中国环境科学
中國環境科學
중국배경과학
China Environmental Science
2015年
9期
2698-2705
,共8页
孙昕%段飞飞%刘凌炜%解岳
孫昕%段飛飛%劉凌煒%解嶽
손흔%단비비%류릉위%해악
分层水环境%等温层曝气%表观水流速度%模型%曝气量%气泡直径
分層水環境%等溫層曝氣%錶觀水流速度%模型%曝氣量%氣泡直徑
분층수배경%등온층폭기%표관수류속도%모형%폭기량%기포직경
Stratified water environments%hypolimnetic aeration%superficial water velocity%model%air flowrate%bubble diameter
等温层曝气器内表观水流速度直接影响等温层曝气的充氧效果,针对表观水流速度难以准确计算的普遍问题,系统分析了曝气室内气水两相流运动所受的驱动能量与损失能量,提出了尾涡和顶部能量损失的无量纲表达式,建立了曝气室内水流的一维水动力学模型,以及基于MATLAB真域算法的模型求解方法.采用美国Prince湖等温层曝气器的实际运行数据,对该模型进行了验证,表观水流速度的预测误差在±8%以内,明显低于现有预测误差±20%.当曝气孔直径为2.6mm、曝气量从0.018m3/h增加到0.063m3/h时,曝气室内表观水流速度随曝气量的增加而增加;当曝气量固定,曝气孔直径从2.6mm减小至0.26mm时,表观水流速度随曝气孔直径的减小而增加,而当曝气孔直径进一步减小至 0.026mm 时,表观水流速度基本不受影响.计算了不同条件下的驱动能量和各项损失能量,揭示了引起表观水流速度变化的内因.建立的水动力学模型可用于指导等温层曝气器的设计和优化.
等溫層曝氣器內錶觀水流速度直接影響等溫層曝氣的充氧效果,針對錶觀水流速度難以準確計算的普遍問題,繫統分析瞭曝氣室內氣水兩相流運動所受的驅動能量與損失能量,提齣瞭尾渦和頂部能量損失的無量綱錶達式,建立瞭曝氣室內水流的一維水動力學模型,以及基于MATLAB真域算法的模型求解方法.採用美國Prince湖等溫層曝氣器的實際運行數據,對該模型進行瞭驗證,錶觀水流速度的預測誤差在±8%以內,明顯低于現有預測誤差±20%.噹曝氣孔直徑為2.6mm、曝氣量從0.018m3/h增加到0.063m3/h時,曝氣室內錶觀水流速度隨曝氣量的增加而增加;噹曝氣量固定,曝氣孔直徑從2.6mm減小至0.26mm時,錶觀水流速度隨曝氣孔直徑的減小而增加,而噹曝氣孔直徑進一步減小至 0.026mm 時,錶觀水流速度基本不受影響.計算瞭不同條件下的驅動能量和各項損失能量,揭示瞭引起錶觀水流速度變化的內因.建立的水動力學模型可用于指導等溫層曝氣器的設計和優化.
등온층폭기기내표관수류속도직접영향등온층폭기적충양효과,침대표관수류속도난이준학계산적보편문제,계통분석료폭기실내기수량상류운동소수적구동능량여손실능량,제출료미와화정부능량손실적무량강표체식,건립료폭기실내수류적일유수동역학모형,이급기우MATLAB진역산법적모형구해방법.채용미국Prince호등온층폭기기적실제운행수거,대해모형진행료험증,표관수류속도적예측오차재±8%이내,명현저우현유예측오차±20%.당폭기공직경위2.6mm、폭기량종0.018m3/h증가도0.063m3/h시,폭기실내표관수류속도수폭기량적증가이증가;당폭기량고정,폭기공직경종2.6mm감소지0.26mm시,표관수류속도수폭기공직경적감소이증가,이당폭기공직경진일보감소지 0.026mm 시,표관수류속도기본불수영향.계산료불동조건하적구동능량화각항손실능량,게시료인기표관수류속도변화적내인.건립적수동역학모형가용우지도등온층폭기기적설계화우화.
Superficial water velocity in a hypolimnetic oxygenator directly influences the oxygenation effectiveness of a hypolimnetic aerator. Aiming at the common problem of poor prediction of superficial water velocity, driving energy and energy losses of the gas-liquid two-phase flow in the aeration chamber were systematically analyzed, dimensionless formulas for calculating the energy losses due to wakes and top were particularly proposed, a one-dimensional hydrodynamic model for the water flow in the aeration chamber was developed, and a analytical solution to this hydrodynamic model was built using the real-domain method of MATLAB. The predicted superficial water velocities were validated against the operation data of hypolimnetic oxygenators installed in Lakes Prince, the United States, the prediction errors fell into the range of ±8%, which were much lower than the exiting prediction errors of ±20%. Under the orifice diameter of 2.6mm, the superficial water velocity increases with the air flowrate when the air flowrate increased from 0.018m3/h to 0.063m3/h; Under fixed air flowrate condition, the superficial water velocity increased when the orifice diameter decreased from 2.6mm to 0.26mm, but it remained unchanged when the orifice diameter further decreased to 0.026mm. Driving energy and energy losses under various conditions were calculated, the inherent factors causing the variations of superficial water velocity were revealed. This developed hydrodynamic model can be used to guide the design and optimization of a hypolimnetic oxygenator.