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[QUOTE=Guest-IJT;146089][b]Name [/b]: Ranganath.N
[b]Email [/b]: ranganath_nag AT yahoo.co.in
[b]Designation / Skillset[/b] : fresher
BE (mechanical), Mtech (mechanical)

[u][b]Resume[/b][/u] :
 
OBJECTIVE
To serve in the competitive industry, with extreme dedication and ethics. Also to implement the knowledge for the growth of organization and grow along with it.
ACADEMIC PROFILE
POST GRADUATION [Pursuing]
Branch Institution University Year of Passing AGGREGATE
Machine Design
[b]USN [/b]: 1BI09MMD12 Bangalore Institute of Technology, Bangalore Visvesvaraiah Technological University, Belgaum 2011 66.45%
(Till third semister)
GRADUATION
[b]Class obtained [/b]: SECOND CLASS
Branch Institution University
Year of Passing
AGGREGATE Percentage
Mechanical Engineering
Visvesvaraiah Technological University, Belgaum
[b]year of passing  [/b]:2009
[b]aggregate percentage [/b]:56.75
MTECH PROJECT WORK
[b]Title  [/b]: “THE ROLE OF RIVET LOAD TRANSFER ON STRUCTURAL INTEGRITY OF FUSELAGE STRUCTURE”
[b]COMPANY  [/b]: BANGALORE AIRCRAFT INDUSTRIES PVT.LTD
- In a metallic airframe, mechanical fastening plays a dominant role in the structural safety. Rivets are designed for efficient load transfer between structural members being fastened.
- Fatigue cracking in the splice joints of the pressurized cabin of a large transport aircraft is the major threat to the structural safety. Such pressurized cabins are designed to be tolerant to such fatigue cracking
- Such a design ensures that fatigue crack will not lead to a catastrophic failure
- In this project the role of rivets in the crack arrest capability of a 2-bay circumferential crack in a fuselage will be investigated. The rivet material, size and pitch will be varied in a parametric study employing finite element analysis approach.
ELECTIVES STUDIED
[b]In Mtech [/b]:
[b]- 1st semester  [/b]: computer graphics
[b]- 2nd semester  [/b]: theory of plasticity
[b]- 3rd semester [/b]: Design for manufacturing and Fracture mechanics
BE PROJECT WORK
[b]Title  [/b]: “DESIGN AND ANALYSIS OF SUBSYSTEM SUPPORT STRUCTURE”
[b]COMPANY  [/b]: ISRO
- Increased accuracy of payloads, the on-orbit structural dynamic behavior of spacecraft is increasingly influencing the design and performance of spacecraft.
- Present work is on the design of a satellite subsystem support structure assembly for mass reduction with safe operating conditions.
- The forces imparted to the spacecraft are important for sensitive instruments.
- In this report a safe configuration is suggested with significant achievement in mass reduction.
ELECTIVES STUDIED
[b]In BE [/b]:
[b]- 6th semester  [/b]: Internal Combustion Engine
[b]- 7thsemester  [/b]: Non Conventional Energy Sources and Foundry Technology
[b]- 8th semester  [/b]: Composite Materials and Non Destructive Testing
TECHNICAL SKILLS
[b]- Software’s  [/b]: Auto CAD, Catia v5 & Msc Nastran Patran (basics)
[b]- Packages  [/b]: MS Office 2007
 
STRENGTHS
- Hardworking and responsible.
- Can work in a group as well as individually.
- Good communication skills.
 
 I here by confirm that the above information furnished by me is correct to the best of my knowledge and belief. 
[b]Date  [/b]: 
 
 RANGANATH.N 
 [b]Place  [/b]: Bengaluru
-------------------------------------------------------
[b]More Information about this submission and submitter [/b]:-
___________________________________________________
Submission ID : 4386897
Date & Time : 19th Jul 2011 6:44 AM (UTC)
IP Address : 117.192.203.72
Browser Info : Mozilla/5.0 (Windows NT 5.1; rv:6.0) Gecko/20100101 Firefox/6.0
Predicted Country : India[/QUOTE]

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