Study on Combustor Outlet Temperature Field of Gas Turbine

Author:

Liu Kai1,Xu Li2

Affiliation:

1. Shenyang Aerospace University

2. Shenyang Ligong University

Abstract

Experimental study on combustor outlet temperature field of heavy-duty gas turbine had been finished on high-pressure test system. Experimental results indicate: The OTDF is sensitive to diameter of dilution holes, and the RTDF is sensitive to location of dilution holes. The test results have important guiding significance and reference value to design, commission and working about the similar combustor.

Publisher

Trans Tech Publications, Ltd.

Reference6 articles.

1. ZHANG Baocheng. Experiment and testing technology of aero-engine [M]. Beijing:Beijing University of Aeronautics and Astronautics Press, 2005. (in Chinese).

2. HU Hao-sheng, ZHAO Jian-xing. A new adjustment method of combustor outlet temperature field [J]. Journal of Aerospace Power, 2007, 04: 1222-1226(in Chinese).

3. ZHANG Zheng, ZHANG Yang. Calculational methods of main impact factor to exit temperature of turbine combustor[J]. Journal of Combustion Science and Technology, 2006, 12(6) (in Chinese).

4. PENG Yunhui, LIN Yuzhen. A preliminary experimental study of pattern factor for a triple swirle combustor[J]. Journal of Aerospace Power, 2007, 22(4). (in Chinese).

5. Arthur H. Lefebvre: Gas Turbine Combustion [M]. Washington D.C., U.S.A.: Taylor& Francis Press, 1998:108-115.

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