发明名称 Airfoil shape of a second stage turbine blade
摘要 <p>The second stage buckets (22) have airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and Z set forth Table I wherein X and Y values are in inches and the Z value is non-dimensional along the bucket centerline coincident with a turbine radius and convertible to a Z distance in inches from the turbine axis by multiplying the Z value by the height of the airfoil and adding the root radius to the result. The X and Y distances may be scalable as a function of the same constant or number to provide a scaled up or scaled down airfoil section for the bucket. The nominal airfoil given by the X, Y and Z distances lies within an envelop of ± 0.160 inches.</p>
申请公布号 EP1400656(A2) 申请公布日期 2004.03.24
申请号 EP20030255774 申请日期 2003.09.16
申请人 GENERAL ELECTRIC COMPANY 发明人 HUMANCHUK, DAVID JOHN;BIELEK, CRAIG ALLEN;BRITTINGHAM, ROBERT ALAN;BALKCUM, JAMES TYSON;JONES, JR., ANDREW
分类号 F01D5/14;(IPC1-7):F01D5/14 主分类号 F01D5/14
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