A study of extractive and remote-sensing sampling and measurement of emissions from military aircraft engines

Aircraft emissions contribute to the increased atmospheric burden of particulate matter (PM) that plays an important role in air quality human health visibility contrail formation and climate change Sampling and measurement of modern aircraft emissions at the engine exhaust plane (EEP) for engine and fuel certification remains challenging as no agency-certified method is available In this paper we summarize the results of three recent field studies devoted to investigate the consistency and applicability of extractive" and optical remote-sensing (ORS) technologies in the sampling and measurement of gaseous and PM emitted by a number of military aircraft engines Three classes of military engines were investigated these include T56 TF33 and T700 & T701C types of engines which consume 70-80% of the military aviation fuel each year JP-8 and Fischer-Tropsch (FT)-derived paraffinic fuels were used to study the effect of fuels It was found that non-volatile particles in the engine emissions were in the 20 nm range for the low power condition of new helicopter engines to 80 nm for the high power condition of legacy engines Elemental analysis indicated little metals were present on particles while most of the materials on the exhaust particles were carbon and sulfate based Alkanes carbon monoxide carbon dioxide nitrogen oxides sulfur dioxide formaldehyde ethylene acetylene and propylene were detected The last five species were most noticeable only under low engine power The emission indices calculated based on the ORS data deviate significantly from those based on the extractive data Nevertheless the ORS techniques were useful in the sense that it provided non-intrusive real-time detection of species in the exhaust plume which warrants further development The results obtained in this program help validate sampling methodology and measurement techniques used for non-volatile PM aircraft emissions as described in the SAE AIR6037 (2009) (C) 2010 Elsevier Ltd All rights reserved