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1st step high pressure turbine bucket wing shape section

机译:第一级高压涡轮叶片翼型截面

摘要

The 1st step bucket (10), X where it states in chart 1, it possesses the wing shape section contour which you follow the Descartes coordinate value of Y and Z substantially, in said chart 1, Z, is vertical vis-a-vis the radius from the turbine centerline and is vertical direction distance from the plane surface which includes X and Y value, as for the said Z value, it is the coordinate which decides the wing shape section contour which X in the aerodynamics section of the radial most inside of the wing shape section, starts from zero inside Y plane surface, in addition X and Y, in each distance Z. X, as for Y and Z value, in order to obtain the wing shape section section for the bucket which it is expanded or is reduced, or, it is possible to be expanded to reduced as an identical constant or a function of numerical value.
机译:第一步铲斗(10)在图1中表示为X,它具有机翼形状截面轮廓,该轮廓基本上遵循Y和Z的笛卡尔坐标值,在上述图表1中,Z相对于垂直所述Z值是距涡轮机中心线的半径,且是距包括X和Y值的平面的垂直方向的距离,该坐标是决定在径向的空气动力学部分中的X最大的机翼形状截面轮廓的坐标。在机翼形状部分的内部,从Y平面内的零开始,再在每个距离Z中从X和Y开始。X的Y和Z值,以获得铲斗的机翼形状部分的截面可以将其扩展或缩小,也可以将其扩展为相同的常数或数值的函数。

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