Jean-Gabriel Trudeau, CPI, M. Eng

• Design, GD&T, CAD and assembly drawings of tooling for composite parts with CATIA V5. • Design of rapid prototyping stereolithography molds of injection parts. • Stress analysis of composite parts using Abaqus. • Redaction of stress test plans and test reports for composite parts.

• Revision and modification of the manufacturing instructions of a prototype composite part for the aerospace industry. • Process optimization for reducing manufacturing cycle time of a structural composite part. • Redaction of traceability and analysis documentation. • Design of a prototype molding technology for composite parts, which included detail, assembly and welding drawings with CATIA. • Purchase orders and follow ups with suppliers to deliver components within schedule and requirements.

• R&D of stiffened, composite panels post buckling methodology for the CSeries aft fuselage. • Interpretation of non-linear analysis results. (Patran / Nastran) • Conservatism verification of the approach. • Integration of methodology to the stress tools.

• Creation and modification of detail drawings for flight test and production aircrafts. • Verification of the position of plies layered by an AFP machine for the aft fuse. • Conception of fittings for an avionic rack. • Rework and optimisation of the passenger, service and cargo door doublers.

• FEM analysis of the effect of curvature of composite panels on buckling behavior. • Modification of VBA tool to integrate methodology. • Elaboration of a test plan to calibrate an ultrasonic C-Scan with porous composite coupons.