PSI - Issue 7

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ScienceDirect Available online at www.sciencedirect.com Av ilable o line at ww.sciencedire t.com S ienceDirect Structural Integrity Procedia 00 (2016) 000 – 000 Procedia Structu al Integrity 7 (2017) 101–108 Structural Integrity Procedia 00 (2017) 000–000 Available online at www.sciencedirect.com Structural Integrity Procedia 00 (2017) 000–000

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2452-3216 © 2016 The Authors. Published by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of PCF 2016. ∗ Corresponding author. Tel.: + 39-02-2399-8248; fax: + 39-02-2399-8263. E-mail address: simone.romano@polimi.it 2210-7843 c 2017 The Authors. Published by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of the 3rd International Symposium on Fatigue Design and Material Defects. One of the main issues of AM parts is the large scatter often associated to their fatigue resistance, in particular in the HCF region (see Beretta and Romano (2017); Wycisk et al. (2013); Leuders et al. (2013)). Even though the fast and progressive improvement of the AM technology is constantly mitigating this issue, the state-of-the-art knowledge of the variables in play do not allow the definition of a robust and reliable method for structural parts qualification. This issue is often overcome by space and aerospace companies by verifying a frozen process and performing extensive test ∗ Corresponding author. Tel.: + 39-02-2399-8248; fax: + 39-02-2399-8263. E-mail address: simone.romano@polimi.it 2210-7843 c 2017 The Authors. Published by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of the 3rd International Symposium on Fatigue Design and Material Defects. * Corresponding author. Tel.: +351 218419991. E-mail address: amd@tecnico.ulisboa.pt 2452-3216 Copyright  2017 The Authors. Published by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of the 3rd International Symposium on Fatigue Design and Material Defects. 10.1016/j.prostr.2017.11.066 One of the main issues of AM parts is the large scatter often associated to their fatigue resistance, in particular in the HCF region (see Beretta and Romano (2017); Wycisk et al. (2013); Leuders et al. (2013)). Even though the fast and progressive improvement of the AM technology is constantly mitigating this issue, the state-of-the-art knowledge of the variables in play do not allow the definition of a robust and reliable method for structural parts qualification. This issue is often overcome by space and aerospace companies by verifying a frozen process and performing extensive test XV Portuguese Conference on Fracture, PCF 2016, 10-12 February 2016, Paço de Arcos, Portugal Thermo-mechanical modeling of a high pressure turbine blade of an airplane gas turbine engine P. Brandão a , V. Infante b , A.M. Deus c * a Department of Mechanical Engineering, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, 1, 1049-001 Lisboa, Portugal b IDMEC, Department of Mechanical Engineering, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, 1, 1049-001 Lisboa, Portugal c CeFEMA, Department of Mechanical Engineering, Instituto Superior Técnico, Universidade de Lisboa, Av. Rovisco Pais, 1, 1049-001 Lisboa, Portugal Abstract During their operation, modern aircraft engine components are subjected to increasingly demanding operating conditions, especially the high pressure turbine (HPT) blades. Such conditions cause these parts to undergo different types of time-dependent degradation, one of which is creep. A model using the finite element method (FEM) was developed, in order to be able to predict the creep behaviour of HPT blades. Flight data records (FDR) for a specific aircraft, provided by a commercial aviation company, were used to obtain thermal and mechanical data for three different flight cycles. In order to create the 3D model needed for the FEM analysis, a HPT blade scrap was scanned, and its chemical composition and material properties were obtained. The data that was gathered was fed into the FEM model and different simulations were run, first with a simplified 3D rectangular block shape, in order to better establish the model, and then with the real 3D mesh obtained from the blade scrap. The overall expected behaviour in terms of displacement was observed, in particular at the trailing edge of the blade. Therefore such a model can be useful in the goal of predicting turbine blade life, given a set of FDR data. Copyright © 2017 The Auth rs. Publis ed by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of the 3rd I ternational Sympos um on Fatigue Design and Material Defects. 3rd International Symposium on Fatigue Design and Material Defects, FDMD 2017, 19-22 September 2017, Lecco, Italy HCF resistance of AlSi10Mg produced by SLM in r lation to the presence of defects S.Romano a, ∗ , S. Beretta a , A. Branda˜o b , J. Gumpinger b , T. Ghidini b a Politecnico di Milano, Dipartimento di Meccanica, Via La Masa 1, I 20156 Milano b European Space Research and Technology Centre, Keplerlaan 1, NL 2200AG Noordwijk Abstract Being able to predict the fatigue resistance of parts produced by additive manufacturing (AM) is a very actual and frequent open issue. The qualification of AM structural parts needs a very costly and time consuming series of fatigue tests, on both samples and full-scale parts. A proper control of the AM process allows obtaining comparable and even better fatigue resistance than standard manufacturing. Despite this, the experimental results often show a large scatter, mostly due to the presence of defects. In this framework, this work summarizes a research activity aiming at modelling the high cycle fatigue (HCF) resistance in presence of defects, focusing on AlSi10Mg produced by selective laser melting (SLM). Two batches of samples were investigated by computed tomography (CT) and tested. A lower bound resistance curve was obtained introducing artificial defects. A fatigue crack growth simulation model based on the maximum defect size is proposed, able to estimate both the life and the scatter of the data in the fully-elastic regi n. Moreover, knowing the size and position of all the defects inside the samples, it was possible to foresee the defect at the origin of fatig e failure and to draw a hazard ranking based on t e ap lied stress intensity factor. c 2017 The Authors. Published by Elsevier B.V. Peer-review und r r sponsibility of the Scie tific Committee of the 3rd Internatio al Symposium o Fatigue Design and Material D fects. Keywords: AlSi10Mg; additive manufacturing; selective laser melting; high cycle fatigue; Kitagawa diagram; probabilistic fatigue life assessment 3rd International Symposium on Fatigue Design and Material Defects, FDMD 2017, 19-22 September 2017, Lecco, Italy HCF resistance of AlSi10Mg produced by SLM in relation to the presence of defects S.Romano a, ∗ , S. Beretta a , A. Branda˜o b , J. Gumpinger b , T. Ghidini b a Politecnico di Milano, Dipartimento di Meccanica, Via La Masa 1, I 20156 Milano b European Space Research and Technology Centre, Keplerlaan 1, NL 2200AG Noordwijk Abstract Being able to predict the fatigue resistance of parts produced by additive manufacturing (AM) is a very actual and frequent open issue. The qualifica io of AM structural parts eeds a very costly and time consuming s rie f fatigue tests, on both samples and full-scale parts. A proper control of the AM process allows obtainin comparable and even better fatigue resistance than standard manufacturing. Despite this, the experimental results often show a large scatter, mostly due to the presence of defects. In this framework, this work summarizes a research activity aiming at modelling the high cycle fatigue (HCF) resistance in presence of defects, focusing on AlSi10Mg produced by selective laser melting (SLM). Two batches of samples were investigated by computed tomography (CT) and tested. A lower bound resistance curve was obtained introducing artificial defects. A fatigue crack growth simulation model based on the maximum defect size is proposed, able to estimate both the life and the scatter of the data in the fully-elastic region. Moreover, knowing the size and position of all the defects inside the samples, it was possible to foresee the defect at the origin of fatigue failure and to draw a hazard ranking based on the applied stress intensity factor. c 2017 The Authors. Published by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of the 3rd International Symposium on Fatigue Design and Material D fects. Keywords: AlSi10Mg; additive manufacturing; selective laser melting; high cycle fatigue; Kitagawa diagram; probabilistic fatigue life assessment © 2016 The Authors. Published by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of PCF 2016. Keywords: High Pressure Turbine Blade; Creep; Finite Element Method; 3D Model; Simulation. 1. Introduction 1. Introduction