Matthew Berden
Vought Aircraft Industries **** Sanford Rd
**** ****** **** ***********, ** 37135
abnd0g@r.postjobfree.com
abnd0g@r.postjobfree.com
Desk: 615-***-**** Cell: (615) 975-
2663
EXECUTIVE SUMMARY
Mechanical engineer specializing in research and development,
manufacturing, domestic and international patents, and project management.
Over ten years of combined experience in aerospace and automotive fields
with cost and technical reporting, 3D solid modeling, and advanced
structural testing.
EXPERIENCE
Vought Aircraft Industries Nashville,
TN
Materials Technical Officer (MTO) June 2009-
present
Lead engineer and investigator for domestic and international supply
chain
Focal for the Airbus A330 wing assembly line maintaining design
changes and inventory
Manage internal machining offloads, supplier re-bids, and down select
new suppliers
Coordinate engineering changes, manufacturing plans, and quality tags
Develop RFQ packages, enter purchase orders, and manage change orders
Tool/Fixture Design Engineer - Cessna Columbus Wings
Feb.2009-May 2009
Design assembly jigs and tooling using Model Based Definition - CATIA
V5 and Enovia
Model and optimize the entire assembly process using Lean
Manufacturing and Six Sigma
Boeing - Integrated Defense Systems (Military Business Unit)
Huntsville, AL
Ground Based Midcourse Defense Flight Test Engineer
Oct.2007- Jan. 2009
Perform flight test design, radar analysis, pre- and post-flight
system analysis, and risk reduction
System Performance Prediction using hardware in the loop and software
component testing
Boeing - Phantom Works (R&D Business Unit) Seattle, WA
Advanced Structures Engineer: Apr. 2004-
Sep. 2007
Developed multifunctional structures for use in primary, secondary and
tertiary applications
Conducted coupon design, testing (core compression, flatwise tensile,
shear, 3pt bend, tensile)
Modified edge closeout design to strengthen the composite panels by
adding doublers and improve manufacturing methods
Managed the manufacturing scale-up from hand built coupons to
machined large scale components by modeling all tools in CATIA V5 and
outsourcing tooling
Developed QA standard methods for core to skin bond quality using
Through Transfer Ultrasonic (TTU) testing
Published and presented at the 2006 NATO Conference on structural and
RF array development, manufacturing build up, and airframe integration
Designed structural test beds for static, dynamic, and acoustic load
environments
Coordinated with the Air Force Research Labs (AFRL) Dayton to
integrate the test fixture designs with their test facilities
Modeled all designs in CATIA V5, developed BOM and assembly plan
Drafted the manufacturing contract and maintained oversight and
buyoff of the final product
Developed the test plans with stress, acoustic, and AFRL engineers
Authored the test reports and the final report which was submitted to
the AFRL Director
Published and presented at the 2007 SAMPE Conference on design
approach, manufacturing scale up, fixture design, and structural tests
Managed and designed a next generation conformal radar for flight test on
AW&CS
Completed design through installation within the 6 month deadline
from project conception
Coordinated with stress engineering using CATIA V5 solid models to
conduct fatigue, decompression, flight loads, and harmonics analysis
Used DFMA by modeling and machining all fastener holes through use of
a laser positioning device which gave locations and vectors for the
existing structure on the aircraft
Created and completed part and installation drawings in CATIA V4 with
AW&CS signoff
Met all requirements, stress, EMI, QA, and customer signoff for a
successful test
Lead and designed a structurally integrated UHF radar for RF and
structural testing
Designed and manufactured a 10 meter symmetric wing using CATIA V5
from conceptual models in V4
Published and presented at the 2005 SAMPE Fall Technical Conference
on design semantics and manufacturing techniques used to develop the
test fixture under budget
Developed a powered wheel landing gear to lower aircraft emissions, US
Patent 7275715
Integrated an electric motor in the forward landing gear which is
powered by the auxiliary power unit which will save fuel by taxiing
without running the main engines, therefore lowering emissions, wear,
and maintenance
Designed and integrated the motor, gearing, wiring, and hub in CATIA
V5
Conducted trade studies on the power consumption, sizing, and
accelerations required
Drafted language and artwork for patent application
Boeing - Commercial Airplanes Everett, WA
Airplane Certification Engineer Apr. 2003-
Mar. 2004
Certification Specialist for Flight Controls and Electrical systems
Performed Type Certification on the 777-300ER
Reviewed and certified all design changes on twin aisle aircraft with
the Designated Engineering Representative (DER) and the Federal
Aviation Administration (FAA)
Flight Controls Design Engineer Apr. 2001-
Mar. 2003
Production support for the 737 and 757
Updated the quality specification of flight control cables after
conducting a long term study on manufacturing (winding rate, coating
thickness, wire material properties) and its affect on creep combined
with temperature variations throughout the year
Performed tolerance analysis on a control column redesign, and
applied GD&T to control variability in the assembly
Conducted cost saving initiatives for 737 and 757 primary flight controls
Redesigned mounting methods and tooling to attach flight controls to
Monolithic bulkheads
Designed Electro-Magnetically Formed (EMF) torque tubes for flap actuation
(High Lift), US patents 6,932,118 & 7,299,826
Certified for production to replace all torque tube designs company
wide
Performed extensive fatigue testing and analysis to understand the
failure mechanism of high energy rate forming
Designed the mandrel to form the tube without heat treatment,
reducing manufacturing time and cost
Co-authored the Boeing Company Standard: "Assembly of Circular Joints
by Electro-Magnetic Compression Forming"
Developed a new process using Stereolithography to physically model new
designs
Performed physical interference checks with large assemblies
Reduced manufacturing cost, and minimize production time
General Motors Truck Division Milford, MI
Vehicle Development Intern May-Sept.
2000
Test and assembly focal for the "Chinese Blazer" program which
outsourced manufacture of the Chevy Blazer using locally made parts
(engine, tires, electronics, A/C, etc.) for use in the country of
origin
Built beta vehicles for future production by stripping existing
models down and rebuilding with development parts
Created a "Youth Initiative Vehicle" by modifying a GMC Sonoma, which
went into production as a special edition
Syron Engineering Saline, MI
Industrial Automation Tooling Intern May
1999 - May 2000
Developed tooling to assist metal forming operations in the
automotive industry by moving stampings from one die to the next
Tested new and existing designs for reliability with accelerated life
cycle testing to determine reliability of transfer tool mounts,
grippers, vacuum cups, and clamps for use in crossbar, tri-axis, and
end-of-arm tooling
Designed new grippers for hydro-formed tube with wide ranging
tolerances and low friction
Composite Testing and Analysis Ann Arbor,
MI
Material Testing Intern Sept. 1998 -
Jan. 1999
Conducted high temperature, creep, and tensile testing of advanced
nickel metal alloys
Performed statistical analysis based on cross-sectional variations of
the grain structure
Business owned and operated by a professor at the University of
Michigan
U of Mich. Ultrafast Laser Lab Ann Arbor,
MI
Machinist Sep. 1996 - May
1997
Designed mechanisms for optics including oscillators, and adjustable
prism/lens fixtures
Performed vertical end mill and engine lathe operations, and shop
maintenance
PUBLISHED WORK
"Structurally Integrated X-Band Antenna, Large Scale Component Wing
Test", Society of Advanced Material and Process Engineers (SAMPE)
Conference, 6 June 2007, Baltimore MD
"Structurally Integrated X-band Array Development", NATO Research and
Technology Organization (RTO) Applied Vehicle Technology Panel
-141/RSM, 020, 17 October 2006, Vilnius, Lithuania
"Development of a Large Scale Test Bed for Evaluation of UAV
Structurally Integrated Antennas", SAMPE Fall Conference 2005, Seattle,
WA
"Methods of Electromagnetic Forming, Current Applications, and
Development Opportunities" Boeing Technical Excellence Conference 4,
February 2003, Seattle, WA
"Factors Influencing EMF and Fatigue life of Torque Tubes in 2024-T3
AL", Boeing Metals Technology Exchange, June 2002, Long Beach, CA
EDUCATION
University of Michigan Ann Arbor, MI
B.S. Mechanical Engineering Dec. 2000
COMPUTER PROFICIENCY
CATIA V5 -
Over two years experience developing large metallic and composite
structures, test fixtures, and lay-up tooling
Performed rapid prototyping using determinant assembly and DFMA
techniques to minimize construction time
Coordinated directly with suppliers and designers using CATIA output
files for manufacturing
Conducted Finite Element Modeling (FEM) analysis on high stress
parts using the CATIA solid model FEM tool
CATIA V4 -
Two years experience integrating new flight control designs for cost
saving initiatives and production support on the 737 and 757
Created part, assembly, and parts list drawings incorporating
Geometric Design and Tolerance (GD&T) techniques
Excel - Extensive experience as an analyst performing advanced graphing,
statistical analysis, budget estimates, and BOM development
Project - Team lead experienced at planning schedules, link to budgets and
headcount estimates, and contract management
Word - Published author in SAMPE, NATO, and Boeing conferences, authored
white papers, wrote monthly status, test completions, and final reports
for military contracts, developed test and assembly plans
PowerPoint - Experienced presenter at internationally recognized
conferences, lead government contract reviews, and create new methods
of data/graphics presentation for management and customers
EXTRA CURRICULAR ACTIVITIES
Boeing Leadership for Advancement and Development of Engineers (BLADE)
group
Team lead of a group of new engineers 1-5 yr to design, manufacture
and test a rocket launched radio controlled airplane
Teach Boeing process for product development
Develop a schedule and monthly budget by component
Grant Proposal Team for Sci-Quest the North Alabama Science Center (non-
profit)
Currently writing a proposal for an interactive rocket exhibit that
begins by educating students on basic rocket science, combine their
knowledge to design their own rockets, and finally test their rocket
interactively in a rocket simulator.
Develop the technical section and tie the exhibit to educational
goals, and workplace development
Member of the Society of Mechanical and Process Engineers (SAMPE)
Write and present at conferences regarding Boeing R&D
Stay up to date on new material technologies and manufacturing
processes for design and analysis of composite structures, and nano-
technology
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