The holed casing treatment is a new type of casing treatment that has self-adaptability for a centrifugal compressor with unshrouded impeller. It was demonstrated experimentally and numerically that both the stall margin and the choked margin of the compressor were able to be expanded by the treatment. Numerical results indicate that there is reinjected flow in the holes when the compressor works at low flow rate conditions, and bypass flow at high flow rate conditions. The key principles for choosing the diameter and the radial position of the hole are presented in this paper. The hole’s diameter is an important parameter for the holed casing treatment. Five numerical cases with different diameters (1.0 mm, 1.5 mm, 2.0 mm, 2.5 mm and 3.0 mm) were carried out to compare the results. The reinjected flow enters into the impeller passage periodically and it tends to increase when the hole diameter gets larger. In the case of 2.5 mm, both the stall margin increment and the efficiency of the compressor were the highest among the five cases. Unsteady simulations suggest that the reinjected flow is not only periodic in time but also periodic in circumferential direction. This is the reason why only 2% of the flow amounts would get 20% of the working range expansion.
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e-mail: xuwei102@sjtu.edu.cn
e-mail: twang@sjtu.edu.cn
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April 2012
Technical Briefs
Numerical Investigation of a Centrifugal Compressor With Holed Casing Treatment
Wei Xu,
Wei Xu
Key Laboratory for Power Machinery and Engineering of Ministry of Education,
e-mail: xuwei102@sjtu.edu.cn
Shanghai Jiao Tong University
, Shanghai 200240, China
Search for other works by this author on:
Tong Wang,
Tong Wang
Key Laboratory for Power Machinery and Engineering of Ministry of Education,
e-mail: twang@sjtu.edu.cn
Shanghai Jiao Tong University
, Shanghai 200240, China
Search for other works by this author on:
Chuangang Gu,
Chuangang Gu
Key Laboratory for Power Machinery and Engineering of Ministry of Education,
e-mail: cggu@126.com
Shanghai Jiao Tong University
, Shanghai 200240, China
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Liang Ding
Liang Ding
Key Laboratory for Power Machinery and Engineering of Ministry of Education,
e-mail: 5010219021@sjtu.edu.cn
Shanghai Jiao Tong University
, Shanghai 200240, China
Search for other works by this author on:
Wei Xu
Key Laboratory for Power Machinery and Engineering of Ministry of Education,
Shanghai Jiao Tong University
, Shanghai 200240, China
e-mail: xuwei102@sjtu.edu.cn
Tong Wang
Key Laboratory for Power Machinery and Engineering of Ministry of Education,
Shanghai Jiao Tong University
, Shanghai 200240, China
e-mail: twang@sjtu.edu.cn
Chuangang Gu
Key Laboratory for Power Machinery and Engineering of Ministry of Education,
Shanghai Jiao Tong University
, Shanghai 200240, China
e-mail: cggu@126.com
Liang Ding
Key Laboratory for Power Machinery and Engineering of Ministry of Education,
Shanghai Jiao Tong University
, Shanghai 200240, China
e-mail: 5010219021@sjtu.edu.cn
J. Eng. Gas Turbines Power. Apr 2012, 134(4): 044502 (4 pages)
Published Online: January 25, 2012
Article history
Revised:
May 12, 2011
Received:
May 12, 2011
Online:
January 25, 2012
Published:
January 25, 2012
Citation
Xu, W., Wang, T., Gu, C., and Ding, L. (January 25, 2012). "Numerical Investigation of a Centrifugal Compressor With Holed Casing Treatment." ASME. J. Eng. Gas Turbines Power. April 2012; 134(4): 044502. https://doi.org/10.1115/1.4004444
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