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[QUOTE=Guest-IJT;102831]RESUME
ROHITH K
#159/12A 19th cross
Lingampally.
Hyderabad
09912264823
Email: savi8.kit AT gmail.com
rohitk AT infotechsw.com

_______________________________________________________________________

OBJECTIVE: A position allowing me to use my experience, knowledge and skills in
the field of Computer Aided Engineering.

SUMMARY:
Ø 2+ Years experience in Gas Turbine Research Establishment.
Ø 3 months of experience in InfoTech. PVT.LTD

SKILLS
CAD Software’s :Auto Cad-2000,Pro-Engineer, Ideas-11Nx.
Meshing Software’s :Hypermesh-7,Ansys,Ideas-11Nx.
Analysis Software’s : Ansys-10, Optistruct 7.

EDUCATION:
Passed B.E (Mechanical) with First Class having aggregate of 70% from K.I.T. College Of Engineering, Tiptur. V.T.U, in June 2006.

Passed PUC with First Class having aggregate of 70% from J.P.U.C college,
Thirthahalli ,Shimoga in 2002

Passed S.S.L.C with First Class having aggregate of 65.12% from J.P.U.C school,
Thirthahalli, Shimoga in 2000

EXPERIENCE:

1. Presently working as a Design Engineer at M/s. InfoTech PVT.LTD., Hyderabad from March 2009 to till date . My responsibilities at work include activities like FE Analysis, FE modeling of gas turbine components, post processing.

2. Previously worked as an Engineer at M/s. Gas Turbine Research Establishment, Bangalore from January 2007 to March 2009 in Structural Mechanics Group. My responsibilities at work include activities like CAD Modeling, FE modeling and CAE Analysis.

PROJECTS

1) 3D and 2D Thermal Analysis of assembled Low Pressure Turbine, Front Retainer Plate, Stub shaft and Sealing. Fatigue Life estimation of Low Pressure Turbine disc.

2) 3D and 2D Thermal Analysis of High Pressure Turbine disc, High Pressure 3rd and 6th stage Compressor discs.
Description:- The objective of the projects is to find the stress distribution in the discs subjected to various types of loadings. A Cyclic symmetric sector of a disc is taken into account & FE model is created in Hypermesh 7, using SOLID 45 for 3D as an element type.
For 2D analysis FE model is created using PLANE 42 as an element type, and Axis Symmetric keyoption is used.
For both 3D and 2D Analysis proper boundary conditions are applied and post processed in ANSYS .

3) 3D-linear, Geometric Nonlinear and Material Nonlinear stress analysis of assembled 2nd stage Low Pressure compressor Disc and Blade .
Description:- The objective is to find the stress distribution in disc, (concentrating in the bore region). FE model is created in Hypermesh 7, by using SOLID 45 as an element type proper Cyclic symmetric boundary conditions are applied and post processed in ANSYS .

4) 3D and 2D shape optimisation of High Pressure Turbine disc.
Description:-The objective of the project is to minimize the volume of the disc by giving various design shapes as design variables, using stress as a constraint. 3D and 2D FE models are created in Hypermesh 7, using SOLID 45 as an element type for 3D, SHELL63,an element type for 2D model & different design shapes have been done using Hypermorphing Technique. Proper boundary conditions are applied & post processed in both Ansys and Optistrut.

5) 3D shapes optimisation of 2nd stage Low Pressure Compressor and 2D shape optimisation of assembled 1st, 2nd & 3rd stage Low Pressure Compressor discs.
Description:- The objective is to minimize the bore stress of the disc by using different design shapes as design variables and displacement as constraint.
3Dand 2D FE models are created in Hypermesh 7, using SOLID 45 as an element type for 3D, plane42 as an element type for 2D model & different design shapes have been done using Hypermorphing Technique. Proper boundary conditions are applied & post processed in both Ansys and Optistrut.

Work Projects AT Infotech:

6) 3D FE modeling and analysis of R6, R7, and R8 High pressure Compressor discs. And preparation of the Reports.
Description:- The objective is to find the stress distribution in disc by interpolating the sub models with global model, FE model is created in Ansys, by using SOLID 45 and SOLID95 as an element type. proper boundary conditions like pressure, temperature mapping cut boundary conditions are applied and post processed in ANSYS .

7) Contact analysis of Forward Thread Tie shaft and Nut assembly.
Description: The objective is to find out the reaction forces, and stresses at the thread location by interpolating the pressure, temperature, and cut boundaries from the Global model.

Personal Details

Father’s Name : Dakappa Gowda K B
Date of Birth : 25-10-1984
Sex : Male
Nationality : Indian
Languages known : Kannada, Hindi, English
References : Available upon request

I hereby declare that the above furnished information is true to the best of my knowledge.

Place:Bangalore (Rohith k)[/QUOTE]

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