PSI - Issue 10

ScienceDirect Available online at www.sciencedirect.com Av ilable o line at ww.sciencedire t.com Sci ceDirect Structural Integrity Procedia 00 (2016) 000 – 000 Procedia Structural Integrity 1 8 18–24 Available online at www.sciencedirect.com ScienceDirect Structural Integrity Procedia 00 (2018) 000 – 000

www.elsevier.com/locate/procedia

www.elsevier.com/locate/procedia

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. © 2018 The Authors. P blished by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/3.0/) Peer-review under responsibility of the scientific committee of the 1st International Conference of the Greek Society of Experimental Mechanics of Materials. 1 st International Conference of the Greek Society of Experimental Mechanics of Materials An indentation methodology for measuring the elastic properties of biological patches used in human carotid endarterectomy I.D. Gavardinas a, *, A.E. Giannakopoulos b a Department of Civil Engineering, University of Thessaly, Pedion Areos, Volos, 38334, Greece b Mechanics Division, National Technical University of Athens, Zografou Campus, Iroon Polytechniou 9, 15780, Athens, Greece Abstract Carotid endarterectomy (CEA) is one of the approaches available for the treatment of atherosclerosis, a common carotid artery disease. Patch angioplasty is the pertinent technique mostly preferred by vascular surgeons. It entails an arteriotomy followed by closure with a textile, polymer or biological tissue patch. We propose a novel indentation methodology as a technique for mech anically characterizing biological patches used in carotid artery repair. The proposed methodology is a simple, yet accurate one, requiring only one initial experimental measurement to support the relevant calculations. Bovine pericardium patches are indented herein. Results, including material properties, are then obtained analytically. The experimental results indicate that indentation is a reliable method to ssess the elastic properties of bovine patches. The modulus f elasticity and r levant indentatio metrics are obtained for wo comm rcial vascular bovine p tches. © 2018 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/3.0/). Peer-review under responsibility of the scientific committee of the 1 st International Conference of the Greek Society of Experimental Mechanics of Materials Keywords: Carotid endarterectomy; biological vascular patch; bovine pericardium; biomaterial characterization; indentation biological patches used in human carotid endarterectomy b a e of the Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license rg/licen y

1. Introduction

© 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. Carotid artery atherosclerosis is the most common cardiovascular disease wherein artery walls start becoming thicker until they ventually occlude. This causes a cessati n of bl od flow, affecting the perfusion of human organs. o o

* Corresponding author. Tel.: +30 242 107 4179; fax: +30 242 107 4169. E-mail address: gavardinas@uth.gr Received: May 16, 2018; Received in revised form: July 30, 2018; Accepted: August 06, 2018

2452-3216 © 2016 The Authors. Published by Elsevier B.V. Peer-review under responsibility of the Scientific Committee of PCF 2016. 2452-3216  2018 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/3.0/) Peer-review under responsibility of the scientific committee of the 1st International Conference of the Greek Society of Experimental Mechanics of Materials. 10.1016/j.prostr.2018.09.004 2452- 3216 © 2018 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/3.0/). Peer-review under responsibility of the scientific committee of the 1 st International Conference of the Greek Society of Experimental Mechanics of Materials * Corresponding author. Tel.: +351 218419991. E-mail address: amd@tecnico.ulisboa.pt