2021
DOI: 10.31399/asm.cp.itsc2021p0695
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Development of Advanced TBC for 1650 °C Class Gas Turbine

Abstract: Increasing operating temperature plays a critical role in improving the thermal efficiency of gas turbines. This paper assesses the capability of advanced thermal barrier coatings being developed for use in 1700 °C class gas turbines. Parts sprayed with these coatings were evaluated and found to have excellent durability and long-term reliability.

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Cited by 4 publications
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“…Recently, the development of heat resistant alloys, hot gas path cooling systems and thermal barrier coatings has allowed a working flow temperature increase from 800 to 1650 • C [10,11]. Foreign advanced CCGT facilities have recently reached net efficiency of 63-64% [12,13]. CCGT facilities based on the 9HA02 or M701JAC Gas Turbines (GT) have electric net efficiency above 64% [11,14,15], which is the highest performance among the commercially available gas fuel power production technologies.…”
Section: Increasing Efficiency Of the Binary Power Cyclesmentioning
confidence: 99%
“…Recently, the development of heat resistant alloys, hot gas path cooling systems and thermal barrier coatings has allowed a working flow temperature increase from 800 to 1650 • C [10,11]. Foreign advanced CCGT facilities have recently reached net efficiency of 63-64% [12,13]. CCGT facilities based on the 9HA02 or M701JAC Gas Turbines (GT) have electric net efficiency above 64% [11,14,15], which is the highest performance among the commercially available gas fuel power production technologies.…”
Section: Increasing Efficiency Of the Binary Power Cyclesmentioning
confidence: 99%
“…Today, most of the electrical and thermal energy in the world is generated at thermal power plants, with its share in generation being more than 60%. The combined cycle gas turbine (CCGT) process remains the most efficient fuel energy conversion technology at the moment, the net electrical efficiency of which can reach 64% [3,4]. Such a high level is due, first of all, to high initial parameters (the temperature at the gas turbine unit (GTU) inlet can reach 1650 • C [5,6]).…”
Section: Introductionmentioning
confidence: 99%