Abstract:Screen internals were used in a two‐dimensional two‐stage internal loop airlift reactor (ILALR). The influence of screens on the hydrodynamics and mass transfer characteristics in the two‐stage ILALR, including gas holdup, mean bubble diameter, bubble rise velocity, and volumetric mass transfer coefficient (KLa), have been experimentally investigated. It is found that screens can efficiently break bubbles up. Radial bubble velocity distribution is more uniform when screens are installed. Mean bubble diameter w… Show more
“…Therefore, various high-efficient ILALRs were developed from the perspective of increasing the gas holdup. 10 − 13 The hydrodynamics of the ILALRs have been studied mainly via experiment 12 , 14 − 19 and computational fluid dynamics (CFD) simulation. 20 − 27 In the experimental studies, gas holdup, mixing time, bubble size, residence time distribution, and liquid circulating velocity can be measured by invasive 7 or non-invasive methods.…”
Global circulation
and liquid back mixing adversely affect the
continuous production of a multistage internal airlift loop reactor.
A contraction-expansion guide vane (CEGV) is proposed and combined
with a two-stage internal loop airlift reactor (TSILALR) to suppress
the liquid back mixing between stages. A computational fluid dynamics
(CFD) simulation is conducted to evaluate the performance of the CEGV
in the TSILALR. The bubble size distribution and turbulent flow properties
in the TSILALR are considered in the CFD simulation by using the population
balance model and RNG
k
-
ε
turbulence
model. The CFD model is validated against the experimental results.
The deviations in the gas holdup and mean bubble diameter between
the simulation and experimental results are less than 8% and 6%, respectively.
The streamlines, flow pattern, bubble size distribution, and axial
liquid velocity in the TSILALRs with and without the CEGV at superficial
velocities of 0.04 and 0.08 m/s are obtained by CFD simulation. It
has been shown that the CEGV generated local circulation flows at
each stage instead of a global circulation flow in the TSILALR. The
average global gas holdup in the TSILALR with a CEGV increased up
to 1.98 times. The global gas holdup increased from 0.045 to 0.101
and the average axial velocity in the riser decreased from 0.314 to
0.241 m/s when the width of the CEGV increased from 50 to 75 mm at
the superficial gas velocity of 0.08 m/s.
“…Therefore, various high-efficient ILALRs were developed from the perspective of increasing the gas holdup. 10 − 13 The hydrodynamics of the ILALRs have been studied mainly via experiment 12 , 14 − 19 and computational fluid dynamics (CFD) simulation. 20 − 27 In the experimental studies, gas holdup, mixing time, bubble size, residence time distribution, and liquid circulating velocity can be measured by invasive 7 or non-invasive methods.…”
Global circulation
and liquid back mixing adversely affect the
continuous production of a multistage internal airlift loop reactor.
A contraction-expansion guide vane (CEGV) is proposed and combined
with a two-stage internal loop airlift reactor (TSILALR) to suppress
the liquid back mixing between stages. A computational fluid dynamics
(CFD) simulation is conducted to evaluate the performance of the CEGV
in the TSILALR. The bubble size distribution and turbulent flow properties
in the TSILALR are considered in the CFD simulation by using the population
balance model and RNG
k
-
ε
turbulence
model. The CFD model is validated against the experimental results.
The deviations in the gas holdup and mean bubble diameter between
the simulation and experimental results are less than 8% and 6%, respectively.
The streamlines, flow pattern, bubble size distribution, and axial
liquid velocity in the TSILALRs with and without the CEGV at superficial
velocities of 0.04 and 0.08 m/s are obtained by CFD simulation. It
has been shown that the CEGV generated local circulation flows at
each stage instead of a global circulation flow in the TSILALR. The
average global gas holdup in the TSILALR with a CEGV increased up
to 1.98 times. The global gas holdup increased from 0.045 to 0.101
and the average axial velocity in the riser decreased from 0.314 to
0.241 m/s when the width of the CEGV increased from 50 to 75 mm at
the superficial gas velocity of 0.08 m/s.
“…A mass transfer enhancement can be safely realized by increasing the gas-liquid interfacial area. For example, by adding internals [18][19][20][21] or changing operation conditions, [22][23][24] the bubble diameter can be effectively decreased, and thus the interfacial area increased. Alcohols, 25,26 surfactants 8,[27][28][29] and electrolytes [30][31][32] are typically added in coalescence systems to inhibit bubble coalescence 33 and increase bubble rigidity, 34 by which bubbles become smaller and a larger interfacial area is obtained.…”
BACKGROUND: Bubble columns have found a wide range of application in biochemical industry. Mass transfer in the bubble column can be manipulated by adjusting the bubble size. Thus, for the design of bubble columns, it is necessary to investigate the behaviors of different-sized bubbles. This work attempts to study the global hydrodynamic and mass transfer characteristics of bubble swarms with Sauter mean diameters (d 32) of 0.38-4.88 mm, from microbubbles to millimeter-sized bubbles, in a co-current bubble column. RESULTS: The specific interfacial areas of the bubble swarms with d 32 of 0.38-1.47 (generated by ceramic membrane module) and 1.05-4.88 mm (generated by plate gas distributor) are 250-1100 and 7-270 m −1 , respectively. The liquid-side mass transfer coefficient (k L) of those two kinds of bubbles are (0.45-1.16) × 10 −4 and (0.58-7.65) × 10 −4 m s −1 , respectively. CONCLUSION: Decreasing the bubble size can effectively increase the volumetric mass transfer coefficient (k L a), especially when the bubble size decreases to several micrometers. The major contribution to the mass transfer enhancement results from the increase of the specific interfacial area. Conversely, the k L decreases clearly. It is demonstrated that Higbieʼs and Frosslingʼs equations can approximate the k L of the bubble swarms with d 32 > 2 mm and d 32 < 2 mm in the bubble column, respectively.
“…The bubble diameter was analyzed using ImageJ software. The bubble diameter for elliptical bubbles was measured by considering the major and minor axis of the bubble as : …”
The hydrodynamics and volumetric mass transfer coefficient play important roles in the design and scale-up of airlift reactors. The effect of surface tension on hydrodynamics and volumetric mass transfer coefficient in internal loop airlift reactors was investigated. With reduction of the surface tension of the fluid, the hydrodynamic parameters raised, namely, gas phase holdup, flow regime transition point, and interfacial area, whereas the bubble diameter as well as the liquid velocity decreased and the volumetric mass transfer coefficient increased. Empirical correlations are proposed for gas-phase holdup and volumetric mass transfer coefficient in terms of dimensionless numbers and can be applied in the design of airlift reactors.
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