Valentin Stefan Voinea

Conceptual Design, Space allocation method and Detail design for VIP Conversion of the COMAC ARJ21-700 (Catia V5 and TeamCenter) Concept definition of the VIP Area (VIP Seats & Tables) taking in account the specific certification requirements (anthropomorphic data, head strike data, seat kinematics, structural provision) Concept definition of the O2 masks location for the VIP configuration taking in account the specific certification requirements (in view/in reach definition, structural provision)

Dassault F5X – Conceptual Design and design check for composite and metallic primary structure of the Tail Empennage (Horizontal Stabilizer, Vertical Tail Plane, Elevators and Rudder (Model Based Design CATIA V6 -V5 (Model Based Design, CPD CPM,FTA, ENOVIA V6 PDM) Gulfstream G650- Design and design check for composite and metallic primary structure of the Tail Empennage (Horizontal Stabilizer, Vertical Tail Plane, Elevators and Rudder)-Model Based Design CATIA V5,FiberSim, FTA, Smarteam PDM)

A350 XWB- Pax Door Surrounding- Design of the composite, metalic and thermoplastic parts of the primary and secondary structure for the PAX Door Surrounding Structure using Catia V5 R18 (CPD –GRID method ,Aerospace Sheet Metal Design, PDM Link and Global VPM)

Camera Installation on the A320- Design (Catia V5 R18) MMA P8-A Tank Design (Military Project)- Catia V5 R18 and SmarTeam PDM BBJ-737-800 Catia V5 Application Support and Methodology VVIP Interior design - Design and Substantiation Report for cabinets and lavatories Boeing 777 Auxiliary Fuel Tank Design CatiaV5 R17 Boeing 777 Auxiliary Fuel Tank Fatigue (Nastran-Patran)

Airbus A350 Fuselage Design Optimization (Glare Skin and Glare Stringers) using Nastran-Patran and Issy. Frame-Stringer Design Automation using Catia V5 R16 and Microsoft Visual Basic, CATScript and KBE (Knowledge Based Engineering)

Airbus A400M- Design for SONACA-BELGIUM- Design of FIXED LEADING EDGE (CATIA V5-R14 and Enovia VPM) Design Principles – Preliminary design Phase 3D Models – Design 3D Models respecting SONACA and AIRBUS procedure documents, rules DMU manufacturing, and clash detection, standards and catalogue, Master Geometry. (Girders, Rear Baffle and Front Baffle) 3D Composite (External envelope of panel, Honeycomb, Ply for each 3D composite model) in accordance with materials, ply repartition and limitation.

Airbus A330-A340 DMU-Design (CATIA V5-R11)-(ATA53-Primary and secondary Structure Design) ATA 53 – Frames, Stringers, Brackets, Seat rail, Cross Beams, Frames Coupling, Stringer Coupling, ATA 25 - Interior design (Window Panel, Door Frame Lining, Angle, Door Frame Panel)