IGTC-126 Research and Development of 300kW Class Ceramic Gas Turbine(Organized Session IV CERAMIC GAS TURBINES)

概要

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As the result of setting the low pressure ratio at 4.5, sizes of the ceramic components forming the gas passage in CGT303 have been increased, and establishing reliability of these components was thought to be the most important task. So, hot spin tests and heat-cycle tests were conducted, in advance of the engine operation, and improvements have been made on their material and constructions. These components are assembled to the engine and the operation is made at the turbine inlet temperature (TiT) of 1,200℃.
公益社団法人日本ガスタービン学会の論文