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New Design of Ignition System of Gas Turbine
Abstract:
This paper is all about a new type of ignition system for igniting the air-fuel mixture within combustion chamber of a gas turbine engine. In this system there will a separate ignition inside the primary combustion chamber which will be outside the main combustion chamber and responsible for igniting main source of air/fuel mixture inside the combustion chamber. This system is designed to overcome several problems of present ignition system of gas turbine engine and also thermal analysis of this new system has been shown in this paper.
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Pages:
1662-1666
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Online since:
July 2014
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© 2014 Trans Tech Publications Ltd. All Rights Reserved
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