TY - JOUR
T1 - Sustainable aviation fuel blends in aircraft piston engine
T2 - Comparative analysis of 30 % vs. 50 % SAF on combustion performance and emission reduction
AU - Chen, Longfei
AU - Zafar, Aaqib
AU - Zhong, Shenghui
AU - Pan, Kang
AU - Wang, Minghua
AU - Fan, Yukun
AU - Zhang, Yang
AU - Shi, Wentao
AU - Xu, Zheng
N1 - Publisher Copyright:
© 2025 Elsevier Ltd
PY - 2025/10/30
Y1 - 2025/10/30
N2 - The integration of Sustainable Aviation Fuel (SAF) blends into heavy-fuel aircraft piston engines (HF-APE) offers a strategic pathway to decarbonizing propulsion systems in general aviation and unmanned aerial vehicles (UAVs). This study presents a comprehensive comparison of combustion behavior and emission characteristics for SAF-biodiesel and SAF-RP-3 blends, utilizing a hybrid experimental-simulation approach. Emissions were measured according to ICAO Annex 16 protocols using precision instrumentation at varying engine speeds. A validated simulation model accurately replicated combustion, gas exchange, and pollutant formation processes. The 50 % SAF +50 % RP-3 blend exhibited the best emission profile, reducing carbon monoxide (CO) by up to 63 % and unburned hydrocarbons (HC) by 75 % compared to biodiesel-dominant blends. In contrast, the 30 % SAF +70 % biodiesel blend resulted in a 19 % increase in nitrogen oxide (NOx) emissions. Particle size distribution (PSD) analysis showed that RP-3 blends reduced nucleation-mode particles by 30–40 % and total particulate matter (PM) emissions by 38 %. Microscopic examination revealed that RP-3-derived particulates were finer, denser, and less porous, suggesting more complete combustion. A notable strength of this study is the integrated use of differential mobility spectrometer (DMS 500) and environmental scanning electron microscope (eSEM) for comprehensive particulate characterization. Simulations revealed that the 50 % SAF +50 % RP-3 blend achieved superior intake (∼10.7 g/s), exhaust (∼13.8 g/s) mass flow rates, brake power (∼81 kW), fuel efficiency (∼217 g/kWh), and a 28 % reduction in CO2 emissions. These findings suggest that SAF-enhanced RP-3 fuels offer significant potential for improving HF-APE performance and sustainability.
AB - The integration of Sustainable Aviation Fuel (SAF) blends into heavy-fuel aircraft piston engines (HF-APE) offers a strategic pathway to decarbonizing propulsion systems in general aviation and unmanned aerial vehicles (UAVs). This study presents a comprehensive comparison of combustion behavior and emission characteristics for SAF-biodiesel and SAF-RP-3 blends, utilizing a hybrid experimental-simulation approach. Emissions were measured according to ICAO Annex 16 protocols using precision instrumentation at varying engine speeds. A validated simulation model accurately replicated combustion, gas exchange, and pollutant formation processes. The 50 % SAF +50 % RP-3 blend exhibited the best emission profile, reducing carbon monoxide (CO) by up to 63 % and unburned hydrocarbons (HC) by 75 % compared to biodiesel-dominant blends. In contrast, the 30 % SAF +70 % biodiesel blend resulted in a 19 % increase in nitrogen oxide (NOx) emissions. Particle size distribution (PSD) analysis showed that RP-3 blends reduced nucleation-mode particles by 30–40 % and total particulate matter (PM) emissions by 38 %. Microscopic examination revealed that RP-3-derived particulates were finer, denser, and less porous, suggesting more complete combustion. A notable strength of this study is the integrated use of differential mobility spectrometer (DMS 500) and environmental scanning electron microscope (eSEM) for comprehensive particulate characterization. Simulations revealed that the 50 % SAF +50 % RP-3 blend achieved superior intake (∼10.7 g/s), exhaust (∼13.8 g/s) mass flow rates, brake power (∼81 kW), fuel efficiency (∼217 g/kWh), and a 28 % reduction in CO2 emissions. These findings suggest that SAF-enhanced RP-3 fuels offer significant potential for improving HF-APE performance and sustainability.
KW - Aircraft piston engine
KW - Aviation combustion performance
KW - Aviation emission reduction
KW - Emission index
KW - Particle size distribution
KW - Particulate matter
KW - Sustainable aviation fuels
UR - https://www.scopus.com/pages/publications/105012734319
U2 - 10.1016/j.energy.2025.137882
DO - 10.1016/j.energy.2025.137882
M3 - 文章
AN - SCOPUS:105012734319
SN - 0360-5442
VL - 335
JO - Energy
JF - Energy
M1 - 137882
ER -