Aerospace / Automotive Engineering:Research and Development in Advanced Composite Materials and the New Technologies. Support to prototype realization and testing in Advanced Composite Materials. Health monitoring in real time with embedded sensors. Multiphysics simulations and support in CAD / FEM / CAM.Civil Engineering:Advanced Composite Materials for heat shield and passive firefighting protection for buildings.Dynamic Fire Simulation for Structures. Heat transmittance evaluations for buildings.No-invasive methods to identify troubles and failures in pipings. Solar panels applications. Follow our LinkedIn page:https://www.linkedin.com/company/ares-engineering-solutions/#aresengineeringTo collaborate in projects or for simple curiousity, You can join our group:https://www.linkedin.com/groups/4062429/

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In Diehl Aviation I worked on all Airbus programs: from the Single Aisle and Long Range to the A350 and A380 families, supporting the improvement of JCRs in the cabin interiors panels. The task was to validate the FEM results with tests considering the weight limit for the parts in Composite Materials. Stress Reports, Similarity Statements, Test Reports and Technical Documentations were my daily workload as well as calculation with Hypermesh, Nastran and Optistruct. The weight was recorded in Teamcenter/SAP and calculated with macros starting from the DWGs and CAD models. In this experience I got the certification in Teamcenter and in Optistruct.

Focal Point Stress for MAP Team A350 XWB Pax Doors.I supported stress analysis for Type Certification Report of passenger doors structures, FEM investigations for structure improvements, in metal and Composite Materials parts. I supported test validation of FE Models and I worked on Quality Notes and Concessions from the manufacturing for composite parts and structures assemblies to create an Techical Repair Manual for international Suppliers.

I supported the new car development with CAD parametric models to help the homologation process for all type of vehicle since the very beginning stages.I worked on CAD DMU for theassembly overview of Gallardo, Aventador and Huracan CAD models.I was delighted to support the prototypes realization.

To improove the RTM technology, I worked on two projects to realize advanced composite materials structures for aerospace applications. The first one was called Firb for Alenia Aermacchi, in this project I performed linear and non linear static FEM analysis to verify the structural integrity and to optimize thickness of a Beam, that enables the Trust Reverser movement of an Airbus A380 engine. The target was to realize that Beam in composite materials instead of metal. The second project was called Meta for Alenia Aeronautica.Meta's task was to realize an advanced composite materials structure able to accomplish simultaneously to mechanical, electrical, thermal and acoustic requirements.In this project I performed FEM analysis and I molded experimental panels with the RTM technology to be tested in laboratory, in compliance with the ASTM requirements, to verify all the project aims.

As an Aerospace Designer / Structure Analyst Engineer for the Department of Aerospace and Astronautic Engineering of University "La Sapienza" in Rome, I worked on two projects called "Prin" and "Macmes" (for CIRA) either with the purpose to build up an aeronautical panel in advanced composite materials with embedded sensors inside to monitoring the structure health in real time. In those projects I defined a specimens geometry with CAD software and I studyed FEM analysis of the specimens behaviour. In compliance with ASTM requirements those specimens were tested in order to validate the target properties and to proceed to the realization of the aeronautical panels.Previously I worked on project Elimat for AgustaWestland. The purpose was to improve the RTM technology to mold a AW139 helicopter component. To achieve the target, different steps were followed: drawing the mold with CAD software, simulating the component behaviour with FEM software knowing its loads and constraints, and simulating the injection process of the resin into the mold designed before. At the same time, experimental tests were executed in the University laboratories to proceed in the realization of the mold, at first, and the component, later on.During the Master period, I also worked on the project Flecs for Thales Alenia Space in Turin, Italy. My tasks were to verify the safety coefficients of a space structure by using FEM software like Nastran and to find critical points for stress or strains values. I personally presented those results at the Flecs Progress Meeting 5th at the ASI site in Rome, Italy.

My main activities and responsibilities as an analyst engineer were: writing aircraft Business Plan, compiling Technical Status Report to evaluate the aircraft maintenance status and verifing the concerning Log Books, getting through to the worldwide brokers and answering to clients’ request about our aircraft, checking the aircraft compliance with EASA / JAR OPS 1 requirements, finding the optimum market solution for our client, writing the Aircraft Purchase Agreement and compiling all the documentation for the Authorities as ENAC, CAA, LBA or for the Embassies in the international transactions.