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Sogeti High Tech
- Stress Engineer & Project Manager
Paris
maintenant
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Sogeti High Tech
- WP Stress Leader
Paris
2010 - maintenant
SOGETI HIGH TECH for Airbus EDSIB, A350 - 1000 Stress MLGB Focal Point :
- Gear Beam attachment architecture principles: sensitivity & comparative studies from dedicated GFEM. Pre-sizing, updating & weight estimation.
- Optimization of different principles of MLGB with NASTRAN (sol200).
- Lateral vertical panel and canted beam junction sizing.
- WP follow-up of the Sogeti High Tech stress team (4 people).
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Sogeti High Tech
- Stress Engineer
TOULOUSE
2009 - 2010
SOGETI HIGH TECH for Airbus EDSAK, SASt support–Stress Engineer :
- Focal point for ISAMI, PATRAN, NASTRAN and Composite Application incidents.
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Sogeti High Tech
- Project Manager
TOULOUSE
2009 - 2009
SOGETI HIGH TECH for Airbus EDSIY2, « A3OX B3 Architecture principles : Nose Fuselage & Centre Section» project – Project Manager :
- Technical follow-up of the project team (9 people): Financial quotation, quality, planning, reporting, inputs/outputs validation, financial follow-up.
- Excel tool creation for ISAMI calculation management: Pre & post-processing, property modifications & GFEM updating.
- Pre-sizing of the A3OX Rib1 of the CWB with ISAMI.
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Sogeti High Tech
- Official Airbus Stress Trainer
TOULOUSE
2008 - 2008
SOGETI HIGH TECH for Airbus « Structure Academy », «A350XWB Learning Materials » project – Airbus Official Stress Trainer:
- Creation of « Stress composite A350XWB » learning materials: Large Damage, Reparability, Bolted Repairs Sizing, Bonded Repairs Sizing, Fuselage Stiffened Panel, Box Cover Stiffened Panels, Circumferential Joints and Damage Tolerance.
- Trainer of the Transnational Composite Trainer: Open Hole, Large Damage, Reparability, Bolted Repairs Sizing, Bonded Repairs Sizing et Circumferential Joints.
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Sogeti High Tech
- Stress Engineer / Project Manager
TOULOUSE
2008 - 2009
SOGETI HIGH TECH for Airbus EDSIY2, « A3OX B1 BIS Nose Fuselage» project - Project Manager:
- Technical follow-up of the project team (5 people).• GFEM updating & SE reduction.
- Sensitivity Analysis of several PC of frame15 of the NLGB.
- Pre-sizing of the PA B1Bis fuselage (stability & damage tolerance).
- Sensitivity Analysis in stability of the stringer run-outs of the skin with Composite Applic.
- A3OX NLGB DFEM creation with PATRAN.
- Excel tool creation to automatically update the AssistLink files.
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Sogeti High Tech
- Stress Engineer
TOULOUSE
2005 - 2008
SOGETI HIGH TECH for Airbus TNEG, « NOFUDEM » (full-scale A3OX Nose Fuselage demonstrator) - Stress engineer:
- Crash & explosive depressurisation load cases of the GFEM. GFEM updating & SE reduction.
- Detailed studies & optimization of the frame mouse holes. Creation of DFEM with PATRAN and sensitivity studies with NASTRAN.
- Pre-sizing of the composite skin and stringers of the NF lower bay (IMA/M21E) in stability and damage tolerance.
- Detailed FEM for the bolted-titan doublers of corners of the nose landing bay. Automatic tool with Visual Basic for loading of the refined FEM based on PSN23. Detailed FEM for the bolted-titan doublers of corners of the nose landing bay. Automatic tool for loading of the refined FEM based on PSN23.
- Pre-sizing of the cockpit floor with two different composite materials: HR NCF/RTM6 (LRI) and AS4-PEEK (TP).
- Definition and sizing of characteristic floor pieces for mechanical tests. Test request for the crossbeam flexion test.
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Sogeti High Tech
- Stress Engineer
TOULOUSE
2005 - 2005
SOGETI HIGH TECH – Training period « Shape optimization with Nastran applied to different aeronautic structures ».
- Shape optimization of the A400M Nose Fuselage PAX door corners and pocket thicknesses.
- Shape optimization of a composite rib of CWB.
- Shape and thickness optimization of A340 frames.
