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Numerical analysis of characteristics of biogas and
syngas combustion
T. Boushaki, K Shway, H. Zaidaoui, P Gillon, B. Sarh
To cite this version:
T. Boushaki, K Shway, H. Zaidaoui, P Gillon, B. Sarh. Numerical analysis of characteristics of
biogas and syngas combustion. 9th European Combustion Meeting, Apr 2019, Lisboa, Portugal.
�hal-02113607�
Numerical analysis of characteristics of biogas and syngas combustion
T. Boushaki*, K. Shway, H. Zaidaoui, P. Gillon, B. Sarh
ICARE – CNRS, Universty of Orleans, 1C av. de la Recherche Scientifique, 45071 Orléans, France
* toufik.boushaki@cnrs-orleans.fr
9th European Combustion Meeting, ECM2019, 14-17 April, Lisboa, Portugal
RenewValue Project
European project: ERANETMED2-72-169
RQ2: Energy and Environment
Collaborative Innovation Project - Mobility
Subject: Local sustainable renewable energy supply for vulnerable
communities in arid and semi-arid Mediterranean zones (MENA)
Partners
: ICARE CNRS (France), Universität Rostock, DBFZ (Germany), Ibn
Tofail University (Morocco), INSAT and ENIT (Tunisia), Politecnico di Torino (Italy)
Duration : 3 years (2018-2021)
ICARE tasks and objective of the study
Development of modular adapted energy concept
Gasifier - multi-fuel burner - boiler
Characterization of syngas and biogas flames
Experimentally: stability, pollutant emissions, temperature
Numerically: Calculations of laminar burning velocity, flame
temperature, pollutants (NOx, CO)…
This poster: some results of calculations
COSILAB: Combustion Simulation Laboratory
Numerical
simulation
tool
for
laminar
combustion problems 0D, 1D and recently
2D. Here, calculations of flame 1D (RUN 1DL)
Laminar flame velocities (S
L
)
Flame temperatures (T
f
)
Chemical species distributions
Pollutant emissions (NO, CO…)
Pathways of chemical reactions
Combustion characteristics _ calculations
Reference case
CH
4-air
Biogas flame
Syngas flame
For different parameters : T, P, Xi,
φ
With different mechanisms of reactions
Case of CH
4
-air flame
10 15 20 25 30 35 40 0,7 0,75 0,8 0,85 0,9 0,95 1 1,05 1,1 1,15 1,2 1,25 1,3 L a m in a r b u rn in g v el o ci ty , SL (c m / s) Equivalence ratio GRIMECH 298K Skeletal 30 species San Diego NIU GALWAY Boushaki al. 2012 Coppens et al. 2007 Halter et al. 2005 Bosschaart and Goey 2004 Gu et al. 2000
Vagelopoulous and Egolfopoulos 1998 Y.L.Chan et al.2015
Zahedi et al. 2014 Law et al. 1993 Van Maaren et al. 1994
CH4-air à 298K, 1 bar 0 20 40 60 80 100 300 350 400 450 500 SL [c m /s ec ] Ti [K] Cosilab GRIMECH 3.0 E. Hu et al. 2012 Han et al. 2007 Mishra et al. 2003 Hill et al. 1988 Garforth et al. 1978 10 15 20 25 30 35 40 1 2 3 4 5 Sl [c m /s e c ] Pi[bar] CH4-air, 298K, =1 GRIMECH3.0 L. Puzetti et Al. 2017 O. Park et Al. 2011 Rozenchan et Al. 2002 GU et Al. 2000
Laminar burning velocity with equivalence
ratio: CH
4
-air, at 298 K, 1 bar
Laminar burning velocity with initial
temperature and pressure : CH
4
-air, 1 bar,
Φ
=1
Results are validated, with 4 mechanisms
of chemical reactions
S
L
with T
i
:
Heating of gas intake
induces a better combustion
S
L
with P
i
COSILAB
2D. Here, calculations of flame 1D (RUN 1DL)
Biogas flame calculations
Syngas flame calculations
0 5 10 15 20 25 30 35 40 0,7 0,9 1,1 1,3 SL [c m /s ec ]
80% CH4-20% CO2 / air, 1 bar, 298K
GRI MECH 3.0 San Diego mechanism H.O.B. Nonaka et al. 2016 Zahedi et al. 2014 10 15 20 25 30 35 40 0% 5% 10% 15% 20% 25% 30% 35% 40% 45% 50% S L ( cm /s )] CO2 S L=f(%CO2) à 298K, 1 bar
Flame velocity with equivalence ratio: CH
4-CO2 (90/10 and 80/20%)
Flame velocity with CO
2Results validated by experiments from the literature
Laminar burning velocity (S
L
) decreases with CO
2
addition
0 5 10 15 20 25 30 35 40 0,7 0,8 0,9 1 1,1 1,2 1,3 Sl [c m /s ec ] 90% CH4-10% CO2/ air, 1 bar, 298K GRI MECH 3.0 GRI SKELETAL MECHANISM San Diego mechanism H.O.B. Nonaka et al. 2016 Chan et al. 2015 Zahedi et al. 2014 0 10 20 30 40 50 60 70 80 90 100 0,5 1 1,5 2 2,5 3 3,5 4 4,5 5 Sl [c m /s ec ]
90% CO-10% H2 / air , 1 bar, 298 K
Cosilab 2018 (included mechanism)
CRECK Modeling Group, E. Ranzi et al. (Politecnico di Milano) S. Da vis et al. (University of Dela ware)
A. Keromnes et al. (NIU Galway) N. Bouvet et a l. 2011 M.I. Hassan et al. 1997
0 50 100 150 200 0,5 1,5 2,5 3,5 4,5 SL [c m /s ec ] 50% CO/ 50% H2
Cosila b 2018 (icluded mecha nism)
CRECK Modeling Group, E. Ra nzi et al. (Politecnico di Mila no) S. Davis et a l. (University of Dela wa re)
A. Keromnes et a l. (NIU Galway) Y. Zhang et a l. 2014 N. Bouvet et a l. 2011 C. Pratha p et a l.2008 M.P. Bruke et a l. 2009 H. Sun et a l. 2007 M.I. Ha ssa n et al. 1997 I.C. McLea n et a l. 1994
Laminar burning velocity of CO-H
2
-air flames: 90/10% and 50/50 % CO-H
2
Results are compared and validated with experimental results
With +H : S max at
Φ
=2.5 (CH -air: at
Φ
= 1.05)
1750 1800 1850 1900 1950 2000 T f [K ] CO2 T f=f(%CO2) à 298K, 1 bar
Temperature, NOx and CO emissions of CH
4
-CO
2
-air flames with CO
2
0,5 1 1,5 2 2,5 3 0 10 20 30 40 50 M a ss f r a c ti o n ( × 1 0 -5 ) % CO2 NOx 2 2,5 3 3,5 0 10 20 30 40 50 M a ss f ra ct io n (× 1 0 -2) % CO2 CO emissions
Flame temperature decreases with CO
2
addition
NOx
with CO
2
CO
with CO
2
It is necessary to find a good balance to meet the standards
Acknowledgements:
This work is supported by the ANR (Agence
Nationale de la Recherche), the CNRS and the University of Orléans:
Eranet-Med II (RenewValue), LABEX CAPRYSSES (ANR-11-LABX-0006-01).
With +H
2
: S
L
max at
Φ
=2.5 (CH
4
-air: at
Φ
= 1.05)
+ H
2
S
L
; S
Lmax
: 190 at 50% of H
2
, 90 at 50%H
2
against 38 cm.s
-1
CH
4
-air
+ H
2
: higher reactivity, higher flammability limits, higher velocity, higher T
1800 1900 2000 2100 2200 98% CO 2% H2 90% CO 10% H2 80% CO 20% H2 70% CO 30% H2 60% CO 40%H2 50% CO 50%H2 Tco m b [K ] Syngas, 1 bar, 298 K, =1 20 30 40 50 60 70 80 90 100 110 120 98% CO 2% H2 90% CO 10% H2 80% CO 20% H2 70% CO 30% H2 60% CO 40%H2 50% CO 50%H2 Sl [c m /s ec ] Syngas, 1 bar, 298 K, =1
H
2CO
H
2CO
Laminar burning velocity of CO-H
2-CO
2-air
H
2fixed
CO