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SINTEF 04/18/23
CONTROL OF VOC EMISSION FROM CRUDE OIL TANKERS
Otto M.Martens, MSc. Norwegian Marine Technology Research Institute (MARINTEK)Ole Oldervik, MSc. PhD. SINTEF Civil and Environmental EngineeringBengt Olav Neeraas, MSc. PhD. SINTEF Energy ResearchTerje Strøm, MSc. SINTEF Applied Chemistry
SINTEF 04/18/23
Results from study on reduction of VOC emission from Crude oil tankers
• Focus on shuttle tankers and FSO/ FPSO• Simulation of :
– evaporation rates for individual volatile compounds– gas emission rates– composition of emitted gas
• Reduced emission by combination of control techniques:
– sequential transfer of tank atmosphere (STTA)– reliquefaction of VOC– absorption of VOC in cargo oil
SINTEF 04/18/23
INTRODUCTION
• The VOC emission represents:– a loss of considerable monetary value– harmful consequences to the environment
• National goal of 30 % NMVOC emission• 50 % of emission in Norway from offshore loading• Actions taken:
– gas return and recovery plant at the Sture terminal– absorption plant on M/T “Anna Knutsen”– recondensation plant on M/T “Navion Viking”– several R&D projects and measurement series performed
• VOC diluted in inert gas creates a problem
SINTEF 04/18/23
The VOCON RESEARCH PROJECT
Sponsors- Statoil UBT/PRA
- Saga Petroleum ASA
- BP International Ltd
- Shell Expro
- Norsk Hydro
- Kværner Ship Equipment
- Aker Engineering,
- Umoe Technology Sandsli
- Bergesen DY AS
- Navion
- Norwegian Petroleum Directorate
- Det Norske Veritas
- Norwegian Council of Research
- Norwegian Maritime Directorate
- MARINTEK/SINTEF
Performed by SINTEF
Content :• Emission measurements
onboard• Developed emission
simulation program• Evaluated concepts for
VOC emission control– Required 75 % reduction of
NMVOC emission
SINTEF 04/18/23
The Simulation Program HCGas
• Typical components considered :
– C1, C2, C3, i-C4, n-C4, i-C5, n-C5, C6, C7, C8, C9, C10+, N2, CO2 , O2 • Transportation in liquid and gas phases by solving one dim
diffusion/ convection equation for each component• Local equilibrium at the free surface gives mass transfer of
each component between the phases• Mass continuity eq. for each tank and flow eq. for each pipe
used to compute flow• Loading and discharging rates specified• Temperature specified in liquid phase as f(time, space)• Temperature specified in gas phase as f(time, space) or
computed
SINTEF 04/18/23
Simulated cases
ST L
StoreT ransport
Case B: STL
ST T A
VOCrecovery
Shuttle
T ranspor t
Store
Case A: GBS
ST T A
VOCrecovery
Shuttle FPSO
Case C: FPSO
StoreT ransport
VOCrecovery
GasreturnST T A
Shuttle
Shuttle
StoreT ranspor t
FSO
Case D: FSO
VOCrecovery
GasreturnST T A
• 140300 m3 cargo capacity all ships
• shuttle tanker and STL loaded and discharged from 3 similar tank groups in series
• average sea condition offshore
• fairly volatile crude
• shuttle tanker– loading rate 2.2 m3/s– discharge rate 2.7 m3/s
SINTEF 04/18/23
SHUTTLE TANKER - BASE CASE
Figure 3 Gas flow out of tanks - Base Case
Time (h)0 2 4 6 8 10 12 14 16 18 20 22 24
Flo
w ou
t o
f ta
nk
s (
Nm3
/h)
0
2000
4000
6000
8000
10000
12000
14000
Figure 4 Composition of gas out of tanks - Base Case
Time (h)0 2 4 6 8 10 12 14 16 18 20 22 24V
olu
me
fra
cti
on
in
ga
s o
ut
of
tan
ks
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8C1
C2
C3
iC4
nC4
iC5
nC5
C6+
N2+O2
CO2
Figure 5 Relative composition of hydrocarbon gas
out of tanks - Base Case
Time (h)0 2 4 6 8 10 12 14 16 18 20 22 24
Re
l. f
rac
tio
n H
C i
n g
as
ou
t o
f ta
nks
0.00
0.05
0.10
0.15
0.20
0.25
0.30
0.35
0.40rel C1
rel C2
rel C3
rel iC4
nC4
rel iC5
rel nC5
rel C6+
Figure 6 Volume fraction of hydrocarbon gas
emitted from tanks - Base Case
Time (h)0 2 4 6 8 10 12 14 16 18 20 22 24
Vo
lum
e f
ra
cti
on
HC
ga
s
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
SINTEF 04/18/23
SHUTTLE TANKER - BASE CASE
Figure 7 Molecular weight of hydrocarbon gas
emitted from tanks - Base Case
Time (h)0 2 4 6 8 10 12 14 16 18 20 22 24
Mo
lecu
lar w
eig
ht
(kg/k
mol)
40
42
44
46
48
50
52
54
56
58
60
Figure 8 Volume fraction hydrocarbon gas at
two levels inside the tank - Base Case
Time (h)0 2 4 6 8 10 12 14 16 18 20 22 24
AL
FA
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
Top Tank 1 Half Height Tank 1 Top Tank 2 Half Height Tank 2 Top Tank 3 Half Height Tank 3
Figure 9 Mass of gas emitted from tanks - Base Case
Time (h)0 2 4 6 8 10 12 14 16 18 20 22 24
Ac
cu
mu
late
d m
as
s
(kg
)
0
25000
50000
75000
100000
125000
150000
175000
200000
Emitted VOC
Emitted IN
Emitted C1
SINTEF 04/18/23
SHUTTLE TANKER - STTA
• Emission of NMVOC:– base case 193000 kg– base case with STTA
169000 kg
• Compared to base case STTA gives:
– reduced flow rate– reduced emission– reduced running time and
better condition for recovery plant
Crude
STTAGas out
Figure 13 Volume fraction hydrocarbon gas emitted
from the tanks - Shuttle Tanker with STTA
Time (h)0 2 4 6 8 10 12 14 16 18 20 22 24
Vo
lum
e f
ra
cti
on
HC
ga
s
0.0
0.1
0.2
0.3
0.4
0.5
0.6
0.7
0.8
0.9
1.0
SINTEF 04/18/23
Shuttle Tanker with STTA and liquefaction plant
Case NMVOCemissionreduction(wt. %)
Reducedemisson
(ton NMVOC)
Maximumcompressor power
(kW)
Energyconsumption
(kWh)
Relative averageenergy
consumption (kWh/kgNMVOC)
Plantcomplexity
BaseCasewithoutSTTA.Recovery onshuttle
75 145 1 900 28 000 0.19 - VOC compressor.- Refrig.plant.- Requires drying of VOC/inert gas
BaseCase withSTTA.Recovery onshuttle
75 144 1 600 21 000(no operationthe first two
hours)
0.15 - VOC compressor.- Refrig. plant.- Requires drying of VOC/inert gas- STTA
L iq u id N M V O C
R e frig era tio np lan t
D ry erV O Cc o m p res so r
U n co n d e n se d g as
F ig u r e 1 1 . R e l iq u e f a c t io n p la n t in p r in c ip le .
Combi-nation
Endtemperature
(0C)
Endpressure
(bar)
RecoveredNMVOC
plant alone(wt %)
Totalcompr.power(kW)
a -20 7 71.4 1521b -30 5 72.6 1673c -40 3.5 74.0 2071
SINTEF 04/18/23
Shuttle Tanker with STTA and absorption plant
Case NMVOCemissionreduction (wt. %)
Reduced emisson(ton NMVOC)
Maximumcompressorpower (kW)
Energy consumptionincl. crude pump
(kWh)
Relative average energyconsumption(kWh/kgNMVOC)
Plantcomplexity
BaseCase withoutSTTA.Recovery onshuttle
75 145 1 500 22 905 0.16 - VOC compressor.- Crude pump.- Absorption column
BaseCase withSTTA.Recovery onshuttle
80 131 1 450 21 708 0.14 - VOC compressor.- Crude pump.- Absorption column- STTA
Figure 17. Schematic outline of absorption plant.
SINTEF 04/18/23
Gas Return from Shuttle Tanker to FSOwith STTA on shuttle tanker and liquefaction plant on FSO
Table 7. Calculated recovery rates
Comb Temp.[0C]
Pres.[bar]
NMVOCrecovery period 1[wt.%]
TotalNMVOCrecovery[wt.%]
a -20 7 87.4 77.1b 15 20 87.8 77.4
Figure 18 Flow out to the atmosphere from the FPSO/FSO and the Shuttle Tanker
Time (h)
0 12 24 36 48 60 72 84 96 108 120 132 144
Flo
w o
ut
to a
tmo
sp
he
re (N
m3 /
h)
0
2000
4000
6000
8000
10000
Figure 19 Volume fraction hydrocarbon gas out to the atmosphere from the FPSO/FSO and the Shuttle Tanker
Time (h)
0 12 24 36 48 60 72 84 96 108 120 132 144
Vo
lum
e fr
acti
on
HC
gas
0.00.10.20.30.40.50.60.70.80.91.0
0
1 0 0
2 0 0
3 0 0
4 0 0
5 0 0
0 5 0 1 0 0 1 5 0
T im e (h )
Sha
ft p
ower
(kW
),
Acc
.rec
. NM
VO
C (t
on)
0
1 0 0 0 0
2 0 0 0 0
3 0 0 0 0
4 0 0 0 0
5 0 0 0 0
Acc
.Ene
rgy
(kW
h)
P o w e r N M V O C
E n e rg y
F ig u re 2 0. P o w e r re q u irem en t, a cc um u latedre c ov ere d N M V O C a nd ac c um ulate d e ne rgy
c o n sum ptio n for c a se 2 .
SINTEF 04/18/23
CONCLUSIONS
• STTA combined with recovery plant reduces :– required peak power– energy consumption– process equipment dimensions (slightly)
• Economy of combination must be evaluated for each ship• Compared to absorption plant a reliquefaction plant :
– requires higher power– becomes more complex– produces VOC to be used as fuel
• Gas return to FSO requires small plant to satisfy specified reduction of NMVOC emission
• HCGas is a powerful tool for computing evaporation and emission from various crude types and cargo handling procedures