PSI - Issue 2_B

ScienceDirect Available online at www.sciencedirect.com Av ilable o line at ww.sciencedire t.com ScienceDirect Structural Integrity Procedia 00 (2016) 000 – 000 Procedia Struc ural Integrity 2 (2016) 2757–2763 Available online at www.sciencedirect.com ScienceDirect Structural Integrity Procedia 00 (2016) 000–000 Available online at www.sciencedirect.com ScienceDirect Structural Integrity Procedia 00 (2016) 000–000

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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. 21st European Conference on Fracture, ECF21, 20-24 June 2016, Catania, Italy Ratcheting Strain Accumulation Due to Asymmetric Cyclic Loading of Zircaloy-2 at Room Temperature R. S. Rajpurohit*, N.C. Santhi Srinivas, Vakil Singh Department of Metallurgical Engineering, Indian Institute of Technology, (Banaras Hindu University), Varanasi 221005, India * rsrajpurohit.rs.met13@iitbhu.ac.in Abstract Asymmetric stress cycling leads to accumulation of plastic strain which is called as ratcheting strain. The problem is generally associated with nuclear fuel cladding materials used in nuclear power plants and in pressurized pipe lines. In the present investigation asymmetric stress controlled fatigue tests were conducted with three different parameters namely, mean stress, stress amplitude and stress rate (keeping two parameter constant and varying third parameter) to see the plastic strain accumulation and its effect on fatigue life of Zircaloy-2 at room temperature. The tests were conducted with mean stress varying from 80 to 150 MPa, stress amplitude varying from 270 to 340 MPa and stress rate va ying from 30 to 750 MPa/s respectively. Th experimental outcomes show that with increase in mean stress and stress amplit de, the ratcheting strain accumulation incr ases with reduction in fatigu life. However, crease i stress rate leads to improvement in fatigue life of the material due to small ratcheting strain accumulation. Cyclic softening is bserved during initial cycles fo lowe values of mean stress and stress amplitude and cyclic hardening is pr dominant for igher values f mean stress a d stress amplitude. However, cyclic hardening is observed with increase in stress rate. © 2016 The Authors. Published by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of ECF21. Keywords: Zircaloy-2; asymmetric stress cyclic loading; ratcheting strain; Mean stress; stress amplitude; stress rate and plastic strain. 1. Introduction Zirconium and its alloys are widely used as structural material for components of nuclear reactors because of their inherent low neutron absorption cross section [Lin et al. (2004)], excellent mechanical properties [Mallipudi et al. (2012), Lee and Hong (2011)] and corrosion resistance [Guo et al. (2012)]. It has been observed that zircaloy-2 clad fuel tubes are subjected to cyclic loading with non-zero mean stress and hence cyclic accumulation of plastic strain occurs and causes yielding of the material [Gaudin and Feaugas (2004)], often known as ratcheting fatigue, or cyclic creep, proposed by [Hübel (1996)]. Fuel tubes are subjected to primary load in the axial and circumferential 21st European Conference on Fracture, ECF21, 20-24 June 2016, Catania, Italy Ratcheting Strain Accumulation Due to Asymmetric Cyclic Loading of Zircaloy-2 at Room Temperature R. S. Rajpurohit*, N.C. Santhi Srinivas, Vakil Singh Department of Metallurgical Engineering, Indian Institute of Technology, (Banaras Hindu University), Varanasi 221005, India * rsrajpurohit.rs.met13@iitbhu. c.in Abstract Asymmetric stress cycling leads to accumulation of plastic strain which is called as ratcheting strain. The problem is generally as ociat d wi h nu lear fuel cladding aterials used in nuclear power pl nts and in pressurized pipe lines. In the present investigation asymm tric stress controlled fatigue t sts were conducted with hree different parameters nam ly, mean stress, stres amplitude and stre s rate (keeping two parameter constant and varying third parameter) to see the plastic strain accumul tion and its effect on fatigu life of Zircaloy-2 a room temper ture. The tes s were conducted with mean stre s varying from 80 to 150 MPa, str ss ampl tud varying from 270 o 340 MPa and stress ra varying from 30 to 750 MPa/s r spectively. The experimental outc mes show that wi h increase in mea stress and stress amplitude, the ratcheti strain accumulation increases with reduction in fatigue lif . owever, increase in stre s rate lead to imp oveme t in fatigue life of he material due to small r tche ing strain accumulation. Cyclic softening is observ d during initial cycles for lower values o mean str ss and stress a p itude and cyclic h rdening is predom nant for higher values of mean stress and stress amplitude. H wev r, cyclic h rdening is observ d with increase in stres rate. © 2016 The Authors. Published by Elsevier B.V. Peer-review under espons bility of the Scientific Committee of ECF21. Keywords: Zircaloy-2; asymmetric stress cyclic loading; ratcheting strain; Mean stress; stress amplitude; stress rate and plastic strain. 1. Introduction Zirconium and its alloys are widely used as structural material for components of nuclear reactors because of their inherent low neutron abso ption cross section [Lin et al. (2004)], excelle t mecha ical p oper ies [Mallipudi et al. (2012), Lee a d H g (2011)] and corrosion resistance [Guo et al. (2012)]. It has been observ d that zircaloy-2 cl d fuel tubes are subjected to cyclic loading with non-zero mean stress and hence cyclic accumulation of pl stic strain occurs and causes yiel ing of the m terial [Gaudi and Feauga (2004)], often known s ratcheting fatigue, or cycl c creep, proposed b [Hübel (1996)]. Fuel tubes are subjected to primary load in the axial and c rcumferential Copyright © 2016 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/). Peer-review under responsibility of the Scientific Committee of ECF21. © 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.

* Corresponding author. Tel.: +351 218419991. E-mail address: amd@tecnico.ulisboa.pt 2452-3216 © 2016 The Authors. Published by Elsevier B.V. Peer-review und r responsibil ty of the Scientific Committee of ECF21. 2452-3216 © 2016 The Authors. Published by Elsevier B.V. Peer review under r sponsibility of the Scientific Committee of ECF21.

2452-3216 © 2016 The Authors. Published by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of PCF 2016. Copyright © 2016 The Authors. Published by Elsevier B.V. This is an open access article under the CC BY-NC-ND license ( http://creativecommons.org/licenses/by-nc-nd/4.0/ ). Peer review under responsibility of the Scientific Committee of ECF21. 10.1016/j.prostr.2016.06.344

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