Guilhem MARTEAU
Stress Lead at PFW Aerospace GmbH- Claim this Profile
Click to upgrade to our gold package
for the full feature experience.
-
English -
Topline Score
Bio
Credentials
-
Stress Specialist
AP1020
Experience
-
PFW Aerospace GmbH
-
Germany
-
Aviation and Aerospace Component Manufacturing
-
200 - 300 Employee
-
Stress Lead
-
Jan 2022 - Present
Stress Lead on A220 High Pressure Ducting Systems
-
-
Stress Lead Engineer
-
Apr 2018 - Present
A350XWB-900 et A350XWB-1000 Fuselage BASI (Fuselage Bleed Air System Integration) ATA 36 et ATA 21-60. - Focal on Stress activities - Concession (Task 300 and 400) - Production Support - Test Qualification Support - Certification Post Mod -900 and -1000
-
-
-
-
Focal Stress Engineer
-
Jan 2014 - Mar 2018
A350XWB-900 et A350XWB-1000 Fuselage BASI (Fuselage Bleed Air System Integration) ATA 36 et ATA 21-60. - Focal on Stress activities - Concession (Task 300 and 400) - Production Support - Test Qualification Support - Certification -900 and -1000 A350XWB-900 et A350XWB-1000 Fuselage BASI (Fuselage Bleed Air System Integration) ATA 36 et ATA 21-60. - Focal on Stress activities - Concession (Task 300 and 400) - Production Support - Test Qualification Support - Certification -900 and -1000
-
-
-
PFW Aerospace GmbH
-
Germany
-
Aviation and Aerospace Component Manufacturing
-
200 - 300 Employee
-
Stress Engineer
-
Sep 2010 - Dec 2013
A350 XWB Fuselage BASI (Fuselage Bleed Air System Integration). System installation of the BLEED and TRIM pneumatic system and FUEL system for A350.· - FEM construction 1D and 2D (PATRAN/NASTRAN)· - Static (Linear and Non-Linear), Buckling and Fatigue (Endurance and Windmilling) analysis· - Aircraft Deflection analysis· - Air Systems studies (Pressure and Temperature analysis) - Hand Calculations (AIRBUS Static and Fatigue Methodologies, MTS, Niu)· - Drawing check - Concession - Production Support - Test Qualification Support - Stress Report writing
-
-
-
-
Stress Engineer
-
Apr 2010 - Sep 2010
Graduation Project : “Study of influence due to damage tolerance for the laminated composite fuselage A350”· - Parametric FEM construction (2D and 3D) of a composite stiffened panel inserted in DFEM composite fuselage A350 (SAMCEF). - Buckling analysis Graduation Project : “Study of influence due to damage tolerance for the laminated composite fuselage A350”· - Parametric FEM construction (2D and 3D) of a composite stiffened panel inserted in DFEM composite fuselage A350 (SAMCEF). - Buckling analysis
-
-
-
-
Stress Engineer (Internship)
-
Jun 2009 - Sep 2009
Project : “Weight Optimization of Laminated Composites under Buckling”· Project : “Weight Optimization of Laminated Composites under Buckling”·
-
-
Education
-
ISMANS CESI
Engineer's degree (Master 2), Stress analysis (Linear, Non-Linear), Structure optimisation, -
CPGE Joffre
Bac +2, Études générales