L. Kattner et al.: Monitoring compliance with sulfur content regulations of shipping fuel
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Atmos. Chem. Phys., 15,10087-10092, 2015
ble measurement conditions and at the same time provide a
compact and transportable set-up. Data were stored in an in
tegrated data logger with the time resolution of 1 min. De
spite different time resolutions of the instruments, we used
data normalised to 1 min, which is sufficient for the analy
sis of emission events with a duration in the order of several
minutes.
NO*, SO2 and O3 were measured with instruments from
the Horiba AP-370 series, which are certified instruments
according to EU directives (EN14211 for NO*, EN 14212
for SO2 and EN 14625 for O3) used by German authorities
for standard air pollution measurements. CO2 was measured
with a Licor 840A analyser. The O3 measurements were not
used for this study and are just mentioned for completeness.
For SO2: the Horiba APSA-370 is based on the UV-
fluorescence method, using the excitation of SO2 molecules
by UV light and measuring the fluorescence which is a func
tion of SO2 concentration. The response time of the instru
ment is specified to be less than 120 s. Calibration was car
ried out with a standard gas mixture from Air Liquide with
a concentration of 99.7 ppb SO2 with an accuracy of 5 %. In
addition, a daily control was obtained by the measurement
of zero gas produced with a scrubber, and span gas from an
internal permeation source with 175 ppb SO2. There is a NO
cross sensitivity for SO2 which gives an SO2 signal for 0.8 %
of the NO signal. We have determined this value of 0.8 % via
a set of six calibration measurements of different NO con
centrations between 100 and 470 ppb.
For NO* : the Horiba APNA-370 measures the chemilumi
nescence of NO molecules reacting with O3. To obtain in
formation about the NO2 concentration, the device contains
a deoxidation converter to transfer NO2 molecules to NO.
The NO2 concentration is calculated by the difference of total
NO*, representing NO + NO2, and NO without conversion.
The response time for measurement of both gases is 90s.
The instrument is calibrated with an Air Liquide standard
gas mixture with a concentration of 216.0 ppb NO and an ac
curacy of 5 %. A daily control with scrubber-produced zero
gas and an NO2 span gas of 105 ppb is also implemented.
For CO2: the Licor 840A is a non-dispersive infrared gas
analyser. It has a response time of 1 s and was calibrated
with two Air Liquide standard gas mixtures with 306.6 and
990.0ppm CO2 with an accuracy of 2 %.
The trace gas measurements were complemented with
measurements of wind, temperature, air pressure and precip
itation by a compact weather station (Lufft WS600). With
an AIS (automatic identification system) receiver the infor
mation transmitted by passing ships was collected, which in
cludes identification number, name and type of the ship as
well as position, course and speed.
3 Data analysis
To obtain the sulfur content of ship fuel in use, the enhance
ment of SO2 and CO2 in measurements affected by exhaust
gases is measured, and the ratio of these SO2 and CO2 peaks
is used to calculate the fuel sulfur content. The combination
of the trace gas peak time, the wind direction and the AIS in
formation enables the identification of the peak-related ship.
When wind conditions are favourable for measurements,
the plumes of ships passing the instrument leave a distinc
tive enhancement of the measured component against back
ground concentrations. Since this enhancement is most sig
nificant in NO measurements, and NO is an indicator for
recent combustion processes, these NO peaks are used to
identify the time stamp of a ship emission event. For these
time stamps, peaks in CO2 are then identified, which is more
complicated because background concentrations are larger
and more variable due to the surrounding vegetation. Back
ground signals for each gas are determined via a customised
running mean filter. The SO2 signals are only analysed for
those events for which there was a significant CO2 peak and
a clearly determinable background. For all peaks the indi
vidual peak area above the background concentration is de
termined. This accounts for the difference in peak width for
each gas due to different time resolutions of the respective in
struments. The peak area value of the SO2 peaks is corrected
with 0.8 % of the peak area value of the NO peaks to ac
count for the cross sensitivity. With the assumption that fuel
contains 87 ± 1.5 % carbon (Cooper et ah, 2003) and 100 %
of the sulfur and the carbon content of the fuel are emitted
as SO2 and CO2 respectively, the sulfur fuel content (SFC)
mass percent can be calculated as follows:
SFC[%] =
S[kg]
fuel [kg]
SO2 [ppm] • A(S)
CO2 [ppm] • A(C)
SO2 [ppb]
r L -[ • 0.232 [%]
CO2 ppm
87 [%]
(1)
where A(S) is the atomic weight of sulfur and A(C) the
atomic weight of carbon. Using this formula, it is relatively
simple to calculate the sulfur content for each set of peaks.
For a discussion about the uncertainties of this formula see
Sect. 3.1.
The second part of the data analysis is the attribution of the
identified emission events to individual passing ships. Within
30 min before each event, which is characterised by the time
the emissions arrive at the instruments, the AIS data are anal
ysed for ship positions close to the measurement site. In com
bination with wind information, this yields the identification
of the individual ships which have caused the emission in
most cases. The time the plume travels from being emitted
to being analysed is about 2 to 10 min, depending on wind
speed and direction. However, there are events in which there