Design and operational behaviour of the rear stages of an industrial axial compressor

被引:0
|
作者
Eisenberg, B
机构
来源
THERMAL TURBOMACHINERY: TURBOCOMPRESSORS IN INDUSTRIAL USE | 1998年 / 1425卷
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D O I
暂无
中图分类号
O42 [声学];
学科分类号
070206 ; 082403 ;
摘要
Due to mass flow adaptations of the downstream process Industrial Axial-flow compressors need wide operating ranges. To meet these requirements a new blading for the rear stages was designed which enabled a large extension of the performance curves between surge and choke line. Measured performance of a 6 stage research compressor having repeating blading showed aspired high efficiencies together with a wide operating range. These improvements are attributed to the optimised design with CD-profiles together with the choice of a high degree of reaction for this application. Calculated performance maps with different guide vane positions show a good agreement of the measured surge-lines with the theoretical performance range of the different profile sections.
引用
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页码:105 / 119
页数:15
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