TUONG (BILL) LY (Page * of *)

***** **** **, ***********, ** 92683 Linkedin Profile: https://www.linkedin.com/in/billly

Mobile Phone: 714-***-**** Email Address: ac0zmj@r.postjobfree.com

OBJECTIVE:

To obtain a position in Structural/Mechanical Engineering.

QUALIFICATION:

U S Citizen. Secret Clearance: Interim (DOD Investigation completed July 2007).

Experience in Commercial and Military Aircraft/Spacecraft design:

CATIA V5 (18,000 hr.), NX5 (18,000 hr.), Solidworks 3D and Simulation (5,000 hr.), Mathcad 14, FiberSIM.

Details Part, ASME Y14.5M-2009, Large Assembly and Installation Drawings; Surfacing and Solid Design.

Knowledge of 3D Printing, Computer Hardware, Internet, Hardware Connection and PC diagnostic software, Window 7 and 10, and MS Office 365. Familiar with Unix OS.

Fuselage and Wing Structures, Bolt Joints, Space Vehicle Mechanisms, Thermal Insulation, Propulsion, Fuel Tank, Cargo Systems, Payload Accommodation; Flight Deck Instrumentation Modification and Electrical Installation.

MRB Activity, Quick Action Engineering Order; knowledge of different forms of Composite Materials and Aluminum Alloys, Springs and Bearings, Cables System, Dissimilar Metals, LSP and EMC, 3D-Printing.

Worked well in Team Environment.

Knowledge of Stress Hand Calculation, Layout, Load Path and using Mathcad/MS Excel Spreadsheets.

Release systems: Enovia Matrix (Engineering Central) and SmarTeam, Team Center PDM, iMan, EDDS/ECC, EEO and Boeing Nonconformance System.

EDUCATION, CERTIFICATION & TRAINING:

ROP Education Center, Orange County, CA: Advanced Level Solidworks, and Fabrication of 3D Printed parts.

BOEING/UCLA-EXTENSION, Seal Beach, 2016: Advanced Development and DTaD (Matel and Composite Materials).

MS, Engineering, CSU Long Beach, CA. Majors: Aerospace and Mechanical Engineering.

BS, Mechanical Engineering, San Diego State University, CA.

Publication/MS Thesis: “Modeling of delamination buckling in the laminated plate.”

Courses: Aircraft Structures Design, Composite Material Analysis, Machine Design, Vibration, Mechanisms,

Finite Element and Thermal Analysis.

Honor Societies: Tau Beta Pi and Pi Tau Sigma.

Certificates: Engineer-In-Training, CA, XE062820.

Machine Shop Technology, San Diego, CA.

Teacher Training, Vietnamese Language & Culture Schools of Southern California Association.

Training: CATIA V5: Advanced Design, Drafting and DMU Navigation/Kinematics.

Pro/Engineer Wildfire 5.0, Basic and Advanced classes. Vistagy FiberSIM.

Boeing Lean Principle, Northrop Grumman and Boeing Ethics Policies and ITAR, NASTRAN.

Northrop Grumman Composite Material and Aircraft Fatigue Design.

Lockheed Martin JSF Light Weight Design.

UCLA Extension/TRW Training: Spacecraft Systems and Structures Design.

HOBBIES & ACTIVITIES:

Boy Scout Merit Badge Counselor, Troop 1961, Huntington Beach, CA: Coaching boy scouts Merit Badges of Engineering, Composite Materials, Citizenships.

PROFESSIONAL EXPERIENCE:

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The Boeing Company, Long Beach, CA (05/2011 – 09/2016), Structures and Payloads Engineer IV-700 Series: Modified and Designed Support Structures for Antenna’s. Supported 747 Air Force One’s Nitrogen Tank project. 737 Electrical Wirings.

787-8, -9: Fuselage Product Support: MARM’s, Thermal Insulation design, PR and Orphan Issues. Trained assisted others

MARM procedure and Enovia and Catia V5.

BAE Systems (Tier 1 Engineering), Composite Structures Inc., Brea, CA, (09/2010-05/2011), Structures/Mechanical Engineer-

Airbus A350 XWB/COMAC C919 NB- APU Inlet Duct and Door Assy – Designed composite duct/splitter utilizing BMI, Honeycomb core and Rohacell foam core materials. Assist program manager in Critical Design Review; and review all 3D Catia models and 2D detail and assembly drawings of BAE and Honeywell. Create mass properties of entire inlet duct systems. Support Manufacturing Engineering and Tooling, and Honeywell in GD&T and design detail.

Northrop Grumman Corp. (iConnect Staffing), Redondo Beach, CA, (06/2009-06/2010), Senior Structures/Mechanical Engineer-

JWST Spacecraft BUS – Design and release drawings for Restraint and Release Mechanism System for Solar Array. Prepared layouts of Radiator Panel Support, Cone Stiffeners, Hold Down and Release Mechanism, Cable and Strut Systems.

The Boeing Company (Midcom), Long Beach, CA (08/2007-01/2009), Structural/Equipment Engineer-

C130 Avionics Modernization Program: Modernized and reorganized Flight Deck Pilot/Copilot Consoles, Pedestal, Miss Instrument, Overhead and Anti-ice panels. Reinforced and modified equipment panel and structure.

Northrop Grumman Corp., El Segundo, CA, (2002-07/2007), Structural Design Engineer-

F-35 Fighter Airframe Structures – Designed and released PDM BTP packages for Duct Frames and Inlet Lip Fairings. Prepared layouts of Integral Fuel Tank, Gun Integration, Forward-Duct Frames, Lower Skin Intercostals and Gas-Sealing Closeout. Redesigned Inlet Lip Fairings structure for lighter weight and simplified complex surfaces of Mold Line interfaces for lower cost.

The Boeing Company (ITS), Huntington Beach, CA, (1998-2002), Structural Design Engineer-

* NASA Space Station: Prepared Field Engineering Change, modification and advanced EO, disposed PR. Designed

the support and thermal insulation for Space Station Trusses. Resolved EMC and Dissimilar metals of Truss Structure

and Thermal Blankets. Supported NASA Kennedy Space Center Assembly Production.

Received Boeing Space Station S0 Production Support Award.

* USAF Delta III/IV- CBC Structures- modified Heavy, 5M and 4M UG production drawings for first flight.

Prepared test drawings of composite-material interstage shell. Prepared layouts of Medium, 5M, and Heavy rockets’

Assemblies of payload Fairings and Adaptor, Upper Stage, CBC, Engines and Launch Pad. Arranged IPD data

sheets of major joint assemblies. Designed support structures and insulation installation for booster, engine section

and liquid oxygen tank. Created production drawing Schedule.

* USAF Delta IV-Propulsion Released propellant line propulsion installation. Supported Static Fire test. Incorporated

Quick Action, modification and advanced EO’s. Designed support and aero-thermal insulation booster for OML lines.

Received Boeing Static Fire Propellant Line Propulsion Support Award.

Northrop Grumman Corp. (Chipton Ross), El Segundo, CA, (1997-1998), Structural Design Engineer-

Kistler RLV Payload Accommodation- Prepared layouts the telescope forward fairing: separation nuts fittings, composite shell, longitudinal and axial restraint system, jack screws hinge and motor fittings. Designed nose dome door frames, articulation pulleys, lock support structures, and Graphite/BMI fairing panel.

The Boeing Company, Huntington Beach, CA, (1994-1997), Mechanical Design Engineer-

* Hughes Aircraft Company- HS 702, 601 HP- Customized Support Fitting of

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antenna waveguides for saving weight and space on the radiator panels. Designed thermal OMUX and IMUX

doublers. Utilized potted Inserts and hybrid brackets on Al Honeycomb Core Composite Panel for reducing weight.

* NASA Space Station Alpha - Designed and provided structural supports for the acoustic and thermal testing of a

radiator for avionics equipment. Prepared layouts for avionics system structures, close-out and primary structures of

space truss. Prepared detail and assembly drawings of Pressurized Mating Adapter.

Northrop Grumman Corp. (Butler Services), El Segundo, CA, (1992-1994)

* Structural Design Engineer- Navy F/A-18 E/F Center Fuselage- Responsible for the design of dorsal covers, fuel

tank access doors utilizing graphite epoxy skin with cocured integral stiffness. Interfaced with avionics, fuel system

and NT groups to provide clearance and support requirements.

* Flight Test Design Engineer,Navy F/A– 18 E/F - Responsible for the instrumentation installation on Hydraulic

Lines and Structures. Installed Strain Gage Coupons on structure and hydraulic lines.

McDonnell Douglas Corp, DAC, Long Beach, CA, (1986 – 1992), Structural Design Engineer-

* MD-11 Fuselage & Cargo Systems- Furnished modification/variation drawing for auxiliary fuel tank - designed the

intercostals to support the removable auxiliary tank. Reworked Crash Barrier Net for Combi Freighter main deck,

repaired floor panels and floor beams. Designed support for cargo door sill and drain lines of cargo compartment.

* MD-90/80 Fuselage & Wing- Prepared layouts for the integral auxiliary fuel tank to prevent formation of ice on

wing surface. Resolved manufacturing problems and improved existing products (including wheel well, wing joint,

pressure bulkhead, control surface and mechanisms, drag fitting, dorsal fin). Trained Material Review Board.

* USAF C-17 Aft Fuselage & Cargo Door- Prepared layouts for (Six-Bar Linkages) Upper Pendulum and Lower

Latches, utilized Stress and Kinematics Analysis. Responsible for selecting bushing and bearing for latch Linkages.

Installed Hydraulic Cylinders and Electric Sensors. Designed Flight Test Skid, intercostals, precision-forged latch

fittings and links. Trained other engineers in computer-aided design.

REFERENCES: AVAILABLE UPON REQUEST

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