Deputed at Onsite location - Caterpillar; Worked in Machine System Simulation (MSS) Team in VPD Group in ITDDSPOC for Enclosure projects from Hydraulic Excavator Development Center (HEDC), CAT Japan

On-roll: GGS Information Services India Private Limited, ChennaiDomain: Hydraulic ExcavatorHydraulic Excavator products worked on:NGH Series (313, 320, 325, 330, 335, 336, 345, 349) ; Other Series (314 E, 323 FN, 329 F, 335 F, 349 D2)G load & Modal Analysis, Linear Contact Analysis, Comparative Analysis, Wind load & Step load AnalysisPull load & Modal Analysis performed for testing the strength of the Hand Rail designsBolt Strength Analysis for the bolts used in Plastic Door and Hand RailLMT Xmsn AIQ ECM Enclosure - Linear & Modal Analysis; 740 B - Articulated Truck - ECM Stiffness AnalysisFE discretization of the complete enclosure assembly as per HEDC modeling guidelines (313 NGH, 335 NGH, 335 F)Runs off-shore supplier teams for timely delivery of multiple simultaneous projectsManagerial experience in understanding client requirements and coordination with project teams

Deputed at Onsite location - Atlas Copco; Supported for onsite CAE projects in GECIASupported for offsite projects like Non-linear Static Analysis of Test rig and fixtures, Modal analysis of Impeller

Deputed at Onsite location - Atlas Copco; Worked in CAE group in GECIA

Extensively trained on Compressor, Turbine and Heavy Engineering Structures as per Atlas Copco StandardsHands-on-experience in real-time projects using FE tools like HyperMesh, HyperView and Abaqus

On-roll: ProSIM R&D Private Limited, BangaloreDomain: Compressor, Dryer & Pressure VesselStructural Strength Calculations of Skid and Supports for the loading conditions that includes Operational, Wind, Seismic, Transportation, Lug lifting, Fork lifting, Ice & Snow loading and Lug proof testLoad values needs to be calculated based on the specified codes and standards like ASCE, UBC, BS-EN, IBCFork Lifting Simulations with Linear Contacts that includes Contact parameters, Master and Slave surfaces definedContact simulation results were found and the von-Mises stress values are within the AISC allowable limitBurst Pressure Simulation for CPN Vessel to check the burst pressure value of the vesselDesign pressure value is applied on the internal faces of the vessel and the bolting locations are constrained in all DOFsThe pressure values are increased in an incremental way (step-by-step) by defining multiple sub-cases in the same simulation and the intermediate results are checked against the yield limitPressure value for which the stress is marginally less to the ultimate limit is defined as the burst pressure valueAutomation Project: Bolt Strength Calculation - Automated BDF file and Report generationIntegral part in the successful implementation of GECIA-CAE Process Manager for Pre-processing & Post-processingFE discretization of Skid and Support structures, Support Brackets and Lugs in HyperMeshAttended several training programs in Altair Office for Auto-meshing, Automation and OptimizationReceived excellent appreciation from the top management for successful completion and timely delivery of projects

Domain: Aircraft Structures & FE MethodologiesExpertise in Meshing of Wing Components, Loads extraction, Hand Calculations and Global to Local Model ConversionStructural Analysis of Aircraft Skin and Stringer, Stress analysis of Aircraft Wing Rib and SparAutomation Projects: BDF Generator for Multiple Load cases, Automated Truss ResolutionGood exposure on Hand Calculations of Aircraft Structural Components using Bruhn and Niu Methods

Domain: Aircraft StructuresFE discretization of Aircraft Wing Rib and Spar, Wing Box Segment in HyperMesh to meet the specified quality criteriaTrained in Meshing Techniques of HyperMesh including MS Extraction, Shell & Solid Mesh, Sheet (Plastic) MeshCreated Automated Templates using VBA Macros for Section Analysis and Digitization of MMPDS (Material Library)

Completed the course Analysis 003 that includes Analytical Methods, FEA: MSC Patran/Nastran, HyperMesh, ANSYSAero Structural Fundamentals, Project Preparation using FEA & Classical Analysis Methods