Key Technologies for Ultra-High Temperature Gas Turbines
2020-2-25 · six elements (shielding coating, cooling technology, combustor, turbine, compressor and heat-resistant material) of a 1700°C-class gas turbine from 2004 to 2007. The second step aimed at practical application from 2008 to 2011. The results of this project were reflected in the development of the 1600°C-class J-type gas turbine.
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