West Hartford
CT, US
Dilip M Shah
Glastonbury
CT, US
Agent
Carlson Gaskey & Olds
Assignee
United Technologies Corporation
CT, US
IPC
C22C 19/05
F01D 5/14
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