A Simplified Model of Semi-Open Impeller Stage and Analysis of its Effects on the Transient Flow

Article Preview

Abstract:

The centrifugal compressor is one type of vital energy conversion equipment and its unsteady characteristics are extremely complex in actual operation. A semi-open impeller stage with inlet guide vanes, an impeller and a diffuser in a centrifugal compressor was concerned. For simulation of unsteady flow, the full-passage model of the integrate stage requires much more simulating time and memory space, higher computer configuration. Therefore, a single-passage simplified model was established for unsteady analysis. The internal flow characteristics and aerodynamic load on the blade obtained by the simplified model were also compared with that by the full-passage model. The result shows that the precision of the simplified model can meet the engineering requirement. Compared with the full-passage model, the simplified model can give a relatively true reflection of the local flow characteristics and the aerodynamic load on blade surfaces, but it ignores the unevenness resulted from unsteadiness along circumferential direction. Only high-frequency information is retained in aerodynamic load analysis while low-frequency one is diluted. However, as far as the local flow pattern or high-frequency information resulted from unsteady effects is concerned, the simplified model provides the advantages of higher computational efficiency and lower hardware requirements.

You might also be interested in these eBooks

Info:

Periodical:

Pages:

82-86

Citation:

Online since:

December 2014

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2015 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

* - Corresponding Author

[1] Ni RH. A Multiple Grid Scheme for Solving the Euler Equations [J]. AIAA Journal, (1982).

Google Scholar

[2] Wang Yonghong. Research on numerical methods of the three dimensional unsteady flow in turbomachinery and parallel computational algorithms [D]. Nanjing University of Aeronautics and Astronautics, 2007. DOI: 10. 7666/d. d038435.

Google Scholar

[3] Rai M M. Navier-Stokes simulations of rotor-stator interaction using patched and overlaid grids. Journal of Propulsion and Power, 1987; 3: 389-396.

DOI: 10.2514/3.23003

Google Scholar

[4] JClark J P, Stetson G M, Magge S S, et al. the effect of airfoil scaling on the prediction unsteady loading on the blade of a 1 and 1 /2 stage transonic turbine and a comparision with experimental results. Proceedings of the IGTI: ASME Turbo Expo, 2000; 8.

DOI: 10.1115/2000-gt-0446

Google Scholar

[5] WANG Yuan-gang, HUANG Xiu-quan. Investigation into Effects of Blade Count on Unsteady Flows in Turbomachines. [J] Science Technology and Engineering, 2012, 12(10): 1671—1815.

Google Scholar

[6] LI Ya, Huang Xiu-quan, WANG Yuan-gang. Investigation into effects of blade sectors scaling on the aerodynamic loads. [J] Science Technology and Engineering, 2013, 13(11): 1671-1815.

Google Scholar

[7] Xi Guang, Liu Lei, Jiang Hua, et al. Numerical investigation of stator clocking in a centrifugal compressor[J]. Journal of Engineering Thermophysics, 2008, 29(9) 1495-1498.

Google Scholar

[8] Zhou Li, Xi Guang, Cai Yuanhu. Numerical and experimental investigation to unsteady igv-impeller-diffuser interaction [J]. Chinese Journal of applied mechanics, 2008, 25(2) 202-207.

Google Scholar

[9] Xie Rong, Hao Muting, Guan Liang; Miao Weidong; Shi Yanjun. Study on methods of numerical simulation of transient flow in the semi-open impeller stage of a centrifugal compressor. [J] Energy Education Science and Technology Part A: Energy Science and Research, 2014, 32(2) 1085-1092.

Google Scholar