Engineer Engineering

Education

Master of Science in Aerospace Engineering (2005)

Bachelor of Computer Science (2003)

Summary

Proficient in Static, Fatigue and Damage Tolerance analysis including FEM (finite element modeling) of primary and secondary structure for commuter and transport category aircraft structure.

Engineering Software: FEM (finite element modeling): Patran, Femap, Nastran (MSC.Nastran, NEi Nastran, NX Nastran), Catia V5 (Elfini), ABAQUS. SolidWorks, AutoCAD, FEDAMS, IDTAS and FAMOSS. Catia V5, Enovia, Catia V4, PDM / API and most in-house software at the Boeing Company including PSDS, PDM, EPIC, IWS and REDARS. Sound knowledge of BDM (Boeing Design Manufacturing), BDS (Boeing Design Standards) and ASME.

Computer Systems and Software: Unix workstations, Windows, MS Office and applied software including most applications.

Programming Languages: Excel Macro, *NIX scripts, Windows scripts, Python, C/C++, FORTRAN, Auto Lisp (AutoCAD).

Experience

10/2014 – 07/2015: Structural Analysis Engineer, Boeing, Renton, WA

737-MAX. Thrust Reverser.

Responsibilities included Non-conformal requirements control with following Structural analysis efforts in order to meet an original design requirements and manufacturing process on TR including composite structural elements and Titanium Inner Wall engineering development units:

- Delegated to be focal of non-conformance requirement process control(NCR) for 737-MAX TR within structural engineering group

- Evaluating discrepant conditions occurred along engineering development process and structural elements affected

- Performing a stress analysis addressing NCR conditions on subject discrepancies

- Creating dispositions based on structural analysis

- Developing a repair proposal, if the condition found not structurally satisfactory

- Interfacing with Boeing authority representatives(AR) for FAA approval process according to requirements

- Interfacing with Quality Engineering group on assessing damages impact

- Communicating with suppliers toward Boeing structural standards implementation.

09/2013 – 10/2014: Structural Analysis Engineer, Boeing, Renton, WA

737-Classic, 737-NG, 757. Structural Repairs.

Nacelle structure including composite and metal structural elements, such Inlet, Fan Cowl, Thrust Reverser, Nozzle etc.

Tasks included:

- Providing instant support for worldwide single aisle fleet with maintenance and repair service requests etc.

- Interfacing with Design team for generating and validating repair procedures, using Structural Repair Manual (SRM), and utilizing other other methods.

- Providing structural analysis substantiation for modified or repaired components.

- Support 737 production and rate increases.

- Working experience with a variety of composite materials, metals, Boeing specs and finishes, and FAA requirements.

04/2012 – 09/2013: Stress Engineer, Progresstech / Spirit Aerosystems, Wichita, KS

747-8. Strut. Damage Tolerance.

Engineering tasks included:

- Generating methodology for Damage Tolerance analysis for type certification including variety of structural elements.

- Using FEM for internal loads calculation reflecting structure changes assumptions

- Proccesing loads obtained in FEM

- Performing Initial Flow and Residual Strength analysis to define initial crack length

- Evaluating Crack grouth propagation with further analyisis to meet inspection requirement objective

- Writing type certification Stress Check notes based on analysis performed.

04/2011 – 03/2012: Stress Engineer, Progresstech / Spirit Aerosystems, Wichita, KS

777-300(200). Sustain.

Structural Repair Manual (SRM) structural analysis substantiation for modified or repaired components.

- Providing support for twin aisle fleet with maintenance and repair service requests etc.

- Generating and validating Structural Repair Manual (SRM) analysis based on nominal

- Providing structural analysis substantiation for modified or repaired components

- Working experience with a variety of composite materials, metals, Boeing specs and finishes, and FAA requirements.

- Writing Stress Check notes based on SRM analysis performed.

05/2010 – 04/2011: Stress Engineer, Progresstech / Spirit Aerosystems, Wichita, KS

747-8. Sustain.

Tasks included structural analysis. Substantiation of the Nacelle Inlet structure, to reflect updated loads and temperatures:

- Performing stress analysis using hand calculation supported by Finite Element Modeling of metallic Inlet structural elements such are: Anti-ice system, Inlet Lip-Skin and perforated acoustic panel

- Writing Stress Check notes based on analysis performed.

10/2009 – 04/2010: Stress Engineer, Progresstech / Spirit Aerosystems, Tulsa, OK

787-8. Airframe Structure. Wing Movable leading edge.

Assigned to perform following tasks for 787-8 Wing Moveable Leading Edge composite and metallic structure:

- Metallic ribs and attachments static and fatigue analysis

- Utilizing self-created methodology of hand analysis

- Developing and processing internal loads using FEM

- Composite Cove Edge Skin hand analysis supported by FEM

- Writing type certification Stress Check notes based on analysis performed.

05/2009 – 10/2009: Stress Engineer, Progresstech / Boeing, Everett, WA

787-9. Airframe Structure. Fuselage Hybrid Floors structure.

Structural analysis and substantiation of the 787-9 fuselage structure including Hybrid Floor Beams, Frames, and composite attachments. Tasks included:

- Structural sizing using classical hand calculation methods supported by CAD/Finite Element Modeling using CATIA V5/Elfini, Abaqus, PASTRAN / NASTRAN.

- Responsibilities included providing support in an integrated design team environment to support initial design / weight optimization efforts.

- Supported structural sizing efforts using hand calculation supported by FEM.

04/2008 – 05/2009: Stress Engineer, Progresstech / Spirit Aerosystems / Cessna aircraft Company, Wichita, KS

Cessna Citation Columbus business jet. Airframe structure. Fuselage.

Engineering tasks:

- Supporting structural sizing efforts with further analysis provided for: Tail cone Baggage Door, Cabin Main Entry Door and Escape Hatch structure

- Generating Stress analysis plan

- Finite Element Modeling in FEMAP and CATIA V5 utilizing self-created macro for linear and non-linear solving methods.

- Performing Stress analysis using classic hand analysis using self-created automated calculation procedure

- Writing Stress Check notes based on analysis performed.

04/2006 to 03/2008: Stress Engineer, Progresstech / Boeing, Everett, WA

747-8. Airframe structure. Fuselage.

Assigned to perform following tasks for 747-8 Frames metallic structure:

- Support of structural modification efforts for Everett, WA and MBDC (Moscow Boeing Design Center) modification design

teams of the 747-8F fuselage structure, Sections 44.

- Providing structural analysis for modified structural components of fuselage frames

- Using classic hand analysis along with Boeing tools

- Structure included Fuselage Section 44, 42 and 46 Upper frames.

03/2005 to 03/2006: Structural Engineer, Progresstech / Boeing, Everett, WA

747-LCF. Airframe structure. Fuselage.

Assigned to perform following tasks for 747-LCF Frames metallic structure:

- Provided stress analysis support of structural modification efforts for Everett, WA and MBDC (Moscow Boeing Design Center) modification design teams of the 747-LCF fuselage structure, Sections 44.

- Tasks included engineering design work on the Boeing 747-LCF Freighter Program.

- Structure included Fuselage Section 44 Lower structure such Floor Beams and Intercostals.

07/2003 to 02/2005: Associate Engineer, Antonov, Kyiv, Ukraine.

AN-148. Airframe structure. Fuselage.

Structural design support of Airframe Primary Structure including solid design and drafting for primary structure parts and assemblies of the AN-148. Using computer-aided software such as CATIA V5 and SolidWorks providing macro coding (C++ language) for the procedure automation.

02/2002 to 02/2003: Associate Engineer and Research Assistant, Propulsion Engineering Faculty, National Aerospace University, Kharkiv, Ukraine.

Position involved computer interpretation of paper technical drawings for design and subsequent manufacture of metal patterns for a variety of aircraft engine components using computer-aided design tools such are Euclid and Unigraphics.

Skills

Structural Repairs

Aerospace

Propulsion Systems

Durability and Damage Tolerance

Catia / Enovia

Aircraft

Stress Analysis

Aircraft Design

Finite Element Analysis

Nastran / Patran

Composites

Metallic Structure

Trainings and Certificates

MSC. Software: Patran / Nastran

FEMAP (NX Nastran, NEi Nastran)

Durability and Damage Tolerance

Training on CATIA V5 and Enovia

Training on CATIA V4/PDM MBDC)

Training on Boeing Company engineering analyses tools including IAS, SA, PDM-API, PLINQ/PRON, Bridge/ Web Spot Trainer, APARD and FAMOSS.

Languages

1) English – Fluent

3) Français – Débutant

2) Український – Рiдна мова

References and Recommendations

Available upon request

Contact this candidate