一种离心式压缩机回流器的改进

本文探讨对一种双级离心压缩机中回流器叶片型线的设计改进,采用机翼形状叶片型线替代等厚度叶片型线,并通过压缩机的性能测试验证该方案的可行性。

This article probes into the program that airfoil vane replaces equal thickness vane in the centrifugal compressor return channel. Performance test of the centrifugal compressor make sure the design program