Severe erosion in the lower cone and in the upper dipleg of second stage cyclones have been observed in commercial cyclones. The main objective of this study is to shed light on the mechanism by which this erosion takes place, and how different design and operating parameters affect the erosion. Experimental data on how parameters such as the cyclone length-to diameter ratio (L/D), inlet solids loading and gas outlet velocity affect second stage cyclone erosion are presented. The outlet gas velocity was varied by changing the size of the vortex tube diameter. The effect of a vortex stabilizer on cyclone cone erosion is also discussed

Cocco, Ray

Karri, S. B. Reddy

Knowlton, Ted

English

Engineering Conferences International

Engineering Conferences InternationalECI Digital Archives10th International Conference on CirculatingFluidized Beds and Fluidization Technology -CFB-10Refereed ProceedingsSpring 5-3-2011Erosion in Second Stage Cyclones: Effects ofCyclone Length and Outlet Gas VelocityS. B. Reddy KarriParticulate Solid Research, Inc., USARay CoccoParticulate Solid Research, Inc., ray.cocco@psrichicago.comTed KnowltonParticulate Solid Research, Inc., USAFollow this and additional works at: http://dc.engconfintl.org/cfb10Part of the Chemical Engineering CommonsThis Conference Proceeding is brought to you for free and open access by the Refereed Proceedings at ECI Digital Archives. It has been accepted forinclusion in 10th International Conference on Circulating Fluidized Beds and Fluidization Technology - CFB-10 by an authorized administrator of ECIDigital Archives. For more information, please contact franco@bepress.com.Recommended CitationS. B. Reddy Karri, Ray Cocco, and Ted Knowlton, "Erosion in Second Stage Cyclones: Effects of Cyclone Length and Outlet GasVelocity" in "10th International Conference on Circulating Fluidized Beds and Fluidization Technology - CFB-10", T. Knowlton, PSRIEds, ECI Symposium Series, (2013). http://dc.engconfintl.org/cfb10/40EROSION IN SECOND STAGE CYCLONES: EFFECTS OFCYCLONE LENGTH AND OUTLET GAS VELOCITYS. B. Reddy Karri*, Ray Cocco and Ted M. KnowltonParticulate Solid Research, Inc.4201 W. 36th Street, Chicago, IL 60632, USAABSTRACTSevere erosion in the lower cone and in the upper dipleg of second stage cycloneshave been observed in commercial cyclones. The main objective of this study is toshed light on the mechanism by which this erosion takes place, and how differentdesign and operating parameters affect the erosion. Experimental data on howparameters such as the cyclone length-to diameter ratio (L/D), inlet solids loadingand gas outlet velocity affect second stage cyclone erosion are presented. Theoutlet gas velocity was varied by changing the size of the vortex tube diameter. Theeffect of a vortex stabilizer on cyclone cone erosion is also discussed.INTRODUCTIONPetroleum refineries have increased their focus on improving unit reliability, andreducing operational and maintenance costs. Because their cyclones have highefficiencies, fluidized catalytic cracking unit (FCCU) process operators are nowconcerned with longer campaign durations, and would like to improve cyclonereliability. The 2008 NPRA survey and other surveys (1,2) revealed that FCCUcyclone reliability (3,4) was a major concern for refineries. The most pervasiveproblem is erosion in secondary cyclones in the lower cone and upper dipleg, whichis the focus of this study.There is a fundamental difference between first and second stage FCC cyclones inregard to erosion patterns. Highly-loaded first stage cyclones normally experienceno cone erosion, whereas lightly-loaded second stage cyclones can have severecone erosion. This seems to be counter-intuitive, but can be explained by thedifferences in the solids flow patterns and vortex lengths, as shown in Figure 1.Due to the high solids loading and the low gas inlet velocity in a typical FCCUprimary cyclone, gravitational force plays a key role. As a result, the solids appear tofall rapidly down into the cyclone cone and dipleg, as shown in Fig. 1, taking only oneto two full turns before exiting the cyclone. The vortex length in a highly-loaded2Primary Cyclone Secondary Cyclone(High Loading) (Low Loading)Solids Flow Path(Outer Vortex) Many More Turns onTighter Radius: SpinsFaster – Hence MorePotential for ErosionLonger , Energetic,Inner VortexInner VortexFigure 1. Schematic Depiction of First and Second-Stage Cyclone Operationprimary cyclone is much shorter, because the high solids loading dampens theformation of a long vortex. Therefore, the vortex does not “whip” the solids at a highvelocity around the cone as in a primary cyclone.In a typical second stage cyclone, the solids loading is approximately 1/1000 to1/10,000 of the loading in the first stage cyclone. Due to the light solids loading andhigh gas velocity, the inner vortex is relatively long and energetic. As the swirlingsolids in the outer vortex approach the cone in a second stage cyclone, the long,rapidly-rotating vortex accelerates the solids stream and causes it to intensify itsrotation because of the conservation of angular momentum. The solids in a second-stage cyclone typically take four to seven turns before exiting the bottom cone, andthe spinning continues into the top portion of the dipleg below the cone. Most ofthose spins are located in the lower part of the cone and in the upper dipleg wherethe small diameters result in high angular velocities. The rapidly-rotating solidsstream coupled with the unstable, continuous movement of the vortex causessignificant erosion in the cone and at the top of the dipleg of second-stage cyclones.EXPERIMENTALThe testing was structured to benchmark three possible solutions to mitigate theerosion occurring in second-stage cyclones: 1) increasing cyclone length-to-diameterratio (L/D), 2) increasing the angle of the cone, and 3) adding a vortex stabilizer.The cyclone test facility used in the study is shown in Fig. 2. It consisted of a 0.91-m-diameter fluidized bed, a 0.2-m-diameter standpipe approximately 17 m in length;a slide valve to control the solids flow rate around the unit; a 0.2-m-diameter riserapproximately 21 m tall; a 0.48-m-diameter first stage cyclone; and the 0.43-m-diameter second stage cyclone.3Air was used as the conveying gas inthe test unit. The solids used wereequilibrium FCC catalyst with a median(dp,50) particle size of 75 m. The fines(material < 44 microns) concentrationin the catalyst was approximately 8wt.%. The particle density of thecatalyst was 1490 kg/m3. Loadings tothe second stage cyclone were variedbetween 0.001 to 0.21 kg/m3. Thesecondary cyclone was constructedmodularly for easy change ofdimensions. A schematic drawing ofthe second stage cyclone is shown inFig. 3 for several different barrellengths. Multiple coatings of drywalljoint compound were added to theinside of the cyclone before each test.The amount of erosion occurring in thecyclone was measured by the weightloss of the drywall compound occurringover a certain period of time.Figure 3. Schematic Drawing of Different Cyclone L/D's [cm]RESULTS AND DISCUSSIONEffect of Increased Cyclone L/DL/Db = 3.1 L/Db = 4.1 L/Db = 5.19"[22.86]9"[22.86] 1'-9"[53.34]2'-814"[81.92]4"[10.16]1'-5"[43.18]414"[10.80]7°6"[15.41]2'-814"[81.92]4"[10.16]1'-9"[53.34]1'-5"[43.18]7°1'-5"[43.18]2'-814"[81.92]4"1'-5"[43.18]1'-9"[53.34]7°1'-5"[43.18]1'-5"[43.13]79°20-cm Riser20-cm Standpipe2nd Stage Cyclone151617 1813R14R1st Stage CycloneDiverter Valve12RAutomatic L-Valve11RReceiving Tankon Load Cells10R0.91-m -BedFigure 2. Schematic Drawing ofCyclone Erosion Test Unit4Figure 4. Photograph of Erosion ofDrywall Joint Compound in theCone of a Second-Stage CycloneThe study found that the erosion took placeprimarily in the bottom 1/3 of the cone ofthe secondary cyclone”. A photographillustrating this effect is shown in Fig. 4.This figure shows that the drywall coatingwas completely eroded from the bottom1/3 of the cone, whereas the remainingdrywall was mostly intact.Cyclone lengths were increased byincreasing the length of the cyclone barrelto give length-to-diameter (L/D) ratios of3.1, 4.1 and 5.1. In these tests, the inletgas velocity to the cyclone was 19.8 m/sand the outlet gas velocity was 27 m/s.The results of the testing to determine theeffect of cyclone L/D is shown in Fig. 5.As can be seen, the erosion ratedecreased with increasing cyclone L/D.The measured erosion rate at an L/D of 5.1was about 70% of the erosion rate of thecyclone with an L/D of 3.1.Barrel erosionrates were alsomeasured in thetests and werefound to be muchlower than theerosion rates inthe cone (Fig. 5).Measured barrelerosion ratesranged between85 to 105 g/h,which was about15% of the coneerosion rate forthe cyclone withan L/D of 3.1, andabout 20% for acyclone with anL/D of 5.1.Effect of Cone LengthThe effect of cone length on cyclone cone erosion was tested by adding a longercone so that the cone angle from the horizontal increased from 79 to 84º. Thisincreased the cone length from 0.82 to 1.68 m. When comparing the two coneconfigurations, the overall length of the cyclone was held constant.0100200300400500600700800Cone BarrelErosionRates,g/h3.14.15.1Material: FCC Eq. CatalystUgi: 19.8 m/sUgo: 27 m/sCyclone Size: 43-cmInlet Type: TangentialLi : 0.011 kg/m3L/Db:Figure 5. The Effect of Second-Stage Cyclone L/D on ConeErosion and Barrel Erosion5As shown in Fig. 6, the cyclone with the longer cone had a higher erosion rate at lowoutlet gas velocities than the cyclone with the shorter cone but longer barrel.However, the erosion rate became approximately equal to the erosion rate of theshorter cone at the highest outlet gas velocity. The trend of the two curves wasexactly opposite. For the cyclone with the shorter cone, the erosion rate increasedwith gas velocity, whereas for the longer cone the erosion rate decreased with gasvelocity. For an outlet gas velocity of approximately 27 m/s, the erosion rate for theshort cone cyclonewas approximately800 g/h, while theerosion rate for thelong cone cyclonewas approximately1800 g/h, a factor of2.25. However,even at the highestoutlet gas velocities,which were outsidetypical operatingoutlet velocities ofsecondary cyclones,the longer cone didnot have asignificantadvantage over the shorter cone in regard to cone erosionVortex StabilizersTo determine the effect of adding a vortex stabilizer on cone erosion, a flat-diskvortex stabilizer was added in thecyclone cone, approximately 1/3of the cone length from itsbottom, at the top of the region inwhich the cone erosion was mostsignificant. A photograph of thedisk is shown in Fig. 7.The location of the vortexstabilizer was selected to be atthe top of the high-erosion sectionof the cone. It was thought thatadding the vortex stabilizer 1/3 ofthe cone height from the bottomof the cone would prevent high-velocity spinning solids in thatregion and reduce erosion. Thepurpose of the flat plate (or thevortex stabilizer) was to stabilizethe central vortex. It wasexpected that the influence of thevortex would end at the plate, andFigure 6. The Effect of Cone Length on Second-StageCyclone Cone Erosion0 10 20 30 40 50 60050010001500200025000 50 100 150 200Ugo, m/sConeErosionRate,g/hUgo, ft/sLonger Coneshorter coneMaterial: FCC Eq. CatalystUgi: 19.8 m/sCyclone Size: 43-cmInlet Type: TangentialLi : 0.032 kg/m3; L/Db: 5.179°4"[10.16]1012"[26.78]714"[18.42]StabilizerDiskThree SupportsNo ErosionFigure 7. Photographs and SchematicDrawing of the Vortex Stabilizer and Supports6the number and intensity of the solids spirals below the plate would be reduced.The effect of adding the vortex stabilizer disk on cyclone cone erosion is shown inFigs. 8 and 9 for cyclones with L/Ds of 3.1 and 5.1, respectively. It was found thatcone erosion for a cyclone with a vortex stabilizer was significantly lower than that fora cyclone without a vortex stabilizer. Cone erosion was found to increase linearlywith increasing gas velocity for a cyclone without a vortex stabilizer. However, coneerosion in a cyclone with a vortex stabilizer decreased slightly with increasing gasoutlet velocity. The decrease in erosion is counter-intuitive. However, this can beexplained by the fact that the vortex diameter is smaller when the diameter of theoutlet tube is decreased. Thisincreases the distance betweenthe vortex and the cone wall,which then reduces thecentrifugal force (and, therefore,the solids velocity) on the solidsrotating in the cone. Thereduction in force on the solidsappears to explain the decreaseof cone erosion vs. gas outletvelocity for a cyclone with avortex stabilizer (Figs. 8 and 9).For the shorter cyclone, thecone erosion rate wasapproximately 2100 g/h for thecyclone without a vortexstabilizer at an outlet gasvelocity of 15.2 m/s. Thecorresponding cone erosionrate for the cyclone with avortex stabilizer at the sameoutlet gas velocity was about1400 g/h. The cone erosionrate with the vortex stabilizerwas about 67% of the coneerosion rate for the cyclonewithout the vortex stabilizer.However, at an outlet gasvelocity (45.7 m/s) closer toactual practice, the coneerosion rate for a cyclone withthe vortex stabilizer was onlyabout 600 g/h. Thecorresponding cone erosionrate for a conventional cyclone without a vortex stabilizer was about 2900 g/h. Thiswas a factor of about 4.8.For the cyclone with an L/D of 5.1, the overall cone erosion rates were lower. Thiswas expected because the tests with the longer cyclone described above gave lowercone erosion rates than shorter cyclones. As with the shorter cyclone, the trendlinesFigure 8. The Effect of Gas Outlet Velocity onSecond-Stage Cyclone Cone Erosion forCyclones With and Without a Flat-Plate VortexStabilizer0 20 40 6005001000150020002500300035000 50 100 150 200Ugo, m/sConeErosionRate,g/hUgo, ft/sw/o diskw/ diskMaterial: FCC Eq. CatalystUgi: 19.8 m/sCyclone Size: 43-cmInlet Type: TangentialLi : 0.032 kg/m3; L/Db: 3.10 10 20 30 40 50 60020040060080010001200140016000 50 100 150 200Ugo, m/sConeErosionRate,g/hUgo, ft/sw/o diskw/ diskMaterial: FCC Eq. CatalystUgi: 19.8 m/sCyclone Size: 43-cmInlet Type: TangentialLi : 0.032 kg/m3; L/Db: 5.1Figure 9. The Effect of Gas Outlet Velocity onSecond-Stage Cyclone Cone Erosion Rate forCyclones With and Without a Flat-Plate VortexStabilizer7of cone erosion rate vs. outlet gas velocity were linear. Similarly, the curve for theconventional cyclone erosion rate without a vortex stabilizer increased withincreasing gas velocity, and the curve for the cyclone erosion rate with the vortexstabilizer decreased slightly with increasing gas velocity. However, as with theshorter cyclone, the cyclone with the vortex stabilizer was found to have much lowererosion rates than the conventional cyclone without the vortex stabilizer. Comparingthe cone erosion rates at an outlet gas velocity of 45.7 m/s, the conventional cyclonewithout a vortex stabilizer had a cone erosion rate of approximately 1200 g/h, whilethe cyclone with the vortex stabilizer had a cone erosion rate of about 240 g/h. Thisis a factor of approximately 5 - similar to what was found for the shorter cyclone.Why does the vortex stabilizer decrease cone erosion? It appears that the stabilizerprevents the vortex from "whipping" the solids around at high velocities below thestabilizer in the region where high cone erosion rates are experienced for a cyclonewithout a vortex stabilizer. Below the stabilizer, the high-velocity central vortex doesnot really exist. Therefore, this reduction in the spinning solids velocity at the wallleads to a significant reduction in erosion. A comparison of the cone erosion ratesfor various second-stage cyclone configurations is given in Table 2.Drywall joint compound was also added to the disk to see if the upper surface of thevortex stabilizer would erode. However, essentially no erosion was measured on theupper surface of the disk, and no erosion was found on the supporting rods.Shell Experience with Vortex StabilizersIn the 1980’s, Shell had over 30 FCC units, mostly with cyclones without vortexstabilizers, which were found to be the number one cause of all FCC unscheduledshutdowns. Shell started using the vortex stabilizer (5) in the early 90’s. Fig. 11shows the result of how the vortex stabilizer reduced overall FCC unscheduled downtime.Table 2. Comparison of cone erosion rates for different cyclone configurationsL/D(-)VelocityInlet, m/sVelocityOutlet, m/sErosionReductionFactorConeErosionRate, g/hShort Cyclone 3.1 19.8 45.7 Base 2850Long Cyclone 5.1 19.8 45.7 >2 1200Long Cone 5.1 19.8 45.7 >2 1200Vortex Stabilizer 3.1 19.8 45.7 >4 650Vortex Stabilizer 5.1 19.8 45.7 >11 240Using 1992 data as the base line, Fig. 11 shows that cyclones with the vortexstabilizer reduced the total unit down time of all FCC units in the Shell system by afactor of 10 over a period of 8 years.80%10%20%30%40%50%60%70%80%90%100%1992 1993 1994 1995 1996 1997 1998 1999Severity(Incl.nearmisses)[NumberofEvents*Duration]1992=100%Total Severity of Cyclone ProblemsFigure 10. Cyclone Severity vs. TimeCONCLUSIONSSecond stage cyclone cone erosion is a pervasive problem in FCCU operation,which can be significantly improved by incorporating the use of a vortex stabilizer.Vortex stabilizers were more effective in reducing second stage cyclone coneerosion than increasing cyclone barrel or cone length.REFERENCES1. Solomon Associates LLC , 2006 Solomon FCC Events Determining TAR TimingSurvey, 20062. Grace Davison Survey, FCC Conference in Dublin, California, USA, 20023. Zenz, F.A., Cyclone Separators, in Manual on Disposal of Refinery WastesVolume on Atmospheric Emissions, Chapter 11, American Petroleum Institute,Pub. No. 931, Washington, D.C. (1975).4. Tenney, Ed., FCC Cyclone Problems And How They Can Be Overcome WithCurrent Designs, Presented at the Grace-Davison FCC Technology Conference,Toledo, Spain (1992).5. Chen, Y., Karri, S.B.R., Knowlton, T.M., Winning in the Downturn: How toImprove FCC Unit Reliability and Reduce Costs via Improved CycloneTechnology, NPRA Meeting, Phoenix, AZ (2010).6. Sexton, J., Karri, S.B.R., Knowlton, T.M., “What is Happening Above YourFluidized Bed?” Tools to Maximize FCC Unit Reliability and Turnaround Cycles,NPRA Meeting, Phoenix, AZ (2010).

Erosion in Second Stage Cyclones: Effects of Cyclone Length and Outlet Gas Velocity

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Erosion in Second Stage Cyclones: Effects of Cyclone Length and Outlet Gas Velocity

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