|
|
|
|
   
|
||||||
|
|
Industry: Aerospace
Resides:
Salary: Open
Relocate: Yes
On
the Market:
Objective Aerospace Engineering/CAD position. Education Georgia
Institute of Technology, Atlanta, Georgia -Bachelor Degree of Aerospace
Engineering Spring, 2000 Darton
Community College, Albany, Georgia - Associates Degree of Engineering,
Summer 1998 Work Experience 8/2002-Present (Company) Aeronautical
Engineer The
main task that I was involved in while I was at (Company) was helping
to install the FLIR system onto the C-130 aircraft. I helped to design
several of the boxes for some of the electronic components that made up
part of the FLIR system. I was also responsible for the attachment design,
stress analysis, drawing creation, and written reports for these components.
I preformed hand stress calculations for the AAQ-22 adapter ring that
held the FLIR turret onto the aircraft. I was responsible for generating
3-D models for FEM analysis using the PRO-E MECHANICA package. I was also
involved with reviewing the aerodynamic load report for the FLIR turret. 6/2001-5/2002 Middle River Aircraft,
Baltimore, MD (Contractor for Echelon
service company) Designer/Engineer During my employment period
with MRAS I was part of a 7 man design team for a package of doors from
the RAH-66 Comanche helicopter. My main responsibility was the E-Bay door
re- design. The original design for this door did not take into account
maintainability and damage tolerance issues. It was also 20% heavier than
the new design required. The composite honeycomb core used to stiffen
the door panels also posed challenges in forming to the tight bend radius
required. I participated in examining several options to design a door
that would meet the structural requirements, but was also able to be manufactured
economically. I was involved in several studies used to determine the
minimum number of composite plies that would meet the structural requirements,
the deflection requirements, along with the very tight weight requirements.
I gained extensive 3D modeling experience using the SKIN, SOLIDE, SOLIDM,
SURF1, SURF2, FIBERSIM, KINEMATICS and the KINEMUSE functions in CATIA.
I was charged with the 3D modeling of the E-bay door, the installation
drawing, the assembly drawing, the ply lay-up books, the BOM, weight estimation,
setting up Power point presentations for design reviews, and coordinating
data with the structural analyst. I also helped with designing some of
the machined fittings and the door struts for the Weapons Bay Door. I
helped to design the hinge-spring mechanism for the Main Landing Gear
Door/ Flapper Door. I also designed the fittings and hinges on the Main
Landing Gear Door/ Flapper Door. 1/2001-4/2001 Lockheed Martin Marietta, GA (Contractor for CDI Corp) Designer/Engineer During my employment period
with Lockheed Martin, the main project I worked on was the wire harness
diagrams for the COLT system. I also had an opportunity to gain experience
with schematic diagrams for electronic filters, and other circuit cards
as well. I was involved in designing a heat sink for a component of the
COLT. I also designed some 3D models for some of the cable connectors.
I helped to design some of the rubber seals that were used with the glass
displays. ASME Y14.5 GD&T was the standard used in dimensioning these
seals, due to dimensional deviations due to temperature fluctuations.
I am also familiar with standard CATIA solid modeling procedures including,
but not limited to SOLIDE, SURF1, SURF2, AUXVIEW1, AUXVIEW2, and DIMENS2.
I am also familiar with standard machining drafting procedures. I am familiar
with National Aerospace Standard Fasteners, along with MIL-HNDBK- 5H for
aerospace structural materials. 7/2000-11/2000 (Company filed Chapter 13) Ayres Corp, Albany, GA Designer/Engineer During my
employment period with Ayres Corp, the main project I worked on was the
assembly diagrams for the fuselage of the LM-200 airplane. I helped to
design some of the bulkhead fixtures. The bulkhead for the rear of the
plane had to be moved back 10 inches to accommodate additional cargo volume.
This involved becoming familiar with seat track installations, HI-LOK
fasteners, NAS rivets bulkhead fittings, structural frames, bulkhead gussets,
and shear web design. This also involved helping to design and place additional
longerons to help stiffen the bottom part of the fuselage. I had to do
some stress analysis to determine the sizing for some of the shear webs,
along with the sizing of some of the floor columns. I also became familiar
with MIL HNDBK 5-H standards for aerospace materials. I am familiar with
flat pattern layouts. I am also familiar with standard machining drafting
procedures. I have also had experience with EO forms, and Bill of Materials
forms. Skills Proficient
in CATIA (over 2500 hours) Security ClearancePending Activities American
Institute of Aeronautics and Astronautics Eagle
Scout, BSA, 1990 References
- Available upon request
|
|
|
|
