Robert Irick Email & Phone Number

Bethesda, Md, Us

F-35

St Charles, Missouri, Us

Bell Helicopter V280Bombardier L85, Global ExpressHonda Jet: HA-420Lockheed Martin: F-35 Joint Strike FighterTriumph/Vought: Boeing 787- DreamlinerGulfstream: 650Triumph Aerostructures: Bombardier Global: Montreal, Canada. Weight Savings Team. Responsible for Layout and Redesign of Wing Structure for Weight Savings. Prepared reports identifying structure for weight savings estimates. Conceptual layouts for Trailing Edge, Flap Spars, and Flap Structure. Catia V5, ENOVIA. Bell Helicopter/Spirit: V280 Valor: Responsible for Layout and design of Fuselage and Cockpit primary structure, including bulkheads, keels, floor beams, and Frames. Prepared MBD for release using Catia V6, ENOVIA. Honda Jet: HA-420: Weight reduction program. Responsible for layout and redesign of Wing Front Spar for weight reduction. Layout, design, and release completed with CATIAV5 and PDM Teamcenter.Lockheed Martin: F-35 Joint Strike Fighter: Forward Fuselage. Responsible for Engineering Design Changes for Forward Fuselage. Incorporated AEA & CR changes on Details, Assembly/INSTL Drawings. Released Engineering RERC Package in PDM Teamcenter in CATIA V4 & V5.Vought: Boeing 787- Dreamliner: Vought - Weight Improvement Program. Responsible for layout and Redesign of Section 47 Frames and Shear Ties for Weight Reduction. Composite parts modeled in CATIA V5 with Knowledge Based Engineering Applications. Prepared and Released Assemblies (ARM) for Section 47. Released in ENOVIA data manager.Gulfstream: 650: Spirit – Responsible for layout & design of Wing Flap Leading Edge, Trailing Edge Skins, and Access Doors. Modeled in Catia V5, and Release in ENOVIA.

San Diego, California, Us

Bombardier L85SMI/TriumphResponsible for the stress analysis for Fuselage Frames, intercostals, backup fittings, and Brackets/Clips. Prepared stress reports, SCN's to support production release. Completed FEM Surveys, Free Body Surveys with Slim/Vision, Patran.

Bethesda, Md, Us

F-35 Joint Strike FighterF-16 Fighting FalconT-50 KAI Golden EagleF-22 RaptorF-35 Joint Strike Fighter: Responsible for layout & design of bulkheads for the Forward Fuselage. Released Build-to-Package (BTP) reduced dimension drawings with CATIA V4/V5. Proficient with PDM-TeamCenter. Layout, design, and release completed with CATIAV4 & CATIAV5. F-16 Fighting Falcon-Tactical Aircraft Program. Responsible for the layout/design of the Peace Marble II conformal dorsal & fuel tank configuration. Prepared and Released UAE Systems PAO tubing and systems Drawings using CATIA V4.1.9.T-50 International Aircraft Program: Worked onsite in Sachon, South Korea; Technical Advisor for the layout, design and drawing release of Fuselage Bulkheads, and Wing Attachment Carry-Thru Bulkheads for the Center Fuselage with Korean Aerospace. F-22 Raptor- Tactical Aircraft Program: Responsible for modifications of the Bulkhead/Skin Panel interface resulting from tolerance stack-up interference. Layout/design completed through CATIA V4.1.9 parametric design.

Fort Worth, Texas, Us

Armed Reconnaissance Helicopter- XworkXV-22 Osprey Military Tiltrotor Program- XworkXAH-1Z Cobra Military HelicopterArmed Reconnaissance Helicopter- XworkX: Responsible for preparing Mock-Up and Modification drawings for the Bell 206 Helicopter airframe to accommodate new structure including weapons pylon, FLIR, and instrument panel. V-22 Osprey Military Tiltrotor Program- XworkX: Responsible for the modification & design of the V-22 Trainer Wing and Nacelle Structure. Prepared Layout, Design, and Modification Drawings with CATIA 4.1.9. AH-1Z Cobra Military Helicopter Modifications Program: Responsible for the design of Composite Panels, and Engine Deck Structure to accommodate extended fuselage & increased loads. Layout, Design, and Release completed though Unigraphics V15/IMAN parametric design.

Falls Church, Va, Us

NASA/FAA Air Traffic Software: Development of adaptation software to generate complex algorithms to predict trajectories, spacing and sequencing of air traffic for DFW Airport. Responsible for the development, debugging, testing, & releasing of new software solutions by using C/C++ with UNIX Solaris 1.2, Clearcase.

Arlington, Va, Us

737-X 767-400ER747-400X737-X - Main Cargo Door:. Responsible for the initial design of the fuselage frames, intercostals, and cam-latch fittings. Catia V4.1.9 parametric design. Production parts released using Catia.767-400ER - Wing Box/Major Fittings:. Responsible for the initial design and modeling of the drag brace fitting, flap back-up fittings, forgings and Major Fittings of the wing box, using CATIA V4.1.9 computer and parametric design.

MD-XXMD-11747-400X Special Field Assignment: - Industry assist for initial design of the wing, skin panels and stringers. Responsible for the design/modeling of detailed parts of the using Catia V4.1.8 computer & parametric design.MD-XX: Conceptual design for the wing: Responsible for the initial design of primary structure of the trap panel, center wing box, front & rear spar layout drawings utilizing Unigraphics V11 parametric design.MD-11: - Composite Structure Design of flap hinge fairing. Design includes preliminary composite analysis; symmetric ply lay-up; layer orientation; tapered splicing of sections. Layout/drawing released in IMAN.

Bachelor Of Science (B.S.), Mechanical Engineering

Master Of Science (M.S.), Mechanical Engineering