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nexteam engineering
- Program manager
2016 - maintenant
Programme manager for Nexter system on mag 58 support installation for amx10RC and Leclerc:
- projet responsable
- engineering leader: design & Stress
- manufacturing
- Nexteam / Nexter focal point
- schedule management
- cost management
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Nexteam Engineering
- Stress Leader
2015 - maintenant
Beluga XL Nose fuselage belly door (NEXTEAM) – Stress Leader
Role: Stress Leader, Stress expert Mechanism (kinematic, dynamic and sizing), DFEM expert + Method focal point on Cargo Access door:
- Belly door and CAD engineering costing + Nexteam bill of specification answer redaction.
- First maturity of door design phases: conception of structure & stair mechanism.
- Kinematic study of the door stair mechanism.
- Mechanism part calculation: DFEM (ANSA, PATRAN-NASTRAN), analytical calculation.
- DFEM door structure + post treatment : static, modal analysis, buckling, FDT
- Stress Lead: stress team management, scheduling, focal point STELIA / NEXTEAM.
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NEXTEAM Engineering
- Project Manager
2014 - maintenant
Turbomeca Carter TPH-TL (NEXTEAM) - project manager
Role: Project manager:
- Engineering lead.
- Schedule management: engineering + manufacturing.
- Manufacturing lead.
- Focal point Turbomeca / Nexteam
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NEXTEAM Engineering
- Project Manager
2014 - maintenant
Nexter: Tank's fire joystick design upgrade + manufacturing project manager
- Engineering and manufacturing costing.
- Electronical component buying and supplier management
- Engineering lead (joystick body design)
- Schedule management: engineering + manufacturing.
- Manufacturing lead.
- Focal point Nexter / Nexteam
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Spirit AeroSystems
- Stress Leader
Montoir-de-Bretagne
2012 - 2014
: A350-900 XWB S15 (Spirit AeroSystems) - Support system & fixed bracket
Stress Leader, Airbus / Spirit Focal Point for IP validation + stress dossier management.
* Managing IPs validation (loaded & unloaded in red area) in stress point of view (tracker file):
* Bracket stress analysis: static + windmilling. ;
* Backup analysis (Crossbeams) or interface loads for primary structure teams.
* Management of dedicated stress team (Progress Tech (Russia), Infosys engineers in TLS & India).
* FLS bracket & Airbus Misc bracket dossier: FF and certification dossier management:
* FLS bracket dossier scheduling and work in progress management.
* Management of offshore stress team working on analyses to perform and dossier redaction.
* Other commodities dossier (USP, LJP and PDS): interface between US teams and Airbus.
* Answer US team question: save time on stress dossier work to perform (loads to use, methods...) ;
* Clarify Airbus requirement (dossier templates, methods).
* Transfer Airbus requirement to US stress leaders: help communication between AIF & Spirit US.
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Aerolia
- Stress Engineer
Colomiers
2012 - 2012
* Check RSP certification dossier: SOCATA - FAIRING, SONACA, LATECOERE-landing gear bay.
* Methods improvement - SOCATA: DFEM (ANSA, PATRAN-NASTRAN), analytical calculation.
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Latécoère
- Mechanism stress engineer
Toulouse
2011 - 2012
, COMAC 919 overwing doors (LATECOERE)
* First maturity of door design phases (MATA, B and C): conception of door mechanism (lock, lift, vent flap).
* Kinematic study of the mechanism and the door lift.
* Mechanism part calculation: DFEM (ANSA, PATRAN-NASTRAN), analytical calculation.
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NEXTEAM Engineering
- Stress Leader & stress engineer
2010 - maintenant
A350 cockpit escape hatch and avionic access doors (AEROTEAM-Services)
1- Mechanism stress engineer
* First maturity of door design phases (MATA, B and C): conception of door mechanism
* Kinematic study of the mechanism and the door lift.
* Mechanism part calculation: DFEM (ANSA, PATRAN-NASTRAN), analytical calculation.
* DFEM door structure + post treatment : static (ISAMI), modal analysis, buckling
2- Stress Leader on Certification phase: stress team management, scheduling, focal point Aerolia/ATS.
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Latécoère
- Stress leader
Toulouse
2008 - 2010
, A330-200 GMF Nose fuselage (LATECIS): SRM (Structural Repair Manual)
Role: SRM stress leader.
* SRM static analysis on FLS and T12: frame + skin analysis, buckling, orbital and lateral junction.
* SRM stress team management (6 engineers): training, scheduling of work, check of analysis, meeting of WIP with Airbus and Claims.
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Latecoere
- Ingénieur calcul porte A380
Toulouse
2008 - 2009
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Latécoère
- Stress engineer
Toulouse
2007 - 2008
, A380 PAX Doors (LATECOERE)
: certification dossier + SRM dossier
* Static door structure analysis: buckling, super stiffener
* Focal point between Latecoere and the team working to update the analysis and the dossier.
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ALEMA CONCEPT
- Stress engineer
2006 - 2007
* Nose fuselage lateral panel: buckling of panel, super stiffeners analysis, junction analysis (Assist tools)
* ACSA tools use: PSN15, PSN3, PSN4 and PSN13 for tensor extraction.
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Latécoère
- Stress engineer
Toulouse
2006 - 2006
Dassault Falcon 7X (LATECOERE)
: certification dossier
* Aeronautical structure static sizing methods learning: Bruhn, Niu, Dassault methods
* F7X T5: buckling of all panels (junction, upper and lateral), super stiffeners analysis and junction analysis.
