Łukasz Szczypiń

GE Aviation Systems

-Confidently undertaking aircraft stress calculations, and produce clear, concise reports and other documentation, of appropriate quality.
-Performing static stress calculations of aircraft structures using a range of standard hand calculation and finite element methods utilising PATRAN, HyperMesh and NASTRAN to assess design solutions for a whole range of tasks ranging from concept design through to detailed design drawings.
-Performing fatigue and damage tolerance analysis when required
-Assist in the Structural design process to help ensure optimised design quality

GE Aviation Systems

-Designing aircraft metallics or high-tech composites structures ( Carbon fibre reinforced epoxy polymers – in autoclave processing,monolithic and sandwich structures)
Preparing 3D models (CATIA), composite lay-ups (FiberSIM), Drawings in accordance with ASME Y14.5-2009.
-Definig assembly and repair technology.
-Preparing tolerances analysis for large assemblies using statistical tools.
-Preparing and presenting technical data to internal and external customers
-Documenting and communicating results of technical data generated
-Developing and sharing CATIA custom-made tools ad scripts among worldwide design teams.