Stall Inception Process and Prospects for Active Hub-Flap Control in Three-Stage Axial Flow Compressor

被引：1

作者：

Okada, Tomoya ^{[1
]}

Kawajiri, Atsushi ^{[1
]}

Ohta, Yutaka ^{[2
]}

Outa, Eisuke ^{[2
]}

机构：

[1] Waseda Univ, Grad Sch Sci & Engn, Shinjuku Ku, Tokyo 1698555, Japan

[2] Waseda Univ, Dept Appl Mech & Aerosp Engn, Shinjuku Ku, Tokyo 1698555, Japan

来源：

JOURNAL OF THERMAL SCIENCE | 2008年 / 17卷 / 04期

关键词：

axial flow compressor; rotating stall; active stall control; stall inception; stall precursor;

D O I：

10.1007/s11630-008-0324-2

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

The possibility to apply the active hub-flap control method, which is a proven rotating stall control method for a single-stage compressor, to a 3-stage axial compressor is experimentally discussed, where complex rotating stall inception processes are observed. The research compressor is a 3-stage one and could change the stagger angle settings for rotor blades and stator vanes. Sixteen rotor blade/stator vane configuration patterns were tested by changing stagger angle for the stator vanes. By measurement of surface-pressure fluctuation, stall inception processes are investigated and the measured pressure fluctuation data is used as a predictive signal for rotating stall. The experimental results show that the stall detection system applied to active hub-flap control in a single-stage compressor could be usefully applied to that in a 3-stage compressor with a more complex stall inception process.

引用

页码：324 / 330

页数：7