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23-Chem-B4 Biochemical Engineering · December 2014

Question 1 of 5: Oxygen-Transfer Capacity of a Stirred-Tank Aerator

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

National Exam 04-Chem-B4, Biochemical Engineering — Dec 2014. 3 hours, Closed-Book Exam (any non-communicating calculator permitted). Per the exam notes, FIVE (5) questions constitute a complete paper and all five must be answered; most require a short-essay-format answer.

Reference texts: Shuler & Kargi, Bioprocess Engineering: Basic Concepts, 2nd ed.; Bailey & Ollis, Biochemical Engineering Fundamentals, 2nd ed.; Madigan et al., Brock Biology of Microorganisms, 13th ed.

Question 1: Oxygen-Transfer Capacity of a Stirred-Tank Aerator (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given.

QuantitySymbolValue
Working liquid volumeVL10 m³
Impeller diameter (Rushton turbine)Di0.936 m
Impeller speedn1 rps (60 rpm)
Broth densityρ1000 kg/m³
Broth viscosityμ1×10-3 Pa·s
Power numberNp6
Gassed/ungassed power ratioPg/P0.6
Operating temperature, part (a)t15°C
Operating temperature, part (b)t215°C
O2 mole fraction in air / total pressureyO2, P0.21, 760 Torr

Find. (a) The maximum volumetric O2-transfer rate (g O2·m-3·h-1) deliverable to the broth at 5°C; (b) a qualitative judgement, supported by the same correlations, on whether O2 supply is more or less likely to be limiting at 15°C.

Approach. Compute the impeller's ungassed power from the power-number definition, apply the given gassed/ungassed ratio to get Pg, feed Pg/VL into the given kLa correlation, and combine with the saturation DO concentration (from the given solubility equation, using the maximum possible driving force C*−0) to get the maximum oxygen-transfer rate (OTRmax = kLa·C*). Repeat the saturation-concentration step at 15°C to quantify how the ceiling moves.

Mair spargerRushton turbinestirred-tank aeratorV_L = 10 m3, D_i = 0.936 m, n = 1 rpsFig. 1 — stirred-tank aerator: Rushton-turbine power drives gas-liquid mass transfer (k_La)
Fig. 1 — stirred-tank aerator: the Rushton turbine's gassed power sets kLa via the given correlation.
Check: the solubility equation is used exactly as printed, with P = total pressure (760 Torr) and p = O2 partial pressure = yO2·P (159.6 Torr), per the question's own labelling "P, p = total and partial pressure (oxygen)" and its explicit instruction to use the given mole fraction and total pressure to evaluate them.
  1. Confirm the turbulent regime (power number is valid as a constant). $$N_{Re}=\frac{nD_i^2\rho}{\mu}=\frac{(1)(0.936)^2(1000)}{1\times10^{-3}}=\boxed{8.76\times10^5}$$ Well above the ∼104 threshold for a fully turbulent impeller, so Np=6 is valid as a constant (no Reynolds-number correction needed).
  2. Ungassed impeller power from the power-number definition. $$P=N_p\,\rho\,n^3D_i^5=(6)(1000)(1)^3(0.936)^5=\boxed{4311\ \text{W}}=4.311\ \text{kW}$$
  3. Gassed power and specific power input. The given ratio Pg/P=0.6 converts ungassed to gassed (aerated) power directly: $$P_g=0.6\times4311=2586\ \text{W}=2.586\ \text{kW}\quad\Rightarrow\quad \frac{P_g}{V_L}=\frac{2.586}{10}=0.2586\ \text{kW/m}^3$$
  4. Volumetric mass-transfer coefficient from the given correlation. $$k_La=9.09\times10^{-4}(0.2586)^{0.7}=3.527\times10^{-4}\ \text{s}^{-1} =\boxed{1.270\ \text{h}^{-1}}$$
  5. (a) Saturation DO concentration at 5°C and maximum OTR. The O2 partial pressure is p=yO2·P=0.21×760=159.6 Torr, so $$DO^{*}=\frac{(760-159.6)(0.678)}{35+5}=\boxed{10.18\ \text{ppm}}\ (=10.18\ \text{g/m}^3)$$ Taking the maximum possible driving force (bulk liquid essentially depleted, CL→0) gives the ceiling on volumetric O2 flux: $$OTR_{max}=k_La\cdot DO^{*}=(1.270)(10.18)=\boxed{12.9\ \text{g O}_2\,\text{m}^{-3}\text{h}^{-1}}$$
  6. (b) Repeat the saturation step at 15°C. kLa is unchanged (the correlation depends only on Pg/VL, not on T), but the solubility equation's denominator (35+t) grows with t: $$DO^{*}_{15^\circ C}=\frac{(600.4)(0.678)}{35+15}=8.14\ \text{ppm}\quad\Rightarrow\quad OTR_{max,15^\circ C}=(1.270)(8.14)=\boxed{10.3\ \text{g O}_2\,\text{m}^{-3}\text{h}^{-1}}$$ The maximum deliverable rate falls by a factor DO*(15)/DO*(5) = 0.80 — about 20% lower — purely from the temperature-dependence of oxygen solubility, with the mass-transfer coefficient itself unaffected.
QuantityValue
Impeller Reynolds number8.76×105 (turbulent)
Ungassed power, P4.31 kW
Gassed power, Pg2.59 kW
kLa1.27 h-1 (3.53×10-4 s-1)
DO* at 5°C10.18 g/m³
(a) Max O2 flux at 5°C≈12.9 g O2·m-3·h-1
DO* at 15°C8.14 g/m³
Max O2 flux at 15°C≈10.3 g O2·m-3·h-1 (−20% vs. 5°C)

(b) Yes, oxygen supply is more likely to become limiting at 15°C than at 5°C. Two effects work in the same direction: the maximum deliverable O2 flux itself falls by ∼20% because the equilibrium solubility of oxygen in water decreases as temperature rises (the given correlation's denominator grows with t, and physically warmer water simply holds less dissolved gas), while the mixing power and hence kLa are essentially unchanged (no explicit T-dependence in the given correlation, and viscosity/density changes over this range are modest). At the same time, the microorganisms' demand for oxygen (the specific oxygen-uptake rate) typically rises with temperature following Arrhenius-type kinetics, up to the organisms' thermal optimum. A plant that was already close to its 5°C transfer ceiling of ∼12.9 g·m-3·h-1 would therefore be squeezed from both sides at 15°C — a lower supply ceiling and a higher demand — making oxygen limitation more, not less, likely.

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