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Development and Testing of the 13MW Class Heavy Duty Gas Turbine MF-111 PUBLIC ACCESS

[+] Author Affiliations
Eiji Akita, Kuniaki Aoyama, Yoshiaki Tsukuda, Ichiro Fukue, Sunao Aoki

Mitsubishi Heavy Industries, Ltd., Takasago, Japan

Paper No. 87-GT-37, pp. V004T10A014; 6 pages
doi:10.1115/87-GT-37
From:
  • ASME 1987 International Gas Turbine Conference and Exhibition
  • Volume 4: Heat Transfer; Electric Power
  • Anaheim, California, USA, May 31–June 4, 1987
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7926-9
  • Copyright © 1987 by ASME

abstract

A new 13 MW class heavy duty gas turbine “MF-111” with the combustor outlet temperature of 1250°C (1523 K) was developed and tested.

The thermal efficiency of MF-111 is designed to be 32% for simple-cycle and 45% in combined-cycle operation.

MF-111 has single-shaft configuration, 15-stage axial flow compressor, 8 cannular type combustors and 3-stage axial flow turbine.

Advanced cooling technology was incorporated for the turbine and the combustor design to be capable of higher combustor outlet temperature.

The prototype was shoptested at full load in April, 1986. The performance and the metal temperatures of hot parts were confirmed to well satisfy the design goal. The first machine of MF-111 started the commercial operation from August, 1986 and has logged satisfactory operations.

Copyright © 1987 by ASME
Topics: Gas turbines , Testing
This article is only available in the PDF format.

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