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Volume 4: Cycle Innovations; Electric Power; Industrial and Cogeneration; Manufacturing Materials and Metallurgy | 2006

Development of Elemental Technologies for Advanced Humid Air Turbine System

Hidetoshi Kuroki; Takanori Shibata; Tomomi Koganezawa; Nobuaki Kizuka; Shigeo Hatamiya; Shinya Marushima

The Advanced Humid Air Turbine (AHAT) system improves the thermal efficiency of gas turbine power generation by using a humidifier, a Water Atomization Cooling (WAC) system, and a heat recovery system, thus eliminating the need for an extremely high firing temperature and pressure ratio. The following elemental technologies have been developed to realize the AHAT system: (1) a broad working range and high-efficiency compressor that utilizes the WAC system to reduce compression work, (2) turbine blade cooling techniques that can withstand high heat flux due to high-humidity working gas, and (3) a combustor that achieves both low NOx emissions and a stable flame condition with high-humidity air. A gas turbine equipped with a two-stage radial compressor (with a pressure ratio of 8), two-stage axial turbine, and a reverse-flow type of single-can combustor has been developed based on the elemental technologies described above. A pilot plant that consists of a gas turbine generator, recuperator, humidification tower, water recovery system, WAC system, economizer, and other components is planned to be constructed, with testing slated to begin in October 2006 to validate the performance and reliability of the AHAT system. The expected performance is as follows: thermal efficiency of 43% (LHV), output of 3.6 MW, and NOx emissions of less than 10 ppm at 15% O2. This paper introduces the elemental technologies and the pilot plant to be built for the AHAT system.© 2006 ASME


Archive | 2004

Turbine power plant, installation process and removal process of the turbine power plant

Hidetoshi Kuroki; Isao Takehara; Yasuyuki Watanabe; Seisaku Takihana


Archive | 2011

Member having internal cooling passage

Nobuaki Kizuka; Yasuhiro Horiuchi; Shinya Marushima; Hidetoshi Kuroki


Archive | 2011

GAS TURBINE SHROUD WITH CERAMIC ABRADABLE LAYER

Yoshitaka Kojima; Hideyuki Arikawa; Akira Mebata; Tadashi Kasuya; Hiroyuki Doi; Kunihiro Ichikawa; Takao Endo; Kazuto Mikazuki; Hidetoshi Kuroki


Archive | 2005

Heat resisting steel, gas turbine using the steel, and components thereof

Masahiko Arai; Hirotsugu Kawanaka; Hiroyuki Doi; Isao Takehara; Hidetoshi Kuroki


Archive | 2003

GAS TURBINE AND COOLING AIR INTRODUCING METHOD

Hidetoshi Kuroki; Eitaro Murata; Isao Takehara; Noriaki Tanaka; 英太郎 村田; 宜昭 田中; 竹原 勲; 英俊 黒木


Archive | 2002

Turbine power plant

Hidetoshi Kuroki; Isao Takehara; Yasuyuki Watanabe; Seisaku Takihana


Archive | 2012

Ni-BASED FORGING ALLOY, AND GAS TURBINE USING THE SAME

Takashi Shibayama; 隆史 芝山; Shinya Konno; 晋也 今野; Hiroki Kamoshida; 宏紀 鴨志田; Hidetoshi Kuroki; 英俊 黒木; Jun Sato; 順 佐藤


Archive | 2012

Axial-Flow Compressor and Modification Method

Hironori Tsukidate; Hidetoshi Kuroki; Atsushi Sano


Archive | 2011

Guide vane assembly for axial compressor

Atsushi Sano; o Hitachi; Hidetoshi Kuroki; Hironori Tsukidate; Hidetaro Murata; Nobuaki Kizuka

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