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\pard\intbl\nowidctlpar\fi-360\li360\qj\tx360\f1\'d8 \f0 Captain of the cricketteam in school level. \par\pard\intbl\nowidctlpar\fi-360\li360\sl480\slmult1\qj\tx360\f1\'d8\tab\f0 Gotbest student award in SSC\par\pard\intbl\brdrb\brdrs\brdrw15\brsp40 \shading1000\li-170\ri-170\sa120\qj\bCOMPETENCIES\par\pard\intbl\fi-450\li460\qj\tx10\b0\f1\'d8\tab\f0 CAE : HYPERMESH,MSC NASTRAN &

PATRAN\par\pard\intbl\qj\par\pard\intbl\fi-710\li720\qj\tx460\f1\'d8\tab\f0 CAD : AUTOCAD, CATIA V5\par\pard\intbl\qj\par\pard\intbl\brdrb\brdrs\brdrw15\brsp40 \shading1000\fi-900\li730\ri-155\sa120\qj\bWORK EXPERENCE\par\pard\intbl\qj\b0 \par16 Months of work experience and good theoretical knowledge in Aircraftstructures.\par\par\pard\intbl\sl360\slmult1\qj\tx0\tx1908\b Company : \b0 InfotechEnterprises Limited \par\pard\intbl\nowidctlpar\sl360\slmult1\qj\tx0\tx1908\b Working :

\b0 Since Aug 18, 2008\par\b Department : \b0 Aerospace\b \b0\par\pard\intbl\nowidctlpar\sl360\slmult1\qj\tx0\tx1630\tx1908\b Designation:\cf3\b0 Design Engineer\par\pard\intbl\nowidctlpar\sl360\slmult1\qj\tx0\tx1908\par\pard\intbl\shading1250\keepn\s4\fi270\li-270\ri-720\qj\tx0\tx1908\cf0\b PROJECTSUMMARY\par\pard\intbl\nowidctlpar\sl360\slmult1\qj\tx0\tx1908\cf3\parProject Title : \cf0\b0 Structural design of Fixed Leading Edge ofG650\par\b Client : \b0 Gulfstream Aerospace, US\par\b Software Used : \b0 CATIA V5 R17\par\b Role : \b0 Team Member\b\par

Duration : \b0 3 months\par\pard\intbl\qj\cell\row\trowd\trgaph170\trleft-810\trrh15329\trpaddl170\trpaddr170\trpaddfl3\trpaddfr3\clshdng1000\cellx2880\cellx10260\pard\intbl\qj\b\par

\par\par\pard\intbl\fi-426\li426\qj\par\par\cell\pard\intbl\fi-1886\li1900\qj\par\parDescription \b0 \b :\b0 Project involves Structural Design of FixedLeading Edge for Gulfstream Aerospace of GVI P20 Aircraft. Design targets are

weight reduction of wing and 50% part count reduction by designing part asstandard, increase strength by designing in subassemblies like clips, ribs,intermediate ribs, plenum beam, splice strap, Intercostals etc. All CATIA modelshave been developed by using Relational Layout Modeling (RLM) technique for easymodification.\par\pard\intbl\fi-1890\li1900\qj\par\par\par\pard\intbl\nowidctlpar\fi-1900\li1900\sl360\slmult1\qj\tx1691\cf3\b Project Title: \cf0\b0 Drafting 3D CATIA models for D-jet\par\b Client : \b0 Diamond Aircraft Industries, Canada.\par

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\b Software Used : \b0 CATIA V5 R17\par\b Role : \b0 Team Member\b\par\pard\intbl\nowidctlpar\fi-1900\li1900\sl360\slmult1\qj\tx1596\tx1691 Duration: \b0 2 months\par\pard\intbl\nowidctlpar\fi-1900\li1900\sl360\slmult1\qj\tx1540\b Description: \b0 This project involves generating manufacturing drawings and installationdrawings using GD&T as per ASME Y14.5 1994 standards for the given 3D CATIA models(customer inputs).\par

\pard\intbl\fi-1890\li1900\qj\b Role Played : \b0 I was responsible forcreating 2D drawings by studying 3D part and sheet metal models and also appliedGD&T.\par\par\par\b\par\pard\intbl\nowidctlpar\fi-1900\li1900\sl360\slmult1\qj\tx1691\cf3 Project Title: \cf0\b0 FE Modeling and Analysis of Aircraft Interiors\par\b Client : \b0 Midcoast Aviation, US.\par\b Software Used : \b0 Hyper mesh, MSC Nastran & Patran\par\b Role : \b0 Team Member\b\par\pard\intbl\nowidctlpar\fi-1900\li1900\sl360\slmult1\qj\tx1596\tx1691 Duration: \b0 2 months\par

\pard\intbl\fi-1890\li1900\qj\b Description : \b0 The scope of the projectis to prepare an FE Model and the QAS report of the aircraft Interiors. Theaircraft interiors consist of galleys, storage cabinets, closets, bulkheads, sideledges, etc. FE Modeling of panels is done for all the honeycomb panels with Nomexand Norlam type. The assembly is constrained at the floor attachments to simulatethe seat track at one end and at the other end to simulate the connection to theframes by tie rod. The aircraft interiors are analyzed for the flight, emergencylandings, abuse and rapid loss of pressure.\b\cell\row\trowd\trgaph170\trleft-810\trrh15329\trpaddl170\trpaddr170\trpaddfl3\trpaddfr3\clshdng1000\cellx2880\cellx10260\pard\intbl\qj\par

\par\par

\par\par\cell\parAnalysis done :\par\pard\intbl\fi-360\li720\qj\tx720\b0\f2\'b71\tab\f0 FEA of the interiors andmethod of application of loads.\par\f2\'b72\tab\f0 Modal analysis check of the monument\par\f2\'b73\tab\f0 Static analysis of the monument for the four load cases.\par\f2\'b74\tab\f0 Load Extraction for all the components like tie rods, hinges,latches, panel loads, inserts, panel attachments, pins, etc.\par\f2\'b75\tab\f0 Stress analysis of components like lug, tie rod tube, inserts,brackets, honeycomb panels, seat tracks. \par\pard\intbl\li720\qj\par

\par\pard\intbl\nowidctlpar\fi-1900\li1900\sl360\slmult1\qj\tx1691\cf3\b Project Title: \cf0\b0 FE MODEL REGISTRATIONS FOR AIRBUS A400M\par\b Client : \b0 GKN Aerospace.\par\b Software Used : \b0 MSC Nastran & Patran\par\b Role : \b0 Team Member\b\par\pard\intbl\nowidctlpar\fi-1900\li1900\sl360\slmult1\qj Duration :\b0 3 months\par\pard\intbl\nowidctlpar\fi-1900\li1900\sl360\slmult1\qj\tx1900\b Description: \b0 The scope of the project is to check the element quality, shell orientationand material orientation according to the client\rquote s requirement and make

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necessary changes on the element if it does not satisfy the requirements of theclient. Generate new bulk data file and run the bdf in Nastran for Normal modesand Linear Static Analysis. Results in op2 and f06 format are delivered to thecustomer along with a detailed report for the registration of the FE model for theAirbus UK which gives all the details of the FE model and plots of thedisplacement and stress tensors.\par\b\par\pard\intbl\qj\b0\par

\pard\intbl\shading1250\keepn\s4\fi270\li-270\ri-720\qj\b STRENGTHS\par\pard\intbl\nowidctlpar\qj\b0 Hard Working, Self Confidence, positive thinking\par\pard\intbl\sl360\slmult1\qj\tx1380\par\pard\intbl\brdrb\brdrs\brdrw15\brsp40 \shading1000\li-170\ri-170\sa120\qj\bHOBBIES\par\pard\intbl\qj\b0 Cooking, watching animation pictures\par\pard\intbl\brdrb\brdrs\brdrw15\brsp40 \shading1000\li-170\ri-170\sa120\qj\bDeclaration\par\pard\intbl\qj\b0 I hereby declare that the above-mentioned information is correctup to my knowledge and I bear the responsibility for the correctness of the above-mentioned particulars \par

\par\par

Date:yours faithfully,\parPlace:\iK.Satish Kumar\cf1\i0\par\cf0\b\cell\row\pard\qj\b0\par}#