+ Leonardo S.P.A. Helicopters Division (Cascina Costa)REACH Regulation ▪ Predisposizione di flussi interni e relative procedure per la gestione sistematica delle prescrizioni REACH/SCIP ▪ Verifica/Controllo dell’applicazione delle necessarie azioni e rispetto delle relative deadline a carico delle singole funzioni aziendali: - Verifica degli obblighi di registrazione delle sostanze in quanto tali o in quanto contenute in miscele (Titolo II del regolamento REACH) - Verifica degli obblighi di autorizzazione (Titolo VII del regolamento REACH) - Verifica degli obblighi di restrizione anche in relazione con obblighi di etichettatura e imballaggio per prodotti destinati ad uso professionale/industriale (Titolo VIII del regolamento REACH) - Verifica degli obblighi di notifica delle sostanze contenute in articoli (Titolo II del regolamento REACH) - Verifica della comunicazione all’interno della catena di approvvigionamento (Titolo IV del regolamento REACH) - Verifica della conformità delle (e)SDS (articolo 31 ed allegato II del regolamento REACH) - Verifica dell’obbligo di redigere la relazione sulla sicurezza chimica e dell’obbligo di applicare e raccomandare misure di gestione dei rischi (Titolo II e Titolo V del regolamento REACH) - Verifica della conformità con gli obblighi di conservazione delle informazioni (articolo 36 del regolamento REACH)

+Leonardo S.P.A (Venegono(VA))Stress & fatigue analysis primary structure:Structural analysis, Fatigue, Static FEM, Buckling, hand calculations on M346 wing box .

+Leonardo S.P.A ,Italy (Pomigliano(Na)):ATR New Air Management System: -Structural analysis on primary and secondary structures due to the strengthening of ACU, VCS, ECS, conditioning pack for ATR 42/72.Preliminary structural analysis and drawing approval.Preparation and checking of reports related to structural analysis.

+Composite generator tool. -Develop a tool that automatically allows the transformation from a metal component to the corresponding composite component.Transformation from to metal to the composite is performed through an optimization processing.Metall structure analysis is performed with classical theory.Composite structure analysis is performed with classical theory of laminate (CLT).The lamination criterion for the optimization processing has been considered.The numerical implementation and graphic interface has been performed by “ Python 3.5”

+ MBDA, Italy (Fusaro (Na)) :Industrialization and validation of production line:-Industrialization and validation line:-Team support industrialization and validation of production line.-Development activities of improvement plans and technical support to the lines integration and test antenna.-Technical support activities with the aim of manage the process of Non-Conformance.-Definition of any plans for improvement based on the analyzed data.-Issuing periodic reports on the production line status.-Participation in regular meetings for sharing of data processed by the business bodies.-Document management with Teamcenter platform and SAP.

+ Alenia S.P.A, Italy (Pomigliano(Na)):Modelization and simulation of Horizontal Multispar Box. Stress analysis:Structural analysis & certification on primary structure of Bombardier C-Series Horizontal & Vertical tail:-Fatigue-Static FEM-Buckling-Hand calculations-Determination of the margins of safety performing the necessary FEM(Nastran) calculations and producing documentation.

+ Alenia S.P.A,Italy (Pomigliano(Na)):Modelization and simulation of Horizontal Tail Tip. Stress and fatigue analysis.Structural analysis & certification on primary structure of Bombardier C-Series Horizontal & Vertical tail:-Fatigue-Static FEM-Buckling-Hand calculations-Determination of the margins of safety performing the necessary FEM(Nastran) calculations and producing documentation.

+ Alenia S.P.A, Italy (Pomigliano(Na)):Static and Buckling analysis of an innovative spar assembly loaded as a cantilever beam. Test setup and evaluation of critical condition and producing documentation.

+Numerical Analysis for Crashworthiness of composite fuselage with MSC Nastran SOL 700:-Construction of special lay up of composite material. -Use of failure criteria Tsai Wu and Chang Chang. -Study on the numerical stability with the central difference method. -Use of Contact algorithms Penalty method, Kinematic constrain, Distributed parameter . -Analysis of passive safety and standard criteria.+Structural topological optimization methodologies for the preliminary design of a wing for a new generation of regional aircraft (ANSYS;modeFRONTIER)

AIRBUS, France(Saint Nazaire):+Structural analysis on fuselage of civil transport aircraft Airbus A380: -Non-conformance (concessions). Static and Fatigue analysis to verify the structural capability.-Non-conformance (concessions). Static and Fatigue analysis to assure the integrity of the structure. -Stress support to the structural repair manual of the A380 fuselage defining the most critical damages and areas, designing the most adequate repairs together with the design team and calculate the repairs in order to assure the integrity of the component after being repaired. -Check the stress and fatigue requirements and produce the corresponding documentation.

+Pilot floor, Cockpit emergency floor, Front doors, Avionic Door of civil transport aircraft Bombardier C-Series:-Structural analysis. Fatigue, static FEM, buckling, with MSC Nastran. -Stress reporting. -FEM modeling and hand calculations of the pilot floor, cockpit emergency floor, front doors, the primary structure of the forward fuselage and Avionic Door.-Reduce the weight of the structure members, keeping the required stiffness.-Support the design team in the definition process of the new solutions for the structure.

+ Alenia Aeronautica, Italy (Pomigliano(Na)):Final internship for the Master degree:-Numerical Analysis for Crashworthiness of composite fuselage with MSC Nastran SOL 700.-Construction of special lay up of composite material. Use of failure criteria Tsai Wu and Chang Chang. -Study on the numerical stability with the central difference method. Use of Contact algorithms Penalty method, Kinematic constrain, Distributed parameter . -Analysis of passive safety and standard criteria.

+ Alenia Aeronautica, Italy (Pomigliano(Na)):Final internship for the Bachelor degree,Stress static and Buckling Analysis on A380 fuselage panels welded with Laser Beam Welding:-Fem analysis with Msc Nastran SOL 101, 105. -Analytical calculation with theory of column buckling.-Use of light alloys weldable. -Applications of laser beam welding.