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Frontiers of Mechanical Engineering

ISSN 2095-0233

ISSN 2095-0241(Online)

CN 11-5984/TH

邮发代号 80-975

2019 Impact Factor: 2.448

Frontiers of Mechanical Engineering  2016, Vol. 11 Issue (3): 219-226   https://doi.org/10.1007/s11465-016-0394-x
  本期目录
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.

Key wordsremanufactured impeller    fatigue life    impeller failures    finite element analysis (FEA)
收稿日期: 2016-03-27      出版日期: 2016-08-31
Corresponding Author(s): Huajun CAO   
 引用本文:   
. [J]. Frontiers of Mechanical Engineering, 2016, 11(3): 219-226.
Lei XU,Huajun CAO,Hailong LIU,Yubo ZHANG. Assessment of fatigue life of remanufactured impeller based on FEA. Front. Mech. Eng., 2016, 11(3): 219-226.
 链接本文:  
https://academic.hep.com.cn/fme/CN/10.1007/s11465-016-0394-x
https://academic.hep.com.cn/fme/CN/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  
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  
Fig.1  
Fig.2  
Fig.3  
Fig.4  
Fig.5  
Fig.6  
Fig.7  
Fig.8  
Load amplitude/MPa Cycling life
625 2.81×107
650 2.33×107
675 2.37×107
Tab.3  
Percentage of rated speed/% Maximum laser cladding residual stress/MPa
115 279
100 349
90 418
80 488
70 558
Tab.4  
Fig.9  
Fig.10  
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  
Fig.11  
Fig.12  
Fig.13  
1 Farrahi G H, Tirehdast M, Masoumi Khalil Abad E, Failure analysis of a gas turbine compressor. Engineering Failure Analysis, 2011, 18(1): 474–484
https://doi.org/10.1016/j.engfailanal.2010.09.042
2 Hou J F, Wicks B J, Antoniou R A. An investigation of fatigue failures of turbine blades in a gas turbine engine by mechanical analysis. Engineering Failure Analysis, 2002, 9(2): 201–211
https://doi.org/10.1016/S1350-6307(01)00005-X
3 Ren W, Dong S, Xu B, Process optimization and forming repair of laser remanufacture for FV520(B) steel blade simulator. Journal of Materials Engineering, 2015, 43(1): 6–12 (in Chinese)
4 Ren W, Dong S, Xu B, Analysis of three-dimension deformation for thin-walled blade simulator repaired by laser deposited. Transactions of the China Welding Institution, 2015, 36(6): 52–56 (in Chinese)
5 Liu C, Liu S, Gao S, Fatigue life assessment of the centrifugal compressor impeller with cracks based on the properties of FV520B. Engineering Failure Analysis, 2016, 66: 177–186
https://doi.org/10.1016/j.engfailanal.2016.04.028
6 Wang R, Zhang X, Tu S, A modified strain energy density exhaustion model for creep-fatigue life prediction. International Journal of Fatigue, 2016, 90: 12–22
https://doi.org/10.1016/j.ijfatigue.2016.03.005
7 Liu S, Liu C, Hu Y, Fatigue life assessment of centrifugal compressor impeller based on FEA. Engineering Failure Analysis, 2016, 60: 383–390
https://doi.org/10.1016/j.engfailanal.2015.11.035
8 Schijve J. Fatigue of Structures and Materials.Beijing: Aviation Industrial Press, 2014
9 Kong F R, Ma J J, Kovacevic R. Numerical and experimental study of thermally induced residual stress in the hybrid laser—GMA welding process. Journal of Materials Processing Technology, 2011, 211(6): 1102–1111
https://doi.org/10.1016/j.jmatprotec.2011.01.012
10 Ramamurti V, Subramani D A, Sridhara K. Free vibration analysis of a turbocharger centrifugal compressor impeller. Mechanism and Machine Theory, 1995, 30(4): 619–628
https://doi.org/10.1016/0094-114X(94)00056-Q
11 Witek L. Experimental crack propagation and failure analysis of the first stage compressor blade subjected to vibration. Engineering Failure Analysis, 2009, 16(7): 2163–2170
https://doi.org/10.1016/j.engfailanal.2009.02.014
12 Zhang M, Wang W, Wang P, Fatigue behavior and mechanism of FV520B-I in ultrahigh cycle regime. Procedia Materials Science, 2014, 3: 2035–2041
https://doi.org/10.1016/j.mspro.2014.06.328
13 Zhang Y, Xu B, Wang H, An experimental analysis of fatigue behavior of welded impeller made by FV520B stainless steel in over-speed preloading process. Engineering Failure Analysis, 2016, 59: 111–121
https://doi.org/10.1016/j.engfailanal.2015.09.006
14 Chu Q, Zhang M, Li J. Failure analysis of impeller made of FV520B martensitic precipitated hardening stainless steel. Engineering Failure Analysis, 2013, 34(1): 501–510
https://doi.org/10.1016/j.engfailanal.2013.07.003
15 Wang S, Wu Y, Hua G, Study on new correction method of S-N curve for metallic material. Hot Working Technology, 2011, 40(8): 35–37 (in Chinese)
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