Gas Turbine

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SEMINAR REPORT
2012-13

GAS TURBINE

GUIDE : Dr. B.M. SUTARIA,
ASSOCIATE PROFESSOR,
SVNIT

PREPARED BY:

VIJAY J VERMA (U09ME644)
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SARDAR VALLABHBHAI NATIONAL INSTITUTE OF TECHNILOGY

CERTIFICATE
This is to certify that the project entitled “GAS TURBINE” has been submitted by the following student under my guidance in partial fulfilment of the degree of Bachelor of Technology in Mechanical Engineering from Sardar Vallabhbhai National Institute of Technology, Surat during the academic year 2012-2013.

VIJAY VERMA U09ME644

They have successfully and satisfactorily completed their PROJECT PRELIMNARY in all respect. We certify that the work is comprehensive, complete and fit for the evaluation.

Dr. B. M. SUTARIA Dr. H. K. RAVAL
Project guide, HOD, MED,
Asst. professor, SVNIT,Surat.
MED, SVNIT, Surat.

EXAMINERS: SIGNATURE WITH DATE 1.___________________________________ _______________________ 2.___________________________________ _______________________ 3.______________________________ ___________________ -------------------------------------------------

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ACKNOWLEDGEMENT

I take this opportunity to express my profound gratitude and deep regards to my guide Dr. B.M. SUTARIA, Associate Professor, Mechanical Engineering Department, SVNIT, for his exemplary guidance, monitoring and constant encouragement throughout the course of this project. The blessing, help and guidance given by him time to time shall carry us a long way in the journey of life on which we are about to embark.

I am thankful to Dr. H.K.RAVAL, Professor and Head of Mechanical Engineering Department, SVNIT. I am also thankful to our evaluators for their time and patience, as well as for providing this opportunity which helped me in gaining further knowledge and to make this project report successfully.

I would also like to thank the Mechanical Engineering department and all the people who provided us with their help. -------------------------------------------------

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Gas turbine

A gas turbine, also called a combustion turbine, is a type of internal combustion engine. It has an upstream rotating compress or coupled to a downstream turbine, and a combustion chamber in-between. Energy is added to the gas stream in the combustor, where fuel is mixed with air and ignited. In the high pressure environment of the combustor, combustion of the fuel increases the temperature. The products of the combustion are forced into the turbine section. There, the high velocity and volume of the gas flow is directed through a nozzle over the turbine's blades, spinning the turbine which powers the compressor and, for some turbines, drives their mechanical output. The energy given up to the turbine comes...
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