Edmond J. Limoge

*** ******** *****

Williston, VT 05495

802-***-**** cell

e-mail: acgt9g@r.postjobfree.com

BACKGROUND SUMMARY

Mechanical/Aerospace engineer with over 29 years experience in design,

analysis and testing of a wide range of products. Expertise in stress and

vibration analysis, manufacturing processes, optimization, failure

analysis, and design reapplication/reuse. Proven knowledge of aircraft

structures and components, mechanical systems and installation design.

Strong communication skills, excellent problem solver and dependable team

member.

PROFESSIONAL EXPERIENCE

Rotary Dynamics, LLC, Owner and Executive Director 2002-

Contract engineering design and analysis. Clients and projects:

ipCapitol Group

Subject matter expert for commercial/military patent review for

aerospace customer. Remote sensing (satellite, SAR, LIDAR, etc

applicability for infrastructure use for manufacturing customer (issued

3 patents).

Goodrich

Mechanical packaging of the electronic brake actuator controller for

Boeing 787. Pro-E modeling with ANSYS finite element analysis. DO-160

and MIL-810 requirements. Finite element analysis of the electronic

brake actuator load cell. Identifying non-current/non-conforming

materials and replacing them with current specifications (SAE/ASTM).

MRB and CCB responsibilities. Determining structural weld

classifications (NADCAP) for aircraft components. Engineering change

order (ECO) generation. RoHS/REACH analysis of product families.

Concepts NREC

Lead engineer for composite structures for wave energy converter.

Structure is an offshore energy generating platform. Responsible for

writing specifications, performing analysis and directing designers for

turbine structures.

AUT Industries

ITAR registration and licensing officer for thin walled aerospace

applications

Engineering Analyst, Aerojet

Performed static and dynamic analysis on nonlinear materials and

structures for various rockets (Trident, JCM, Javelin, SSST, Orion CEV,

T3, Hell Fire ER, PAC3 CRI, PAC3 MSE and Mk-104). Analysis was done

with SDRC/UGNX, NASTRAN, SAAS and ABAQUS software packages and hand

calculations. Statistical analysis was used to determine the aging

characteristics of several rocket motor grains. Complete stress

analysis was done on several programs with high pressure/high

temperature rocket casings (metallic and composite) and nozzles

(advanced materials). Margins of safety were determined for all

analysis. Familiar with JANNAF requirements.

Project Engineer, Protech

Technical/Project leader for the development of an urban assault door

breaching munition for the Marine Corps. Responsible for the design,

development, test and evaluation of all aspects of the program.

Responsible for communicating progress to the customer with written

documentation and presentations. Responsible for leading a team

consisting of engineers, designers, technicians and support personnel.

Responsible for the development of a high pressure composite pressure

vessel, numerical analysis, failure analysis and computational fluid

dynamics. Analysis was performed to determine the proper design and

configuration for a Small Arms Protective Insert (SAPI) for the bullet

proof vest worn by the US military. Significant ballistic improvement

was obtained.

Senior Aerospace Engineer, Goodrich Aerospace

1997-2002

Performed stress, dynamic, thermal and fatigue analysis for aircraft

fuel components and electronic packages. MRB, CCB experienced. Provided

preliminary design/critical design detail and finite element analysis using

SDRC design and analysis software. Instrumental in vibrational and thermal

environmental test setup and data retrieval performed on electronic

packages. Worked as Systems Engineer and wrote the mechanical diagnostics

specifications for UH-60A Blackhawk helicopter.

. Wrote $1 million capital acquisition request for SDRC software package

purchase.

. Designed and analyzed mechanical package for remote data concentrator for

on time delivery after starting 30 days behind schedule.

. Led installation design and certification efforts for CH-53E (largest

helicopter in the free world) HUMS system consisting of over 3000 parts.

Contract Engineer, Limoge Aerospace 1989-

1999

Consulted for and provided design for various engineering projects.

Provided manufacturing technology training for Simmonds Precision and

failure analysis for the Liberty Mutual. Sample contracts include:

. Structural Analyst (New World Power): Performed stress, dynamic, thermal

and fatigue analysis for wind turbine structures, structural components

and aerodynamic components. Utilized ALGOR finite element analysis

software for all analysis. Projects included preliminary and critical

design detail.

. Design Engineer (Iroquois MFG. CO.): Designed, developed, tested and

evaluated hydraulically-actuated hoisting mechanism used in trucking

industry, including tooling and implementation of manufacturing.

Optimized current industry design for better packaging and performance

using state of the art optimization techniques and materials. Reduced

mechanism weight using high strength low alloy steel (HSLA) and reduced

propensity for corrosion at joints using nitride coated steel. Developed

kinematic synthesis computer code for design and verification, also using

ALGOR finite element code for stress verification. Developed static test

plan, designed test bed and executed stress and cyclical testing.

Applications Engineer, LIVECO Inc. 1991-

1994

Provided technical support for customers, developing/designing

apparatus and procedures for use with mechanical test equipment pertaining

to biomaterials and pharmaceutical applications. Observing member of

OIML/NIST committee on mechanical testers, voting member of ASTM E28

committee on mechanical testers. Integral in the development of software

for real time data acquisition. Developed expertise in biomaterials, food

texture analysis, polymers and component analysis.

. Developed test apparatus and procedure for in vitro testing of corneal

tissue and contact lenses. Procedure and apparatus based on application

of nonlinear shell theory.

. Developed procedure for testing edible thin films.

. Developed procedure and test apparatus for testing insect wing strength.

Aerospace Engineer, National Aeronautics and Space Administration (NASA)

1985-1989

Performed stress analysis on advanced launch vehicles and structures.

Implemented design and applications of advanced materials. Developed

finite element models for stress, strain and vibro-acoustic loads

simulation and analysis. Technical consultant to management and industry.

Managed technical programs, solicited funding for advanced technology

programs from upper management and NASA headquarters, evaluated proposals

and monitored contractors.

. Merit pay increase (NASA quality step increase)

. Manned Flight Awareness Award

. Group Achievement Award for Shuttle-C avionics study

. Advanced Composite training at Marshal Space Flight Center

. Filament wound pressure vessel design for hypergolic and mono-golic

propellants

. Technical lead for the Advance Composite Inter-tank.

. Technical lead for the Advanced fly-back booster

. Marshall Space Flight Center Point of Contact for the National Aerospace

Plane using advance composites and high temperature structures.

. Advanced Solid Rocket Motor design and analysis using filament wound

composites.

TEACHING EXPERIENCE

Adjunct Instructor of Mechanical Engineering, University of Alabama,

Huntsville, Dynamics and Statics instructor, 1987 - 1988.

. Multicultural Services Award.

Instructor of Mathematics, Community College of Vermont, Elementary

Statistics, Basic Math, Basic Algebra, College Algebra, and Technical Math

Instructor. 1989 - 1994.

Adjunct Instructor of Mechanical Engineering, University of Vermont,

Teaching instrumentation and analysis fundamentals to Mechanical and

Biomedical Engineering students in a laboratory setting, including the use

and analysis of material, fluid, thermal and vibration testing equipment,

1990-1991.

. Graduate Teaching Fellowship.

Adjunct Instructor of Aeronautics and Astronautics, Embry-Riddle

Aeronautical University, Instructor of aircraft structures and design at

the undergraduate and graduate level, 1995 - 1997.

. Taught first graduate level class in aerospace sciences in Vermont.

Advanced flight vehicle design and analysis (pressure vessels,

trajectories, etc

PUBLICATIONS

"Testing Mechanical Strengths of Edible Films." Chen, H., Banerjee,

R., and Limoge, E., Paper presented at Eastern Food Conference, Natick, MA.

October 1993.

"Relaxation Testing with Miniature Mechanical Testers." Paper presented at

American Chemical Society National Conference, Chicago, IL. August 1993.

"Surface Roughness and Vibration Study of an Accelerometer Mount used in a

Helicopter Health Usage and Management System." Hochmann, David, Limoge,

Ed, Bechhoefer, Eric and Cihlar, David

EDUCATION

A.B.D. Mechanical Engineering, University of Vermont, Research based

on vibrational damping of structural joints, area of focus on large

structures.

Master of Science Mechanical Engineering, June 1990, University of Alabama,

Huntsville, Thesis: "Optimum Ring Frame Size and Spacing to Inhibit

Yielding in Short Cylindrical Sections."

Bachelor of Aerospace Engineering, June 1985, Auburn University

CERTIFICATION

. NAUI Dive Master

.

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