Final Report of the Key Technology Development Program for a Next-Generation High-Temperature Gas Turbine-Reference-Cited by-同舟云学术

Final Report of the Key Technology Development Program for a Next-Generation High-Temperature Gas Turbine

Published:1997-07-01 Issue:3 Volume:119 Page:617-623
ISSN:0742-4795
Container-title:Journal of Engineering for Gas Turbines and Power
language:en
Short-container-title:

Author:

Sato M.¹,Kobayashi Y.¹,Matsuzaki H.¹,Aoki S.²,Tsukuda Y.²,Akita E.²

Affiliation:

1. Tohoku Electric Power Co., Inc., Sendai, Japan

2. Takasago Machinery Works, Mitsubishi Heavy Industries, Ltd., Takasago, Japan

Abstract

There is a strong demand for efficient and clean power-generating systems to meet recent energy-saving requirements and environmental regulations. A combined cycle power plant is one of the best solutions to the above [1]. Tohoku Electric Power Co., Inc., and Mitsubishi Heavy Industries, Ltd., have jointly developed three key technologies for a next-generation 1500°C class gas turbine. The three key technologies consist of: (1) high-temperature low-NOx combustion system. (2) row 1 turbine vane and blade with advanced cooling schemes, and (3) advanced heat-resistant materials; (2) and (3) were verified by HTDU (High Temperature Demonstration Unit). This paper describes the results of the above-mentioned six-year joint development.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Link

http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/119/3/617/5615889/617_1.pdf

Reference5 articles.

1. Hori et al., “Outline of Plan for Advanced Research Gas Turbine,” ASME Paper No. 81-GT-28, ASME JOURNAL OF ENGINEERING FOR POWER, Vol. 103, Oct. 1981.

2. Kano et al., “Development Study of 1500°C Class High Temperature Gas Turbine,” ASME Paper No. 91-GT-297.

3. Matsuzaki et al., “Investigation of Combustion Structure Inside Low Nox, Combustors for a 1500°C-Class Gas Turbine,” ASME Paper No. 92-GT-123.

4. Amagasa et al., “Study on the Turbine Vane and Blade for a 1500°C Class Industrial Gas Turbine,” ASME Paper No. 93-GT-414. ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER, Vol. 116, 1994, pp. 597–604.

5. Sato et al., “High Temperature Demonstration Unit for a 1500°C Class Gas Turbine,” ASME Paper No. 94-GT-412.

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