2015
DOI: 10.1016/j.apenergy.2015.04.044
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Fuel flexibility, stability and emissions in premixed hydrogen-rich gas turbine combustion: Technology, fundamentals, and numerical simulations

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Cited by 223 publications
(108 citation statements)
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“…The highest TOTs which do not exceed 650°C are observed in the case of the most advanced gas turbines operating under a high turbine inlet temperature (1500°-1600°C [28]). The following examples can be quoted: Westinghouse 501G (597°C) [21], Siemens SGT6-8000H (627°C) [29], GE S107FA (603°C) [30] and GE-P9371FB (644°C) [31].…”
Section: Introductionmentioning
confidence: 97%
“…The highest TOTs which do not exceed 650°C are observed in the case of the most advanced gas turbines operating under a high turbine inlet temperature (1500°-1600°C [28]). The following examples can be quoted: Westinghouse 501G (597°C) [21], Siemens SGT6-8000H (627°C) [29], GE S107FA (603°C) [30] and GE-P9371FB (644°C) [31].…”
Section: Introductionmentioning
confidence: 97%
“…As these mixtures can vary significantly in chemical composition [3], the future combustion systems should be highly fuel flexible [2]. This, in turn, introduces further difficulties [2,6]. Variations in fuel properties can cause operational problems such as thermoacoustic instabilities [7] and flame flashback [6].…”
Section: Introductionmentioning
confidence: 97%
“…In principle, the problem is due to the high reactivity of hydrogen and subsequently higher flame speed of hydrogen blends compared to those of conventional fuels [4,11]. Currently, flame flashback is considered as one of the most significant technical barriers that hinder the development of hydrogen combustion systems [2,6].…”
Section: Introductionmentioning
confidence: 99%
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