Effect of Ambient Temperature on Three-Shaft Gas Turbine Performance under Different Control Strategy

Article Preview

Abstract:

Gas turbine is sensitive to ambient temperature. Different ambient temperature could change the state of the inlet air of compressor and make the gas turbine work in off design conditions. Research the effect of ambient temperature on gas turbine performance is valuable to the long-term safe operation of gas turbine. In this paper, a thermodynamic model of a simple cycle gas turbine which has three shafts was established, and steady-state performance simulation under different ambient temperature was carried out. In the two conditions of 1.0 and 0.35 work states, the effect of ambient temperature on thermodynamic parameters, specific power and thermal efficiency of gas turbine were analyzed. The result shows that: effect of ambient temperature on three-shaft gas turbine is different under different work state, and relevant factors must be considered to select the appropriate control strategy

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 424-425)

Pages:

276-280

Citation:

Online since:

January 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Shu-jian Jiao, The investigate of the development way of China's gas turbine in first half of 21st century. Gas Turbine Technology. 14(1): pp.10-13(2001).

Google Scholar

[2] Brooks, F.J., Performance and characteristics of GE gas turbine. East Steam Turbine. (2): pp.52-65(2005).

Google Scholar

[3] Shi-hang Zhao, Gas turbine cycle and off design performance, Beijing: Tsinghua University Press. pp.2-4. (1999).

Google Scholar

[4] Yong-bao Liu, Jian-hua Gao. Marine Gas turbine power plant. 2009. Beijing. Tidal Press. pp.185-188. (2009).

Google Scholar

[5] W.P.J. Visser, M.J. Broomhead. GSP, A generic object-oriented gas turbine simulation environment. National Aerospace Laboratory NLR(2000).

DOI: 10.1115/2000-gt-0002

Google Scholar

[6] W.P.J. Visser, O. Kogenhop, M. Oostveen. A generic approach for gas turbine adaptive modeling. National Aerospace Laboratory NLR(2004).

DOI: 10.1115/gt2004-53721

Google Scholar