Research on High Temperature Combustor for Advanced Reheat Gas Turbine
Keyword(s):
Preliminary studies on the high temperature combustors (combustor outlet temperature = 1670–1770K) for the prototype advanced reheat gas turbine were carried out under the national project of Japan - Moonlight Project. This paper describes an outline of the studies; (i) application of an advanced ceramic thermal barrier coating and ODS superalloy, (ii) development of the advanced double-wall cooling system, (iii) research on the ceramic tile combustor.
2020 ◽
Vol 20
(5)
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pp. 1765-1770
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2016 ◽
Vol 11
(4)
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pp. 391-400
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1998 ◽
Vol 47
(7)
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pp. 665-671
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2010 ◽
Vol 123-125
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pp. 459-462
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2013 ◽
Vol 467
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pp. 29-34
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2007 ◽
Vol 1
(8)
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pp. 1005-1016
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2014 ◽
Vol 40
(3)
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pp. 4663-4671
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