Emission indices were derived from in-flight measurements of CO, nonmethane
hydrocarbons (NMHCs), H2O, and nonvolatile condensation nuclei in the exha
ust plumes of the Deutsches Zentrum fur Luft- und Raumfahrt VFW 614 (ATTAS)
and NASA DC-8 experimental aircraft. CO emission indices, EIs(CO), of the
ATTAS Rolls Royce M 45H Mk501 engines were determined concurrently by two i
ndependent techniques: monitoring of exhaust emissions using a customized F
ourier transform infrared spectrometer (FTIR) and by simultaneous continuou
s fast CO and CO, measurements. The EIs(CO) determined by FTIR were systema
tically 28% lower than those derived from the CO/CO2 concentration ratios.
The EIs(CO) of the newer and larger CFM 56-2C1 engines, used on DC-g, were
substantially smaller than those of the ATTAS engines. The emission behavio
r of CFM 56-2C1 engines is very similar to CFM 56-3 engines frequently used
on Boeing 737 aircraft. Tn-flight derived EIs(CO) of the ATTAS engines wer
e strongly dependent on the fuel flow rate and agreed well with those calcu
lated from ground-based measurements. Emission indices for individual NMHCs
were determined fi om the concentration ratios of NMHC/CO in the plume of
ATTAS and DC-g and from the EIs(CO) determined by FTIR or derived from the
concentration ratios of CO/CO2. The EIs(NMHC) are highest for alkenes and a
lkynes generated by a cracking of larger fuel molecules and for benzene fro
m unburnt fuel, and they depend strongly on the power setting of the engine
s. As with EIs(CO), the EIs(NMHC) of the CFM 56-2C1 engine tend to be small
er than those of the Rolls Royce M 45H Mk501.