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タイトルTrial operation results of steam cooled M501H type gas turbine
その他のタイトル水蒸気冷却M501H型ガスタービンの試運転結果
著者(日)塚越 敬三; 前川 篤; 伊藤 栄作; 百武 慎徳; 川田 裕
著者(英)Tsukagoshi, Keizo; Maekawa, Atsushi; Ito, Eisaku; Hyakutake, Yoshinori; Kawata, Yutaka
著者所属(日)三菱重工業 原動機事業本部; 三菱重工業 高砂製作所; 三菱重工業 技術本部 高砂研究所; 三菱重工業 高砂製作所; 三菱重工業 技術本部 高砂研究所
著者所属(英)Mitsubishi Heavy Industries Ltd. Power Systems Headquarters; Mitsubishi Heavy Industries Ltd. Takasago Machinery Works; Mitsubishi Heavy Industries Ltd. Takasago Research & Development Center, Technical Headquarters; Mitsubishi Heavy Industries Ltd. Takasago Machinery Works; Mitsubishi Heavy Industries Ltd. Takasago Research & Development Center, Technical Headquarters
発行日2002-10
刊行物名Mitsubishi Heavy Industries Technical Review
Mitsubishi Heavy Industries Technical Review
39
3
開始ページ85
終了ページ89
刊行年月日2002-10
言語eng
抄録The 'H' series gas turbine is a high efficiency and high power output gas turbine. The total thermal efficiency is about 2 percent higher and the output power is about 10 percent greater than that of a G series gas turbine. The reason the 'H' series gas turbine can achieve a higher efficiency and a larger output is that its high temperature turbine first-and second-stage vane/blade are cooled by steam supplied from the bottoming cycle, instead of conventionally used air. Accordingly, the amount of bleed air from the compressor can be reduced. In 1999, the first trial operation of the 'H' series gas turbine was conducted in the in-house verification power generation facility installed at the Takasago Machinery Works of Mitsubishi Heavy Industries, Ltd. (MHI). A second trial operation run was subsequent completed successfully at the same facility in 2001. Consequently, MHI has completed development of this new gas turbine using the prototype of the 'H' series gas turbine. This paper reports on the development of the 'H' series gas turbine.
キーワードgas turbine; steam cooling; compression ratio; steam turbine; combustion gas; heat loss; air cooled condenser; thermal efficiency; ガスタービン; 水蒸気冷却; 圧縮比; 水蒸気タービン; 燃焼ガス; 熱損失; 空冷コンデンサ; 熱効率
資料種別Journal Article
ISSN0026-6817
SHI-NOAA0035807001
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/42331


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