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Results From High Temperature Turbine Test on the HPT of the AGTJ-100A FREE

[+] Author Affiliations
Masashi Arai, Kiyomi Teshima, Sunao Aoki, Hiroyuki Yamao

Engineering Research Association for Advanced Gas Turbines, Tokyo, Japan

Paper No. 84-GT-235, pp. V004T10A027; 8 pages
doi:10.1115/84-GT-235
From:
  • ASME 1984 International Gas Turbine Conference and Exhibit
  • Volume 4: Heat Transfer; Electric Power
  • Amsterdam, The Netherlands, June 4–7, 1984
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7949-8
  • Copyright © 1984 by ASME

abstract

An experimental investigation was conducted through the use of a High Temperature Turbine Developing Unit (HTDU) having the same two stage turbine as the high pressure turbine (HPT) of the AGTJ-100A, to ascertain the aerodynamic performance, cooling characteristics and mechanical reliability. The test was performed in three phases, and the maximum turbine inlet temperature was about 1,573 K. The test results showed that turbine efficiency was 90.2 %, the level of metal temperature for nozzles and blades was as expected, and there was little trouble with the hot parts.

This paper will present these test results.

Copyright © 1984 by ASME
This article is only available in the PDF format.

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