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Fluid-structure Interaction Analysis and Lifetime Estimation of a Natural Gas Pipeline Centrifugal Compressor under Near-choke and Near-surge Conditions 被引量:12

Fluid-structure Interaction Analysis and Lifetime Estimation of a Natural Gas Pipeline Centrifugal Compressor under Near-choke and Near-surge Conditions
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摘要 Up to present, there have been no studies concerning the application of fluid-structure interaction(FSI) analysis to the lifetime estimation of multi-stage centrifugal compressors under dangerous unsteady aerodynamic excitations. In this paper, computational fluid dynamics(CFD) simulations of a three-stage natural gas pipeline centrifugal compressor are performed under near-choke and near-surge conditions, and the unsteady aerodynamic pressure acting on impeller blades are obtained. Then computational structural dynamics(CSD) analysis is conducted through a one-way coupling FSI model to predict alternating stresses in impeller blades. Finally, the compressor lifetime is estimated using the nominal stress approach. The FSI results show that the impellers of latter stages suffer larger fluctuation stresses but smaller mean stresses than those at preceding stages under near-choke and near-surge conditions. The most dangerous position in the compressor is found to be located near the leading edge of the last-stage impeller blade. Compressor lifetime estimation shows that the investigated compressor can run up to 102.7 h under the near-choke condition and 200.2 h under the near-surge condition. This study is expected to provide a scientific guidance for the operation safety of natural gas pipeline centrifugal compressors. Up to present, there have been no studies concerning the application of fluid-structure interaction(FSI) analysis to the lifetime estimation of multi-stage centrifugal compressors under dangerous unsteady aerodynamic excitations. In this paper, computational fluid dynamics(CFD) simulations of a three-stage natural gas pipeline centrifugal compressor are performed under near-choke and near-surge conditions, and the unsteady aerodynamic pressure acting on impeller blades are obtained. Then computational structural dynamics(CSD) analysis is conducted through a one-way coupling FSI model to predict alternating stresses in impeller blades. Finally, the compressor lifetime is estimated using the nominal stress approach. The FSI results show that the impellers of latter stages suffer larger fluctuation stresses but smaller mean stresses than those at preceding stages under near-choke and near-surge conditions. The most dangerous position in the compressor is found to be located near the leading edge of the last-stage impeller blade. Compressor lifetime estimation shows that the investigated compressor can run up to 102.7 h under the near-choke condition and 200.2 h under the near-surge condition. This study is expected to provide a scientific guidance for the operation safety of natural gas pipeline centrifugal compressors.
出处 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2015年第6期1261-1268,共8页 中国机械工程学报(英文版)
基金 Supported by National Natural Science Foundation of China(Grant No51406148) National Science Technology Support Program of China(Grant No.2012BAA08B06) Postdoctoral Science Foundation o China(Grant No.2014M552444)
关键词 three-stage pipeline centrifugal compressor natural gas aerodynamic performance structural durability lifetime estimation choke surge three-stage pipeline centrifugal compressor,natural gas,aerodynamic performance,structural durability,lifetime estimation,choke,surge
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参考文献20

  • 1BURKLIN C E, HEANEY M. Natural gas compressor engine survey for gas production and processing facilities[R]. H68 Final Report. Eastern Research Group, Inc., Morrisville, North Carolina, 2006.
  • 2BOUSQUET Y, CARBONNEAU X, DUFOUR G, et al. Analysis of the unsteady flow field in a centrifugal compressor from peak efficiency to near stall with full-annulus simulations[J]. International Journal of rotating machinery, 2014 (2014): Article ID 729629.
  • 3DICKMANN H P, WIMMEL T S, SZWEDOWICZ J, et al. Unsteady flow in a turboeharger centrifugal compressor: three-dimensional computational fluid dynamics simulation and numerical and experimental analysis of impeller blade vibration[J]. Journal of Turbomachinery, 2006, 128: 455-465.
  • 4XIE Rong, GUAN Liang, HAO Muting. Numerical analysis for blade loading of centrifugal compressor under multi-operating conditions[J]. Information Technology Journal, 2014, 13(2): 286-293.
  • 5ZhouLi,XiGuang,GaoLimin,WangShangjin.NUMERICAL STUDY ON THE UNSTEADY INTERACTION FLOW IN A CENTRIFUGAL COMPRESSOR STAGE[J].Chinese Journal of Mechanical Engineering,2004,17(4):609-613. 被引量:3
  • 6DOWELL1 E H, HALL K C. Modeling of fluid-structure interaction[J]. Annual review of Fluid Mechanics, 2001, 33: 445-490.
  • 7Gene Hou,Jin Wang,Anita Layton.Numerical Methods for Fluid-Structure Interaction—A Review[J].Communications in Computational Physics,2012,12(7):337-377. 被引量:17
  • 8LI Xuefeng, HUANG Xiuquan, LIU Chao. Numerical simulation method for fluid-structure interaction in compressor blades[J]. Applied Mechanics and Materials, 2014, 488-489: 914-917.
  • 9YUAN Shouqi PEI Ji YUAN Jianping.Numerical Investigation on Fluid Structure Interaction Considering Rotor Deformation for a Centrifugal Pump[J].Chinese Journal of Mechanical Engineering,2011,24(4):539-545. 被引量:14
  • 10MARSHALL J G, IMREGUN M. A review of aeroelasticity methods with emphasis on turbomachinery applications[J]. Journal of Fluids and Structures, 1996, 10: 237-267.

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