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TURBINE BLADE, TURBINE, AND METHOD OF TUNING NATURAL FREQUENCY OF TURBINE BLADE

机译:涡轮叶片,涡轮机和调谐涡轮叶片固有频率的方法

摘要

A turbine blade includes: a platform; an airfoil portion extending from the platform in a blade height direction and having a pressure surface and a suction surface extending between a leading edge and a trailing edge; a blade root portion positioned opposite to the airfoil portion across the platform in the blade height direction and having a bearing surface; and a shank positioned between the platform and the blade root portion. The shank has a cross-section which is perpendicular to the blade height direction of the airfoil portion, and in which a line segment connecting a widthwise center position of a leading-edge-side end portion of the shank and a widthwise center position of a trailing-edge-side end portion of the shank is sloped to a center line between a pressure-surface-side contour of the blade root portion and a suction-surface-side contour of the blade root portion.
机译:涡轮叶片包括:平台;翼型部分从平台沿叶片高度方向延伸并具有压力表面和在前缘和后缘之间延伸的抽吸表面;叶片根部与叶片高度方向的平台相对地定位在平台上并具有轴承表面;和位于平台和刀片根部之间的柄部位。柄部具有横截面,该横截面垂直于翼型部分的叶片高度方向,并且其中连接柄部的前缘侧端部的宽度方向位置的线段和宽度方向位置柄部的后缘侧端部倾斜到叶片根部的压力表面侧轮廓和叶片根部的吸入表面侧轮廓之间的中心线。

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