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- W2183075582 abstract "In recent years, turbine inlet temperature becomes higher and higher to grow up the power of gas turbine engines. The hot section parts, such as combustor and turbine, are generally designed as cooling structures which were made of heat resistant metals. However, some organizations research and develop the ceramics parts as next generation materials instead of heat resistant steels. A key technology for this system is the thrust growth of the jet engine without increasing the outer dimensions. For that purpose, turbine inlet temperature must be increased and a ceramic turbine was considered as the most superior choice since air cooled metal turbine is too complicated and expensive. This paper describes the current achievement of the research of the ceramic turbine jet engine. In this study, the ceramic turbine is applied in the aircraft gas turbine engine and the engine testing is demonstrated under full load operating conditions. The successful testing of the ceramic turbine components in the aircraft gas turbine engine has been accomplished." @default.
- W2183075582 created "2016-06-24" @default.
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- W2183075582 date "2002-01-01" @default.
- W2183075582 modified "2023-09-24" @default.
- W2183075582 title "RESEARCH ON APPLICATION OF CERAMIC TURBINE TO JET ENGINE" @default.
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