Ingeniero de calculo

Successfully developed analysis tools for Pylons of the RR Lucia project; This involved developing scripts for
sizing and validating the components using data analysis, hand calculations and FEA.
• Hand calculation of RF and MS for composite strength.
• Hand Calculation of RF and MS for fasteners of the Inner Pylon Fairing Assemblies.
• Mitigation of low RF.

Initiated and led the re-work data analysis substantiation of Reserve Factors and Margins of Safety of Ailerons
and Winglets of Airbus A220 and Bombardier Global 7000 aircrafts.
• Hand calculation of RF and MS for composite strength with the Hashin Criteria.
• Hand Calculation of RF and MS for Bearing Bypass of fasteners.
• Hand Calculation of RF and MS for laminate strength for Large Damage Capability.
• Mitigation of low MS.
• Wrote-up stress report updates and concession reports.
• Served as a thoughtful advisor, working with Engineers and Managers professionals.

Successfully developed Cargo Bay structures for Airbus A319/A320/A321; using data analysis, hand calculations
and finite element analysis (FEA).
• Conducted Static Analysis checks on the forward and aft cargo compartments to support modification
approvals.
• Conducted Structural Optimization (Size, Topology & Topography) of metallic fittings and tension clips.
• Reviewed Damage Tolerance of metallic components on the Cargo Loading Systems Covers.
• Wrote-up of technical documents (Design, Stress Reports, Aircraft Manual Supplements and Test Plans).

Successfully analysed aircraft interior structures such as galleys and storage compartments for Airbus A350;
using data analysis, hand calculations and finite element analysis.
• Performed Static analysis checks on metallic fittings, floor structure and composite panels to support
certification.
• Ran Structural Optimization (Size, Topology & Topography) of metallic fittings for weight reduction.
• Created technical documents (Interface Load Reports, Static Test Plans, Static Load Reports and
Qualification Substantiation Reports).
• Produced stress analysis methods for material, components and assemblies in Mathcad and Excel.
• Automated result extraction for determining RF and MS of composite and metallic components.
• Worked to improve analytical tools with Python, VBA and Mathcad scripts for the analysis of material,
components and assemblies.
• Witnessed static tests of galleys and monuments.

Successfully developed analysis tools for ailerons and flaps of the Bombardier CSeries (CS100) aircraft; This
involved developing a script to validate the components following the strict authority regulations using data
analysis, hand calculations and FEA.
• Conducted Static and fatigue analysis of different flap locations.
• Generated detailed sub-models to complement and validate the FEA and capture localised yielding and
load distribution.
• Performed metallic and composite joint analyses (bearing bypass, pull through and shear-tension) on
fasteners of flaps and ailerons. This task significantly reduced analysis time and helped the client make
decisions based on findings.
• Generated VBA and Patran PCL scripts to automate DFEM result extraction for the stress analyses,
obtaining margins of safety for the joints between skins/ribs/spars/brackets.
• Mitigated low margins using Bombardier methodologies and design manuals.
• Elaborated stress dossiers to support aircraft certification.
• Successfully carried out a detailed investigation to assess the impact of failure of fasteners in critical
locations with FEM and hand calculations.

Research and development of Composite Joints (this included manufacturing and testing of coupons).

Research and development of manufacturing technologies, my final project focused on composite materials.

Studies in Industrial Engineering.