As a Consultant worked on variety of projects for Rolls-Royce aviation engines. Contributed significantly to the Infosys business by playing multiple roles such as Team leader for NPI, Capability Lead for Rotatives team and Project manager for several cost reduction projects. Involved in recruitment, staffing and mentoring, effort estimations. Led NPI projects for IP Turbine disc design and stress analysis to meet Aircraft certification, EASA, FAA requirements. Worked on multiple solutions… Show more As a Consultant worked on variety of projects for Rolls-Royce aviation engines. Contributed significantly to the Infosys business by playing multiple roles such as Team leader for NPI, Capability Lead for Rotatives team and Project manager for several cost reduction projects. Involved in recruitment, staffing and mentoring, effort estimations. Led NPI projects for IP Turbine disc design and stress analysis to meet Aircraft certification, EASA, FAA requirements. Worked on multiple solutions including production, development, instrumentation solutions. Worked as a facilitator for DFMEA, DfM, DfA, DfS. Worked as a Cost team lead for different engines including Trent XWB-84/-84EP, Trent 1000-TEN, Trent 7000, Trent XWB-97 engines. Show less

• As Principal Engineer and component owner, successfully led Rolls-Royce projects for Trent XWB-84/-84EP engines NPI and cost reduction projects.• Led HP compressor project from requirements review (DTA1) to final design review (DTA5) and F-Issue release.• Performed finite element analysis including detailed thermal, structural analysis, low cycle fatigue, handling damage calculations to certification, EASA, FAA requirements.

Overview: As a part of Atkins Aerospace team, worked on Aircraft structures, wing components for Aircraft certifications.Customers: Airbus-UK, Bombardier- Canada, Piaggio & Meggitt-UK.Responsibilities:• Performed fatigue and damage tolerance (F&DT) calculations using Airbus ISAMI tool, written stress dossiers for wing components for the certifications of civil, and military aircraft for Airbus, Bombardier, Piaggio & Meggitt.• Worked on military aircraft Airbus A400M interface… Show more Overview: As a part of Atkins Aerospace team, worked on Aircraft structures, wing components for Aircraft certifications.Customers: Airbus-UK, Bombardier- Canada, Piaggio & Meggitt-UK.Responsibilities:• Performed fatigue and damage tolerance (F&DT) calculations using Airbus ISAMI tool, written stress dossiers for wing components for the certifications of civil, and military aircraft for Airbus, Bombardier, Piaggio & Meggitt.• Worked on military aircraft Airbus A400M interface loads processing, fatigue spectrum and F&DT analysis for wing components including ribs, aft fittings, shear plate, and cleats.• Worked on variety of aircraft structural components including wing box, fuselage, landing gear, horizontal tail plane. Show less

Overview: As part of Infosys engineering team, managed various clients including Alstom gas turbines and IHI Japan.Responsibilities:• Worked as Engineering manager for team of 12 people and 2 project managers.• Involved in Alstom project on composite blade design and IHI centrifugal compressor design & analysis.Highlights:• Established team to support Alstom gas turbines and IHI Japan.

Overview: As Lead engineer and component owner, led design, development and FE analysis of GE gas turbine engine components.Responsibilities:• As a Lead engineer and component owner, led design, development and FE analysis of GE gas turbine engines 6FA, 7EA, 7H, 9H.• Worked on various as turbine components including primary flow path, hot gas path components such as buckets, shrouds, nozzles.• Component owner for compressor discharge casings, combustion wrappers, Inner barrels… Show more Overview: As Lead engineer and component owner, led design, development and FE analysis of GE gas turbine engine components.Responsibilities:• As a Lead engineer and component owner, led design, development and FE analysis of GE gas turbine engines 6FA, 7EA, 7H, 9H.• Worked on various as turbine components including primary flow path, hot gas path components such as buckets, shrouds, nozzles.• Component owner for compressor discharge casings, combustion wrappers, Inner barrels, and bearings.• Led 7EA combustion wrapper root cause analysis (RCA) team. Conducted root cause analysis investigations.• Designed combustion wrapper horizontal joint seal, which got successfully implemented on the production engines as well as in service engines. Resolved combustion wrapper horizontal joint leakage issues which addressed health and safety issue. Provided resolution to the global 7EA gas turbine customers. Show less