Chetan Keshavamurthy
Bis 2008, Mechanical Engineering, Birla Institute Of Technology and Science, Pilani
Munich, Deutschland
Werdegang
Berufserfahrung von Chetan Keshavamurthy
Bis heute 8 Jahre und 2 Monate, seit März 2016
Berechnungsingenieur-Struktur
Rotorschmiede GmbH
Stress Analysis of Co-Axial Ultralight Helicopter Structure
3 Jahre und 7 Monate, Apr. 2011 - Okt. 2014
Senior Stress Engineer / Senior Berechnungsingenieur
Assystem India Private Limited
Stress analysis of Primary and Secondary structures in various Airbus Aircraft Programs (A350, A380, A320 Neo). Generation of Stress Reports and Stress Dossiers. Have been the project focal / point of contact and interacted extensively with the customers during the execution of projects. Have lead project teams of 2 - 10 members.
4 Monate, Mai 2014 - Aug. 2014
Stress Engineer (Onsite) - From Assystem India
Spirit Aerosystems, Kuala Lumpur, Malaysia
Stress calculations for sizing of Root End Fixed Fairing (REFF) assembly components for Airbus A350-900 MSN21. Preparation of Preliminary Stress Sheet (PSS)
9 Monate, Okt. 2012 - Juni 2013
Stress Engineer (Onsite) From Assystem India
Airbus France, Toulouse
Static Strength validation of Central Fuselage junctions (Section 15 - 21) for the Airbus A350XWB-900 aircraft (MSN1) Justification Stress reports for the Central Fuselage junctions (Section 15 - 21) (MSN 1) and Preparation of ACD4 sheets
1 Monat, Dez. 2011 - Dez. 2011
Stress Engineer (Onsite) From Assystem India
Assystem UK, Isle of Man, UK
Sizing Calculations and analysis of Airbus A350-900 Wing Leading Edge System Brackets for MatC configuration. Preparation of Preliminary Stress Sheet (PSS) for the System brackets.
2 Monate, Sep. 2011 - Okt. 2011
Stress Engineer (Onsite) From Assystem India
Assystem UK, Prestwick, Scotland, UK
Updation of Airbus A380 Wing Inner Outer Fixed Leading Edge(IOFLE) Stress Calculations and Stress Dossiers for the revised loads.
6 Monate, Nov. 2010 - Apr. 2011
Technical Lead / Technischer Leiter
CYIENT ((Formerly Infotech Enterprises Pvt. Ltd.), Hyderabad, India
Client: GKN Aerospace - Checkstress calculations and Stress Dossier preparation for Airbus A400M trailing edge devices - Outer False Work (OFW) and Inner Fixed Shroud (IFS)
2 Jahre und 3 Monate, Aug. 2008 - Okt. 2010
Stress Engineer / Brechnungsingenieur
UTC Aerospace Systems (Formerly Goodrich Aerospace), Bangalore, India
Stress Calculations and Stress Reports for Boeing 787-8 and 777F Cargo Handling Systems. Analysis of Boeing 787-8 Aircraft Interior (Flight Deck) and Exterior Lights and Fixtures and preparation of Stress Reports for Lighting Systems. Airbus A380 Gas Generator for Evacuation Slides Analysis for the Evacuation Systems. Airbus A350 Tool Handling Equipment Analysis for Aerostructures Group.
3 Monate, Okt. 2009 - Dez. 2009
Stress Engineer (Onsite) From UTC Aerospace - India
UTC Aerospace Systems - Lighting Systems, Long Island, Ney York, U.S.A
Exposure to various types of testing of Aircraft Interior and Exterior Lights for Boeing 787-8. Detailed documentation of Tests and verification of tests and test reports with Quality Test Procedures.
6 Monate, Jan. 2008 - Juni 2008
Praktikum / Intern (As part of Practice School - Master of Engineering Program)
National Aerospace Laboratories (N.A.L), Bangalore, India
Multidisciplinary Design Optimization of transport aircraft wing.
1 Jahr und 7 Monate, Feb. 2005 - Aug. 2006
Design Engineer / Entwicklungsigenieur
Avasarala technologies, Bangalore, India
Design calculations for Material handling systems and Special Purpose Machinery. Conceptual Design and preparation of Part & Assembly Drawings. FE Analysis of designed components for their Structural Integrity if required
8 Monate, Juni 2004 - Jan. 2005
Design Engineer (Contract) / Entwicklungsingenieur / Konstruktuer
Hindustan Aeronautics Limited (H.A.L), Bangalore, India
Preparation of 3D Models, Engineering Drawings.
11 Monate, Juli 2003 - Mai 2004
Design Engineer - Trainee / Entwicklungsingenieur
Sandhar Group (Zuvor Adeep Group)
• technischen Zeichnungen von Schlösser, Radfelge, Zink-Druckguss Komponenten für den Automotive Bereich • Konzeption von Teilen und Baugruppen; Erstellung von 3D Modellen; Einzelteil und Zusammenbau Zeichnungen
Ausbildung von Chetan Keshavamurthy
2 Jahre, Juli 2006 - Juni 2008
Mechanical Engineering
Birla Institute Of Technology and Science, Pilani
Finite Element Analysis, Theory of Elasticity, Non Destructive testing, Heat Transfer, Machine Technology, Robotics, Computer Aided Analysis and Design.
4 Jahre, Aug. 1998 - Juli 2002
Mechanical Engineering
Bangalore Institute of Technology (Visvesvaraya Technological University)
Strength of Materials, Design of Machine Elements, Kinematics and Dynamics of Machines, Finite Element Analysis, Advanced Material Technology, Experimental Stress Analysis, Fluid Mechanics, Thermodynamics, Heat Transfer, Manufacturing technology.
Sprachen
Englisch
Muttersprache
Deutsch
Fließend