CH E 316 · Separation Processes  ›  Chapter 9 All chapters
Chapter 9

Membranes

No second phase at all — just a wall that some molecules cross faster than others, and a pressure ratio that quietly caps everything you can do with it.

Wankat, Ch. 16 4 interactive apps 5 worked examples Self-marking problem set Prerequisite: Ch. 1
By the end of this chapter you should be able to
  • Place the pressure-driven membrane processes on a size scale, and say what each removes.
  • Distinguish symmetric, asymmetric and composite membranes, and say why the skin is thin.
  • Use the flux equation, and convert between barrer and GPU.
  • Explain the permeability–selectivity trade-off and what an upper bound means.
  • Solve a single well-mixed module for stage cut, permeate purity and recovery.
  • Explain why the pressure ratio, not the selectivity, is often the binding constraint.
  • Turn a stage cut into a membrane area, and invert the calculation to design for a spec.
  • Say how a cross-flow module differs from a well-mixed one, and which model is the safe one.
  • Set up a two-stage cascade with recycle and say when to polish the permeate and when to re-treat the retentate.

A wall that chooses

Every other chapter of this course creates a second phase and lets the components partition into it. A membrane does something different: it puts a barrier between two streams and lets some molecules through faster than others. There is no vapour to condense, no solvent to recover, no adsorbent to regenerate — and, usually, no phase change at all. That is the attraction, and it is also the reason membrane processes are the fastest-growing separations in industry.

membranethickness δFEED SIDEPERMEATE SIDEfeedretentateABpermeate, rich in Ahigh pressure Prlow pressure Pp
Figure 9.1 — A membrane separating a feed from a permeate. Component A crosses easily and B does not, so the permeate is enriched in A and the retentate left behind is enriched in B. The driving force may be a difference in pressure, concentration, chemical potential or electrical potential — this chapter takes the pressure-driven case.
What a good membrane needs
  • High permeability and a thin skin → more flux per square metre → less area to buy.
  • High selectivity → a purer permeate. As §9.4 shows, this fights the first requirement.
  • Defect-free. A pinhole is a short circuit with a selectivity of one, and a very small area of pinhole ruins a very large area of membrane.
  • Mechanical strength, chemical stability and resistance to fouling → a life measured in years rather than months.

9.1 The family of processes

The pressure-driven processes form a continuous family, distinguished by what size of thing they stop.

1 nm10 nm100 nm1 µm10 µm100 µmcharacteristic sizeReverse osmosisions, saltsNanofiltrationdivalent ions, sugarsUltrafiltrationproteins, virusesMicrofiltrationbacteria, fine particlesConventional filtrationsand, gritpressure-driven membrane processessmaller pores → higher pressure, lower flux, finer separationincreasing pore size
Figure 9.2 — The size spectrum. Moving left costs pressure and costs flux: reverse osmosis runs at 15–80 bar and passes litres per square metre per hour, while microfiltration runs at a fraction of a bar and passes hundreds. The mechanism changes across the spectrum too — the right-hand end is genuine sieving by size, and the left-hand end is solution–diffusion, in which the permeant dissolves into the membrane material and diffuses through it.

Gas separation, pervaporation and dialysis sit alongside these. Reverse osmosis alone supplies drinking water to well over a hundred million people, and gas-separation membranes now take CO₂ out of natural gas, nitrogen out of air and hydrogen out of refinery purge gas at very large scale.

9.2 Membrane structure

Symmetricthe whole thickness separatesuniform, 10–200 µmAsymmetrica thin skin on an open supportskin 0.1–1 µmporous supportCompositeskin and support chosen separatelyselective layergutter layerporous supportthe thinner the selective layer, the higher the flux — provided it stays defect-free
Figure 9.3 — Three structures. A symmetric membrane does the separating with its whole thickness, so it is slow. An asymmetric membrane concentrates the resistance into a skin a fraction of a micrometre thick on top of an open support that contributes almost nothing to the resistance — the invention that made reverse osmosis practical. A composite membrane goes further and makes the skin and the support out of different materials, so each can be optimised separately.

The point of all three is the same. Flux goes as , so the whole art is to make the selective layer as thin as it can be made without defects — and then to support it well enough that it survives 60 bar and a decade of service.

9.3 Flux, permeability and permeance

At steady state, the flux of a component through the membrane is proportional to its partial-pressure difference across it:

9.1

with and the total pressures on the retentate and permeate sides. The group — a diffusivity times a solubility — is the permeability, a property of the material alone. Divided by the thickness it becomes the permeance, a property of the finished membrane.

QuantitySymbolUnitDepends on
Permeability1 barrer = 10⁻¹⁰ cm³(STP)·cm / (cm²·s·cmHg)the material only
Permeance1 GPU = 10⁻⁶ cm³(STP) / (cm²·s·cmHg)material and thickness
Why two units, and which one to quote

A polymer chemist reports barrer, because it is the material property that can be compared between laboratories. A process engineer buys GPU, because that is what sets the area. The conversion is one division: a 100-barrer polymer cast as a 0.1 µm skin gives 100×10⁻¹⁰ / (0.1×10⁻⁴ cm) = 1000 GPU. If someone quotes a permeability without a thickness, they have not told you how big your plant will be.

FRPretentate sidepermeate sideflux = −(DH/δ)[ Ppyp− Pryr]the driving force is a difference of PARTIAL pressures
Figure 9.4 — The module and its driving force. Note carefully what appears in Equation 9.1: the difference of partial pressures, not of total pressures. A component can refuse to cross a membrane even with 50 bar behind it, if its partial pressure on the far side is already high enough.
App 1

Flux and the driving force

Set a permeability, a skin thickness and the two pressures, and the app gives you the permeance, the driving force and the flux in units you can buy area with. Watch what happens to the driving force as the permeate composition rises — and notice the pressure at which it reaches zero even though the total pressure difference is still enormous.
The driving force
Partial pressure on each side, against permeate composition.
Area you would have to buy
For 1000 m³(STP)/h of permeating component.
Permeance
GPU
Driving force
cmHg
Flux
m³/m²h
Pressure ratio
Permeate at which J = 0
Area for 1000 m³/h

9.4 Selectivity and the trade-off

The ideal selectivity is the ratio of the two permeabilities,

9.2

and it is the direct analogue of relative volatility2a §2.7. Splitting it into the two factors is worth doing, because they can be engineered separately: a glassy polymer with tight, rigid chains gives a large diffusivity ratio and separates by size, while a rubbery polymer gives a large solubility ratio and can separate a larger, more condensable molecule preferentially — which is how a membrane can be made to permeate propylene ahead of hydrogen.

The permeability–selectivity trade-off

Across essentially every polymer ever measured, the more permeable a material is, the less selective it is. Tightening the structure to discriminate between molecules also slows both of them down. Plotting selectivity against permeability for a given gas pair produces a cloud of points with a clear diagonal frontier that almost nothing crosses — the upper bound, first drawn by Robeson in 1991 and redrawn in 2008. A new material is interesting only if it sits above the line.

The Robeson upper bound

The upper-bound plot is the standard yardstick for a new membrane material. It is reproduced in the lecture slides and is worth looking at in the original, where the data cloud and the fitted bound are shown together for each gas pair.

L. M. Robeson, "The upper bound revisited", Journal of Membrane Science 320, 390–400 (2008). doi:10.1016/j.memsci.2008.04.030 · See also L. M. Robeson, J. Membr. Sci. 62, 165 (1991).

9.5 Designing one module

Take a module well enough mixed that the retentate leaves at the same composition as the gas everywhere inside it. Two things then fix the answer: a mass balance and the ratio of the two fluxes.

Define the stage cut — the fraction of the feed that permeates — and write the balance on the fast component:

9.3

The permeate composition is whatever ratio the two fluxes happen to be in:

9.4

Equations 9.3 and 9.4 are two equations in the two unknowns and . Equation 9.4 is a quadratic in , so the pair can be solved directly — and the two of them together are the whole design.

00252550507575100100stage cut θ (permeate / feed), %permeate purity / recovery, %purityrecoveryyou cannot have both
Figure 9.5 — The trade-off you cannot avoid. Take a small cut and the permeate is pure but you recover almost nothing; take a large cut and you recover nearly everything, at a purity approaching the feed. A single membrane stage cannot give both, which is why real plants use two or three stages with recycle, exactly as a distillation column uses many trays.
App 2

The module designer

One well-mixed stage. Sweep the stage cut and watch purity and recovery trade against each other; raise the selectivity and watch the whole curve lift; then drop the pressure ratio and watch the ceiling come down on top of you regardless of how good the material is. The dashed line is what the pressure ratio alone allows.
Purity and recovery against the cut
The dashed line is the pressure-ratio ceiling.
What selectivity actually buys
Permeate purity at this cut, against α.
Permeate yp
Retentate xr
Recovery
%
Loss of slow component
%
Pressure ratio 1/r
Ceiling on yp

9.6 The pressure-ratio limit

Look again at Equation 9.1. The flux of the fast component cannot be positive unless

9.5

and nothing in that statement mentions the membrane. It is a thermodynamic ceiling set entirely by the pressures. A perfect membrane with infinite selectivity, fed a gas containing 10 % of the fast component through a pressure ratio of 5, cannot make a permeate richer than 50 %.

Which constraint is binding?

The usual rule of thumb compares with the pressure ratio : and the membrane is limiting; and the pressures are limiting, so a better material does nothing and you need compression or a vacuum pump instead. Whole research programmes have been spent raising a selectivity that was never the constraint.

But treat that rule as an asymptote, not a test. It comes from the dilute limit: for small , the membrane alone would give while the pressures allow , and comparing the two is comparing with . Once the feed is not dilute the comparison can point the wrong way. The H₂ preset in App 2 — , , 60/5 bar — has , yet the actual ceiling is , which is above 1 and so cannot bind at all; raising from 80 to 200 still lifts the permeate from 0.952 to 0.979, cutting the impurity by more than half.

The reliable test costs one extra solve of the module: relax each constraint in turn and see which one moves the answer. App 2 reports both — the permeate this membrane would make with an unlimited pressure ratio, and the permeate a perfect membrane would make at this pressure ratio — and names the larger gap.

9.7 From a stage cut to an area

Everything in §9.5 was dimensionless. You now know the permeate composition, the retentate composition and the recovery — and not one number that a vendor could quote you a price against. Nothing so far says how big the thing is.

The step that fixes that is short. Every mole in the permeate got there by crossing the membrane, so the permeate flow and the flux must agree:

9.6

with both fluxes evaluated from Equation 9.1 at the compositions the module actually has on the retentate side and on the permeate side. That last clause is the whole difficulty, and it is why the composition problem has to be solved first.

you CHOOSEstage cut θand the feed rate Fbalance + flux ratioxr and ypEqs 9.3 and 9.4the composition problemthe flux lawJA and JBEq 9.1, at those compositionsthe transport problemyou GETA = θF / (JA+JB)the piece of hardwarethe sizing problemthe design ladder — every membrane sizing calculation runs left to rightYou cannot jump straight to the area. The flux depends on the compositions, and the compositionsdepend on the stage cut — so the composition problem is always solved first.
Figure 9.6 — The design ladder. You choose the stage cut; the balance and the flux ratio give the two compositions; the flux law then gives two fluxes; and only then does the area appear. Every membrane sizing calculation in this course, and in industry, runs left to right along this ladder.
Equation 9.4 was never an extra assumption

Divide Equation 9.6's numerator between the two components and you get and . Take the ratio and the area cancels:

yp/(1 − yp) = JA/JB

which is Equation 9.4. The flux-ratio equation is not a modelling choice — it is the statement that the permeate is made of whatever came through, in the proportion it came through. A useful check on any answer: compute at the end and confirm you get back.

Getting the units right

Permeance is quoted in GPU and pressures in cmHg, so it pays to collapse the conversion once and for all. One GPU is cm³(STP)/(cm²·s·cmHg); multiply by 3600 s/h and by 10⁻² to turn cm³/cm² into m³/m², and

9.7

and with the feed rate also in m³(STP)/h, Equation 9.6 returns square metres directly. Because everything is at standard temperature and pressure, volumes here are just moles in disguise, so the balances of §9.5 carry over unchanged.

The area does not scale with the cut

Here is the base case for the rest of the chapter: 10 000 m³(STP)/h of natural gas containing 10 mol % CO₂ at 50 bar, permeate at 2 bar, on a membrane with a CO₂ permeance of 1000 GPU and a selectivity of 20 (so the methane permeance is 50 GPU). Run the ladder at a series of stage cuts:

θxryp ΔpCO₂
cmHg
JCO₂
m³/m²h
JCH₄
m³/m²h
A
A/θ CO₂ rec.CH₄ lost
0.050.07650.5468204.87.3746.11237.174227.3 %2.5 %
0.100.05910.4678151.65.4576.20885.785746.8 %5.9 %
0.200.03860.345892.73.3376.314207.2103669.2 %14.5 %
0.300.02800.268064.72.3306.364345.0115080.4 %24.4 %
0.400.02180.217349.31.7746.392489.8122586.9 %34.8 %
0.500.01790.182139.61.4276.409638.0127691.1 %45.4 %

Read the last four columns together. Going from θ = 0.10 to θ = 0.20 doubles the permeate flow but multiplies the area by 2.4, and the column headed A/θ shows why: the specific area climbs steadily because the retentate keeps getting leaner and the CO₂ driving force collapses with it — 152 cmHg down to 93. The last mole of CO₂ costs far more membrane than the first. That is the same diminishing return you met as an absorber approached its pinch and as a column approached minimum reflux; here it appears as area rather than as stages.

Notice also that barely moves — 6.11 up to 6.41 — because the methane driving force is dominated by the 3750 cmHg of feed-side partial pressure and hardly notices what the permeate is doing. Almost all of the flux variation in a gas-separation membrane is in the fast component.

Designing to a spec, not to a stage cut

No customer ever asks for a stage cut. They ask for a pipeline gas below 2 % CO₂, or a permeate above 40 % CO₂, or 80 % of the CO₂ captured. Each of those is a single equation in the single unknown θ, because every quantity in the table is a monotonic function of the cut:

The specBehaviour with θθ requiredA, m²What else you get
permeate at 40 % CO₂yp falls0.150144recovery only 60.1 %
capture 80 % of the CO₂recovery rises0.295338permeate down to 27.1 %
residue at 2 % CO₂xr falls0.44155139 % of the methane lost

Three specs, three completely different plants — and the third one is a disaster. Meeting a pipeline specification with a single well-mixed stage throws away two-fifths of the product gas, because the only way to strip the retentate that far is to permeate almost half the feed, and at α = 20 nearly four-fifths of what permeates is methane. That single line is the reason §9.9 exists.

Which end are you specifying?

A permeate spec is cheap: take a small cut and you get a clean permeate almost for free. A retentate spec is expensive, because it is the last traces that are hardest to remove and the driving force is smallest exactly where you need it most. Before you size anything, find out which end of the process the customer actually cares about — it changes the answer by an order of magnitude, not a few percent.

9.8 Cross-flow: the module is not a stirred tank

The well-mixed model made a strong claim: every square metre of membrane sees retentate at , the exit composition. In the base case at θ = 0.20 that means the whole module works against 3.86 % CO₂ when the gas entering it is at 10 %. That is plainly pessimistic — the first stretch of membrane sees the feed at full strength.

A real spiral-wound or hollow-fibre module is much closer to cross-flow: the retentate travels along the module in something like plug flow, its composition falling as it goes, while the permeate is swept off the far face and never mixes back. Each element of area then works against the local composition.

WELL MIXEDthe conservative model — and the easy oneone composition everywhere: xrFRP0.00.20.40.6position through the module →mole fractionpermeate y = 0.3458retentate x = 0.0386feedboth flat — one contact, one answerCROSS-FLOWwhat a real module actually doesx falls as the gas travels alongFRP0.00.20.40.6position through the module →mole fractionlocal permeate y *the permeate you collectis their average: 0.4219local retentate x0.0195Same feed, same membrane, same stage cut θ = 0.20. Cross-flow makes the richer permeate — 0.4219 against 0.3458 —because the first stretch of membrane sees gas at full feed strength instead of at the exit composition.
Figure 9.7 — The two mixing models, at the same feed, membrane and stage cut. Well mixed (left): one composition throughout, so the permeate is a single number. Cross-flow (right): the retentate falls from 0.10 to 0.0195 along the module and the local permeate falls with it, from 0.6285 at the inlet to 0.1971 at the outlet. What you collect is their flow-weighted average, 0.4219 — a decidedly better permeate than the well-mixed 0.3458, from exactly the same hardware.

The bookkeeping is a differential version of Equation 9.3. Let be the retentate flow remaining and its composition. In a slice that permeates , the material removed has the local permeate composition , so , and

9.8

where , and are all evaluated at the local using the same Equations 9.1 and 9.4 as before. Integrate from until . The permeate you actually collect is the mixed average of everything produced along the way, which the overall balance hands you for free:

9.9

Two integrations and you are done. The comparison, on the base case:

θ permeate yp retentate xr area, m² CO₂ recovery
mixedcross-flow mixedcross-flow mixedcross-flow mixedcross-flow
0.050.54680.58540.07650.074537.134.227.3 %29.3 %
0.100.46780.53490.05910.051785.775.946.8 %53.5 %
0.200.34580.42190.03860.0195207.2184.969.2 %84.4 %
0.300.26800.32080.02800.0054345.0321.980.4 %96.2 %
0.400.21730.24830.02180.0011489.8471.686.9 %99.3 %

Cross-flow wins on every column, and the gap grows with the cut. At θ = 0.30 the well-mixed model predicts a residue of 2.80 % CO₂ where cross-flow gives 0.54 % — a factor of five, and comfortably the difference between meeting a pipeline spec and not meeting it.

Which model should you design with?

Both, in the right order. Well mixed is conservative on both counts at once: it under-predicts the separation and over-predicts the area, so a plant sized on it will not disappoint. It is also a two-equation hand calculation, which makes it the right model for a first pass, an exam and a sanity check. Cross-flow is closer to what a module does, and it is what you use once the flowsheet is settled and the number matters. Real modules are somewhere between the two, and countercurrent designs — where the permeate is swept back along the module against the feed — do better than either. The ranking is exactly the one you found for extraction cascades in Chapter 77 §7.2: co-current worst, cross-flow better, countercurrent best. It is the same argument about where the driving force is spent, made in a different piece of hardware.

App 3

The design calculator

The full ladder, both mixing models, in both directions. Give it a stage cut and it sizes the module; give it a spec and it finds the cut that meets it — or tells you the spec is out of reach and names the best a single stage can do. Watch the area curve bend upwards as you push the retentate leaner — and watch the gap between the two mixing models open up as the cut rises.
Membrane area against the stage cut
Both models, so you can see the penalty for assuming the module is stirred.
Composition along the module
The local retentate, the local permeate and their running average.
Stage cut θ
Area
Permeate yp
Residue xr
Recovery
%
Slow gas lost
%
Permeate flow
m³/h
Total flux
m³/m²h

9.9 Two stages and a recycle

Figure 9.5 and the spec table in §9.7 both end at the same wall: one membrane stage is one contact, and one contact cannot give a high purity and a high recovery. A distillation column escapes that wall by doing the separation many times over and sending product back — and a membrane plant escapes it in exactly the same way, by putting a second module in and recycling one of its streams.

(a) PERMEATE cascade — polish the permeate for PURITYproduct 82.0 % CO₂ at 57 % recovery; 225 + 24 = 248 m² of membranefeed 10 % CO₂stage 1residue4.6 % CO₂permeate 39.4 %recompress2 → 50 barstage 2PRODUCT 82.0 % CO₂recycle21.1 % CO₂16 % of the feed(b) RETENTATE cascade — re-treat the residue for RECOVERYresidue on spec at 2.0 % CO₂ losing 15 % of the methane, not 39 %; 221 + 144 = 365 m²feed 10 % CO₂stage 1PRODUCT 37.9 % CO₂retentate 4.4 %stage 2RESIDUE2.0 % CO₂recycle its permeate, 20.1 % CO₂12 % of the feedThe recycle is the reflux. It costs a compressor — and it is the only waya membrane plant escapes the single-stage trade-off.
Figure 9.8 — The two useful two-stage arrangements, both on the base case. (a) A permeate cascade recompresses the stage-1 permeate and polishes it in stage 2; the stage-2 retentate, still well above feed strength, goes back to the front. Use it when you want a pure permeate. (b) A retentate cascade re-treats the stage-1 retentate to drive it down to spec, and recycles stage 2's CO₂-rich permeate. Use it when you want a clean residue without throwing away the product gas.

Why it needs iteration

The recycle is what makes this more than two module calculations in a row. Stage 1 no longer sees the fresh feed; it sees the fresh feed plus the recycle, at a composition you cannot know until you have solved stage 2 — which needs stage 1's answer. The standard remedy is the one every recycle problem in the course uses: guess, go round, repeat.

  1. Guess the recycle flow and its composition — zero and will do.
  2. Mix: and .
  3. Solve stage 1 at its cut, then stage 2 on whichever stream it treats.
  4. Read the new recycle off stage 2 and go back to step 2. Stop when it stops moving.

On the base case this converges in about twenty passes and is entirely undramatic — the recycle is a modest fraction of the feed, so the loop is well damped. When you check your answer, do it on the overall balance, , which knows nothing about the recycle and is therefore an independent test.

(a) The permeate cascade — buying purity

Take the base case at θ₁ = 0.20 and θ₂ = 0.30. The recycle settles at 1628 m³/h of 21.1 % CO₂, which lifts the stage-1 feed from 10.0 % to 11.56 % and its permeate to 39.4 %. Stage 2 works on that 39.4 % gas and produces:

flow, m³/hCO₂area, m²
feed to stage 1 (fresh + recycle)11 6280.1156
stage-1 permeate → compressor23260.3939225
stage-2 retentate → recycle16280.2112
product (stage-2 permeate)6980.820324
residue (stage-1 retentate)93020.0460

An 82 % CO₂ product at 57 % recovery, from 248 m² of membrane. The point is not that 82 % is high — it is that a single stage cannot reach it at all. Push the cut of a single stage to zero and the permeate tends to its ceiling of ; every value above that is off the map for one contact, no matter how much area you buy. The second stage does not merely improve the answer, it enlarges the set of achievable answers — which is precisely what reflux does for a column.

The bill is the compressor. Recompressing 2326 m³(STP)/h from 2 to 50 bar takes about 480 kW of ideal duty, and that single number usually decides whether a two-stage membrane plant is built or an amine unit is built instead.

(b) The retentate cascade — buying recovery

Now the other spec: the pipeline wants the gas below 2 % CO₂. §9.7 did it in one stage, at θ = 0.441 and 551 m² — and lost 39 % of the methane. Put stage 1 at θ₁ = 0.20 and let stage 2 finish the job at θ₂ = 0.130, recycling stage 2's permeate:

Route to 2 % CO₂ in the residuearea, m²export gasCH₄ lostcompressor
one well-mixed stage, θ = 0.4415514412 m³/h at 20.1 %39.2 %none
retentate cascade, θ₁ = 0.20, θ₂ = 0.130221 + 144 = 3652231 m³/h at 37.9 %15.4 %238 kW

The cascade meets the same specification with a third less membrane (365 against 551 m²) and loses about two-fifths as much methane — 15.4 % against 39.2 %, a ratio of 0.39 — for one compressor of 238 kW. The methane saved is the difference, 3524 − 1387 = 2137 m³(STP)/h; the 1387 m³/h is what the cascade still throws away. At any plausible gas price those 2137 m³/h pay for the compressor many times over — which is why essentially every CO₂-removal membrane plant in the world has a recycle in it, and why a single-stage answer to a retentate spec should always make you suspicious.

Reading the two arrangements

They are the two halves of a distillation column wearing different clothes. The permeate cascade concentrates what came through — an enriching section. The retentate cascade strips what stayed behind — a stripping section. In both cases the recycled stream is the one that is neither product nor waste but sits at an intermediate composition, and returning it to a point of matching composition is the same principle that puts the feed tray of a column where it belongs, back in Chapter 44a §4.7. Membrane plants stop at two or three stages only because every stage needs its own compressor, and compressors do not get cheaper the way trays do.

App 4

The two-stage cascade

Both arrangements, with the recycle solved properly. The bars show where every mole of feed ends up. Start with the single stage that meets your spec, then switch the cascade on and watch the loss column shrink — and watch the recycle, and the compressor with it, grow as you push the second stage harder.
Product purity against recovery
The single stage traces a curve; the cascades sit above it, where one contact cannot go.
Where the feed ends up
Per 100 units of feed, split by component.
Product purity
Recovery
%
Residue
Slow gas lost
%
Recycle
% of feed
Feed to stage 1
Total area
Compressor
kW

9.10 Modules and contactors

Area is everything, so membranes are sold as modules that pack a great deal of it into a small volume. Spiral-wound modules roll flat sheets and spacers around a central permeate tube and reach roughly 1000 m² per cubic metre; hollow-fibre modules bundle tens of thousands of fibres a fraction of a millimetre across into a shell-and-tube arrangement and reach ten times that, at the price of being much harder to clean.

A membrane contactor is a different idea altogether. Here the membrane does no separating — it is a microporous wall whose only job is to hold a gas and a liquid in contact at a fixed, known interfacial area without them mixing. The separation is still absorption, exactly as in Chapter 66 §6.1; the membrane just replaces the packing and removes any possibility of flooding, entrainment or foaming. It is one of the more elegant hybrids in the subject.

9.11 Worked examples

Worked example 9.1From a polymer to an area

A polymer has a CO₂ permeability of 100 barrer and is cast as a composite membrane with a 0.10 µm selective layer. It is to treat natural gas containing 10 mol % CO₂ at 50 bar, with the permeate held at 2 bar and leaving at 50 mol % CO₂. Find the permeance, the driving force, the CO₂ flux, and the area needed to remove 1000 m³(STP)/h of CO₂.

Work it yourself first, then open

Permeance. Divide the permeability by the thickness:

DH/δ = 100×10⁻¹⁰ / (0.10×10⁻⁴ cm) = 1.00×10⁻³ cm³(STP)/(cm²·s·cmHg) = 1000 GPU

Driving force. 1 bar = 75.006 cmHg, and it is the partial pressures that matter:

Prxr = 50(75.006)(0.10) = 375.0 cmHg

Ppyp = 2(75.006)(0.50) = 75.0 cmHg

Δ = 300.0 cmHg

Flux.

J = 1.00×10⁻³ (300.0) = 0.300 cm³(STP)/(cm²·s) = 10.80 m³(STP)/(m²·h)

Area.

A = 1000/10.80 = 92.6 m²

which is a couple of spiral-wound modules — a genuinely small piece of equipment for the duty.

Now look at what dominates. The retentate side contributes 375 cmHg of the driving force and the permeate side subtracts only 75. Drop the feed pressure to 20 bar and the driving force falls to 150 − 75 = 75 cmHg: the area quadruples to 370 m². Membrane plants are compression plants with a membrane attached, and the compressor is usually the larger capital item.

And a warning about the thickness. Halving the skin to 0.05 µm doubles the permeance to 2000 GPU and so halves the area, to 46.3 m² — but a 50 nm film now has to be defect-free over all 46 m² of it, and a single pinhole short-circuits the selectivity of the whole module. That is the entire reason composite membranes exist.

App 1, with 100 barrer, 0.10 µm, 50 bar and 2 bar.

Worked example 9.2How much can one stage do?

The same gas — 10 mol % CO₂ in methane at 50 bar, permeate at 2 bar — is fed to a well-mixed module with . Find the permeate composition, the retentate composition and the CO₂ recovery at stage cuts of 0.05 and 0.20, and say what limits the design.

Work it yourself first, then open

Set up. , so the pressure ratio is 25. Since and , the two constraints are of comparable size — neither dominates, which is the awkward case.

Solve Equations 9.3 and 9.4 together (9.4 is a quadratic in ; iterate on until the balance closes):

θxrypCO₂ recoveryCH₄ lost
0.050.07650.54727.3 %2.5 %
0.200.03860.34669.2 %14.5 %
0.400.02180.21786.9 %34.8 %

Read the table as a designer. At θ = 0.05 you get a decent permeate but leave three-quarters of the CO₂ in the product gas. At θ = 0.40 you capture 87 % of the CO₂ — and throw away 35 % of your methane with it. That methane is the product; losing a third of it is not a rounding error, it is the economics of the plant.

What is limiting? At θ = 0.20 the retentate is 3.86 % CO₂, so the pressure-ratio ceiling is

yp < xr/r = 0.0386/0.040 = 0.965

which is far above the 0.346 achieved, so here the membrane is limiting and a more selective material would help.

Now drop the feed pressure to 8 bar, keeping the permeate at 2 bar, so . You cannot simply reuse the 50-bar retentate here — the whole module re-solves. At Equations 9.3 and 9.4 now give

xr = 0.0680,   yp = 0.228,   ceiling = xr/r = 0.0680/0.25 = 0.272

The permeate has collapsed from 0.346 to 0.228, and it now sits at 84 % of its ceiling rather than 36 % of it. That is what "the pressure ratio is limiting" actually looks like: the achieved composition is pressed up against the bound, not far below it. Put an infinitely selective membrane in at the same cut and you get 0.250 — a gain of two points, for a material that does not exist.

If you want a bound that does not depend on at all, take the limit of a vanishing cut, where the retentate is still the feed: whatever the membrane, and with this one. Always compute the ceiling before you go shopping for a better material — and compute it from the retentate that this module actually produces.

The industrial answer is two stages: take a small cut for a clean permeate, compress it, and pass it through a second module — or take a large cut and recycle the poor-quality permeate to the feed compressor. Every real CO₂-removal plant does one of the two, for exactly the reason the table shows.

App 2, CO₂/CH₄ preset, α = 20, 50 bar and 2 bar. Drag the stage cut across the whole range.

Worked example 9.3Sizing the module

A plant treats 10 000 m³(STP)/h of natural gas containing 10 mol % CO₂ at 50 bar, with the permeate at 2 bar. The membrane has a CO₂ permeance of 1000 GPU and a CO₂/CH₄ selectivity of 20. The module is taken as well mixed and run at a stage cut of 0.20. Find the membrane area, and check the answer two ways.

Work it yourself first, then open

Step 1 — the compositions. This is Worked example 9.2 again: , and solving Equations 9.3 and 9.4 together gives

xr = 0.0386     yp = 0.3458

Step 2 — the driving forces. Convert the pressures once: 50 bar = 3750.3 cmHg and 2 bar = 150.0 cmHg.

ΔpCO₂ = 3750.3(0.0386) − 150.0(0.3458) = 144.7 − 51.9 = 92.7 cmHg

ΔpCH₄ = 3750.3(0.9614) − 150.0(0.6542) = 3605.7 − 98.1 = 3507.6 cmHg

The methane driving force is thirty-eight times the CO₂ driving force. Only the selectivity of 20 keeps the permeate CO₂-rich at all, and you can see the two effects fighting each other in these two numbers.

Step 3 — the fluxes. The methane permeance is 1000/20 = 50 GPU, and Equation 9.7 does the units:

JCO₂ = 3.6×10⁻⁵ (1000)(92.7) = 3.337 m³(STP)/(m²·h)

JCH₄ = 3.6×10⁻⁵ (50)(3507.6) = 6.314 m³(STP)/(m²·h)

Step 4 — the area. The permeate is θF = 0.20(10 000) = 2000 m³(STP)/h, and

A = 2000 / (3.337 + 6.314) = 2000/9.651 = 207 m²

First check — the flux ratio. The permeate should be made of the two fluxes in the proportion they arrive:

JCO₂/(JCO₂+JCH₄) = 3.337/9.651 = 0.3458

which is back again. If this had not closed, the composition solution was wrong.

Second check — one component at a time. Size on CO₂ alone: the permeate carries 2000(0.3458) = 691.6 m³/h of CO₂, so A = 691.6/3.337 = 207 m². Size on methane alone: 2000(0.6542) = 1308.4 m³/h at 6.314 gives A = 207 m². Three routes, one answer.

Is 207 m² a lot? No — a spiral-wound module packs roughly 1000 m² per cubic metre, so this is about a fifth of a cubic metre of membrane, sitting in a pressure vessel you could carry. The compressor upstream is the plant; the membrane is almost an afterthought until you start asking it for a tighter spec.

App 3, well mixed, from a cut, θ = 0.20, with the default base case loaded.

Worked example 9.4Does the mixing model matter?

The same duty, the same hardware, the same stage cut of 0.20 — but now treat the module as cross-flow instead of well mixed. How different is the answer, and which model should the plant be sized on?

Work it yourself first, then open

Set up the integration. March down from 10 000 m³/h, carrying with it through Equation 9.8, and stop at m³/h. At every step the local permeate comes from Equation 9.4 evaluated at the local , not at the exit composition.

The starting point is the giveaway. At the inlet the gas is still at 10 % CO₂, so

y*(0.10) = 0.6285

The first square metre of membrane is making permeate at 63 % CO₂ — nearly twice what the well-mixed model claims the whole module produces. That single number is the entire reason the two models disagree.

Integrating to θ = 0.20:

well mixedcross-flowdifference
permeate yp0.34580.4219+22 %
residue xr0.03860.0195half
CO₂ recovery69.2 %84.4 %+15 points
area207 m²185 m²−11 %

Which way does the error go? Every single line favours cross-flow. The well-mixed model under-predicts the separation and over-predicts the area, so it errs on the safe side twice over. That is an unusually comfortable position for a simplifying assumption and it is why the well-mixed module is the standard hand calculation.

When does it stop being a detail? When the retentate is the spec. Here the two models put the residue at 3.86 % and 1.95 % CO₂ — if the pipeline limit were 2 %, one model says you have failed and the other says you have passed. Push to θ = 0.30 and the gap widens to 2.80 % against 0.54 %, a factor of five. A permeate spec is fairly forgiving of the mixing model; a retentate spec is not.

And the honest caveat. Neither model includes pressure drop along the permeate channel, concentration polarisation at the membrane face, or plasticisation of the polymer by CO₂ at 50 bar. Real modules are rated from measured performance, and cross-flow is the model those ratings are usually fitted with.

App 3: run θ = 0.20 on well mixed, note the readouts, then switch the model to cross-flow. The right-hand panel shows the profile you just integrated.

Worked example 9.5Meeting a pipeline spec without giving away the gas

The same 10 000 m³(STP)/h of 10 % CO₂ gas must be brought to 2 mol % CO₂ to enter the pipeline. Size the single well-mixed stage that does it, then design a two-stage retentate cascade for the same spec, and compare. Take the second stage at whatever cut is needed with θ₁ held at 0.20.

Work it yourself first, then open

One stage. The residue composition falls monotonically with the cut, so bisect on θ until :

θ = 0.441    yp = 0.2013    A = 551 m²

The permeate is 4412 m³/h, and only a fifth of it is CO₂. The other 3524 m³/h is methane — 39 % of the product gas, gone. Whatever that permeate is burnt as, it is not being sold as pipeline gas, and no amount of membrane area fixes it: the loss is set by the selectivity and the cut, and the cut is set by the spec.

Why one stage cannot do better. To take the retentate from 10 % to 2 % you must remove four-fifths of the CO₂, which is 800 m³/h. At a permeate composition of 0.20 that parcel of CO₂ drags 3200 m³/h of methane out with it. The only lever is a richer permeate — and a single stage's permeate is poorest exactly when the cut is largest. The requirement and the mechanism fight each other.

Two stages, retentate cascade. Send stage 1's retentate to stage 2, and recycle stage 2's CO₂-rich permeate back to the front. Iterating on the recycle with θ₁ = 0.20 and bisecting θ₂ to land the residue on 2.00 %:

θ₂ = 0.1297

flow, m³/hCO₂area, m²
fresh feed10 0000.1000
recycle (stage-2 permeate)11570.2013
feed to stage 111 1570.1105
export (stage-1 permeate)22310.3785221
stage-1 retentate → stage 289260.0435144
residue (stage-2 retentate)77690.0200

Check on the overall balance, which knows nothing about the recycle:

10 000 = 2231 + 7769 ✓

10 000(0.100) = 2231(0.3785) + 7769(0.0200) = 844.6 + 155.4 = 1000 ✓

The comparison.

areaexportCH₄ lostcompressor
one stage, θ = 0.441551 m²4412 m³/h at 20.1 %3524 m³/h (39.2 %)none
retentate cascade365 m²2231 m³/h at 37.9 %1387 m³/h (15.4 %)238 kW

Where the improvement comes from. Not from the extra area — there is less of it. It comes from the recycle lifting the stage-1 feed from 10.0 % to 11.05 % CO₂, which raises stage 1's permeate from 20.1 % to 37.9 %. Every mole of CO₂ removed now drags out less than half as much methane. The recycle is not there to add capacity; it is there to enrich the feed. That is exactly what reflux does in a column, and it is why the second stage pays for itself.

The engineering decision. 2137 m³(STP)/h of methane saved is roughly 1.5 t/h of saleable gas, against a 238 kW compressor. The comparison is not close. It also is not free: the compressor is rotating equipment with a maintenance schedule and a failure mode, while the single stage has no moving parts at all. On a remote unmanned wellhead that argument sometimes wins, which is why both flowsheets exist in the field.

App 4: retentate cascade, θ₁ = 0.20, θ₂ = 0.130. Then switch to "One stage" and drag θ to 0.44 to see the loss column jump.

9.12 Check your understanding

Five multiple-choice questions, two short problems and two long ones — 41 marks. Work them offline, then enter your numbers.

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Multiple choice

Short problems

Long problems

Think about it

Why is there no equivalent of a reflux ratio for a membrane?

There is — it is just not called that, and §9.9 is where it appears. A distillation column gets its purity by sending product back down the column and re-separating it many times; a single equilibrium stage could never do what a column does. A membrane stage is one contact, so to get a high purity and a high recovery you have to do the same thing: send the permeate through a second membrane, and recycle the second retentate back to the first feed. That recycle is the reflux, and Worked example 9.5 shows it doing reflux's job exactly — enriching the feed to the first stage so that every mole of CO₂ removed drags out less methane. Like reflux it costs energy, only here the energy is compression rather than reboil. The reason membrane plants rarely go past three stages is that each one needs its own compressor, and compressors do not get cheaper the way trays do.

If the well-mixed model is wrong, why is it the one you are taught?

Because it is wrong in a useful direction and it is solvable by hand. It under-predicts the purity, under-predicts the recovery and over-predicts the area, so a design based on it is conservative on every axis at once — a rare and valuable property in an approximation. It also reduces to two algebraic equations, which means you can carry it into a design review and get an answer in five minutes. Cross-flow needs a numerical integration and gives a number you would not want to defend without knowing the module's internals anyway. The professional habit is to bound the problem with the well-mixed model first, then ask whether the extra fidelity changes any decision. Often it does not — but when the specification is on the retentate, as in Worked example 9.4, it changes everything.

Everything else in this course was governed by an equilibrium. What governs a membrane?

A rate. Distillation, absorption and extraction all reach a genuine equilibrium at each stage and are limited by thermodynamics; the engineering is about approaching that limit efficiently. A membrane never reaches equilibrium — if it did, the flux would be zero. It is a kinetic separation, in which the two components are separated because one moves faster, not because one is more stable. Adsorption sits in between: the equilibrium isotherm governs a PSA cycle, but carbon molecular sieves separate oxygen from nitrogen purely on diffusion rate, which is a kinetic separation in a solid. The distinction is worth carrying: equilibrium separations are bounded by thermodynamics, kinetic ones by transport.

A membrane contactor puts a wall between the gas and the liquid. Doesn't that add resistance?

Yes, and it is worth it. The wall adds a diffusional resistance in series with the two film resistances, which costs some driving force. What you buy is a known and constant interfacial area, decoupled from the flow rates — so there is no flooding limit, no loading limit, no entrainment, no foaming, and the gas and liquid rates can be varied completely independently. In a packed column the interfacial area is a strong and poorly known function of both flows, which is precisely the uncertainty Chapter 10 spends its time managing. Contactors are used where the flows swing widely or where the liquid foams: offshore gas treatment, and blood oxygenators.

Where this chapter connects

Summary & key equations

Transport

Fluxpartial pressures
Permeability, in barrer = 10⁻¹⁰ cm³(STP)·cm/(cm²·s·cmHg) — the material
Permeance, in GPU = 10⁻⁶ cm³(STP)/(cm²·s·cmHg) — the finished membrane
Selectivity — a mobility ratio times a solubility ratio
Upper boundpermeability and selectivity trade off; a material is interesting only above the Robeson line

One well-mixed stage

Balance
Flux ratio,  
Recovery — rises with while purity falls
Pressure-ratio ceiling — independent of the membrane
Which limits? → the material; → the compressor — but that is the dilute asymptote. Test it by relaxing each constraint in turn (App 2), and check : above 1 it cannot bind

Sizing

Area, with both fluxes at the module's own and
Units
Check must return — if it does not, the composition solution is wrong
Design to a spec and fall, recovery rises, all monotonic in — one equation, one unknown
Watch outa permeate spec is cheap; a retentate spec is expensive, and climbs as the residue gets leaner

Cross-flow

Profile, with from Eq 9.4 at the local
Area, also local
Collected permeate — a flow-weighted average, not a point value
Rankingwell mixed < cross-flow < countercurrent; well mixed is conservative on separation and on area

Two stages and a recycle

Permeate cascadepolish the permeate, recycle stage-2 retentate — buys purity, and reaches purities one stage cannot
Retentate cascadere-treat the retentate, recycle stage-2 permeate — buys recovery and a clean residue
Solving ititerate on the recycle; check on the overall balance
What it doesenriches the feed to stage 1 — the reflux of a membrane plant, paid for in compression

Hardware

Structuresymmetric → asymmetric → composite; all to make the selective layer thin
Modulesspiral-wound ≈ 1000 m²/m³; hollow fibre ≈ 10 000 m²/m³ but harder to clean
Contactorthe membrane fixes the interfacial area; the separation is still absorption