Engineer Design

Location:

Torrance, CA

Posted:

July 21, 2018

Contact this candidate

Resume:

CHIN HAI LEE

***** ****** ******,

Torrance, CA**505

Phone: 310-***-**** (H) (O)

Email: **********@*****.***

U.S. citizen

I have been in aerospace industry over 33 years. Down through many different projects, a group lead in CAD/CAM implementation for aircraft like F-35B, Boeing 747-8 cargo. Composite structure is my specialty. I am also proficient in Microsoft PowerPoint, Excel and Word for engineering presentation to peers and managers. Sub-contract various innovative products from air to underwater

WORK EXPERIENCES:

Protean Engineering Corporation, consulting Torrance 2009 Jan – 2018 June

Consulting POC (Physical Optics Cooperation) in towed AUV design, advanced composite and metallic structure renovation and system integration of NAVY submersible AUV. Pool test1, 2, 3

. Innovative watercraft development, design, prototype fabrication 1.

. Watercraft fabrication, test and future advanced modification etc. 2,

. Coastal test of corporate prototype watercraft

Special consulting work at Taiwan in VAWT(Vertical Axis Wind Turbine) project and

UAV full composite structure assembly tooling design for Cotechinc.com

Pioneering composite strut of best sale European E-bike, direct Taiwan work team cut weight 50% of its original metal parts. Employ PATRAN/NASTRAN, Abaqus CAD

New type of composite car wheel center plate is under development for composites rim had past two major aftermarket car loading tests, only final road driving fatigue test past. This product hit the aftermarket car wheel buyers. It’s a hit product alright!

FACC (Fisher Advanced Composite Corporation) Seattle 2012 Nov - 2013 June

Boeing 737 new split scimitar winglet design. Accomplish CDR into production type.

Works done on C919 commercial plane wing spoiler GAS assembly stress analysis and also accomplish CDR, finished detail and production type modification. (CATIA V5)

Modular Wind, Long Beach 50MW wind turbine contract 2008 Oct. – 2009 Jan

Composite wind turbine structure design and analysis, and win a German contract.

Creating first innovative design 3D turbine model, coordinate design and shop interface.

Accumulate wing structure design experience fully merge in wind turbine.

Boeing Commercial Aircraft, Aft fairing structure, Seattle, 2007 Oct. – 2008 May

Accumulated CATIA V5 experiences over 10,000 hours employ ENOVIA for 747-8 Nacelle under wing structure and after fairing redesign get team award 2008.

GD&T for parts design and FT&A 3D dimensioning system.

Composite access panel acoustic fatigue stress analysis.

Protean Engineering Corporation, consultant, Torrance 2006 Oct. – 2007 Sep.

NRAO (National Radio Astronomy Observatory) Nutator - Subreflector design.

Full composite nutator made by 3K woven carbon fiber.

Employ CATIA, PATRAN-NASTRAN composite to successfully accomplish the CDR-II (Critical Design Review) – review team from NRAO University of Virginia

Northrop Grumman ACS, mechanical engineer, El Segundo 2004 June – 2006 Oct

F-35B STOVL subsystem design engineer whose task on fuel system, hydraulic system, structural, Mechanical design and integration. (CATIA, DMU, PDM)

A full training in GD&T and FT&A was conferred a NGC GD&T certificate.

Design integration with tooling and manufacturing for parts completeness.

F-35B Upper Lifting fan door actuator hydraulic system Integration problem solved.

NUCAS (UAV X-47B) and its fuel system integration resolve many technical issues.

Rossi design group, consulting engineer Orange, CA 2002 June – 2004 May

I had Liver transplant success January 12, 2003, was reborn ever since.

Consulting on wing structure design projects (CATIA, Solidworks)

GD&T(Geometric Dimensioning & Tolerance), ASME Y14.5M checks on all detail drawings and stress analysis.

AASI-Mooney Aerospace Group, structure At Long Beach 2000 Aug. – 2002 May

Wing structural design engineer developed Jetcruiser 500 economical turboprop commercial aircraft,

innovative prototype for a full composite aircraft. FAR25 specification enforced. Employ CATIA DMU for Nose landing gear and engine inlet deicing system

ITT Technical Institute instructor, Engineering instructor, Syl 1999 July – 2000 Aug

Instructing college student 3D engineering drawing

Learned student mentoring ability and in after curriculums activities.

Spacecraft Machine Product, CNC engineer Torrance 1997 Aug. – 1999 May

CAM engineer, 3D solid modeler, CNC programmer for B-1parts. Contract work for Disney, TRW, Boeing. employing Virtual Gibbs as CAM tool.

Cost estimation of manufacturing process on the job training, certificate granted.

Aerospace Industrial Development Corp, CAD/CAM lead 1985 – 1997 Feb.

Immigrate to The States on 1997 February from Taiwan

Aircraft structural design engineer, employ CATIA v4, ANSYS as design tool

CAD/CAM team lead, supporting aircraft structural design and interface with shop for prototype production. It includes CAD system training, facility upgrade and work interface with IT department.

Establish CAD/CAM Data sets system for aircraft structure, with early PDM concept of Lockheed-Martin. ( www.aidc.com.tw )

Preliminary and detail design of composite horizontal tail structures of IDF, this project was in cooperation with Lockheed-Martin Fort Worth.

PROFESSIONAL REFERENCES

Craig Henderson, Northrop Grumman Corporation, IPT mechanical lead, 1-310-***-**** and Mark Post, Northrop Grumman Unman-system IPT, 858-***-****.

Hu, Roger, Northrop Grumman Corporation, NGST, 1-310-***-****.

Education & academic background

University of Florida, composite research Lab Ph.D degree conferred 1994

Advanced study in forced and harmonic vibration control of FG/EP composites with embedded SMA (Shape Memory Alloy).

Tooling and fabrication of GR/EP at the research laboratory shop.

University of Florida, composite research Lab MS in Engineering science

Attention: (Achtung) :

Some links are from my personal Google photo database, please feel free to view but please do not copy or download, it may jeopardize your computer

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