叶轮
离心式压缩机
气体压缩机
纬向和经向
总压比
转速
刀(考古)
轴流压缩机
机械工程
机械
材料科学
计算机科学
地质学
物理
工程类
大气科学
作者
C. Xu,Ryoichi S. Amano
摘要
Centrifugal compressor developments are interested in using optimization procedures that enable compressor high efficiency and wide operating ranges. Recently, high pressure ratio and efficiency of the centrifugal compressors require impeller design to pay attention to both the blade angle distribution and the meridional profile. The geometry of the blades and the meridional profile are very important contributions of compressor performance and structure reliability. This paper presents some recent studies of meridional impacts of the compressor. Studies indicated that the meridional profiles of the impeller impact the overall compressor efficiency and pressure ratio at the same rotational speed. Proper meridional profiles can improve the compressor efficiency and increase the overall pressure ratio at the same blade back curvature.
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