Development of a Maintenance Program for Major Gas Turbine Hot Gas Path Parts

Author:

Moritsuka H.1,Fujii T.1,Takahashi T.1

Affiliation:

1. Central Research Institute of Electric Power Industry (CRIEPI), 2-6-1 Nagasaka, Yokosuka City, Kanagawa Prefecture, 240-0196 Japan

Abstract

The thermal efficiency of gas turbine combined cycle power generation plants increase significantly in accordance with turbine inlet temperature. Gas turbine combined cycle power plants operating at high turbine inlet temperature are popular as a main thermal power station among our electric power companies in Japan. Thus, gas turbine hot gas parts are working under extreme conditions which will strongly affect their lifetime as well as maintenance costs for repaired and replaced parts. To reduce the latter is of major importance to enhance cost effectiveness of the plant. This report describes a gas turbine maintenance management program of main hot gas parts (combustor chambers, transition pieces, turbine first stage nozzles and first stage buckets) for management persons of gas turbine combined cycle power stations in order to obtain an optimal gas turbine maintenance schedule considering rotation, repair and replacement, or exchange of those parts.

Publisher

ASME International

Subject

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

Reference4 articles.

1. 1991, “Development and Evaluation of Life and Assessment and Reconditioning Methods for Gas Turbine Blading,” EPRI GS-4302.

2. Soneda, N., and Takao, T., 1993, “Development of Integrated Evaluation Support System for Nuclear Plant Life Extension,” CRIEPI Report T92061.

3. Moritsuka, H., Fujii, T., and Takahashi, T., 1999, “Development of the Gas Turbine Maintenance Optimization Supporting Program—First Report Maintenance Management Basic Program of Main Hot Gas Parts,” CRIEPI Report W98020.

4. Hayakawa, Y., Isobe, N., Sakurai, S., and Kumata, K., 1999, “Life Management System for Hot-Gas-Path Components of Gas Turbine,” ASME Paper 99-GT-428.

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