发明名称 HIGH MODULUS METALLIC COMPONENT FOR HIGH VIBRATORY OPERATION
摘要 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.
申请公布号 KR20060041969(A) 申请公布日期 2006.05.12
申请号 KR20050012517 申请日期 2005.02.16
申请人 UNITED TECHNOLOGIES CORP. 发明人 SHAH DILIP M.;CETEL ALAN D.;STONER ALAN W.;ALLEN WILLIAM P.
分类号 F01D5/28;C22C19/05;F01D5/12;F01D25/00;F02C7/00 主分类号 F01D5/28
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