Component Damage Prediction Analytic • Developed data science-based damage analytics to predict damage on engineering components, usingaircraft engine operational parameters (time series data)• Feature Engineering - Created the summarized features from the time series data• Ensemble (Random Forest, Gradient Boosting) & Regularization algorithms are used for feature ranking• Performed correlation & density plot studies to screen the features• Regression models used to build final predictive models with 68% Rsquare• Collaborated with global teamsPredictive Maintenance of a gas turbine engine part using LSTM RNNs to predict the remaining useful life of the part. - Regression Problem • A 3 layer LSTM Recurrent Neural Networks has used to predict the remaining useful life of the gas turbine part and it is implemented in keras. • Achieved a 60% Rsquare by tuning various hyper parameters GE Health care Hackathon (Team Participation)• Built a deep denoiser CNN model to enhance the PEC scan image features•“Beyond a Gaussian Denoiser: Residual Learning of Deep CNN for Image Denoising “architecture hasconsidered for this problem• Transfer learning has implemented to reduce the computational time• Tensorflow library has used to build this modelLead Engineer - Mechanical Design• Hardware owner of LEAP-1A/1C HPC Extension case and GP7200 A & B Sumps/Bearing compartments.Being a hardware owner, hold and executed the role responsibly by taking care of the process changes, vendor source (VSE) approval for the manufacturing process.• Management award for excellence in hardware ownership and Material Review Board (MRB)certification in structures commodity.

-Led and executed static parts certification, life and design analysis programs across engine lines -Cost focal for the LEAP cost out team. -Effectively communicated and Collaborated with different groups at global sites and executed program plans-Understood the engine service manual (ESM) limits and proactively substantiated the MRBs(Any deviation from drawing) & Field issues appropriately.

Working on gas turbine engines/aircraft engines as a design engineer. And the Roles & Responsibilities are as follows.-Led and executed static parts certification, life and design analysis programs across engine lines -Cost focal for the LEAP cost out team. -Effectively communicated and Collaborated with different groups at global sites and executed program plans-Understood the engine service manual (ESM) limits and proactively substantiated the MRBs(Any deviation from drawing) & Field issues appropriately. -Documented all results of assigned programs with proper review rigor and ensured all deliverables of assigned programs meet the required expectation.