Engineer Mechanical

Shi Guang “Jack” Xu

E-mail: **********@*****.***

Tel: 206-***-**** (cell)

Address: Mukilteo, WA, U.S.A 98275

OBJECTIVE

To obtain an experienced structural analysis/stress engineer position in aerospace industry where I can use my strong

analytical, detail-oriented and interpersonal skills to improve products, reduce costs and lead times, delight customers,

help and mentor others. All the while engaging in new challenges and learning experiences.

SUMMARY of QUALIFICATIONS

Master degree in aerospace engineering and bachelor in Airframe & PowerPlant. 10+ years of recent experience

stress analysis in primary and secondary structure, including fatigue damage and tolerance analysis. Extensive

experience in structural analysis, research, leadership and coaching, problem-solving. Excellent in performing hand

calculations per company or industry standards e.g. Book1, Book2, Bruhn, Niu, Roark, Timoshenko etc. Proficient with

Excel, Mathcad, Femap, Patran, Nastran, Abqus, Hyper mesh. Thorough knowledge of load paths for composite and

metallic structures. Expert at analyzing and solving complex problems, such as durability/damage tolerance analyses,

structure stability analysis (lateral torsion stability), dynamic/static load analysis. My structural analysis works were

repeatedly honored by the Boeing Company via Pride@Boeing achievement awards. Self motivated learner and

professional, capable of working independently or as part of a team.

EDUCATION

Master Aerospace Program in Mechanical Engineering Graduated: October 2006

Concordia University, QC, Canada

Bachelor of Mechanical Engineering Graduated: July 1991

Civil Aviation University of China, TianJin, China

COMPUTER SKILLS: CATIA V4/ V5,ENOVIA, MATLAB, MSC PATRAN/NASTRAN, SIMEXPERT, ABAQUAS, HYPER

MESH, FEMAB, IAS, CWS, MathCAD, MS-Office, Windows.

EXPERIENCE

Structure /Stress Analysis Engineer 02/2007- Present

The Boeing Company - Everett, WA

• Perform structural stress analyses on primary and secondary structure using classical hand and computer

technique to develop high strength/weight ratio structures and verify that structural integrity CFR 14 Part 25

requirements are met.

• Develop load path, initial sizing, strength check note documentation, production support and structural test

support.

• Prepare, document and review strength check note for type certification purpose. Create analytical and FEM

method sheets for the analysis to shorten analysis time and overall efficiency.

• Create formal analysis reports for FAA review (such as “747-8 STA396 door intrusion analysis”); generate

interface load coordinate sheets for internal/external customers; review company and vendor drawings, test plan,

and test result report. Perform root cause investigations through analysis.

• Coordinate with design engineering and related groups to optimize design solutions. Ensure new designed parts

or modified/repair components/assemblies compliance with Boeing standard and FAA requirements .

• Analyze structural parts as well as assembly associated with installation of these parts, analysis load cases

included static, stability, fatigue, vibration, and dynamic load cases;

• Coach less experienced or new engineer. Propose and carry out engineering lean activities (server lean…).

• Quick learner, self-motivated, and multi-tasker. Willing to work any shift.

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Structure Analysis Engineer 06/2006 - 01/2007

Dassult Falcon Jet – Little Rock, AR

Performed structure analysis to support of new aircraft program, Falcon7x.

Performed structure analysis using Finite Element Model and/or classical hand calculation.

Developed structural compliance analysis reports which are met aircraft development and certification

requirement.

Used ENOVIA and CATIA V5/V4 carried out design, use ELFINI perform analysis.

Structure Designer and Analyst 09/2005 – 04/2006

CAMAQ (Comité sectoriel de main-d'œuvre en aérospatiale ) – Montreal, QC

• Worked on aerospace project coordinated by CAMAQ, with the sponsors: Bombardier Aeronautics, Pratt & Whitney

Canada, and Bell Helicopter.

• Developed and demonstrated new pylon structure design.

• Wrote FAA/CAA compliant report.

• Developed pylon 3D layout using CATIA V5.

• Used FEM software (NASTRAN / PASTRAN, ANSYS, FEMAB) to perform static and thermal analysis for primary

and secondary structure.

• Took part in Concept Review, Preliminary Design Review (PDR) and Critical Design Review (CDR)

Aircraft Structure/Mechanical Engineer 07/2000 – 08/2002

Cascade Aerospace Inc.- Abbotsford, BC, Canada

Participates in the design of aircraft repairs, modifications and project developments.

Developed designs considering the requirements of the customer, certification authority, and other project

constraints.

Aircraft Structural/Mechanical Engineer 07/1991 – 05/2000

Guangzhou Aircraft Maintenance Engineering Company – GuangZhou, China

Perform as technical trainer, developed and carried out technical training, such as landing gear system training,

flight control system training, engine/APU starting training, hydraulic system training, air conditioning system

training.

Developed and monitored engineering process, ensure the requirements were being compliance. (such as

developed 777 GE engine run procedure, carried out engine run training, performed test using 777 flight simulator,

kept track individual qualifications)

Coached new mechanic on varies aircraft maintenances: line maintenance, C check; D check, etc.

Academic Projects

Sponsor: P&W Canada

Engine Designer - Gas Turbine Design

• Designed a gas turbine from concept of customer required engine performance.

• Designed turbine and compressor blade, calculate strength, and validate performance

Sponsor: Canada Space Agency

Structure / Stress Analysis - Micro Satellite Case Study

• Designed a Micro Satellite using CATIA V5

• Analyzed strength and tolerance for the structure of Micro Satellite.

• Compared and selected appropriate materials for Micro Satellite

Project Engineer - Safety Screw Remover Design

• Developed the concept of safety screw remover, and designed the remover based on the concept.

• Tested the computerized mock up product.

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