Development of a 1300°C-class Gas Turbine Combustor Burning Coal-Derived Low BTU Gaseous Fuels: (3rd Report, Experimental Evaluation of an Advanced Rich-Lean Combustor)

Mikio Sato; Toru Ninomiya; Toshihiko Nakata; Hiroshi Ishikawa; Toshiyuki Yoshine; Masahiko Yamada

doi:10.1299/kikaib.57.803

Development of a 1300°C-class Gas Turbine Combustor Burning Coal-Derived Low BTU Gaseous Fuels: (3rd Report, Experimental Evaluation of an Advanced Rich-Lean Combustor)

Mikio Sato, Toru Ninomiya, Toshihiko Nakata, Hiroshi Ishikawa, Toshiyuki Yoshine, Masahiko Yamada

Research output: Contribution to journal › Article › peer-review

5 Citations (Scopus)

Abstract

This paper describes the development of a 1300°C class gas turbine combustor burning coal-derived low-Btu gaseous fuels. Coal-derived gaseous fuels contain NH₃ if a gas cleaning system is hot type and NH₃ will be converted to NO_x in the gas turbine combustion process. Combustion tests were conducted by using the newly designed, advanced rich-lean combustor. Combustion stability was excellent for the testing combustor because of a subcombustor, so combustion stability could be obtained even when the calorific value of fuel decreased to about 2600 KJ/m³N. As for NOx emission, NH₃ conversion to NO_x was 40% under the full load condition at 1300°C of the combustor exit gas temperature for 1000 ppmv of NH₃ concentration and 0.7 vol% of CH₄ in the fuel.

Original language	English
Pages (from-to)	803-810
Number of pages	8
Journal	Transactions of the Japan Society of Mechanical Engineers Series B
Volume	57
Issue number	535
DOIs	https://doi.org/10.1299/kikaib.57.803
Publication status	Published - 1991
Externally published	Yes

Keywords

Ammonia
Coal Gasification
Coal-Derived Gas
Combustor
Fuel NO
Gas Turbine

ASJC Scopus subject areas

Condensed Matter Physics
Mechanical Engineering

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10.1299/kikaib.57.803

Cite this

Sato, M., Ninomiya, T., Nakata, T., Ishikawa, H., Yoshine, T., & Yamada, M. (1991). Development of a 1300°C-class Gas Turbine Combustor Burning Coal-Derived Low BTU Gaseous Fuels: (3rd Report, Experimental Evaluation of an Advanced Rich-Lean Combustor). Transactions of the Japan Society of Mechanical Engineers Series B, 57(535), 803-810. https://doi.org/10.1299/kikaib.57.803

Development of a 1300°C-class Gas Turbine Combustor Burning Coal-Derived Low BTU Gaseous Fuels : (3rd Report, Experimental Evaluation of an Advanced Rich-Lean Combustor). / Sato, Mikio; Ninomiya, Toru; Nakata, Toshihiko et al.

In: Transactions of the Japan Society of Mechanical Engineers Series B, Vol. 57, No. 535, 1991, p. 803-810.

Research output: Contribution to journal › Article › peer-review

Sato, M, Ninomiya, T, Nakata, T, Ishikawa, H, Yoshine, T & Yamada, M 1991, 'Development of a 1300°C-class Gas Turbine Combustor Burning Coal-Derived Low BTU Gaseous Fuels: (3rd Report, Experimental Evaluation of an Advanced Rich-Lean Combustor)', Transactions of the Japan Society of Mechanical Engineers Series B, vol. 57, no. 535, pp. 803-810. https://doi.org/10.1299/kikaib.57.803

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abstract = "This paper describes the development of a 1300°C class gas turbine combustor burning coal-derived low-Btu gaseous fuels. Coal-derived gaseous fuels contain NH3 if a gas cleaning system is hot type and NH3 will be converted to NOx in the gas turbine combustion process. Combustion tests were conducted by using the newly designed, advanced rich-lean combustor. Combustion stability was excellent for the testing combustor because of a subcombustor, so combustion stability could be obtained even when the calorific value of fuel decreased to about 2600 KJ/m3N. As for NOx emission, NH3 conversion to NOx was 40% under the full load condition at 1300°C of the combustor exit gas temperature for 1000 ppmv of NH3 concentration and 0.7 vol% of CH4 in the fuel.",

keywords = "Ammonia, Coal Gasification, Coal-Derived Gas, Combustor, Fuel NO, Gas Turbine",

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AB - This paper describes the development of a 1300°C class gas turbine combustor burning coal-derived low-Btu gaseous fuels. Coal-derived gaseous fuels contain NH3 if a gas cleaning system is hot type and NH3 will be converted to NOx in the gas turbine combustion process. Combustion tests were conducted by using the newly designed, advanced rich-lean combustor. Combustion stability was excellent for the testing combustor because of a subcombustor, so combustion stability could be obtained even when the calorific value of fuel decreased to about 2600 KJ/m3N. As for NOx emission, NH3 conversion to NOx was 40% under the full load condition at 1300°C of the combustor exit gas temperature for 1000 ppmv of NH3 concentration and 0.7 vol% of CH4 in the fuel.

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KW - Coal Gasification

KW - Coal-Derived Gas

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Development of a 1300°C-class Gas Turbine Combustor Burning Coal-Derived Low BTU Gaseous Fuels: (3rd Report, Experimental Evaluation of an Advanced Rich-Lean Combustor)

Abstract

Keywords

ASJC Scopus subject areas

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