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PROFESSIONAL PROFILE
A versatile professional seeking a challenging role in technology design & management and apply my experience of multidisciplinary engineering to provide excellent solutions.
WORK EXPERIENCE:
RESEARCH FELLOW, Design System Project Lead – Cranfield-BOEING IVHM Centre, Cranfield University, UK: FEB 2010 – CURRENT
Technology development responsibilities:
· Undertake parametric design, analysis of low bypass turbofan engine serpentine nozzle and computational analysis of designed nozzle.
· IVHM Design system –Generic end to end solution architecture for Integrated Vehicle Health Management. Use cases for Rolls Royce and BAE Systems were used for validations.
· IVHM design for BAE System Warship integrated with Rolls Royce power plant.
· Implementation and modification in design tools and methods, eg QFD, MADe, PICAM and SHOAM (IVHM tool set for BOEING)
· IVHM functionality systems and system implementations for existing EHM tools like Total care for Rolls Royce.
Project Management responsibilities:
· Project Management of aircraft advanced technologies. Prepare statement of cases, sanctions and financial concurrence for sponsored projects.
· Plan, organize and carry out technical review of outsourced work. Ensure compatibility and security of data transfer of sensitive material.
· Assist in preparation of task schedule for technology specific directorates. Organize regular weekly reviews of design teams.
RESEARCH ASSISTANT – National high temperature surface engineering centre – High temperature corrosion laboratory – Surface science and engineering centre - Department of Engineering Materials, Cranfield University, UK.: May 2009 – Jan 2010
PROJECT ENGINEER – (MECHANICAL / AERONAUTICAL) - BHR Group –The Fluid Engineering Research Centre – Cranfield University, UK: SEP 2008 – MARCH 2009
· Stress analysis of Aircraft Structures – Static stressing for turbo machinery bladin fuselage and wing structures. Roughness and impulse testing - Aircraft landing gears
· Stress field analysis for aero structure, modelling of crack growth, crack arrest and fatigue
· Safe Life Structural Design Criterion Analysis for structural failures which occurs in aircraft wings, propeller blades and engine discs
ISRO SATELLITE CENTRE (ISAC), Indian Space Research Organisation (ISRO), BANGLORE,
INDIA – INTERNSHIP – JAN 2006- APRIL2006
· Developing satellite technology and implementation of satellite systems for scientific, technological and application missions.
· Inter-planetary space mission shifting – Mission modelling
LIQUID PROPULSION SYSTEMS CENTRE (LPSC), Indian Space Research Organisation ISRO, BANGALORE INDIA - INTERNSHIP -, OCT 2005- JAN 2006
· Research was focussed on study of Earth Storable and Cryogenic propulsion, stages, associated control systems and components for Launch Vehicle and Spacecrafts.
· Liquid propulsion risk assessment
EDUCATIONAL BACKGROUND & EXPERIENCE:
PhD RESEARCHER – AEROENGINE NOVEL PROPULSION SYSTEM DESIGN & PERFORMANCE
DETERIORATION MODELLING – TECHNO ECONOMIC RISK ANALYSIS (TERA) DEPARTMENT OF PROPULSION, CRANFIELD UNIVERSITY, Jan 2008 – PRESENT
· Invention and generation of stochastic probabilistic distributions to predict aero propulsion performance characteristics
· Analysis of the aero/thermal requirements for Gas Turbine components
· Preliminary and final design studies for Turbo-machinery (Compressor & Turbines)
· Design methodologies for greener efficient combustors
· Development of Techno-economic risk assessment (TERA) framework to predict possible optimized technology selection
· Analysis of the aero/thermal requirements for Aero-engines for predicting performance
· Aircraft trajectory optimizations & multi-disciplinary design optimisations (Boeing)
· Design, planning and implementation of new concepts for Aero-engines (Open rotor Detonators)
· Worked closely with Rolls Royce, AIRBUS, P&W and few leading European universities
MSc – AEROSPACE MATERIALS, DEPARTMENT OF ENGINEERING MATERIALS, UNIVERSITY OF SHEFFIELD, SEP 2006 – SEP 2007 (DISTINCTION)
· Individual Research Project based on design, manufacturing and testing for unique concept Self healing composites for aerospace applications sponsored by AIRBUS.
· Group design project focused on stress field modelling of material for Aero-engine Integration
· Finite element analysis & modelling was extensively used for this research project. analysis was employed to look at the bulging and fatigue crack growth behaviour fuselage pressure bulkhead and wing structures (FEM, CATIA)
· Research study was conducted to understand the impact of nanotechnology for detecting early initiation of cracks in advanced engineering materials.
BTech– AERONAUTICAL ENGINEERING, UNIVERSITY OF BOMBAY, INDIA,SEP 2002- Aug 2006 - (DISTINCTION)
· Research thesis was focussed on developing novel Ion - Solar propulsion systems shifting space activities from one planet to other using Unmanned Space Vehicle.
· Group design project - Estimation of contact conductance for nuclear fuel bundles in Reactor for Aviation Fuel. All the experimentations were carried on at Baba Atomic Research Centre, Mumbai, India.
· Leakage characteristics, heat transfer operations and fluid interaction impacts were modelled and analysed. CFD modelling was used for heat flux flow patterning.
COMPUTER SKILLS:
• Design Tools & Languages: MATLAB, C++, VB, CATIA, CFD, FEA
• Proficiency in MS-Office (Word, Excel, Access, PowerPoint), VBA
| 1 month - Discovery | 400 euros | convert |
| 3 months - Bronze | 1050 euros | convert |
| 6 months - Silver | 1800 euros | convert |
| 12 months - Gold | 2950 euros | convert |