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AXIAL FLOW TURBINE BLADE CASCADE

机译:轴流透平叶栅

摘要

PROBLEM TO BE SOLVED: To provide a novel blend round in which a cost and performance can be compatible with each other by setting specific dimensionless values R/O of a curvature radius R of the blend round with respect to a blade throat width O in sections between a rear edge of a blade and a throat, the throat and a branch point, and the branch point and a front edge of the blade. ;SOLUTION: A first section A from a rear edge 1a of a blade profile to a throat 4 is formed such that a dimensionless value R/O of a curvature radius R of a blend round with respect to a throat width O is maintained at about 0.4. A second section B from the throat 4 upstream to a branch point 7 at a distance substantially equal to a throat length is formed such that the value R/O is consecutively and linearly varied from about 0.4 to about 0.7. In a third section C from the branch point 7 to a front edge 3a of the blade profile, the entire blend round is formed such that the value R/O is maintained at about 0.7. Consequently, it is possible to enhance performance and enlarge the blend round so as to reduce a machining cost.;COPYRIGHT: (C)1997,JPO
机译:要解决的问题:提供一种新颖的混合轮,其中通过设置混合轮的曲率半径R相对于叶片喉部宽度O的特定无量纲值R / O,可以使成本和性能相互兼容。在叶片的后边缘和喉部之间,喉部和分支点之间以及分支点和叶片的前边缘之间。 ;解决方案:形成从叶片轮廓的后边缘1a到喉部4的第一部分A,以使混合圆的曲率半径R相对于喉部宽度O的无量纲值R / O保持在大约0.4。形成从上游的喉部4到分支点7的第二段B,其距离基本上等于喉部的长度,使得值R / O连续地并且线性地在大约0.4到大约0.7之间变化。在从分支点7到叶片轮廓的前边缘3a的第三部分C中,形成整个混合圆,使得值R / O保持在约0.7。因此,可以提高性能并扩大混合圆度,从而降低加工成本。;版权所有:(C)1997,日本特许厅

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