ラジアルタービンに関する実験的研究 : 中間翼の効果

概要

論文の詳細を見る
Experiments were conducted to find out the influence of intermediate blades within the impeller channel on the performance characteristics of a radial turbine. In the first experiments, one or two intermediate blades were installed within each impeller channel respectively, and the influence of the number of intermediate blades upon the performance was examined. The results indicate that the installation of intermediate blades improves the performance considerably. The second experiments concern with the investigation of the effect of the length of the intermediate blade upon the performance for the case of a single intermediate blade in each blade channel. The most favorable length of the intermediate blade obtained from the experiments is about 0.4 or 0.5 times as long as the whole blade length.
一般社団法人日本機械学会の論文
1964-02-25