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Rotor blade row of axial flow turbine, and axial flow turbine

机译:轴流涡轮的转子叶片排以及轴流涡轮

摘要

PROBLEM TO BE SOLVED: To provide a rotor blade row of an axial-flow turbine capable of reducing blade profile loss by matching a geometric blade inlet angle and a working fluid inflow angle while taking change in a radial direction, of an inflow angle near an end wall portion, into consideration, and simultaneously reducing secondary flow loss by reducing interference of secondary flow and a blade negative pressure face generated between blades, in the axial-flow turbine.;SOLUTION: A rotor blade row of an axial-flow turbine composed of a plurality of turbine rotor blades annularly arranged, has an auxiliary blade 3 disposed on at least one of an inner peripheral-side wall surface or an outer peripheral-side wall surface in a turbine radial direction of a flow channel formed between blades of the rotor blade row, having a blade inlet angle smaller than a blade inlet angle of the turbine rotor blade, having a blade outlet angle smaller than a blade outlet angle of the turbine rotor blade, and further having a blade front edge positioned at an upstream side in a working fluid flowing direction with respect to a blade front edge of the turbine rotor blade.;COPYRIGHT: (C)2014,JPO&INPIT
机译:要解决的问题:提供一种轴流式涡轮机的转子叶片排,该叶片排能够通过使几何形状的叶片进口角和工作流体的流入角匹配,同时在径向上改变流入角接近轴流式涡轮机的转子叶片排,考虑到这一点,并通过减少二次流和叶片之间产生的叶片负压面的干扰来同时减少二次流损失。环状地配置的多个涡轮动叶片中的一个具有在形成于该动叶片的叶片之间的流路的涡轮径向上的内周侧壁面或外周侧壁面的至少一方上配置的辅助叶片3。转子叶片行,其叶片入口角小于涡轮转子叶片的叶片入口角,叶片出口角小于涡轮叶片的叶片出口角;并且还具有叶片前缘,该叶片前缘相对于涡轮转子叶片的叶片前缘位于工作流体流动方向的上游侧。; COPYRIGHT:(C)2014,JPO&INPIT

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