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CHECKAERO
- Stress engineer (self employed)
2014 - maintenant
Checker for AIRBUS: certification stress reports, excel sheets, FEM: A320, A340, A400M SRM
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SOGECLAIR AEROSPACE (91 Courtaboeuf)
- Stress engineer (self employed)
2011 - 2014
Structural analysis of engine pylon AIRBUS A320 Neo project. Placed in AIRBUS (Toulouse, France).
.Static calculations of attachments and pylon primary structure using Airbus France soft (ASSIST, ISAMI, Patran/Nastran).
.Preliminary and certification analysis on various technical options for primary structure.
.Technical support for internal team.
.In charge of following secondary structure final certification reports (work subcontracted in Spain).
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AEROLIA - Toulouse France - Sacheon South Korea
- Stress engineer (self employed)
2010 - 2011
Structural analysis of AIRBUS A350 Nose Landing Gear Box project. Placed in AIRBUS (Toulouse, France).
.Static calculations of Roof Panel, Gantries, and various fitting using Airbus France soft (PSN, ASSIST, ISAMI).
.Preparation for static test.
.Technical assistance, placed in KAI (Sacheon , South Korea, 3 months).
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Jet Aviation (switzerland)
- Stress engineer (self employed)
2008 - 2010
Completion analysis of AIRBUS A340-600 / A330 / A319, BOEING B737 / B747 projects.
.Following and checking sub-contractor reports or technical work.
.Primary structure modification and static calculation using FEMAP/NASTRAN.
Linkman for all projects dedicated to BASE 2000 (Irish company based in Belfast).
Analysis reports, drawings: check and release.
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MARSHALL AEROSPACE (England)
- Stress engineer (self employed)
2007 - 2008
Structural analysis of BOEING MMA 737 tank refuelling system.
.Pipes Finite Element Model: using PATRAN/NASTRAN
.Static calculations of pipes and various system structures: valve, pipes, junctions.
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GED (England)
- Stress engineer (self employed)
2006 - 2007
Fatigue analysis of AIRBUS A340 500-600.
.Fatigue calculations of wings (Rear and front spar, top and bottom skin), using Airbus UK fatigue soft (DAMTOL).
.Certification stress reports for final certification.
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Placed in AIRBUS
- Stress engineer (for GECI)
2004 - 2006
GECI (Specialist in aeronautic structures) - Toulouse, Rochefort, Paris France - Charleroi Belgium
Structural analysis of AIRBUS A380 PAX. Placed in AIRBUS (Toulouse, France).
.Static calculations of central orbital junction (at frame 74), using Airbus France soft (PSN, ASSIT).
.Certification stress reports for final certification.
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placed in SOGERMA
- Stress engineer (for GECI)
2003 - 2004
Preliminary stress calculation and meshing of A400M ramp door. Placed in SOGERMA (Rochefort, France).
.Toes Finite Element Model: using PATRAN/NASTRAN
.Static calculations of toes structure: webs, frames, axis.
.Stress analysis reports for submission to Preliminary Design Review.
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Placed in Dassault Aviation
- Stress engineer (for GECI)
2001 - 2003
Preliminary stress calculation and meshing of FALCON F7X back fuselage. Placed in DASSAULT (Paris, France).
.Finite Element Model: weight integration using CATIA
.Static calculations of fuselage structure and stub: webs, frame fittings, hinges.
.Stress analysis reports for submission to Preliminary Design Review and Certification Design Review.
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Placed in SONACA
- Stress engineer (for GECI)
2000 - 2001
Structural analysis of AIRBUS A340 600: slats. Placed in SONACA (Charleroi, Belgium)
.Static calculations of slats structure including training edge, skins, track ribs, using Sonaca's softs.
.Certification stress reports for final certification.
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REALIX (Scientific Engineering) - Toulouse France - San Jose dos Campos (Brazil)
- Stress engineer
1999 - 2000
Preliminary stress calculation of EMBRAER 170: Cargo doors. Placed in LATECOERE (Toulouse France) and EMBRAER (Brazil)
.Finite Element Model: creation and interpretation of aft cargo door using PATRAN/NASTRAN.
.Static hand calculations of door structure including hinge, frames, stringers, skins.
.Stress analysis reports for submission to Preliminary Design Review.
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ASSYSTEM ETUDES
- Stress engineer
Courbevoie
1998 - 1999
ASSYSTEM ETUDES (Specialist in aeronautic structures) -
.Structural analysis: Rear Center Tank AIRBUS A340 500: skin-stringer panel and panels.
.Preliminary stress calculation of Lower Deck Facilities AIRBUS A340 600.Placed in AIRBUS (Toulouse France)
.fuselage skin-stringer panels, floor structure, joint analysis.
.Preliminary stress report preparation leading up to final certification.
