Computational investigation of impeller-diffuser interaction in a centrifugal compressor with different types of diffusers

被引:25
作者
Anish, S. [1 ]
Sitaram, N. [1 ]
机构
[1] Indian Inst Technol, Dept Mech Engn, Thermal Turbomachines Lab, Madras 600036, Tamil Nadu, India
关键词
centrifugal compressor; stage performance; diffuser; computational simulation; VANED DIFFUSERS; FLOW-ANALYSIS; PERFORMANCE; STAGE;
D O I
10.1243/09576509JPE662
中图分类号
O414.1 [热力学];
学科分类号
摘要
A computational study has been conducted to analyse the performance of a centrifugal compressor with different types of diffusers under various levels of impeller-diffuser interactions. Vaneless (VLD), vaned (VD), low solidity vaned (LSVD), and partial vaned diffusers (PVD) are used for this purpose. The study is carried out using commercial software ANSYS CFX. The interaction level is varied by varying the radial gap between the impeller and diffuser by keeping the diffuser vane at three different radial locations. Numerical simulations have been conducted for four different flow coefficients. At design flow coefficient maximum efficiency occurs when the leading edge is at R(3) (ratio of radius of the diffuser leading edge to the impeller tip radius) = 1.10 for all vane-type diffuser configurations. At below design flow coefficient higher stage efficiency occurs when the diffuser vanes are kept far away (R(3) = 1.15) and at above design flow coefficient R(3) = 1.05 gives better efficiency. The highest diffuser pressure recovery coefficient (C(p)) is observed :For VD at design flow coefficient. For VLD, the C(p) value increases with flow coefficient. In the case of VD and LSVD configurations the exit flow from the impeller is disturbed when the diffuser vanes are closer, and these disturbances are more evident in the last 10 per cent of the impeller flow. In the case of the impeller with PVD the interaction effects are minimum.
引用
收藏
页码:167 / 178
页数:12
相关论文
共 16 条
[1]   Impeller-diffuser interaction in centrifugal compressors: Numerical analysis of Raidver test case [J].
Boncinelli, P. ;
Ermini, M. ;
Bartolacci, S. ;
Arnone, A. .
JOURNAL OF PROPULSION AND POWER, 2007, 23 (06) :1304-1312
[2]   A SIMULATION OF THE UNSTEADY INTERACTION OF A CENTRIFUGAL IMPELLER WITH ITS VANED DIFFUSER - FLOW-ANALYSIS [J].
DAWES, WN .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1995, 117 (02) :213-222
[3]   The design and performance results of simple flat plate low solidity vaned diffusers [J].
Engeda, A .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2001, 215 (A1) :109-118
[4]   EXPERIMENTAL-STUDY OF CENTRIFUGAL IMPELLER DISCHARGE FLOW IN VANELESS AND VANED DIFFUSERS [J].
INOUE, M ;
CUMPSTY, NA .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 1984, 106 (02) :455-467
[5]  
Issac J. M., 2004, THESIS IIT MADRAS
[6]   Effect of diffuser vane height and position on the performance of a centrifugal compressor [J].
Issac, JM ;
Sitara, N ;
Govardhan, M .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2004, 218 (A8) :647-654
[7]   A centrifugal compressor stage with wide flow range vaned diffusers and different inlet configurations [J].
Kim, Y ;
Engeda, A ;
Aungier, R ;
Amineni, N .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2002, 216 (A4) :307-320
[8]   DETERMINISTIC BLADE ROW INTERACTIONS IN A CENTRIFUGAL-COMPRESSOR STAGE [J].
KIRTLEY, KR ;
BEACH, TA .
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1992, 114 (02) :304-311
[9]   Computational studies of unsteady flows in a centrifugal compressor stage [J].
Koumoutsos, A ;
Tourlidakis, A ;
Elder, RL .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2000, 214 (A6) :611-633
[10]   Effect of the setting angle of a low-solidity vaned diffuser on the performance of a centrifugal compressor stage [J].
Reddy, TCS ;
Murty, GVR ;
Mukkavilli, P ;
Reddy, DN .
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2004, 218 (A8) :637-646