(Photo to be
attached)
M.Tech. Dissertation Project
(2002):
“Singular
Stress Distribution around an Interface Crack in Whisker Reinforced
Metal
Matrix Composite -- Finite Element Investigation”
Synopsis:
This
dissertation project deals with the study of singular stresses around a penny
shaped interface crack in metal matrix composites. The crack is considered at
the interface of whisker and matrix material. Finite element study is carried
out using the front end commercial software ANSYS (Ver: 5.4) adopting its
fracture mechanics capabilities. Aluminum/Silicon carbide MMC system is
considered in the analysis.
Job
Objective:
An M.Tech (Design) engineer presently working in Geometric Software Solutions Ltd (GSSL) Bangalore with 3+ years of
experience seeking a challenging career in Design and Analysis using state of
the art tools in CAE.
Education:
M Tech (Design Engineering) V T U Karnataka 78% 2003 Mar
BE Mechanical
CAE Software: Abaqus, Hypermesh, Ansys
Fair Knowledge of Nastran, Patran.
CAD Software:
Solid Works, AutoCAD.
1. GEOMETRIC SOFTWARE SOLUTIONS LTD
(GSSL)
Working
as Design Engineer, at Engineering
Service Division
·
Structural static, Dynamic and contact analysis
Using preprocessing using Hypermesh and solver using Abaqus.
·
Finite Element Modeling using Hypermesh.
·
Worked for MSC Software Ltd Pune, for
development of new FEA software for MSC Software, Worked as End user level
Testing for new FEA Software, coordinated
with developers in developing basic functions of FEM for developing new product
from scratch. Worked with developers for
successful launch of first release of software. Written various test cases for
new product. Worked on Nastran Patran for solving static problems.
·
Lead a team of 10 Engineers for
customization of Products using XML programming and interlinking with Solid
works tools to generate desired design for customer with minimal effort.
2. NATIONAL AEROSPACE LABORATORY (NAL)
Worked
as Project Assistant at Closed Circuit Centrifugal compressor test
rig Lab for Development of MICRO
GAS TURBINE and test Rigs.
·
Static structural Analysis of
various Micro Gas turbine parts like compressor, turbine etc
·
Modeling and analysis of turbine and
compressor.
·
Design, modeling and Drawing of compressor
test Rig using Solidworks.
·
Solid modeling and Assembly modeling of Micro Gas turbine using Solid Works
·
Finalizing design, drawing and Detailing,
Providing fits and tolerances for Micro Gas turbine.
·
Responsible for development of Rapid
prototyping of intricate parts of aero engines and manufacture parts using
investment casting.
3. Atlas Gears Ltd (A division of
Worked as an Engineer in Production Planning and Control Department,
Lead a team of five members in planning and project execution for development
work of automobile gears.
·
Work involved daily and monthly scheduling,
process planning and development, time study.
·
Plant Layout, cost estimation and modeling
of process sheets using AutoCAD and Solid works.
·
Inventory control, Pro- E solid modeling.
·
Worked in a team for plant layout
considering various processes, which greatly reduced cycle time and idle time
for production, which earned greater revenue to the company.
i) Centrifugal Compressor analysis (Coupled Field analysis)
This involves couple field analysis of centrifugal compressor,
where compressor experiences various complicated loads like thermal,
structural, vibrational and aerodynamic loads, a finite element analysis is
carried out to find out stresses and deflections developed in compressor due to
these types of loads.
ii) Centrifugal Turbine analysis (Coupled Field analysis)
This involves couple field analysis of centrifugal turbine,
where turbine experiences various high temperature, structural, vibrational and
aerodynamic loads, a finite element analysis is carried out to find out
stresses and deflections developed in compressor due to these types of loads.
iii) Thermal and structural Analysis of bearing housing
Turbine end (MGT)
Analysis is carried out
using Ansys, where various possible configurations are carried out for analysis
and an optimized Housing is developed with minimal thermal transfer rate and
stress.
iv) Design, optimization and FE analysis of turbine Balancing
Disk.
Turbine Balancing disc experiences high temperature and
pressure loads, A optimization study is carried out to minimize the weight and
to maintain maximum possible interference between running shaft and balancing
disc,
Ø
Structural and Modal Analysis of Co-ordinate measuring
Machine. (Assembly Analysis)
An assembly model of CMM machine is meshed using Hypermesh,
Tied contacts are used at various locations where two parts are bolted. There
were around 50 tied contacts. Static and modal analysis is carried out for CMM
machine using Abaqus processor
Ø
Transient Analysis of Speedometer-Casing under various
gravity loads
A speedometer casing is meshed using hypermesh, time
dependent load is applied at the center of the speedometer, and a transient
Dynamic analysis is carried out using Abaqus tool.
Ø Contact and Modal analysis of a
connectors
Non-linear contact
analysis of connectors are carried out for different types of connectors, and
modal analysis carried out for these connectors, pre-processing done using
hypermesh and processing done using Abaqus.
Ø Structural frequency Analysis of ADR Heat
Shields
ADR Heat Shield are
used for Volvo trucks for environment safety, a structural analysis is carried
out to find Stresses developed at the Joints and also Frequency analysis is
carried out for finding out mode shapes in heat shields. Pre-processing done
using hypermesh and processing done using Abaqus.
Ø Structural frequency Analysis of Cooper
Street Lights
A static analysis is
carried out for Cooper Street Lights for its self weight and wind loads and
stresses developed at the brackets are found out, a frequency analysis is
carried out to find first 10 Modes of Vibration using hypermesh and processing
done using Abaqus.
Ø Contact Analysis of Car Window regulator
A contact analysis is
carried our Car Window regulator, where contact region is defined for the pin
and the wheel assembly and between rope and wheel, a force of 600 N is applied
at the end of the rope and analysis is carried out, contact stresses developed are studied. Using
Hypermesh and Abaqus.
Projects:
Ø Design and development of complete Micro
Gas Turbine system
This Micro Gas Turbine is designed to obtain a
power of around 10 kW by converting aero engine into 10 KW power generating
unit. Work involves Finite Element Modeling, Finite Element Analysis, and
communication of FE results to Designers. Complete Assembling of Micro Gas
Turbine using design tools. Following Finite Element analysis is carried out
using Ansys, Abaqus and Hypermesh.
Personal Details:
Father’s Name:
Ganapati V. Naik; Passport Details:
A 6193957 (Valid up to 2008)
Reference:
Mr. Rajendran, Scientist E2. NAL, 080-25051788, 25051787
Contact details:
Address: c/o Mr. Swaminathan, #1312, Off
Permanent: “Sanskriti” bldg, Near
Bhaskar dairy, 2nd main, 7th
cross, Sadashivnagar, Belgaum-590001
Pho: 0831-2473606
Pho: 0831-2473606 Cell:
0-9945939770
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