Design Engineer Project Management

Lokesh Kumar Bailapudi

**** **. ******* ******, ***. A, Detroit, Michigan – 48201

Mobile: 313-***-****,

Email: ******@*****.***, ***************.**@*****.*** Objective:

Seeking for Mechanical Design Engineer Position with NGC, where my strong analytical thinking, problem solving and communication skills can be utilized. An engineering with G.P.A of 3.83 and several projects in my professional life attest to my hard work and enthusiasm for Mechanical Design Engineer position. I have handful of experience in CAD software like AutoCAD, ProE and Solidworks 3D. I used these CAD software for various projects and course works in my both academic and professional career. I did certified training in both AutoCAD, where I learned various tools, like Drawing, Modelling, and Drafting. I have experience in documentation, quality management, reliability analysis, risk management, cost management and product development. With my work experience in gear designing, I strongly feel that I am a strong candidate for this position.

Technical Skills:

Equipment: Engine Test Cell, Arduino control board, DC motors, 3D Printer, CNC Machine (MASTERCAM). Software: AutoCAD (3D Design), CATIA, ProE, SolidWorks, HyperMesh, ANSYS V15 (Workbench & APDL), Abaqus (Non- linear & Fracture Analysis), LS-Dyna (Crash Analysis), Matlab & Simulink, LabVIEW (Control System), Automation Studio 5.0.

Application: Microsoft Office (Word, PowerPoint, Excel, Outlook), Microsoft Project Management. Educational Qualifications:

Master of Science in Mechanical Engineering (2016-Till Present) Wayne State University, Detroit, Michigan 3.83 GPA B.Eng. (Hons) Aircraft Engineering (2012-2015)

University of the Highlands and Islands (UHI), Perth, U.K 3.5 GPA B.Eng. (Hons) Aircraft Engineering (2011-2012)

Andhra University, Visakhapatnam, A.P, India 3.8 GPA Relevant Coursework:

● Fracture Mechanics (Abaqus).

● Finite Element Methods I (HyperMesh).

● Finite Element Methods II (Advanced HyperMesh, Abaqus, LS-Dyna).

● Crashworthiness and Occupant Protection in Transportation Systems I (LS-Dyna). Work Experience:

SRI VENKATESWARA GEAR WHEELS (Sep 2015 - May 2016) Mechanical Design Engineer (Internship)

Generating and Modifying CAD models using AutoCAD Mechanical (3D Modelling) for various gear type

(Spur, helical, bevel, worm, and time pulley) and gear boxes (like planetary gear box and helical gear boxes).

Running FEA (finite element analysis) for various gear types and reporting critical stress area, life cycle, and reliability.

Understanding the design intent and satisfy whole-ship technical requirements.

Assisted senior design engineer in designing a gear box with turning gear mounted on gear box for total gear set as per requirement of BHEL.

Above gear box is used as speed reducer between high speed steam turbine and generator. University of the Highlands and Islands (Hanger 4, Scone Airport, Perth) (Sep 2013 - May 2015) Lab Assistant

Supporting Prof. Pete Peffer and Prof. Tony Potter in designing and manufacturing of Boeing B737 Simulator.

Developing CAD model for force-feedback system and supporting other team members to integrate various sub-system into simulator.

Manufacturing prototypes and part in the simulator using 3D printer and CNC machine.

Documentation of manufacturing procedures, user manual and quality standards.

Teaching Non-destructive Testing Techniques for freshmen.

Conducting test run for Allison 250 C-10D engine. Academic Projects:

Frontal Crash Analysis for Ford E-Series Van (Jan 2017 to Present)

This project aims to identify the capacity of the Ford E-Series van structure to absorb kinetic energy generated in various types of frontal crash as tested by NHTSA (National Highway Traffic Safety Administration) using FMVSS 208 (Federal Motor Vehicle Safety Standards) and IIHS (Insurance Institute of Highway Studies).

Various test criteria like Full Width Frontal Crash, Frontal Offset Crash (40% wall impact), and Small Overlap Frontal Crash

(25% wall impact) are conducted using LS-Dyna Software by impacting vehicle with both rigid and deformable wall.

Overall vehicle deformation, crash pulse, barrier forces, structural deformation forces, trends in kinetic energy and internal energy of various system in vehicle are analysed.

Summarized by reporting modification to the vehicle to increase the absorption of kinetic energy by various critical systems in vehicle. Modifications are increasing material strength of chassis; and morphing chassis geometry. Designing and Programming Allison 250 C-10D engine test cell control system (Sep 2014 to May 2015)

This project aimed to design and program a user-friendly computerized control system replicating old-fashioned hydro- mechanical control system used in Allison 250 C-10D turbo-shaft engine test cell system.

Replaced the mechanical connections with digital based control using Stepped DC motor, several pressure and temperature sensors, Audrino board and LabVIEW software.

Integrating the LabVIEW software model to the test rig, data acquisition system, electronic throttle and Allison 250 C10-D turbo shaft engine.

Project Management Skills, Team Management Skills, and Cost Management Skills are acquired with the help of Project Supervisor Dr. Quasi Al-Hamdan.

Design and Development of a B737 Flight Simulator (Sep 2013 to Aug 2014)

Designed and developed a fully functional B737 Flight simulator.

Using advanced 3D Design software (AutoCAD), nature of the workload and the forces on the control systems are studied.

The CAD model along with sourced technical data was used as a basis for carrying out design validation using stress analysis tools (Autodesk Inventor 2013) and simulation through MATLAB & Simulink.

Contrasting between the precision positioning table and the proposed assembly design, a total savings of £436 (approximately USD 550) was projected.

Design and Development of Bell Mouth Intake Duct for Allison 250 C-10D engine (Sep 2013 to Jan 2014)

CAD model of typical Bell Mouth Intake duct is designed using CATIA V5.

Stress analysis, air flow rate and fluid streamline flow are generated and studied using ANSYS – Fluent Workbench.

Optimization is carried on and successfully increased the rate of air intake by ten percentage without failing the EASA specifications.

Reliability Analysis for SAAB 340B Landing Gear System (Jan 2014 to May 2014)

All sub-systems in landing gear system are studied.

Using Reliability Workbench, reliability of all sub-systems in landing gear are calculated.

Reliability Centred Maintenance, containing results of Reliability Block Diagram (RBD), Pareto Analysis, Fault Tree Analysis

(FTA), Failure mode effects and critical analysis (FMECA), and Decision Tree Analysis (DTA) are reported. Testing of Climb Performance and Thrust Augmentation (Jan 2013 to May 2013)

Project aims to conducted fuel efficiency test on Boeing B757-300 (integrated with two Rolls Royce RB211-5354E engine).

Engine specifications are studied and analytically fuel consumption is calculated.

Developed Matlab Code for calculating fuel consumption of Boeing B737 during Take-Off, Gliding, and landing. Certifications:

EASA IR Part-66 Approved Basic examination (B1.1 licence). Successfully completed thirteen modules related to aircraft maintenance, human resources and airworthiness.

Successfully completed professional certified courses in AutoCAD, Pro-E, CATIA and Ansys from IGIAT. Achievements & Involvement:

Graduated with distinction, Jul 2015.

Affiliate Student Member, RAeS (Royal Aeronautical Society).

Attended 5th Annual RAeS Aero Conference in Perth College, 22nd & 23rd January, 2015. Delivered a speech on ‘Trends and Effects in Aviation Business in UK’ on behalf of Aviation Business Management Department.

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