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首页> 外文期刊>Brazilian journal of chemical engineering >The effects of geometry and operational conditions on gas holdup, liquid circulation and mass transfer in an airlift reactor
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The effects of geometry and operational conditions on gas holdup, liquid circulation and mass transfer in an airlift reactor

机译:几何形状和运行条件对气举反应器中气体滞留,液体循环和传质的影响

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In airlift reactors transport phenomena are achieved by pneumatic agitation and circulation occurs in a defined cyclic pattern through a loop. In the present work, the effect of geometrical relations on gas holdup and liquid velocity, and consequently on the gas-liquid mass transfer coefficient, was studied in a 6-liter airlift bioreactor with A D/A R = 0.63; A D, downcomer cross-sectional area, and A R, riser cross-sectional area. Measurements of the volumetric oxygen transfer coefficient (kLa) were taken in a water-air system using a modified sulfite oxidation method. Different conditions were examined by varying parameters such as superficial air velocity in the riser (U GR), bottom clearance (d1) and top clearance (d2). It was observed from the experimental results that d1 and d2 have a remarkable effect on kLa values. The effect is due to their influence on gas holdup and liquid velocity, consequently affecting kLa. Superficial air velocity in the riser (U GR) ranged from 0.0126 to 0.0440 m.s-1 and kLa varied between 40 to 250 h-1, whereas gas holdup (e) reached values up to 0.2. The volumetric oxygen transfer coefficient (kLa), gas holdup in the riser (eR) and downcomer (eD) and superficial liquid velocity in the riser (U LR) for all the geometrical relations were successfully correlated with dimensionless numbers, namely, the Sherwood number (Sh) and the Froude number (Fr) as well as with geometrical relations such as the bottom space ratio (B = d1/D D) and top space ratio (T = (d2 + D D)/D D).
机译:在空运反应堆中,运输现象是通过气动搅拌来实现的,并且循环通过回路以定义的循环模式发生。在目前的工作中,在A D / A R = 0.63的6升空运生物反应器中研究了几何关系对气体滞留率和液体速度的影响,进而对气液传质系数的影响。 D为下降管截面积,A R为上升管截面积。使用改进的亚硫酸盐氧化方法在水-空气系统中测量体积氧传递系数(kLa)。通过改变参数来检查不同的条件,这些参数包括立管中的表面空气速度(U GR),底部间隙(d1)和顶部间隙(d2)。从实验结果可以看出,d1和d2对kLa值有显着影响。其影响是由于它们对气体滞留率和液体速度的影响,因此影响kLa。立管中的表观风速(U GR)为0.0126至0.0440 m.s-1,kLa在40至250 h-1之间变化,而气体滞留率(e)达到0.2。所有几何关系的体积氧传递系数(kLa),立管中的气体滞留率(eR)和降液管(eD)以及立管中的表观液体速度(U LR)已成功与无量纲数相关,即舍伍德数(Sh)和弗洛德数(Fr)以及几何关系,例如底部空间比(B = d1 / DD)和顶部空间比(T =(d2 + DD)/ DD)。

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