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Candidate's Name , M. SC
151 Fernwood Crescent Royal Palm Beach, Florida 33411
Home: PHONE NUMBER AVAILABLE Cell: PHONE NUMBER AVAILABLE email: EMAIL AVAILABLE
BACKGROUND SUMMARY
Over 30 years of Aerospace experience in ECS, Pneumatics, Apu, Wing and Airframe Ice Protection (Design Analysis, Evaluation, Laboratory & Flight-Test). Icing Wind Tunnel Testing, ECS & Thermal Wing Anti-Icing System Design, Development. Flight Test and Certification of ECS and Thermal Wing Anti-icing Systems. Analytical background in Thermodynamics, Heat Transfer, Gas Dynamics, Fluid Mechanics, Combustion, Machine Design and CFD simulations. Five years of Internal Combustion Engine Research and Development experience. Multilingual, US and Canadian citizen
WORK SKILLS
Technical guidance, Formulation of Concepts; Systems Requirements Definition; Architecture Definition; Trade-off Studies; Performance Analysis; System Modeling, Simulation & Tool Development; Technical Report Writing; Supplier Technical Evaluation; Test & Compliance; Engineering Support to Hardware Design/Fabrication, Sales & Marketing
PROFESSIONAL EXPERIENCE
MITSUBISHI AIRCRAFT, Seattle, U.S Aug 2014 to Date
Project Engineer (Stationed at UTAS in Windsor Locks)
Qualification test planning and test witnessing, Review of Similarity and Analysis reports, function as Test Director during conformity inspections and qualification testing, Interface between MITAC and UTAS. Moved to support flight-testing in Seattle for the new MRJ Regional Jet
BOMBARDIER AEOSPACE, St. Laurent, Quebec July 2013 to July 2014
Ice Protection Engineer (Temporary replacement for Engineer on maternity leave)
Thermodynamics support for the Global 7000/8000 aircraft Wing Anti-Ice System design/development
BUTLER AMERICA, Shelton, Connerticut Nov 2012-June 2013
Ice Protection Engineer
For the Bell model 525 Helicopter
Ice protection system specific test plans
System specific Certification Plans for the Ice Protrection System and Kits
HONDAJET, Greensboro, North Carolina Jan 2011 Nov 2012
Thermodynamics Engineer
Responsible for Developing the Aircraft Wing Anti-icing system and Engine Nacelle Ice protection system
Design Analysis, Performance predictions, planning & conducting Icing Wind Tunnel Testing, Analyze data, write test report, propose Design Improvements for Aircraft Thermal Wing anti-icing system and the Engine Nacelle Anti-Icing System
Flight Test Planning, Support Ground & Flight testing, Analyze Test data.
LEARJET, Wichita, Kansas Sep 2008 Jan 2011
Thermodynamics Engineer
Responsible for Technical Aspects of Flight Testing at the Bombardier Flight Test Center. Provide Thermodynamic Support to Flight Test Activities. Assist in the development of Lear 85 Aeroplane.
Develop Systems Test Requirements, Prepare ground & FlightTest plans, Define Instrumentation; define Test segments, Test profiles, Environmental test conditions.
Assist in the Design, Development and Certification of the Lear85 Thermal Wing Anti-Icing System.
Support Icing Tunnel Testing and Flight Testing of the Lear85 Thermal Wing Anti-Icing system.
Candidate's Name , M. SC
GULFSTREAM AEROSPACE, Savannah, Georgia Aug 2005 Sep 2008
Thermodynamics Engineer
Design Development of Thermal Wing Anti-Icing Systems for new aircraft models.
Design Analysis, System Sizing, Rig testing and Detail Design of the Model G250 business Aircraft Ice protection System.
Transferred to take Design responsibility for the Model G650 Business Aircraft Thermal Wing Anti-Icing system. Requirements definition, Concept definition, Design Analysis, Rig testing and Detail Design of the Thermal Wing Anti-Icing System.
EMBRAER AEROSPACE, Palm Beach Gardens, Florida Jan 2001 - June 2005
Development Engineer
Thermodynamic responsibility for Aircraft models under development and in production
Design analysis of the Pneumatic System and the thermal wing anti-icing system for the ERJ170 and ERJ190 family of passenger jets.
Performance analysis of the Environmental control system for the ERJ190.
Icing tunnel testing of the wing sections and the thermal anti-icing system at NASA Lewis Research Center for the ERJ170 and ERJ190 aeroplanes.
Design of the under wing Electro-thermal de-icing system using Thermal Heating Mats for the ERJ170 (as a backup plan).
Definition of Dry Air and Natural Icing Flight Tetst plans for the ERJ170 wing anti-icing system.
Conceptual design, sizing and selection of components for the JetBlue (ERJ190) In Flight Entertainment System component cooling, definition of cooling test plans and smoke penetration test plans.
Ice shapes predition on the JetBlue fuselage radome housing, on the ERJ145 surveillance aeroplane radar antennas, wing surfaces and fuselage.
BOMBARDIER AEOSPACE, St. Laurent, Quebec March 1984 - Jan 2001
Engineering Specialist
Aircraft Systems Thermodynamic responsibility for Aircraft Models in production or under development.
Analysis of Pneumatic System, ECS, A/C Fuel system and heating/cooling of Brakes for the CL601 Executive Jet. Engine and APU performance prediction using Engine Cycle Decks.
Monitoring and test witnessing rig tests at vendor site.
CRJ 50-pax Avionics cooling test definition, instrumentation definition, conduct tests, analyze data, prepare certification test report.
Conceptual design phases through ground and flight-testing and final certification of the CRJ 50-pax Regional Jet Air-conditioning System and the Thermal Wing Anti-Icing System.
Global Express ECS & APU sizing; full responsibility for the Global Express Thermal Wing anti-icing system design; Flight Test architecture definition, instrumentation definition, flight profiles and environmental conditions definition; Flight-testing in Dry Air and in Natural Icing, data analysis, prepare and submit compliance documents.
Full responsibility for the testing of Global Express wing sections at NASA LEWIS Icing tunnel (3 series of tests). Testing of the BD-700 passenger Regional Jet aircraft wing section at NASA LEWIS icing tunnel.
Conceptual design of the ECS and Wing Anti-icing system for the BRJX 110 passanger Regional Jet.
Nominated as the Airworthiness Design Acceptance Designee for the BD-100 executive jet.
EDUCATION
M.sc. (Internal Combustion Engines) London M.Sc. (Eng.) Moscow
COMPUTER SKILLS AND SPECIALIZED TRAINING
Working experience in STAR_CD, STARCCM, FLUENT, Gambit,
CANICE, LEWICE2D, LEWICE 3D, LEWICE 3.0 & CATIA V5
Trained in the use of CFD++, CADAM
Programming skills in Visual Basic, FORTRAN77, FORTRAN90 and Fortran Basic
Candidate's Name , M. SC
JOB SPECIFIC TRAINING
Airframe Ice Protection (KU), Aircraft Propulsion System Integration (KU)
Auxiliary Power Systems integration for Aircraft (KU) and Aircraft Certification (Bombardier Airworthiness).
LANGUAGES
English (fluent) Russian (fluent) French (student)
PROFESSIONAL MEMBERSHIPS
Registered Professional Engineer, Ontario, Canada. Member of SAE, USA |
