Engineering focal for Gas Turbine static component design & analysis and design owner for highly optimized air-cooled nozzles and shrouds for most advanced industrial gas turbinesOptimized airfoil geometry, cooling and thermal barrier design to maximize component life and turbine performance.Performed component stress analysis, low cycle fatigue, Creep and Oxidation for precise life predictions, Hours/Cycles. Revised LCF & Oxidation analysis templates with BPs/LLs.Responsible for driving direct material productivity and achieve design to cost excellence for GE large industrial gas turbines Review design engineer's task and communicate action items, led weekly meeting to track the progress. Define cost out goals and objectives estimated resource requirements and schedule to meet program needs.Developed should cost approach and performed should cost analysis Responsible for driving a smooth operating and prioritization rhythm for cost out project executions among the team through clear communications.Mentoring new entry-level engineers on execution strategies, design/analysis practices and processes

Responsible for Team quality deliverables of Gas Turbine Nozzle and shrouds design and finite element analysis using ANSYS.Determination of analysis requirements and identification appropriate methods and worked out detailed procedures to perform the required analysis, evaluated the results and guided through Chief engineer’s review.Reviewed Team’s work and ensured quality deliverables on time for Gas Turbine Nozzle, Shroud design & analysis cater to new product introduction programs. Types of analyses include static, dynamic and thermal stress, modal, linear and non-linear material analysis, Calculated the Gas Turbine Nozzles and shrouds Low Cycle Fatigue, HCF, Frequency, Campbell Diagram, Bulk Creep Calculation, Local Creep Evaluation.

Led design calculations and stack-up analysis, thermo-structural analysis of gas turbine hot gas path static Components subjected to transient thermal and mechanical loads. Generated component life numbers for Creep, LCF, and HCF& Oxidation.Created models, drawings, bill of Materials, validated Form-Fit-Function, Led supplier qualification, supported manufacturing issues, field upgrades, provided technical resolutions for customer issues at site.Implemented Six Sigma methodologies in component design using DFSS Tools

Responsible for Design calculations and FE analysis of liquid H2 & O2 propellant tanks and interstate structures and optimization of strength to weight ratio and cost.Defined Mechanical system requirements and worked with cross-functional teams to deliver the system design as per project schedule.Developed system & component level validation test request and test planGenerated qualification and acceptance requirements to qualify the subsystem designs during manufacturing.

Responsible for design, Solid Modelling, design calculations, stack-up analysis, manufacturing planning , cost optimization for various Automobile parts.Design experience for the following dies:-AMBASSADOR door dies i.e., piercing, restrike, forming & deep forming diesLancer floor die.TREKKER bonnet die.