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<pre>Array ( [var] => cut_url ) </pre> Resume for olivier B. for Engineer / Aerospace & Defense in Montreal, Canada. Search More Resumes for Engineer on Resumark.com #MQZRQDRV6
 

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Resume for olivier B. for Engineer / Aerospace & Defense in Montreal, Canada




Occupation: Engineer Industry: Aerospace & Defense
Country: Canada City: Montreal
State: Quebec ZIP: H2J2R3



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Olivier B. rue Berri HJ R QC Montreal tél: Stress analyst Structure idealization Olivier B. years experienced // French nationality TECHNICAL SKILLS * Calculation of composite material structures analytical and FEM methods * Test engineering on full scale composite structure: idealization, gauges predictions and correlations A XWB Fuselage Demonstrator * Detailed FEM and submodelling technique considering fasteners and contacts using HyperMesh and Abaqus CAE. * Training courses about HyperMesh/Abaqus CAE writing and teaching COMPUTER SKILLS Calculation software Nastran/Patran; Appli Compo; ABAQUS; CATIA v Stress; SAMCEF, ISAMI Frame. Language Python, VBA Environment UNIX, WINDOWS VOCATIONAL TRAINING CATIA v Stress: D idealization, part assembly, and postprocessing Jean Rouchon: Certification/Qualification of composite material in aerospace applications days SOGETI: ISAMI Tool days ABAQUS : Obtaining a Converged Solution days ABAQUS : Buckling, Postbuckling and Collapse Analysis days CAPGEMINI : Techniques et Outils de la Gestion de Projet days ABAQUS: Introduction to Abaqus Composite days AIRBUS: Quality control applied to composite material structures day EDUCATIONAL MASTER degree: Materials and Composite Structures University Bordeaux Engineer degree: Physical Engineering option Materials Polytech Clermont Languages English : Read, written, spoken. Since November : Bombardier contractor Montreal Canada * Plateau Bombardier Global / Fuselage Integration * Mission: Stress analysis FEM and analytical methods of fuselage junctions ex: sizing of the orbital joint "cockpitcentre fuselage" Environment: Patran/Nastran sol , , Excel VBA, CATIA v Stress December October : GECI International Toulouse * Plateau Airbus A Nose Fuselage Junction * Mission: Investigation and validation of nonlinear detailed FEM and dedicated stress notes Environment: Patran/Nastran sol , ISAMI Filled Hole, Assist Frame, Patran FastPPh. March November : SOGETI HighTech Toulouse * Plateau Airbus A XWB Rear Fuselage Demonstrator &;Barrel A/B/B refurbishment&; * Mission: Barrel detailed idealization Test predictions Correlations Support for the methods team Idealization and postprocessing of the nonlinear detailed FEMs dedicated to the Barrel A/B/B refurbishment Idealization of more detailed FEMs using the Abaqus submodelling technique. Management and optimisation of the nonlinear calculations parameters Cluster HPC of Marignane and POD HPC of Toulouse Test engineering * DFEM instrumentation, gauges prediction. * Monitoring preparation for the Barrel tests taking place in Hambourg * Secure the tests and followup * Correlation analysis and FEM updating * Support the method team in order to improve sizing tools. Environment: Patran/Nastran sol , HyperMesh v./v., Abaqus v../v../v. July December : SOGETI HighTech Toulouse * Plateau Airbus AM Nose Fuselage Lower Panel * Mission : Stress analysis of metal structures * Sizing justification of the lower unit panel to system junctions * Stress analytical analysis of rod to lug links: tension, compression, unfolding * Vibratory calculation &;wind milling&; * Fasteners calculation tension, shear Environment: Assist Chape, Macro Excel &;Wind milling&; July June : SOGETI HighTech Toulouse * Plateau AM Center Wing Box * Mission : Sizing of CFRP composite structures * Sizing of the front and rear CWB spars * Management of the detailed FEM of the spars * Sizing loop: Stability, DamTol, and calculation of filled and free holes, fasteners. * Weight saving analysis for the spars and stringers * Impact of the systems on the spars * Concessions management {spars, angles, stringers} * Spar angle unfolding Environment: Patran/Nastran reduction, SOL ,ACSA, AppliCompo February April : CTA Bordeaux St MédardenJales * Mission : Sizing of A cockpit composite secondary structures * Management and postprocessing of the global FEM. * Linear static analysis on the composite panels and metal fittings Environment: Logiciel Nastran/Patran; Excel. March July : SAINTGOBAIN VETROTEX Chambéry * Engineer trainee R&D department `TwintexR&; * Mechanical caracterisation of sandwich structures * Making of points bending tests on various sandwich structures * Benchmarking of many laboratories able to caracterise sandwich structures February July : TECHNIMODUL ClermontFerrand * Engineer trainee * Development of a composite material solar panel glass fibre reinforced thermoplastic HOBBIES * Tennis competition for years * Climbing level ca, VTT, Snowboard

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