Development of the Advanced TBC for High Efficiency Gas Turbine

Since 2004, Mitsubishi has been pursuing a 1,700°C gas turbine as part of the Japanese National Project [1][2]. One of the most important key technologies for the target is thermal barrier coatings (TBCs) which are capable of improving cooling efficiency of hot parts. With increasing the turbine inl...

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Veröffentlicht in:	Materials Science Forum 2016-11, Vol.879, p.1980-1986
Hauptverfasser:	Okajima, Yoshifumi, Okada, Ikuo, Torigoe, Taiji, Masada, Junichiro, Tsukagoshi, Keizo
Format:	Artikel
Sprache:	eng
Schlagworte:	Cooling Durability Efficiency Erosion Gas turbines Inlet temperature Materials science Spallation Surface temperature Temperature gradient Temperature gradients Thermal barrier coatings Vanes
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