| Citation: | YANG Chen, TANG Qing, LI Jinguang, et al. Performance analysis of centrifugal compressor based on time-marching one-dimensional method[J]. Journal of Aerospace Power, 2025, 40（9）：20240250 doi: 10.13224/j.cnki.jasp.20240250
|
The one-dimensional method plays an important role in the design and development of centrifugal compressor. A one-dimensional analysis model of centrifugal compressor and corresponding computational program were developed based on the time-marching solving method. To achieve the accurate performance prediction, an inviscid blade force model and a viscous force model were introduced into the one-dimensional governing equations as body-force source terms, to simulate the flow deflection inside the impeller and the viscous effects, respectively. Then, the program was used to analyze both the characteristics of a large-scale centrifugal compressor with low-speed and a high-speed centrifugal compressor, and the predicted results were compared and verified with relevant experimental data or three-dimensional numerical simulations. The results indicated that the model can quickly and accurately evaluate the centrifugal compressors’ performances and the flow parameters distributions inside the impeller passage, which also showed its initial ability to naturally simulate choke condition and its good potential for application in centrifugal compressor performance evaluation during a preliminary design stage.
| [1] |
CAME P M, ROBINSON C J. Centrifugal compressor design[J]. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 1998, 213(2): 139-155. doi: 10.1243/0954406991522239
|
| [2] |
JOLY M, VERSTRAETE T, PANIAGUA G. Full design of a highly loaded fan by multi-objective optimization of through-flow and high-fidelity aero-mechanical performances[C]//Proceedings of ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. Copenhagen, Denmark: ASME, 2013: 2293-2301.
|
| [3] |
JAPIKSE D. Assessment of single-and two-zone modeling of centrifugal compressors, studies in component performance: ASME Paper 85-GT-73 [R]. Houston, US: ASME, 1985.
|
| [4] |
AUNGIER R H. Mean streamline aerodynamic performance analysis of centrifugal compressors[J]. Journal of Turbomachinery, 1995, 117(3): 360-366. doi: 10.1115/1.2835669
|
| [5] |
AUNGIER R H. Centrifugal compressors[M]. New York: ASME Press, 2000.
|
| [6] |
GALVAS M R. Analytical correlation of centrifugal compressor design geometry for maximum efficiency with specific speed[M]. Washington, USA: National Aeronautics and Space Administration, 1972.
|
| [7] |
OH H W, YOON E S, CHUNG M K. An optimum set of loss models for performance prediction of centrifugal compressors[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy, 1997, 211(4): 331-338. doi: 10.1243/0957650971537231
|
| [8] |
COPPAGE J, DALLENBACH F. Study of supersonic radial compressors for refrigeration and pressurization systems: WADC Technical Report 55-257[R]. Ohio, US: Wright Air Development Center, 1956.
|
| [9] |
JOHNSTON J P, DEAN R C Jr. Losses in vaneless diffusers of centrifugal compressors and pumps: analysis, experiment, and design[J]. Journal of Engineering for Power, 1966, 88(1): 49-60. doi: 10.1115/1.3678477
|
| [10] |
JANSEN W. A method for calculating the flow in a centrifugal impeller when entropy gradient are present[C]// Royal Society Conference on Internal Aerodynamics (Turbomachinery). Cambridge, UK: The Royal Society, 1967: 133-146.
|
| [11] |
QIU Xuwen, MALLIKARACHCHI C, ANDERSON M. A new slip factor model for axial and radial impellers[C]//Proceedings of ASME Turbo Expo 2007. Montreal, Canada: ASME, 2007: 957-966.
|
| [12] |
CICCIOTTI M, MARTINEZ-BOTAS R F, ROMAGNOLI A, et al. Systematic one zone meanline modelling of centrifugal compressors for industrial online applications: ASME Paper GT2013-95821 [R] San Antonio, US: ASME, 2013.
|
| [13] |
YANG Mingyang, ZHENG Xinqian, ZHANG Yangjun, et al. Improved performance model of turbocharger centrifugal compressor[C]// Proceedings of ASME Turbo Expo: Power for Land, Sea, and Air. Berlin, Germany: ASME, 2008: 1439-1445.
|
| [14] |
张超炜, 董学智, 刘锡阳, 等. 改进的离心压气机滑移因子模型[J]. 航空动力学报, 2018, 33(9): 2178-2187. ZHANG Chaowei, DONG Xuezhi, LIU Xiyang, et al. Improved slip factor model for centrifugal compressor[J]. Journal of Aerospace Power, 2018, 33(9): 2178-2187. (in Chinese
ZHANG Chaowei, DONG Xuezhi, LIU Xiyang, et al. Improved slip factor model for centrifugal compressor[J]. Journal of Aerospace Power, 2018, 33(9): 2178-2187. (in Chinese)
|
| [15] |
ZHANG Chaowei, DONG Xuezhi, LIU Xiyang, et al. A method to select loss correlations for centrifugal compressor performance prediction[J]. Aerospace Science and Technology, 2019, 93: 105335. doi: 10.1016/j.ast.2019.105335
|
| [16] |
SHAO Wenyang, DU Juan, YANG Jinguang, et al. Investigation on one-dimensional loss models for predicting performance of multistage centrifugal compressors in supercritical CO2 Brayton cycle[J]. Journal of Thermal Science, 2021, 30(1): 133-148. doi: 10.1007/s11630-020-1242-1
|
| [17] |
LÉONARD O, ADAM O. A quasi-one-dimensional CFD model for multistage turbomachines[J]. Journal of Thermal Science, 2008, 17(1): 7-20. doi: 10.1007/s11630-008-0007-z
|
| [18] |
张烔, 杨晨, 吴虎, 等. 基于时间推进的轴流压气机准二维性能分析[J]. 西北工业大学学报, 2020, 38(1): 114-120. ZHANG Tong, YANG Chen, WU Hu, et al. Quasi-2D performance analysis for axial compressors based on time-marching method[J]. Journal of Northwestern Polytechnical University, 2020, 38(1): 114-120. (in Chinese doi: 10.3969/j.issn.1000-2758.2020.01.014
ZHANG Tong, YANG Chen, WU Hu, et al. Quasi-2D performance analysis for axial compressors based on time-marching method[J]. Journal of Northwestern Polytechnical University, 2020, 38(1): 114-120. (in Chinese) doi: 10.3969/j.issn.1000-2758.2020.01.014
|
| [19] |
杨晨. 燃气轮机整机通流模型及其模拟技术研究[D]. 西安: 西北工业大学, 2020. YANG Chen. Study on flow model and simulation technology of gas turbine[D]. Xi’an: Northwestern Polytechnical University, 2020. (in Chinese
YANG Chen. Study on flow model and simulation technology of gas turbine[D]. Xi’an: Northwestern Polytechnical University, 2020. (in Chinese)
|
| [20] |
DU Wenhai, LI Yucheng, LI Longfei, et al. A quasi-one-dimensional model for the centrifugal compressor’s performance simulations[J]. International Journal of Heat and Technology, 2018, 36(2): 391-396. doi: 10.18280/ijht.360202
|
| [21] |
YANG Chen, WU Hu, YANG Jinguang, et al. Time-marching throughflow analysis of multistage axial compressors based on a novel inviscid blade force model[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(14): 5239-5252. doi: 10.1177/0954410019840588
|
| [22] |
HIRSCH C, WARZEE G. A finite-element method for through flow calculations in turbomachines[J]. Journal of Fluids Engineering, 1976, 98(3): 403-414. doi: 10.1115/1.3448341
|
| [23] |
CETIN M, UECER A, HIRSCH C, et al. Application of modified loss and deviation correlations to transonic axial compressors: AGARD-R-745[R]. Paris, France: Advisory Group for Aerospace Research and Development Publications, 1987.
|
| [24] |
YANG Chen, DU Juan, ZHANG Hongwu, et al. Time-marching throughflow analysis of centrifugal compressors with boundary conditions based on Newton’s method[J]. Applied Sciences, 2022, 12(13): 6576. doi: 10.3390/app12136576
|
| [25] |
DAILY J W, NECE R E. Chamber dimension effects on induced flow and frictional resistance of enclosed rotating disks[J]. Journal of Basic Engineering, 1960, 82(1): 217-230. doi: 10.1115/1.3662532
|
| [26] |
HATHAWAY M D, CHRISS R M, STRAZISAR A J, et al. Laser anemometer measurements of the three-dimensional rotor flow field in the NASA low-speed centrifugal compressor: NASA-TP-3527[R]. Cleveland, US: NASA, 1995.
|
| [27] |
SKOCH G J, PRAHST P S, WERNET M P, et al. Laser anemometer measurements of the flow field in a 4∶1 pressure ratio centrifugal impeller: ASME Paper 97-GT-342 [R]. Cleveland, US: ASME, 1997.
|
DownLoad:
