“凹槽导流片式”机匣处理的结构尺寸优化研究

推进技术 ›› 1998, Vol. 19 ›› Issue (1): 71-75.

“凹槽导流片式”机匣处理的结构尺寸优化研究

杜辉,朱俊强,楚武利,刘志伟

西北工业大学航空动力与热力工程系;西北工业大学航空动力与热力工程系;西北工业大学航空动力与热力工程系;西北工业大学航空动力与热力工程系

发布日期:2021-08-15

OPTIMIZATION OF STRUCTURAL PARAMETERS OF RECESS VANED CASING TREATMENT

Dept.of Aeroengine Engineering,Northwestern Polytechnical Univ ,Xi′an,710072;Dept.of Aeroengine Engineering,Northwestern Polytechnical Univ ,Xi′an,710072;Dept.of Aeroengine Engineering,Northwestern Polytechnical Univ ,Xi′an,710072;Dept.of Aeroengine Engineering,Northwestern Polytechnical Univ ,Xi′an,710072

Published:2021-08-15

摘要/Abstract

摘要： 针对一种可提高压气机裕度而又不牺牲效率的新型处理机匣，进行了较为系统的几何尺寸优化研究。借助单级轴流压气机实验台，详细地研究了轴向叠合量、容腔尺寸及内置导流片数目对压气机性能的影响，归纳出若干该型处理机匣的设计准则，具有工程实用价值。

关键词: 轴流式压缩机;机匣;最佳结构设计;参数最优化

Abstract: An experimental investigations have been carried out in the influence of structural parameters of recess vaned casing treatment on the efficiency and the stall margin of an axial flow rotor.Tests were conducted under the condition of different axial positions,number of vanes and different length of the casing treatment to define the optimum position.In each case,the characteristics with casing treatment were compared to that with solidwall.The increases of operating efficiency in the flow without drops were observed.The results can be used as a guide for the selection of configurations in the casing treatment design

Key words: Axial flow compressor;Casing +;Optimum structural design;Parameter optimization

杜辉,朱俊强,楚武利,刘志伟. “凹槽导流片式”机匣处理的结构尺寸优化研究[J]. 推进技术, 1998, 19(1): 71-75.