A Gas-Turbine with Approximate General Carnot Cycle and Its Performance Prediction

Zhong Li; Da Long Zhang; Jian Feng Li; Ding Hua Yang; Wen Jun Qin; Gen Sheng Yang; Xiao Lin Wang

doi:10.4028/www.scientific.net/AMR.960-961.1134

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 960-961A Gas-Turbine with Approximate General Carnot...

A Gas-Turbine with Approximate General Carnot Cycle and Its Performance Prediction

Abstract:

Based on polytrophic process of air compression and gas combustion inside the turbine isothermally, an approximate gas-turbine with General Carnot cycle and relevant implementing schemes are suggested. Its performance was predicted with mathematics model compared with traditional one. The results show that the heat efficiency of the suggested gas turbine is higher than the traditional one. The suggested cycle combines the gas cycle and steam cycle, of which the NOx emission can be easily decreased

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Periodical:

Advanced Materials Research (Volumes 960-961)

Pages:

1134-1141

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.960-961.1134

Citation:

Cite this paper

Online since:

June 2014

Authors:

Zhong Li, Da Long Zhang*, Jian Feng Li, Ding Hua Yang, Wen Jun Qin, Gen Sheng Yang, Xiao Lin Wang

Keywords:

Combustion in the Turbine, Gas-Turbine, General Carnot Cycle

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* - Corresponding Author

References

[1] Wang Rugen, Gao Kunhua. New technology of aero-engine. Beijing: Aviation Industry Press. (2003).

Google Scholar

[2] Li Shuying Zheng Qun et al. Cycle Analysis of Gas Turbine with Water Injection into Inter-Stage of its Compressor. Ship Engineering. 2001 . 3，pp.28-33.

Google Scholar

[3] Siregnano W A, Liu F. Performance Increases for Gas-Turbine Engines through Combustion inside the Turbine. Journal of Propulsion and Power. 15(1) No. 1, Jan-Feb 1999, pp.111-118.

DOI: 10.2514/2.5398

Google Scholar

[4] Liu F, Siregnano W A. Turbojet and Turbofan Engine Performance Increases through Turbine Burners. Journal of Propulsion and Power. Vol. 17, No. 3, May-June 2001, pp.695-705.

DOI: 10.2514/2.5797

Google Scholar

[5] Yan Jialu. Engineering Thermodynamics. Beijing: Higher Education Press. (2001).

Google Scholar

[6] Shen Bingzheng. Device of Gas turbine. Beijing: China Machine Press. (1981).

Google Scholar

[7] WU Guang2liang, LIU Run-zao, et al. Studing on High Temperature Air Combustion Using Reaction Engineering Method. Journal of Iron and Steel Research. Vol. 16, No. 2 Apr. (2004).

Google Scholar

[8] AI Yuan-fang, JIANG Shao-ji, et al. Experimental Study of High-temperature Air and Flameless Combustion and Its Flame Characteristic. Journal of Engineering for Thermal Energy & Power. 2001, 16(6). p.615~617.

Google Scholar