发明名称 |
AIRFOIL SHAPE FOR A TURBINE BUCKET |
摘要 |
Fourth stage turbine buckets 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 values are non-dimensional values from 0 to 1 convertible to Z distances in inches by multiplying the Z values by the height of the airfoil in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete airfoil shape. 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 ±0.150 inches in directions normal to the surface of the airfoil.
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申请公布号 |
US2005013695(A1) |
申请公布日期 |
2005.01.20 |
申请号 |
US20030621460 |
申请日期 |
2003.07.18 |
申请人 |
HYDE SUSAN MARIE;BY ROBERT ROMANY;SCHAEFFER JON CONRAD;SIMS CALVIN LEVY;BOISCLAIR MICHAEL ERNEST |
发明人 |
HYDE SUSAN MARIE;BY ROBERT ROMANY;SCHAEFFER JON CONRAD;SIMS CALVIN LEVY;BOISCLAIR MICHAEL ERNEST |
分类号 |
F01D5/18;F01D5/00;F01D5/14;(IPC1-7):B63H1/26 |
主分类号 |
F01D5/18 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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