LOTFI E. EL-BAYOUMY

Yorba Linda, CA **** Tel: 714-***-****

e-mail: adbh3e@r.postjobfree.com linkedin.com/in/lotfi-el-bayoumy Stress, Vibration and Structural Integrity Expert

Leading Teams and Ensuring Aerospace Structural Integrity Senior Level Stress & Vibration Analyst with substantial track record of managing and leading effective aerospace technical solutions, from concept through detailed design to qualification tests. Known for excellence in proofing structural integrity of aerospace and mechanical systems and for solving complex engineering problems. Experience with both commercial and military aircraft, including fixed and flexible wing, manned and unmanned. Projects include the F-35, MQ-25, K-46, QUESST, NEXUS, B787 and A-350. Lead from a “Do It Right the First Time” mentality. Hold Ph.D. in Aerospace Engineering. Chair of multiple professional committees. Published multiple articles. Hold US Patent. Areas of Expertise include:

Vibration Analysis & Test Support Finite Element Analysis (FEA) Modal Analysis

Fracture Mechanics Damage Tolerance Dynamic System Modelling

Actuation System Modelling Isolation System Design Rotating Machinery Diagnostics

Gear Design & Optimization Fatigue Assessment

TECHNICAL SKILLS HIGHLIGHTS

Extensive Product Line Base Comprising: Electromechanical Actuation Systems, A/C Jet Engines, Turbo machinery, Airframe Structures, Hydraulic & Pneumatic Systems, APU’s, HPU’s, EPU’s, ECU’s, AMAD’s, EMAD’s, Helicopter Transmissions, Winches, Hoists, and Cargo Handling Systems.

Complete mastery of a wide spectrum of Analytical Techniques including FEA, Shock & Vibration Analysis Modal Analysis Testing, Signature Analysis, Machine Monitoring & Built-in Diagnostics, Acoustics, Damage Tolerance, Fracture Mechanics, Fatigue, Gear & Bearing Technology, and Mechanism Analysis.

Proficiency of most popular Computer Codes including: ANSYS, NASTRAN, PATRAN, UG-NX, Solid Works, PRO/E, MECHANICA, MATLAB, MathCad, NASGRO, A. B. Jones Bearing Programs and a Variety of Gear Programs.

Engineering Management of Multi-Disciplinary Groups Comprising Structural Analysis, System Simulation, Reliability, Test Engineering, Technical Services and Required Staffing. EXPERIENCE IN DETAIL

MOOG AIRCRAFT GROUP, Torrance, CA September 1996 – September 2019 Supplying innovative product solutions to aerospace offering flight and engine control, including most military and commercial aircraft in existence.

SENIOR STAFF ENGINEER/PRODUCT INTEGRITY ENGINEERING MANAGER/IR&D MANAGER Led, managed, supervised, organized, and executed all principal engineering activities for proofing High Lift & Utility Actuation Systems on Military & Commercial Aircrafts, including MQ-25, KFX, KC-46, NEXUS, QUESST, F-18, F-35, F-22, C-5, T-50, V-22, A330, A330, G450, G250, G500, G600, G650, 787, A350.

Set up project budgets and schedules, ensured cost containment, on-time delivery, product quality.

Lead the preparation of successful proposals.

Contributed subsystem level architecture, verification and validation approaches, component level contract requirements, requirements compliance assessment, government regulations, cost estimates and technical write-ups.

Lotfi E. El-Bayoumy 714-***-**** adbh3e@r.postjobfree.com Page 2 of 2

Provided motivation, support and guidance during all phases of Product Development, including analysis, design and test.

Achieved quality results on time and on budget.

Formed & lead all R&D (Research & Development) teams advancing Aircraft Actuation Systems.

Organized and taught a series of Training Seminars in Professional Engineering Disciplines.

Instituted, in coordination with Information Technology, a continuing program that upgraded analytical capability. Substantially increasing the speed of the analysis and achieving higher levels of accuracy.

Created and communicated effective presentations to customers during all phases of the program.

Resolved issues emanating from product deficiency and took corrective action to mitigate them.

Developed new formulas for quantifying damping and dynamic amplification factors of mechanical and structural components, which has a direct impact on structural element sizing.

Instituted and directed weekly design and analysis reviews to gauge and meet program schedule. RECENT KEY ACCOMPLISHMENTS BY AIRCRAFT

MQ-25 – Managed to incorporate an optimized mounting system for wing-fold actuation system, in a very tight envelope, meeting all flight loads, shock and vibration requirements.

F-35 – Ensured through detailed vibration analysis that all leading edge and wing-fold actuation components are properly monitored during the test to guard against extraneous damaging inputs

KC-46 – Guided the customer to come up with the proper vibration and shock input for the boom and hoist actuation system and followed through to ensure that the entire system pass the test without failure.

A-350 – Managed, directed and executed all analysis efforts on the complex trailing edge actuation system consisting of rotary actuators, down-drives, angle gearboxes and wing-tip brakes. OTHER RELEVENT EXPERIENCE

LUCAS AEROSPACE (Currently, Triumph Gear Systems)

(Formerly, Western Gear Corporation), Geared Systems Division, Park City, UT ENGINEERING TECHNOLOGY MANAGER

SUNDSTRAND CORPORATION (Currently Hamilton Sundstrand), Rockford, IL. GROUP ENGINEER/ CHIEF OF DYNAMICS

PRATT & WHITNEY AIRCRAFTE. Hartford, Conn.

ADVANCED VIBRATION ANALYST

EDUCATION

Ph.D. - Solid Mechanics, New York University

M.Sc. - Aeronautical Engineering, Cairo University B.Sc. - Aeronautical Engineering, Cairo University PROFESSIONAL & HONOR SOCIETIES

Chair, AIAA Orange County Section

Ex-Chair, Acoustics, Shock & Vibration Committee, SAE Member, AAM, AIAA, ASME PTGC, SAE G-5

New York University Honors Scholar

Member, Sigma Gamma Tau (National Aerospace Honor Society) Listed in Who is Who in the West, Who is Who in Aviation, and Who is Who in Finance and Industry PUBLICATIONS & PATENTS

Extensive List of Publications Covering a Wide Area of Engineering Disciplines Including Vibration Control, Turbo machinery, Gearing, Structural Stability, and Stress Analysis. United States Patent, Patent No.: US 8,118,958 B2, COMPOSITE RING GEAR WITH METALLIC GEAR INSERT, AND METHOD OF FORMING SAME.

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