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 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