Design Engineer Mechanical
Resume:
ROMAN ENRIQUE ARREOLA
MECHANICAL DESIGN ENGINEER
CEL: 626-***-****
E-MAIL: adcr60@r.postjobfree.com
I am clearable. Completed NASA Tier 1 Background check called EQUIP.
US CITIZEN. I DO NOT HAVE A SECRET CLEARANCE.
SKILLS:
CREO V2, V4, and V5
CATIA V5, DRAFTING, PART DESIGN, ASSEMBLY DESIGN WORKBENCHES - 11,000 HRS R23 (DRAFTING, CAT PART, AND CAT PRODUCT)
UGII thru UGNX6, UGNX10 – 27,500 Total HRS+ of UGNX
PDM, TEAMCENTER
ENOVIA – BOEING VERSION, RELETASE ACTIONS AND SIGN-OFFS
WINDCHILL V11- PRODUCT LIFECYCLE MANAGEMENT ENVIRONMENT
G D & T Standards used: MIL STD DOD-863B, ANSI Y14.5-2009, ANSI Yo14.5-1994.
IEEE, ATA 100, Mil STD 50881
PC Software: IVT, Diol, Radars, Multimate, Word Perfect, Word, Power Point, Windows
Team Player and interfaced with various customers, extensively. was involved with contstructive meetings, developed design concepts, 3D models, Assy’s and detailed drawing’s in Structures, Tooling, GSE, Interiors, Environmental, Electrical, Flight Controls. I also helped mentor my co-workers with various issues.
CSR Experience within the companies I worked for and the companies vendors. I use to
Coordinate and worked out solutions to any issues that came up.
WORK EXPERIENCE:
NASA, KENNEDY SPACE CENTER, FL 02/26/2018 – 06/07/2019 (Contract:Insight Global/JACOBS LAB) (Mobile Launcher)
Mechanical Designer:
For TOSC Designed and Incorporated changes for GSE Drawings in ICPSU, Shop Aides (Tooling) modeled fixture brackets, Hypergol Fluids Piping re-routing, Landing and Recovery, Environmental, and Structural using Creo and Windchill release sys. In the SOPE MPPF Landing and Recovery group, fixed product structure, WT parts and Parametric attributes for drawings in Windchill.
Honeywell, Torrance, CA 05/30/2017 – 10/06/2017 (Contract:Nesco/Manpower) (Turbochargers-Automotive)
Mechanical Designer:
Analyzed machined parts: mass measurement (Turbochargers-Auto)
2D/3D Detail, Assembly and Installation Design creating Castings and machined parts and drafting them up on Catia V5 (Turbochargers-Auto)
Boeing Aircraft, Long Beach, CA 06/27/2011 – 07/29/2016 (Direct) BCA, (767 Tanker and 777)
Mechanical Design Engineer:
Subsystems – Electrical Design Secondary Support Brackets (767 and 777)
Updated Composite floor beams (777)
2D/3D Structural Detail, Assembly and Installation design(767 and 777)
Electrical – Cars, ELR’S and DCN’S for Product Support Assembly line(767)
Software Tools used were ENOVIA, CATIA V5, PDM, IVT and DIOL(767)
Updated Electrical drawings on NX10. (C-17)
Interior Design Created Blanket(insulation) Drawings (777) CATIA V5
Subsystem Secondary Structures: Checked Model, Detail and Assembly Parts in CATIA V5 and using Enovia for Product Support Assembly Line.
Bell Helicopter Textron, Grand Prairie, TX. 07/20/2010 – 02/11/2011 (Contract:Global Tech) (V22)
Tool Mechanical Designer:
Designed Tool Fixtures and Jig Drawings on UG NX5 and NX6 (1200 HRS+).
Designed Tool Fixtures, Baseplates, small tools Through ECN’s by written/verbal instruction.
Created Tool Assembly Drawings and detail parts using CATIA V5, UGII NX5, VISIPRISE and TEAMCENTER software were used to create these models and drawings.
Boeing Helicopters, Mesa, Az. 11/21/2008 – 06/01/2009 (Contract:Chipton Ross) (Apache)
Mechanical Design Engineer:
Subsystems Secondary Structures Designed Sheet metal brackets included flat patterns in the Un-Dimensioned Drawings using UGII NX5 and NX6 (1,000 HRS+) SKETCHER and TEAMCENTER.
Piper Aircraft, Vero Beach FL. 07/21/2008 – 10/19/2008 (Contract:Precision Resources)(Piper Aircraft)
Tool Mechanical Designer:
Redesigned a spar drill tool fixture by added a clamping system and redesigned steel tubing,base plates, angles, support stops and locating pilot hole supports on UGII NX5
Rockwell Collins, Irvine, Ca. 08/27/2007 – 04/03/2008 (Contract:Additional Tech. Support)(Embraer and Boeing 787 Aircraft)
Flight Controls/Tool Mechanical Design Engineer:
Designed shutoff valves, Fuel Sticks, and actuator Tooling Fixture for Airbus.
Program Tools used NX3, Teamcenter, and Catia V5.
(JPL) Jet Propulsion Laboratory, Pasadena CA 01/30/2006 – 07/01/2007 (Contract:SBAR) (Aquarius Satellite, Rover)
Mechanical Designer:
GSE Ground Support Equipment for the Rover Thruster
Designed a lower and upper hinge assembly, this contained small actuators, sensors, Tool Test Stands and other machined mechanisms, which attaches to the satellite Aquarius
Program tools used NX3, NX4 (2,500 HRS+) and TEAMCENTER.
BOEING AIRCRAFT, Long Beach, CA. 8/26/2003 – 4/29/2005 (Contract:Inconen), (C-17 Program)
Mechanical Design Engineer:
Systems Liaison Support and Modification kits – Equipment support
Electrical Systems Support bracket and wire harness installations
Tools used NX2 and UGMAN
KAISER ELECTRONICS, San Jose, CA. 07/2002 – 12/2003 (Contract:National Eng.), (HUD Display
Electro-Mechanical Design Engineer:
Designed HUD display tools that support optics.
Designed EM display package
Program Tools used were UGII V17
AEROJET, Sacramento, CA. 12/2001 – 4/2002 (Contract:Two Roads), (EKAV)
Mechanical Design Engineer:
Designed a supply Module for EKV(Vehicle Exo atmospheric Kill Vehicle
(Worked with Raytheon navigation system)
(DFMA) Designed propulsion fuel lines, valves, diverts, and gyro locks.
BOEING AIRCRAFT, Long Beach, CA. 4/2001 – 9/2001(Contract:), (717 Program)
Environmental Mechanical Design Engineer:
Designed the environmental composite ram air duct for the Boeing 717
KAISER ELECTROPRECISION, Irvine, Ca. 09/2000 – 3/2001 (Contract), (F14 and Hawker Aircraft)
Flight Controls Mechanical Design Engineer:
Redesigned the F14 switch bank and the Hawker actuator assy on UG V15
designed a pedestal assembly which included cranks, top plate, and other parts on UGII VI3
KAISER ELECTRONICS, San Jose, Ca. 10/13/1999 – 09/08/2000 (Contract), (HUD display Tools)
Electro-Mechanical/Tool Design Engineer:
Designed HUD display Tools that support optics.
Designed Multifunction Display
Program Tools used: UGII V15
EDUCATION:
MOUNT SAN ANTONIO COLLEGE, Walnut, CA
Associate of Arts Degree 1983.
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