Dipl.-Ing. Vincenzo Fabio Di Giacomo

Preventive Quality Manager for Exteriors, Composite, Body in White and Chassis from the concept to the pre-series phase. Deep knowledge of 5S, 9S, 8D, APQP, PPAP, FMEA, FMECA, SPC processes, IATF16949 standards and VDA from 1 to 6 Guidelines. Applying Lean Methods such as LPPD, Six Sigma, Kaizen, Ishikawa, Pareto, Poka Yoke. Audi Akademie Certifications Acquired: QPN Integral Methode, Two Day Production Acceptance, AVON Training Approver, TEVON 3 Qaulitätssicherung Grundlagen

Responsible to manage the complete composite product development during the stages of Laboratory testing (characterisation and validation), Engineering, Simulation and Manufacturing, checking the compliance of the Quality and the Materials within the VW Group /Laboratory Responsibilities / Engineering Responsibilities / Manufacturing Responsibilities / VW Group Responsibilities / Quality Responsibilities

ACRC Simulation Team Leader. Technical management of the external subcontractor for FE analysis work packages. Planning and Timeline. Static and Dynamic Stress Analysis for Composite and Prototype Parts, Fatigue & Damage Tolerance, Analysis of Full Vehicle Crash Results. Component Testing, Laminate prediction, Layup definition, drapeability analysis, Springback prediction. Structural optimization for manufacturing activities such as PrePreg, Out of Clave, Press Moulding, RTM, Forged Composite.

Technical Manager: Team Management, Technical Evaluations. Fatigue&DT Lead on A380-800 Batch1, Batch2 and Batch 3 Passengers Doors. SAFE Crack Propagation Analysis. Fatigue and Damage Tolerance. Stress Analysis. Hand-calculations according to HSB. Interface Loads Analysis. Fatigue Reports final check. Clean Sky JTI (Joint Technology Initiative) CoP Technical Director Main Project: “Advanced, high aspect ratio Transonic Laminar Wing for Regional Aircraft with Load Control & Alleviation devices"

Task Coordination and Stress Analysis on, Primary Structure, Lining Scaffolding Secondary Structure and Integrated Composite Structure of Airbus A400M. Hand-calculations according to HSB. Modal Analysis. Fatigue and Damage Tolerance. Interface Loads Analysis. Stress Reports. Interface Loads Reports. Decision Reports. Feasibility Studies

FEM Analysis to solve fatigue and damage tolerance issue on integrated primary structure: main frame, main landing gear support and windshield surrounding of new PIAGGIO P1XX business jet.

Aerospace Structures, Aerodynamics, Flight Mechanics, Aircraft Systems