SANTHOSH R. N.
#03, 1st Floor, 5th Cross, Gokul Nagar, Doddakallasandra.
Bangalore-560062
+91-97423 62137 [email protected]+91- 99645 55764
[email protected] Summary of Skills: Accomplished
Mechanical Engineering and Masters in Aircraft Design with solid
background in design and analysis. Hands on experience in cad
modelling using CATIA and AutoCAD. Skills and expertise in aircraft
structures, its assemblies and sub assemblies. Good in hand
calculation of structures and idealization of structures for
analysis. Experience in MSC Nastran for numerical analysis,
creation of finite element model, specifying material properties,
boundary conditions, meshing and post processing and interpretation
of results. Familiar with Matlab codes for analytical calculation.
Adequate in GD&T, stack up analysis, knowledge in ASME Y 14.5 M
1994. Jigs and fixtures design for machining and assembly. Strong
exposure in manufacturing, all types of manufacturing process,
preparation of project plan, process plan, control plan, gauge
plan, selection of materials, estimation and costing. Area of
interest is aircraft structural design, analysis and
composites.Education Qualification:
M. Sc. [Engg.] in Aircraft Design from Coventry University, UK.
(2014)B.E in Mechanical Engineering from VTU, Belguam.
(2011)Diploma in Mechanical Engineering from DTE, Karnataka.
(2008)ITI in Tool & Die Maker from NCVT. (2005)Software
Tools:Engineering Applications:CATIA V5 R19, 3DCSMSC Nastran and
Patran
Programming Languages:
MATLAB, MS ExcelProfessional Experience:TataHAL Technologies
Jan2014-Till dateConsultant Design Engineer [Deputed to HAL LCA-PG]
3D modelling, Drafting, checking 2D and 3D models of front fuselage
of LCA and generated deviation report. Established assembly
sequence for front fuselage. Studied 2D drawing and identified
critical dimensions and ICY features. Applied functional tolerance
and annotations for 3D models in FTA work bench. Prepared of
baseline for stack up analysis. Created assembly sequence by moves
in 3DCS, applying GD&T, used point based and feature based
measurements and Stack up analysis has been done. Idealization of
structures as cantilever beam, simply supported beam and plate with
concentrated load, truss member and performed hand calculation.
Columns were idealized and found out buckling critical loads
analytically. Determined the maximum load it can withstand by
calculating reserve factor and margin of safety for Lockheed Martin
horizontal tail, Rudder assembly jig and scaffolds structure and
prepared report.Maini Global Aerospace Apr 12- Aug13
Engineer- Engineering Dept.
Created 3D model and detailing of model, designed project plan,
process planning, control plan, jigs and fixture. Material
selection, estimation and costing. Selection of tools for
machining, preparation of tool layout. Preparation of gauge plan
and measuring techniques. Review customer standards and Aerospace
standards. Created Routing and BOM in SAP. Analysis and prediction
of failure by FMEA, used quality tools like 7 QC Tools.TRACKMATES
Sep 05- Nov 07
Technician (part time)
Worked on turning, milling, grinding machines and CNC machines.
Strong experience on machining, all kind of manufacturing
processes. Worked in finishing process like grinding, burnishing,
lapping and honing.
Worked on special process, plating, anodising, blackening,
passivation. Worked on continuous improvement in reduction of cycle
time, machining in minimum set up and reducing set up time by
implementing in jigs and fixtures. (SANTHOSH R. N.)
