Aerospace Design Engineer

HIGHLIGHTS •Excellent knowledge of Airframe Structures Design, and Systems Integration •11 years experience as a Design Engineer •Specialization in Composite Structures Design and Optimization (Catia v5, MSC.Nastran/Patran/Laminate Modeller, FiberSIM ) EDUCATION •Master Degree “Engineer, Avia - Helicopter Department, Mechanical Engineer” Moscow Aviation Institute MAI, Moscow Russia (2000, Design of Airframe Structures) COURSES •Composite Basic and Advance FiberSim Course by VISTAGY - VISTAGY certificate •Composite Aircraft Structures Engineering Course - Boeing certificate •Composite Structures Course (BDC, Moscow) •MSC.Laminate Modeler (PAT 325) - MSC certificate •MSC.Nastran “Analysis of Composite Materials” (NAS 113) - MSC certificate •GD&T Training (Boeing, Everett) •Release Process Course (Boeing, Everett) PROFESSIONAL EXPERIENCE •BOMBARDIER “Learjet 85” – Black Diamond (November 2009 – present) Wichita, KS -Baggage Bay structures -Pylon structures •BOEING – CTSinternational (April 2008 – April 2009) Everett, WA -787-9 Aft Wheel Well Bulkhead concepts Sec-45 -787-9 Side Fitting and Lower Chords Sec-45 •Airbus - ECAR (January 2007 – March 2008) Moscow, RUSSIA -A330-200 GMF Sec-16 -A320 Composite Multispar Flap (RTM technology investigation) •BOEING – Progresstech (April 2002 – January 2007) Moscow, RUSSIA -747-8 Composite Leading Edge -787-8 Composite Leading Edge -787-8 Window Frames -7E7 Pre-Prod Fuselage Barrel Test -7E7 One Piece Barrel Development Test -777 AFIT 200LR Sec-44 -777 wing 200LR -747 ENG AFIT-PCIP-STA520 -747 PCIP bulk cargo floor -747 XQLR Sec-48 Bulkheads •TSAGI – MAI post graduation (June 2001 – May 2003) Zhukovskiy, RUSSIA -Tu-324 Flap (stress analysis & optimization composite structures MSC.Nastran/Patran) •Tupolev (September 1999 – March 2002) Moscow, RUSSIA -Tu-214 aft fuselage modification for new Aft Engine -A3XX fuel tanks location & wing spars Work Details: -Materials: Composite, Titanium and Aluminum structures. -Processes: Composite “prepreg lay-up” and RTM, milling, chemic-milling, sheet metal and extruding. -Parts: Aircraft sections (frames, skins, stringers, beams, window frames, fittings, clips and others), Flaps & Leading Edges (skins, ribs, spars), Pylon, Interiors (floor & sidewall panels). -Design: Lay-outs, details, assemblies, FT&A (3D annotations), drawings. -Stress: analyze and optimization using Catia v5 & MSC.Patran/Nastran (no hand calculation). Static Load cases. COMPUTER SKILLS •CATIA V5, ENOVIA (Boeing, Airbus, Bombardier) 12.000 hours - Part Design - Generative Shape & Advance Surface Design - FiberSim (composite module by VISTAGY corp.) - Sheet metal - Drawing - Assembly - GD&T and 3D annotation - MBD (Model Base Definition) •CATIA V4 (Boeing) 4.000 hours - Part Design - Advance Surface Design - Generative Aerospace Sheet-Metal - Drawing - CATIA Finite Elements Structure Analysis (Elfini) •MSC.Nastran\Patran (Airbus, TSAGI-Moscow post graduate) 4.000 hours - Mesh modeling - Composite parts (PCOMP cards & Laminate Modeler) - SOL101 Linear static - SOL103 Normal modes - SOL105 Buckling - SOL200 Composite optimization (Weight minimization, DESVAR, DRESP, DCONSTR…) •Pro\Engineer, CADDS 5 (Tupolev, Moscow) 2.500 hours - Part Design - Surface Design •WINDOWS - MS Office and others. Basics of UNIX.

Aerospace Engineer

Wichita, KS