Predictive design approach of high-cycle fatigue limit of shot-peened parts
This attempt proposes an engineering design approach to predict the high-cycle fatigue limit of shot-peened parts. The effects of the shot peening surface treatment on the high-cycle fatigue performance of Waspaloy, a nickel superalloy widely used in the airframe sector, are investigated. The propos...
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| Published in | International journal of advanced manufacturing technology Vol. 93; no. 5-8; pp. 2321 - 2339 |
|---|---|
| Main Authors | , , , , |
| Format | Journal Article |
| Language | English |
| Published |
London
Springer London
01.11.2017
Springer Nature B.V Springer Verlag |
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| Abstract | This attempt proposes an engineering design approach to predict the high-cycle fatigue limit of shot-peened parts. The effects of the shot peening surface treatment on the high-cycle fatigue performance of Waspaloy, a nickel superalloy widely used in the airframe sector, are investigated. The proposed approach consists in (i) predicting the initial shot peening surface properties, (ii) simulating the evolution of the shot peening surface properties occurring during fatigue loading, and (iii) deducing the new fatigue limit of the shot-peened surface in the case of tensile, torsion, and combined tensile-torsion loading. The physical model is implemented and analyzed using the finite element analysis. The mathematical model sheds light on the evolution of the shot-peened surface performance. It allows determining the influence of the industrial parameters in order to optimize the shot peening process operating conditions. The prediction of the fatigue performance for different shot peening conditions leads to have physically consistent results. |
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| AbstractList | This attempt proposes an engineering design approach to predict the high-cycle fatigue limit of shot-peened parts. The effects of the shot peening surface treatment on the high-cycle fatigue performance of Waspaloy, a nickel superalloy widely used in the airframe sector, are investigated. The proposed approach consists in (i) predicting the initial shot peening surface properties, (ii) simulating the evolution of the shot peening surface properties occurring during fatigue loading, and (iii) deducing the new fatigue limit of the shot-peened surface in the case of tensile, torsion, and combined tensile-torsion loading. The physical model is implemented and analyzed using the finite element analysis. The mathematical model sheds light on the evolution of the shot-peened surface performance. It allows determining the influence of the industrial parameters in order to optimize the shot peening process operating conditions. The prediction of the fatigue performance for different shot peening conditions leads to have physically consistent results. This attempt proposes an engineering design approach to predict the high-cycle fatigue limit of shot-peened parts. The effects of the shot peening surface treatment on the high-cycle fatigue performance of Waspaloy, a nickel superalloy widely used in the airframe sector, are investigated. The proposed approach consists in (i) predicting the initial shot peening surface properties, (ii) simulating the evolution of the shot peening surface properties occurring during fatigue loading, and (iii) deducing the new fatigue limit of the shotpeened surface in the case of tensile, torsion, and combined tensile-torsion loading. The physical model is implemented and analyzed using the finite element analysis. The mathematical model sheds light on the evolution of the shot-peened surface performance. It allows determining the influence of the industrial parameters in order to optimize the shot peening process operating conditions. The prediction of the fatigue performance for different shot peening conditions leads to have physically consistent results. |
| Author | Petit, E. J. Fathallah, R. Seddik, R. Rabii, Ben Sghaier Atig, A. |
| Author_xml | – sequence: 1 givenname: R. surname: Seddik fullname: Seddik, R. email: seddik.raoudha@yahoo.fr organization: National Engineering School of Sousse, University of Sousse – sequence: 2 givenname: E. J. surname: Petit fullname: Petit, E. J. organization: Laboratoire d’Etude des Microstructures et de Mécanique des Matériaux, Université de Lorraine – sequence: 3 givenname: Ben Sghaier surname: Rabii fullname: Rabii, Ben Sghaier organization: National Engineering School of Sousse, University of Sousse – sequence: 4 givenname: A. surname: Atig fullname: Atig, A. organization: National Engineering School of Sousse, University of Sousse – sequence: 5 givenname: R. surname: Fathallah fullname: Fathallah, R. organization: National Engineering School of Sousse, University of Sousse |
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| CitedBy_id | crossref_primary_10_1007_s11665_019_03891_w crossref_primary_10_1007_s00170_017_1450_3 crossref_primary_10_1007_s00170_018_2029_3 crossref_primary_10_1007_s00170_019_03632_2 crossref_primary_10_1007_s00170_017_1033_3 crossref_primary_10_1007_s11665_022_06594_x |
| Cites_doi | 10.1179/mst.1998.14.7.631 10.1016/j.surfcoat.2010.08.105 10.1016/S0168-874X(98)00057-2 10.1051/mattech/198775120493 10.1016/j.surfcoat.2015.09.026 10.1016/j.proeng.2011.11.084 10.1016/S0142-1123(96)00064-3 10.1016/S0924-0136(01)00601-X 10.1016/j.advengsoft.2009.03.013 10.1016/j.ijfatigue.2010.08.012 10.1016/j.msea.2011.04.004 10.1016/S0924-0136(99)00153-3 10.1016/j.msea.2006.03.097 10.1016/j.jallcom.2016.01.119 10.1016/S0734-743X(01)00043-4 10.1016/0045-7949(90)90083-E 10.1016/j.surfcoat.2012.03.078 10.1016/j.ijfatigue.2012.10.008 10.1016/S0749-6419(96)00037-X 10.1016/S0142-1123(01)00205-5 10.1016/j.msea.2010.07.010 10.1016/j.ijfatigue.2005.02.001 10.1179/026708303225003027 10.1016/j.msea.2010.09.050 10.1016/j.ijfatigue.2009.01.012 10.1016/j.surfcoat.2012.03.057 10.1016/j.ijfatigue.2004.03.007 10.1016/j.jmatprotec.2005.02.139 10.1002/3527606580.ch37 10.1007/s00170-016-9532-1 |
| ContentType | Journal Article |
| Copyright | Springer-Verlag London Ltd. 2017 Copyright Springer Science & Business Media 2017 The International Journal of Advanced Manufacturing Technology is a copyright of Springer, (2017). All Rights Reserved. Springer-Verlag London Ltd. 2017. Distributed under a Creative Commons Attribution 4.0 International License |
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| Issue | 5-8 |
| Keywords | Shot peening Ni-based superalloy Waspaloy Cyclic work hardening Residual stress Surface damage Fatigue performance prediction |
| Language | English |
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| SubjectTerms | Airframes CAE) and Design Computer simulation Computer-Aided Engineering (CAD Design engineering Engineering Engineering Sciences Evolution Fatigue limit Finite element method High cycle fatigue Industrial and Production Engineering Lasers Mathematical models Mechanical Engineering Mechanics Mechanics of materials Media Management Nickel base alloys Order parameters Original Article Predictions Product design Shot peening Superalloys Surface properties Surface treatment Torsion Waspaloy |
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| Title | Predictive design approach of high-cycle fatigue limit of shot-peened parts |
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