Internship Programme Delhi : www.ilo.org International Labour Organization

[muthukalee]

Internship

The Knowledge Team is looking for an intern (see the Terms of reference - (pdf 41 KB)) to assist all the main knowledge management functions, mostly extracting, analyzing and packaging knowledge, in order to make it accessible, build competencies of microinsurers and advocate for microinsurance. Deadline to apply is April 11th.

Fellowship programme

Fellowships allow young professionals to gain hands-on experience in microinsurance by working onsite in a microinsurance programme under the remote guidance of a mentor and, at the same time, to build the institutional capacity of the host organization. The assignments, based in developing countries, last from 6 to 12 months. Fellows are provided with monthly stipends that vary by host country and experience. Fellowships are learning opportunities and not offers of employment.

Please only apply to the position for which you feel most qualified. In your application correspondence, please tell us from which sources you heard about the opportunity (Newsletter, Media, blogs, Linked in, Twitter, etc.). Eventually, due to the high number of applications, we will only communicate with short listed candidates.

India Deadline Application 31 March 2011
The United Nations Development Programme (UNDP) is supporting the Emmanuel Hospital Association (EHA) with a project focussed on "Strengthening of Rashtriya Swasthya Bima Yojana (RSBY: National Health Insurance Scheme) through Community Engagement and Voluntary Benchmarking Network for Healthcare Quality Management". The project seeks a Microinsurance Fellow to assist its development and delivery through working with the project team on data analysis, process alignment and product development. The assignment offers a practical opportunity for developing "hands-on" insights to health microinsurance in India, including a large, dynamic national social protection scheme

http://www.ilo.org/public/english/em...ortunities.htm

[Guest-IJT]

Name : prabakaran R
Email : praba22aero AT rocketmail.com
Designation / Skillset : knowledge in CATIA,pro-e,Autocad,ANSYS.Interested in aircraft maintenance and production.
sir, i am a B.E-aeronautical engineer(fresher),looking for the job.so please call me if you have vacancies.thank you

Resume :

POSITION SOUGHT :
Design Engineer/Maintenance Engineer.
CAREER OBJECTIVE :
I am interested in any position that encompasses my current skill set. I always aim to update my knowledge and skill in accordance with latest trends and confident of handling bigger and complex tasks. I assure to work towards the growth of the organization.
PROFESSIONAL SUMMARY :
B.E- Aeronautical Engineering
Batch : 2007-2011
College : Jaya Engineering College, Chennai.
University : Anna University, Chennai.
EDUCATIONAL QUALIFICATION :
- Under graduation : 2007-2011 76%
B.E Aeronautical Engineering
Jaya Engineering College
Chennai.
- Higher secondary education : 2005-2007 89%. Rajavignesh hr.sec. school
- High school education : APRIL-2005 89%
Govt.high school,
Nallampalayam
SKILL SET :
- I have good knowledge in following software.
CAD Modeling Tool : CATIA V5-R15, AutoCAD, Pro-e, ANSYS.
SPECIAL SKILLS :
- I am skilled in Engineering drawings
- I can motivate others in work.
- I can be a good leader for a team.
- I can handle situations under pressure.
- I can be a good team worker.
STRENGTHS :
- Aptitude for creative work
- Passion to work on CAD.
- Good team player.
PROJECT DETAILS :
I. Failure investigation of compressor rotor blade :
The aim of the project is to investigate the cause for failure in gas turbine compressor rotor blades using stress analysis method.The blade,disc and spacer assembly of the compressor rotor blade is modeled using CATIA and meshed using gambit
The analysis is carried out for two cases using tecplot.For case -1 :disc sector –blade assembly and for case-2:disc sector- blade –spacer assembly. The analysis concludes that the spacer in contact with blade platform surface act as the stress raiser that initiate the crack.
Further a failure model for different crack lengths is modelled using CATIA and analysed using ANSYS.From that variation of stress intensity factor for different parameters are plotted .From that recommendation for future work is given to reduce stress.
2.Design of supersonic business jet :
We propose a design of supersonic mid-long-Range business jet intended to have a cruise mach no of 2.1 and cruise altitude of 55000ft and Range of 4000nm.all the essential calculations are made theoretically for the design.
AREAS OF INTEREST :
- Aircraft maintenance
- Aircraft propulsion
- Aircraft Structures.

Your’s faithfully,
Place :
Date : (R.PRABAKARAN)
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More Information about this submission and submitter:-
___________________________________________________
Submission ID : 4443212
Date & Time : 4th Aug 2011 4:52 AM (UTC)
IP Address : 14.96.214.177
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