发明名称 |
TURBINE BUCKET PROFILE YIELDING IMPROVED THROAT |
摘要 |
Turbine frequency tuning, fluid dynamic efficiency, and performance can be improved using a particular airfoil profile, which can be used to determine a throat between adjacent airfoils. By shaping the throat according to the particular profile, the total pressure at an endwall can be energized, improving performance of the turbine. |
申请公布号 |
US2015107266(A1) |
申请公布日期 |
2015.04.23 |
申请号 |
US201314061146 |
申请日期 |
2013.10.23 |
申请人 |
General Electric Company |
发明人 |
Gustafson Ross James;Jayana Srinivasa Govardhan;Kareff Spencer Aaron;Nanda Dipesh Dinesh |
分类号 |
F01D5/02 |
主分类号 |
F01D5/02 |
代理机构 |
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代理人 |
|
主权项 |
1. In a turbomachine including a row of substantially identical buckets circumferentially mounted on a rotor, each bucket including a respective airfoil with opposed pressure and suction sidewalls extending chordwise between opposed leading and trailing edges and spanwise between a root and a tip, a flow passage between each pair of airfoils, each flow passage comprising:
a pressure sidewall of a first airfoil; a suction sidewall of a second airfoil substantially facing the pressure sidewall of the first airfoil; and a throat including an area defined at least in part by a minimum gap between the pressure sidewall of the first airfoil and the suction sidewall of the second airfoil for each corresponding chord along spans of the first and second airfoils, a width of the throat at at least one of the tips or the roots of the airfoils being no more than about 15% more than a width of the throat at a respective first or second distance from the at least one of the tips or the roots. |
地址 |
Schenectady NY US |