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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Fujiwara, H., Salman, P., Ando, S., Ishikawa, H., Nakaya, S., Tsue, M., & Okai, K. (2021). Emission Characteristics and Flame Stability in HEFA Fueled Gas Turbine Combustors. In Green Energy and Technology (pp. 323–356). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-15-5667-8_13
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