A study on LBG-fueled 1500°C-class gas turbine combustor for use in IGCC (1st report, design study and atmospheric combustion test of a combustor)

Takeharu Hasegawa; Mikio Sato; Tohru Ninomiya; Toshihiko Nakata

doi:10.1299/kikaib.64.582

A study on LBG-fueled 1500°C-class gas turbine combustor for use in IGCC (1st report, design study and atmospheric combustion test of a combustor)

Takeharu Hasegawa, Mikio Sato, Tohru Ninomiya, Toshihiko Nakata

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

Abstract

The development of "integrated coal gasification combined cycle systems" ensures cost-effective and environmentally-sound options for fulfilling future power generation needs. In our laboratory, we are developing a 150 MW, 1 500°C-class gas turbine combustor for IGCC by using an air-blown coal gasifier both to enhance thermal efficiency and to reduce NO_x emission from the plant. This paper descrides the design of the 150 MW, 1 500°C-class gas turbine combustor, at atmospheric pressure for IGCC based on the stable and low-NO_x combustion technology developed to date. Combustion tests are conducted and the performance of this combustor is evaluated. Test results confirm the excellent performance of the combustor for use in a gas turbine in IGCC and project bright prospects as a high temperature, low NO_x combustion technology of the low calorific fuel.

Original language	English
Pages (from-to)	582-589
Number of pages	8
Journal	Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
Volume	64
Issue number	618
DOIs	https://doi.org/10.1299/kikaib.64.582
Publication status	Published - 1998 Feb
Externally published	Yes

Keywords

Ammonia
Coal gasification
Combustion
Combustion products
Gas turbine
Low btu fuel
Nitrogen oxides

ASJC Scopus subject areas

Condensed Matter Physics
Mechanical Engineering

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10.1299/kikaib.64.582

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A study on LBG-fueled 1500°C-class gas turbine combustor for use in IGCC (1st report, design study and atmospheric combustion test of a combustor). / Hasegawa, Takeharu; Sato, Mikio; Ninomiya, Tohru; Nakata, Toshihiko.

In: Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, Vol. 64, No. 618, 02.1998, p. 582-589.

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

Hasegawa, T, Sato, M, Ninomiya, T & Nakata, T 1998, 'A study on LBG-fueled 1500°C-class gas turbine combustor for use in IGCC (1st report, design study and atmospheric combustion test of a combustor)', Nihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, vol. 64, no. 618, pp. 582-589. https://doi.org/10.1299/kikaib.64.582

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abstract = "The development of {"}integrated coal gasification combined cycle systems{"} ensures cost-effective and environmentally-sound options for fulfilling future power generation needs. In our laboratory, we are developing a 150 MW, 1 500°C-class gas turbine combustor for IGCC by using an air-blown coal gasifier both to enhance thermal efficiency and to reduce NOx emission from the plant. This paper descrides the design of the 150 MW, 1 500°C-class gas turbine combustor, at atmospheric pressure for IGCC based on the stable and low-NOx combustion technology developed to date. Combustion tests are conducted and the performance of this combustor is evaluated. Test results confirm the excellent performance of the combustor for use in a gas turbine in IGCC and project bright prospects as a high temperature, low NOx combustion technology of the low calorific fuel.",

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author = "Takeharu Hasegawa and Mikio Sato and Tohru Ninomiya and Toshihiko Nakata",

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AB - The development of "integrated coal gasification combined cycle systems" ensures cost-effective and environmentally-sound options for fulfilling future power generation needs. In our laboratory, we are developing a 150 MW, 1 500°C-class gas turbine combustor for IGCC by using an air-blown coal gasifier both to enhance thermal efficiency and to reduce NOx emission from the plant. This paper descrides the design of the 150 MW, 1 500°C-class gas turbine combustor, at atmospheric pressure for IGCC based on the stable and low-NOx combustion technology developed to date. Combustion tests are conducted and the performance of this combustor is evaluated. Test results confirm the excellent performance of the combustor for use in a gas turbine in IGCC and project bright prospects as a high temperature, low NOx combustion technology of the low calorific fuel.

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A study on LBG-fueled 1500°C-class gas turbine combustor for use in IGCC (1st report, design study and atmospheric combustion test of a combustor)

Abstract

Keywords

ASJC Scopus subject areas

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