|
Microscopic Characteristics of Soot Derived from an Aviation Piston Engine Fueled with Sustainable Aviation Fuel |
DOI:10.13949/j.cnki.nrjgc.2025.03.002 |
Key Words:sustainable aviation fuel(SAF) soot particle chemical composition crystallite reactivity |
|
Hits: 68 |
Download times: 7 |
Abstract:The microscopic characteristics of soot particles emitted by a piston aircraft engine using 100% hydro-processed esters and fatty acids-sustainable aviation fuel (HEFA-SAF) and conventional jet fuel RP-3 at three operation modes (idle, cruise and takeoff) were analyzed. The results show that the carbon-to-oxygen (C/O) ratios of soot aggregates were observed to be larger under take-off conditions for HEFA-SAF and under idle conditions for RP-3. For both fuels, the reactivity of nanostructures was observed to decrease with increasing engine load. Soot particles derived from HEFA-SAF were observed to possess smaller mean primary particle diameters than those from RP-3 at all load conditions. However, under idle conditions, RP-3 soot particles exhibited relatively lower reactivity, whereas HEFA-SAF soot particles demonstrated even lower reactivity under takeoff conditions. Through experimental data analysis, it is established that the C/O ratio, internal nanostructures, and the degree of graphitization of soot particles exhibited significant coupling relationships with engine loads. Notably, the chemical composition of aviation fuels is demonstrated to show distinct non-linear trends in influencing these critical microstructural parameters. The phenomenon fundamentally originates from the complex synergistic effects between fuel atomization/mixing processes and high-temperature pyrolysis reaction kinetics occurring across different temporal scales. |
View Full Text View/Add Comment Download reader |