Results From the Phase II Test Using the High-Temperature Developing Unit (HTDU)

[+] Author and Article Information
S. Aoki, K. Teshima, M. Arai

Engineering Research Association for Advanced Gas Turbines, Tokyo 105, Japan

H. Yamao

Research and Development Center, Mitsubishi Heavy Industries, Ltd., Tokyo, Japan

J. Eng. Gas Turbines Power 110(2), 251-258 (Apr 01, 1988) (8 pages) doi:10.1115/1.3240114 History: Received February 24, 1987; Online October 15, 2009


Phase II of the high-temperature turbine test was performed using the H igh-T emperature D eveloping U nit (HTDU). This unit has the same two stages as the high-pressure turbine of the AGTJ-100A reheat system. The purpose of the Phase II test was to investigate the potential of candidate technologies that may be applied to the advanced engine, the AGTJ-100B. Cooling characteristics of several cooling schemes for the first stage blades, and the performance of thermal barrier coating employed on the first stage nozzles and blades, were investigated. This paper presents the Phase II test results.

Copyright © 1988 by ASME
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