CHARACTERIZATION OF FOAMING BEHAVIOR IN AMINE-BASED CO2 CAPTURE PLANTS Research Review Meeting January 10 – 11, 2008 University of Texas at Austin, Texas BHURISA THITAKAMOL AND AMORNVADEE VEAWAB Faculty of Engineering, University of Regina CANADA 1 OUTLINE Introduction Objectives Experiment Results and discussions Foam model Conclusions Future works Acknowledgements INTRODUCTION Foaming problem in the CO2 absorption process One of the most severe operational problems causing extra expenditures Occurring in both an absorber and a regenerator during plant start-up and operation Causing many adverse impacts on the plant operation Impacts based on plant experiences Excessive loss of alkanolamine solvents Premature flooding Reduction in plant throughput Off-spec products High alkanolamine carryover to downstream plants 5 6 9 INTRODUCTION Research on foaming problem: For the CO2 absorption process in gas treating services Research group Alkanolamine type Contaminant Operating condition Pauley et al., 1989 MEA DEA MDEA Two formulated MDEA (with non specified additives) Formic acid Acetic acid Propionic acid Butyric acid Pentanoic acid n-hexanoic acid Octanoic acid Decanoic acid Dodecanoic acid Liquid hydrocarbon Atmospheric pressure McCarthy and Trebble, 1996 DEA Methanol Corrosion inhibitor Antifoam agent Lubrication oil Organic acid Degradation product Suspended solid 20 - 85oC 0.1 - 3 MPa Harruff, 1998 DGA 93oC up to 6.9 MPa Current foaming knowledge in the CO2 absorption process for a coal-fired power plant is limited: The application of the CO2 absorption process is relatively new for a coal-fired power plant. No reports of plant experiences and research work has published. OBJECTIVES To obtain comprehensive foaming information from bench-scale experiments under well-simulated environments. To reveal the parametric effects as listed below on foaming Gas flow rate Solution volume CO2 loading Alkanolamine concentration Solution temperature Degradation product Corrosion inhibitor Alkanolamine type To establish the foam model to predict a steady-state pneumatic foam height (H) from the physical properties and operating conditions 7 EXPERIMENTS The pneumatic method modified from the standard ASTM D892 (ASTM, 1999) Recorded foam volume Emitted to atmosphere Drying column F Gas mass flowmeter Flowmeter N2 cylinder Test Cell Immerse heater with thermometer Temperature bath 8 9 EXPERIMENTS Recorded data: Foam volume (cm3) vs. Time (min) for each minute during the 25minute blowing time 150 3 300 Average steady foam volume (cm ) Recored foam volume (cm3) 350 Raw data 250 200 150 100 50 120 0 0 5 10 15 20 o (average steady foam volume) 90 60 30 0 25 5 Time (min) The foaminess coefficient () (Bikerman, 1973) o G ; o = Average foam volume (cm3) G = Gas flow rate (cm3/min) 10 15 Time (min) 20 25 10 RESULTS AND DISCUSSIONS EFFECT OF GAS FLOW RATE At 20 – 80 cm3/min, N2 flow rate , At 80 – 110 cm3/min, N2 flow rate , CONSTANT Foaminess cofficient (min) 6.0 3 kmol/m3 2.0 kmol/m MEA 2.0 5.0 kmol/m3 5.05.0 kmol/m3 MEA 4.0 3.0 Working flow rate at 94 cm3/min 2.0 1.0 0.0 0 20 40 120 100 80 60 3 Nitrogen flow rate (cm /min) 140 160 (Test condition: 2.0 & 5.0 kmol/m3 MEA, 400 cm3 solution volume, 0.40 mol/mol CO2 loading and 40oC) 11 RESULTS AND DISCUSSIONS EFFECT OF SOLUTION VOLUME At 200 – 400 cm3, solution volume , At 400 – 700 cm3, solution volume , CONSTANT Foaminess coefficient (min) 1.0 0.8 0.6 0.4 Working Volume at 400 cm3 0.2 0.0 0 200 400 600 800 3 Solution volume (cm ) (Test condition: 2.0 kmol/m3 MEA, 94 cm3/min N2, 0.40 mol/mol CO2 loading and 40oC) 12 RESULTS AND DISCUSSIONS EFFECT OF MONOETHANOLAMINE (MEA) CONCENTRATION MEA concentration , initially and then 25oC 40oC 50oC 70.00 60.00 50.00 40.00 0.80 0.0 Decreased surface tension 0.60 Increased bulk liquid absorber Absorber toptopviscosity Absorber bottom absorber bottom 0.40 0.0 2.0 4.0 6.0 MEA concentration (kmol/m3) (Test condition: MEA, 94 cm3/min N2, 400 cm3 solution volume, absorber top: 0.20 mol/mol CO2 loading/ 40oC & absorber bottom: 0.40 mol/mol CO2 loading/ 60oC) 8.0 2.0 4.0 6.0 MEA concentration (kmol/m3) 8.0 Surface tension of CO2-unloaded aqueous MEA solution replotted from experimental data [Vázquez et al., 1997] 4.0 Predicted viscosity (mPa.s) Foaminess coefficient (min) 1.00 Surface tension (mN/m) 80.00 absorber top 3.5 absorber bottom 3.0 2.5 2.0 1.5 1.0 0.5 0.0 0.0 2.0 4.0 6.0 8.0 MEA concentration (kmol/m3) Predicted viscosity of CO2-loaded aqueous MEA solutions from correlation [Weiland et al., 1998] RESULTS AND DISCUSSIONS 65.000 , initially Surface tension (mN/m) EFFECT OF CO2 LOADING CO2 loading and then 1.50 40 40o C 60.000 55.000 50.000 60 60o C 45.000 90 90o C 40oC 3, 40o C 22,kmol/m 60oC 3, 60o C 22,kmol/m 33,kmol/m 40oC 3, 40o C 33,kmol/m 60oC 3, 60o C 0.00 0.20 0.40 0.60 CO2 loading in solution (mol CO2/mol MEA) 1.00 Surface tension of CO2-loaded aqueous MEA solution measured by Spinning Drop Interfacial Tensiometer Model 510 0.50 Increased bulk liquid viscosity Decreased surface tension 0.00 0.00 0.10 0.20 0.30 0.40 0.50 CO2 loading in solution (mol CO2/mol MEA) 0.60 Predicted viscosity (mPa.s) Foaminess coefficient (min) 13 4.0 3.5 3.0 40oC 40oC 60oC 60oC 90oC 90oC 2.5 2.0 1.5 1.0 0.5 0.0 (Test condition: 5.0 kmol/m3 MEA, 94 cm3/min N2, 400 cm3 solution volume and 40, 60 and 90oC) 0.00 0.20 0.40 0.60 CO2 loading in solution (mol CO 2/mol MEA) Predicted viscosity of 5.0 kmol/m3 MEA solution from correlation [Weiland et al., 1998] RESULTS AND DISCUSSIONS 14 EFFECT OF SOLUTION TEMPERATURE , 1.60 0.20 0.20 mol CO2/mol MEA 1.40 0.40 mol CO2/mol MEA 0.40 Reduced bulk viscosity 1.20 Decreasing 1.00 0.80 0.60 0.40 0.20 0.00 40.0 50.0 60.0 70.0 80.0 90.0 Solution temperature (o C) (Test condition: 5.0 kmol/m3 MEA, 94 cm3/min N2, 400 cm3 solution volume and 0.20 & 0.40 mol/mol CO2 loading) Predicted viscosity (mPa.s) Foaminess coefficient (min) Solution temperature 2.5 2.0 1.5 1.0 0.5 0.0 40.0 0.20 mol/mol CO2 loading 0.40 mol/mol CO2 loading 50.0 60.0 70.0 80.0 Solution temperature (oC) 90.0 Predicted viscosity of 5.0 kmol/m3 MEA solution from correlation [Weiland et al., 1998] RESULTS AND DISCUSSIONS EFFECT OF DEGRADATION PRODUCT Most degradation products added into aqueous MEA solution induce foam. Degradation product Average (min) None 0.80 0.015 Ammonium thiosulfate 0.97 0.049 Glycolic acid 0.94 0.028 Sodium sulfite 0.92 0.042 Malonic acid 0.92 0.016 Oxalic acid 0.90 0.038 Sodium thiocyanate 0.90 0.015 Sodium chloride 0.89 0.004 Sodium thiosulfate 0.85 0.018 Bicine 0.85 0.015 Hydrochloric acid 0.83 0.037 Formic acid 0.83 0.033 Acetic acid 0.82 0.043 Sulfuric acid 0.77 0.034 (Test condition: 10,000 ppm of degradation product, 5.0 kmol/m3 MEA, 94 cm3/min N2, 400 cm3 solution volume, 0.40 mol/mol CO2 loading and 60oC) 15 16 RESULTS AND DISCUSSIONS EFFECT OF CORROSION INHIBITOR 1.20 70.000 1.00 Surface tension (mN/m) Foaminess coefficient (min) Corrosion inhibitors added into aqueous MEA solution enhance . 0.80 0.60 0.40 0.20 0.00 1 MEA 2 3 NaVO 3 3 Na24SO3 CuCO Corrosion inhibitor (Test condition: 1,000 ppm of corrosion inhibitor, 5.0 kmol/m3 MEA, 94 cm3/min N2, 400 cm3 solution volume, 0.40 mol/mol CO2 loading and 60oC) 65.000 60.000 55.000 MEA w/o inhibitor MEA+NaVO3 MEA+CuCO3 MEA+Na2SO3 50.000 45.000 40.000 0 0.5 1 1.5 Corrosion inhibitor Surface tension of 5.0 kmol/m3 MEA solutions containing no CO2 loading at 25oC with/without 1000 ppm corrosion inhibitor (measured by KrÜss Tensiometer K100 using the Wihelmy plate’s principle) 17 RESULTS AND DISCUSSIONS EFFECT OF ALKANOLAMINE TYPE Foam formation in MEA and MDEA but not in DEA Only small amount of foam in AMP+MEA solution with the mixing ratio of 1:2 mol/mol Average MEA 0.85 0.004 DEA No foam MDEA 4.0 2.0 0.0 0.32 0.019 AMP No foam MEA + MDEA (1:1) No foam MEA + MDEA (2:1) No foam MEA + MDEA (1:2) No foam DEA + MDEA (1:1) No foam DEA + MDEA (2:1) No foam DEA + MDEA (1:2) No foam MEA + AMP (1:1) No foam MEA + AMP (1:2) No foam MEA + AMP (2:1) 0.13 0.001 (Test condition: 4.0 kmol/m3 total alkanolamine conc., 94 cm3/min N2, 400 cm3 solution volume, 0.40 mol/mol CO2 loading, 60oC and mixing ratio of blended solution = 1:1, 2:1 and 1:2 (mole:mole)) MEA (Maham et al., 2002) DEA (Teng et al., 2002) MDEA (Teng et al., 2002) AMP (Henni et al., 2003) 6.0 0.0 2.0 Alkanolamine conc. 4.0 (kmol/m3) 6.0 Viscosity of CO2-unloaded aqueous alkanolamine solution at 60o replotted from experimental data Predicted viscosity (mPa.s) Type of alkanolamine Viscosity (mPa.s) and AMP solutions Single alkanolamine 8.0 2.5 Blended alkanolamine 1:2 1:1 2:1 2.0 1.5 1.0 0.5 0.0 MEA+MDEA DEA+MDEA MEA+AMP Type of blended alkanolamine Predicted viscosity of the CO2-unloaded aqueous blended alkanolamine solution (4.0 kmol/m3 total alkanolamine conc. and 60oC) from Grunberg and Nissan’s equation (Mandal et al., 2003)) 18 FOAM MODEL: LITERATURE Researcher Foaming system Solution Method Proposed equation Gas Ito and Fruehan (1989) 28%Cao-42%SiO230%FeO slags Argon Dimensional analysis = (, , ) 5.7 102 Jiang and Fruehan (1991) 30%FeO (Cao/SiO2=1.25) and 0%FeO (Cao/SiO2=1.25) slags Argon Dimensional analysis = (, , , g) 359 Zhang and Fruehan (1995) 40%Cao-40%SiO215%Al2O3-5%FeO slags Argon Dimensional analysis = (, , , g, Db) 1.2 115 0.2 0.9 Db Ghag et al (1998) Water + 78 – 95% glycerinate +SDBS N2 Dimensional analysis 1. = (, , , g, Db); is surface tension depression 2. = (g, , Db, EM); EM is surface elasticity 3. = (g, , Db, Eeff); Eeff is effective elasticity g 2.02 106 1.32 g2.32 Db3.64 5.43 105 EM0.89 g1.89 Db2.78 1 106 Eeff g2 Db3 Pilon et al (2001) Results from other research works Dimensional analysis of the governing equation for the pneumatic foam layer proposed by (Bhakta and Ruckenstein, 1997) j jm H 2905 2.6 ro g1.8 Pilon and Viskanta (2004) Results from other research works Dimensional analysis of the governing equation for the pneumatic foam layer proposed by (Bhakta and Ruckenstein, 1997) + Prediction of minimum superficial gas velocity (jm) H 2905 0 .8 j jm 2 .6 ro g1.8 0 .8 16 19 FOAM MODEL: DEVELOPMENT START Process parameter: 1. MEA concentration (M) 2. Solution temperature (T) 3. Superficial gas velocity (j) 4. Minimum superficial gas velocity (jm) 5. Initial liquid volume (Vlig) 6. CO2 loading (aCO2) Physical properties: 1. Surface tension () 2. Gas density (G) 3. Liquid density (L) 4. Liquid viscosity (L) 5. Water viscosity (w) Surface tension prediction using Wilson equation (Chunxi et al., 2000) Liquid density prediction using Weiland’s correlation (Weiland et al., 1998) Liquid viscosity prediction using Weiland’s correlation (Weiland et al., 1998) Define the control surface for the pneumatic foam layer END Governing equation Pilon et al (2001) YES Dimensional analysis Find K and n: H Re Ca K Fr ro R2 à 1.0 Sr à 0.0 Initial guess for bubble radius (ro) n Modified Laplace equation Pc Pin Pout Hpredict’s trend @ Hexp’s trend Adjust new ro NO END R2 à 1.0 and Sr à0.0 Hpredict’s trend @ Hexp’s trend Recalculating ro NO YES YES NO 2 ro 20 FOAM MODEL: RESULTS Foaming height equation 1.22 j j m H 172059 3.44 ro g 2.22 where ro 2 101.325 Pout INSIGNIFICANT Pout = Pdispersion + Pfoam + P* 80.00 Parity chart 110.30M 1.1210 T 2.5210 j 3.2610 3 * Hexp (mm) P 60.00 P 40.00 R² = 0.84 20.00 104.01M 7.9110 T 3.6210 j 3.0210 0.00 0.00 3 20.00 40.00 60.00 Hpredicted (mm) 80.00 3 9.6510 3 1.3710 3 Vlig aCO 2 4 2 7.1110 4.8310 Vlig j 2 2 L w L when % 53% when 53 % L w 73% 1.4110 104.06M 9.0410 T 1.1810 aCO 3 P* 3 1.6810 2 5.9410 4 Vlig aCO 2 3 * 3 L 3 when w 73% % L L 21 35.00 70.00 30.00 60.00 Foam height (mm) 25.00 20.00 15.00 10.00 Experiment Predicted 5.00 200 400 600 40.00 30.00 Experiment - 2M Predicted - 2M Experiment - 5M Predicted - 5M 20.00 10.00 0.00 0.00 0 50.00 0 800 40.00 60.00 35.00 50.00 30.00 25.00 20.00 15.00 Experiment - Bottom Predicted - Bottom Experiment - Top Predicted - Top 10.00 5.00 0.00 0.0 2.0 4.0 6.0 MEA concentration (kmol/m3) 8.0 Foam height (mm) Foam height (mm) Solution volume (cm3) 50 100 Experiment - 40 Experiment - 60 Experiment - 90 200 60.00 Predicted - 40 Predicted - 60 Predicted - 90 40.00 30.00 20.00 10.00 50.00 40.00 30.00 20.00 Experiment - 0.2 Predicted - 0.2 Experiment - 0.4 Predicted - 0.4 10.00 0.00 0.00 0.0 150 Gas flow rate (cm3/min) Foam height (mm) Foam height (mm) FOAM MODEL: RESULTS 0.2 0.4 CO2 loading (mol/mol) 0.6 0.0 20.0 40.0 60.0 80.0 100.0 Solution temperature (oC) CONCLUSION 22 Solution volume affects when it is small. Increasing the solution volume to a certain quantity results in a constant foam volume or . An increase in gas flow rate decreases . The gas flow rate can lead to a constant when increases to a certain value. Ranges of solution volume and gas flow rate that lead to a constant were found for the CO2aqueous alkanolamines. These ranges enable the generation of foam data that do not depend on solution volume, gas flow rate, pore size of gas disperser, and dimension of test cell. Variations in MEA concentration, CO2 loading and solution temperature affect . An increase in temperature decreases . increases and then declines with increasing MEA concentration and CO2 loading. Most degradation products and corrosion inhibitors enhance . MEA, MDEA and AMP + MEA (1:2 mixing mole ratio) generate apparent foams FOAM MODEL is established to predict the steady-state pneumatic foam height from the physical properties and operating conditions and also to identify the important dimensionless numbers for a scaling-up hydrodynamic experiment. 23 FUTURE WORK FOAM MODEL Sensitivity analysis of input parameters on the predicted foam height. Model improvement by incorporating the minimum superficial gas velocity predicted based on the one-dimensional drift-flux model (Pilon and Viskanta, 2004) HYDRODYNAMIC Study the foaming behavior occurred in the packed absorber during absorption process based on dimensionless numbers in terms of the foaming tendency and the foam stability by measuring and foam half-life, respectively. Investigate the effect of foaming on the hydrodynamic parameter s (e.g., pressure drop, liquid holdup and flooding point) of the packed CO2 absorption column based on dimensionless numbers. à FOAMING CHART 21 ACKNOWLEDGEMENT Faculty of Graduate Studies and Research (FGSR), University of Regina Faculty of Engineering, University of Regina The Natural Sciences and Engineering Research Council (NSERC) 24