ashish sharma

* GE Aviation Munich, Thermal System Design – 9X NPI *  Coordinating 9X module design with RSP partners *  Coordinating thermal technology activity with university and SME through Clean Sky 2 program *  Actively pursuing several ideas to convert into patents *  Working on engine thermal management for current and future engine architecture

* Cornerstone Engineering Development Program *  Advance Course in Engineering *  Two Technical Assignment (6 month each), Working with different discipline *  Leadership training - FOL, BELS, Presentation, Coaching, Facilitation, Hiring, Influencing, Communication, Innovative problem solving, Managing at GE, Thriving in matrix structure organization, intercultural differences, Change acceleration process, project management *  Jet Engine Tear-down School (dismantling and assembling the CF34-8E engine at Cincinnati University) *  TRIZ (theory of inventive problem solving) L1 & L2 expert

* GE Aviation Bangalore, Thermal System Design – Large and small commercial engine *  GEnx compressor and turbine center frame thermal design, analysis, testing and validation *  CF34 -8 high pressure compressor thermal validation with test data *  Compressor design practice update based on learning from engine program *  CDN cavity design with thermal and CFD analysis

* Sterlite Group of Industry *  Mechanical Maintenance of cranes and equipment in plant *  Support leadership in planning and expansion of aluminum extraction plant

* GE Aviation Munich, Thermal System Design – 9X NPI *  High pressure compressor rig design for thermal system, testing and supporting thermal validation *  Worked in multi discipline team for advance seal design, lead thermal and flow design *  Coordinated 9X low pressure turbine design with global team *  Deliver R&T road map for thermal system for next generation technologies