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Frontiers of Mechanical Engineering

ISSN 2095-0233

ISSN 2095-0241(Online)

CN 11-5984/TH

Postal Subscription Code 80-975

2018 Impact Factor: 0.989

Front. Mech. Eng.    2016, Vol. 11 Issue (3) : 219-226    https://doi.org/10.1007/s11465-016-0394-x
RESEARCH ARTICLE
Assessment of fatigue life of remanufactured impeller based on FEA
Lei XU1,Huajun CAO1,*(),Hailong LIU1,Yubo ZHANG2
1. The State Key Laboratory of Mechanical Transmission, Chongqing University, Chongqing 400030, China
2. National Key Laboratory for Remanufacturing, Academy of Armored Forces Engineering, Beijing 100072, China
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Abstract

Predicting the fatigue life of remanufactured centrifugal compressor impellers is a critical problem. In this paper, the S-N curve data were obtained by combining experimentation and theory deduction. The load spectrum was compiled by the rain-flow counting method based on the comprehensive consideration of the centrifugal force, residual stress, and aerodynamic loads in the repair region. A fatigue life simulation model was built, and fatigue life was analyzed based on the fatigue cumulative damage rule. Although incapable of providing a high-precision prediction, the simulation results were useful for the analysis of fatigue life impact factors and fatigue fracture areas. Results showed that the load amplitude greatly affected fatigue life, the impeller was protected from running at over-speed, and the predicted fatigue life was satisfied within the next service cycle safely at the rated speed.

Keywords remanufactured impeller      fatigue life      impeller failures      finite element analysis (FEA)     
Corresponding Author(s): Huajun CAO   
Online First Date: 26 July 2016    Issue Date: 31 August 2016
 Cite this article:   
Lei XU,Huajun CAO,Hailong LIU, et al. Assessment of fatigue life of remanufactured impeller based on FEA[J]. Front. Mech. Eng., 2016, 11(3): 219-226.
 URL:  
https://academic.hep.com.cn/fme/EN/10.1007/s11465-016-0394-x
https://academic.hep.com.cn/fme/EN/Y2016/V11/I3/219
Component Weight percentage/(wt.%) Component Weight percentage/(wt.%)
C ≤0.07 Cr 13.00?14.50
Si ≤0.07 Cu 1.30?1.80
Mn ≤1.00 Nb 0.25?0.45
P ≤0.03 Mo 1.30?1.80
S ≤0.03 Fe Balance
Ni 5.00?6.00
Tab.1  Chemical composition of FV520B
Parameter Value
Yield stress, MPa 1029
Tensile strength, MPa 1170
Young’s modulus, GPa 210
Density, kg/m3 7860
Vickers hardness, HV 380
Poisson’s ratio 0.3
Tab.2  Mechanical compositions properties of FV520B
Fig.1  Remanufactured impeller
Fig.2  Dynamic-balancing experiment on remanufactured impeller
Fig.3  Full sized model of the remanufactured impeller
Fig.4  Mesh model of the impeller
Fig.5  Procedure of FEA process
Fig.6  Aerodynamic load set
Fig.7  von-Mises stress of the remanufactured impeller
Fig.8  S-N curve of the impeller
Load amplitude/MPa Cycling life
625 2.81×107
650 2.33×107
675 2.37×107
Tab.3  Experiment life of specimen [12]
Percentage of rated speed/% Maximum laser cladding residual stress/MPa
115 279
100 349
90 418
80 488
70 558
Tab.4  Working speed and laser cladding residual stress
Fig.9  Load in rated speed
Fig.10  Counting process of load cycles in rated speed
Revised load amplitude/MPa Simulated cycling life Experimental cycling life
556.9 1.33×108 2.81×107
578.5 7.29×107 2.33×107
601.4 6.64×107 2.37×107
Tab.5  Fatigue life simulation and experimental results
Fig.11  Result of simulated analysis on fatigue life in different rotating states
Fig.12  Fatigue life under different maximum residual stresses
Fig.13  Fatigue life nephogram with the maximum residual stress of 488 MPa
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