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Erschienen in:
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2021 | OriginalPaper | Buchkapitel

Emission Characteristics and Flame Stability in HEFA Fueled Gas Turbine Combustors

verfasst von : H. Fujiwara, P. Salman, S. Ando, H. Ishikawa, S. Nakaya, M. Tsue, K. Okai

Erschienen in: Sustainable Development for Energy, Power, and Propulsion

Verlag: Springer Singapore

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Abstract

Combustion rig tests of an RQL (rich burn quick quench lean burn) gas turbine combustor and of a single concentric lean-burn combustor were performed using kerosene (Jet A1), 100% hydro-treated ester and fatty acid (HEFA) alternative jet fuel and their blends. The results showed a clear tendency of suppression of non-volatile PM (nvPM) emission with an increase in the blending ratio of HEFA. Combustion test results were examined with the help of basic atmospheric and high-temperature and high-pressure testing. Blowout conditions and flame oscillations are also discussed.

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Vorheriges Kapitel Mitigation of Thermoacoustic Instability Through Amplitude Death: Model and Experiments
Nächstes Kapitel Aerothermal Technologies for Low Emissions Combustors
Fußnoten
1
AIAA 2016-4953 [18] and AIAA2019-1772 [19]: reprinted with permission of American Institute of Aeronautics and Astronautics, Inc.
 
2
AIAA 2018-1474 [20]: reprinted with permission of American Institute of Aeronautics and Astronautics, Inc.
 
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Metadaten
Titel
Emission Characteristics and Flame Stability in HEFA Fueled Gas Turbine Combustors
verfasst von
H. Fujiwara
P. Salman
S. Ando
H. Ishikawa
S. Nakaya
M. Tsue
K. Okai
Copyright-Jahr
2021
Verlag
Springer Singapore
Buch
Sustainable Development for Energy, Power, and Propulsion

Print ISBN: 978-981-15-5666-1

Electronic ISBN: 978-981-15-5667-8

Copyright-Jahr: 2021

DOI
https://doi.org/10.1007/978-981-15-5667-8_13