[0003] According to WHO statistics, less than 0.007% of all
water on the earth is readily accessible for human
consumption. About a billion people lack access to safe
drinking water. More than 3.5 million people die every year
due to water-related diseases. Water insecurity is one of the
leading causes for school dropouts, especially among girls,
and more than 200 million working hours are spent (almost
exclusively by women) daily for the collection of domestic
water.
[0004] The water crisis is worsened in arid parts of the world
due to abuse of groundwater, water-intensive crop cultivation,
rapid industrialization, and changing lifestyle. In some dry
regions, the appearance of fog in the early morning is common.
Fog is a completely untapped water resource. Fog harvesting
provides an opportunity to "produce" water locally for rural
communities, which will reduce the stress on groundwater.
Consider a country like Chile, where a persistent advection
fog is occurs due to the long and mountainous coastline. By
one estimate, 10 billion m <3 >of fog water per year is
available in Chile. Currently, water consumption in northern
Chile is 391 million m <3 >per year, i.e., only 4% of
the total water content in the fog. Water collection from fog
harvesting thus has enormous potential to locally satisfy the
need for a pure and dependable supply of water in arid
locations.
SUMMARY
[0005] Highly efficient permeable structures for collection of
liquid droplets or small particles are described. The surface
wetting properties and topography of the material can guide
the design of the permeable structures. For example, the fog
harvesting ability of woven meshes can be increased greatly by
judiciously choosing the physico-chemical properties of the
mesh surfaces. A working model for the interaction of liquid
with the permeable structures allows design of highly
efficient liquid collecting structures for a variety of
possible conditions.
[0006] The permeable structures can be used for applications
including fog harvesting; elimination of mist in engines and
turbines; or elimination of small droplets or colloidal
particles in the chemical process industries. These mist
eliminators decrease pressure drops across unit operations,
such as distillation columns, and therefore save energy
required for pumping. Filters based on the permeable
structures can selectively capture hazardous colloidal
emissions based on size.
[0007] In one aspect, a device for collecting droplets of a
liquid from an aerosol can include an aerosol-permeable
structure including strands having a characteristic radius,
and a characteristic spacing, a characteristic spacing ratio,
wherein the outermost surface of the strands includes a
material having a low contact angle hysteresis for the liquid.
[0008] In certain circumstances, the material and the
characteristic spacing can be selected such that liquid
droplets adhered to the structure will drain from the
structure under gravity....
BRIEF DESCRIPTION OF THE DRAWINGS
[0033] FIG. 1 is a series of microscope images of
various permeable structures with different wire radii (R)
and spacing ratio (D*).
[0034] FIGS. 2A-2C are a diagrams depicting fog
flow through a woven mesh surface, and a contour plot of the
fog harvesting efficiency. FIG. 2A is an illustration
indicating the stream surfaces of fog laden wind and their
divergence after passing through a woven mesh surface. FIG.
2B is an enlarged drawing focusing on the interaction
between incoming fog droplets and a horizontal mesh element.
FIG. 2C is a contour plot of the fog harvesting efficiency
([eta]) s a function of the ratio of radius of the fog
droplets to the radius of the wire (R*=r fog/R) and the
spacing ratio of the woven mesh (D*=(R+D)/R).
[0035] FIGS. 3A-3E represent two factors that
reduce collection efficiency, and the surface modification
design space that depicts the relative resistance to
re-entrainment and drainage. Two factors that inhibit fog
harvesting and reduce collection efficiency are ( FIG. 3A)
re-entrainment of collected droplets in the wind and ( FIG.
3B) blockage of the mesh. FIG. 3C shows a plot that
identifies the range of droplet sizes where the forces of
adhesion dominate the drag forces, and establishes a
criterion for a threshold droplet size for re-entrainment.
FIG. 3D shows a plot that represents a second constraint
arises from comparing the weight of the droplet with the
surface pinning force arising from contact angle hysteresis.
The threshold size where gravity dominates hysteretic
pinning can be decreased by minimizing CAH=cos [theta]
rec-cos [theta] adv. FIG. 3E shows a graph depicting the
design space constructed from two dimensionless parameters
related to work of adhesion (abscissa) and contact angle
hysteresis (ordinate) depicts the relative resistance to
re-entrainment and drainage. Measured values for droplets of
water (V ''10 [mu]L) deposited on several different coatings
are shown in the plot. Wetting characteristics corresponding
to a higher work of adhesion and lower contact angle
hysteresis are ideal for the maximum fog collection
efficiency.
[0036] FIG. 4 is a contour map of the predicted
aerodynamic capture efficiency of fog droplets of radius r
fog using a mesh with a wire radius R and a spacing ratio
D*, assuming a wind velocity of 2 m/s. The efficiency is
expected to increase with decreasing R (increasing R*) and
at an intermediate value of D*.
[0037] FIG. 5 illustrates clogging and bridging
problems associated with draining of collected liquid and a
how a coating having a low contact angle hysteresis and a
high receding contact angle can address these problems.
[0038] FIGS. 6A-6B show contour plots of fog
harvesting efficiency of woven mesh surfaces with either (
FIG. 6A) a polypropylene (PP) coating, or ( FIG. 6B) a
POSS-PEMA coating.
[0039] FIG. 7 illustrates a fabrication process of
liquid-collecting permeable surfaces with different
wettability by dip-coating and spray-coating.
[0040] FIG. 8 is a schematic depiction of an
artificial fog harvesting experimental setup. The
experiments were carried out in a humidity chamber at
T=26[deg.] C., and a relative humidity of 100% to eliminate
the effects of condensation and evaporation of water.
[0041] FIGS. 9A-9D illustrate results of fog
harvesting experiments with woven wire meshes of different
dimensions and surface coatings. FIGS. 9A-9C show design
chart based on spacing ratio D* and dimensionless width R*.
FIG. 9D displays the experimentally observed collection
efficiency for the 5 dip-coated wire meshes along with
coated and uncoated Raschel mesh.
[0042] FIG. 10 is shows predicted fog harvesting
efficiency for a double layered Raschel mesh (blue) and for
a woven mesh with R=127 [mu]m and D*=3.5 (red) under
different conditions of fog droplet size and wind velocity.
Velocities and fog droplet radii were: (1) 0.5 m/s and 3
[mu]m; (2) 0.5 m/s and 6 [mu]m; (3) 2 m/s and 3 [mu]m
(conditions used in lab experiments); (4) 2 m/s and 6 [mu]m;
(5) 8 m/s and 3 [mu]m; and (6) 8 m/s and 6 [mu]m (Chilean
fog conditions).
[0043] FIG. 11 is a schematic diagram depicting a
water droplet on a cylindrical mesh filament.
[0044] FIG. 12 is a micrograph depicting a coated
mesh.
[0045] FIG. 13 is a diagram and graph depicting
contact angles of water droplets on surfaces.
DETAILED DESCRIPTION
[0046] A design framework can guide the design and selection
of a liquid-collecting structure having enhanced efficiency
for a given environmental or operating condition. Accordingly,
engineered surfaces can have significantly higher liquid
collection efficiency compared to current structures, such as
Raschel meshes used in fog harvesting. The understanding
provided by this framework can facilitate effective fog
harvesting across many regions and conditions.
[0047] The design framework is independent of any specific
material used on the permeable structures. Therefore, mesh,
spring, or other permeable structures could be manufactured
using materials that have desirable bulk properties (such as
strength, ease of working, weight, cost, durability, and
others). The permeable structures can be conformally coated to
achieve desired surface properties (e.g., texture and wetting
properties). For example, a metallic mesh can be mechanically
robust, both structurally and against environmental wear and
tear. A metallic mesh can retain a complex 3-dimensional
structure that can further enhance the efficiency of liquid
collection. The design framework can be applied to generally
to permeable motifs, including multiple mesh systems. The
design framework provides a way to selectively filter droplets
or particles based on size and/or velocity in an aerosol,
cloud, or fog.
[0048] An aerosol is a suspension of liquid droplets or fine
solid particles in a gas. The particles are sufficiently small
that they remain suspended rather than falling or settling out
of the suspension. One typical example of an aerosol is a
suspension of liquid particles in air. In a natural setting,
an aerosol of water in air is typically referred to as fog (if
close to the ground) or a cloud (if high above the ground).
[0049] Liquid aerosols typically include droplets having a
size in the micrometer regime. For example, fog, mist, or
colloidal particles of water in air typically have a size in
the range of about 1 [mu]m to about 40 [mu]m. These
particles/droplets are too small to settle down under gravity;
they undergo Brownian motion and cannot be collected by
gravity-based techniques. These droplets, however, have
significantly higher density than the surrounding air mass.
Therefore, when an aerosol flows around a solid object, the
particles cannot follow the streamlines. They continue to
travel along their initial trajectory and as a result, are
intercepted by the solid object. Langmuir and Blodgett and
many other researchers studied the efficacy of cylindrical
objects in the capture of such small-sized particles. See, for
example, Langmuir, I.; Blodgett, K. B. A mathematical
investigation of water droplet trajectories US Air Force Tech.
Rep. No. 5418: 1946; p 68; and McComber, P.; Touzot, G.,
Journal of Hydrometerology 1981, 38, 1027-1036; each of which
is incorporated by reference in its entirety. They concluded
that the efficiency of fog harvesting ([eta]) increased as the
radius of the cylindrical obstacle (R) decreased.
[0050] Aerosol-permeable structures (also referred to herein
simply as "permeable structures") can be used to collect
liquid droplets from the aerosol. An aerosol-permeable
structure is a structure, having many small openings, pores,
or channels through which the aerosol can pass. Preferably,
the structure is sufficiently permeable to the aerosol that
when the aerosol is part of a moving current, the aerosol
passes primarily through the aerosol-permeable structure,
rather than being primarily diverted around the structure (as
would occur in the case of a solid structure). As the aerosol
passes through the permeable structure, droplets impact the
permeable structure and are retained there. As more droplets
impact, the droplets coalesce. The coalesced droplets can then
be collected (e.g., by flowing or dripping from the structure
by gravity, or by mechanical agitation of the structure to
dislodge the coalesced droplets).
[0051] Permeable structures suitable for liquid collection can
be formed of any material possessing the necessary
permeability to the aerosol. For example, the permeable
structure can be a mesh, such as a woven mesh. A mesh includes
many interlaced or interconnect strands. The strands can be
filamentous, being much longer than they are wide. The strands
can be generally cylindrical in shape. The strands can be of
any material, for example, natural fibers, polymers, metals,
or composite materials. The strands have an outermost surface,
the properties of which can affect the efficiency of liquid
collection (discussed below). The strands can be formed of a
single first material, e.g., a metal, in which case the first
material forms the outermost surface. In other cases, the
strands can be coated with a second material (e.g., a strand
composed of a metal and having a polymer coating on the
metal). In this case, the second material forms the outermost
surface of the strand, and the properties of the second
material, rather than the first material, will influence the
liquid-collecting properties of the permeable structure. In
cases where the strands are coated, the coating can be applied
prior to forming the mesh, or after the mesh is formed.
[0052] The mesh can have a regular or irregular pattern of
strands. In some cases, the strands of a mesh can have
different radii; in other cases, the strands will all have the
same radius. A regular pattern of strands involves a set of
strands aligned in parallel with each other and repeating at
regular intervals. Typically it also involves a second set of
strands aligned in parallel with each other but set at an
angle to the first set. In one simple example, the mesh can
have a simple pattern with two sets of strands set at right
angles, and repeating with the same interval in both
directions.
[0053] A mesh, particularly a simple mesh, can be
characterized according to the dimensions of the mesh and its
component strands. Thus, a simple mesh can have strands having
a characteristic radius. The strands can have a characteristic
spacing between adjacent parallel strands. Typically the
spacing will be the same along both the length and width, but
this is not necessarily so. Thus, a mesh can have a first
characteristic spacing in one direction, and a different
second characteristic spacing in the other direction. The mesh
can also have a characteristic spacing ratio, which relates
the characteristic radius to the characteristic spacing, as
explained further below. The spacing ratio describes the
closeness of the mesh, in other words, across a large section
of the mesh, how much surface area the strands cover.
[0054] A spacing ratio, D*, can be defined as follows: if R is
the cross-sectional radius of a strand, and 2D is the spacing
between adjacent strands, the spacing ratio is defined as
D*=(R+D)/R. The closeness of the mesh can also be represented
as a shading coefficient (SC), which is the fraction of
projected area that is occluded by the solid mesh texture.
[0055] The permeable structure can be coated with a material
chosen for its surface properties, for example, its wetting
properties. Wetting properties include hydrophobicity,
hydrophilicity, oleophobicity, oleophilicity, advancing
contact angle, receding contact angle, static contact angle,
contact angle hysteresis and other properties. Suitable
coating materials include polymers (e.g., hydrophobic
polymers). One such example is polyhedral oligomeric
silsesquioxanes (POSS), and blends of POSS with other
polymers, such as polyacrylates and fluoropolymers, for
example, Tecnoflon. Exemplary polyacrylates include
poly(methyl methacrylate), poly(ethyl methacrylate), or
poly(butyl methacrylate). Other materials can be added to the
coating material to afford other properties, such as titania
particles, (e.g., titania nanoparticles) which can exhibit
photocatalytic self-cleaning properties. The coating material
can also be chosen for its texture. In some cases, the
material may be smooth; or it may have a degree of roughness.
Roughness may be found at the nanometer scale, the micrometer
scale, or larger scales. A second liquid (ex. Krytox oil)
which is insoluble in water can be impregnated in the
asperities of the texture.
[0056] Polyhedral oligomeric silsesquioxanes (POSS) molecules
have a rigid silsesquioxane cage surrounded by optionally
substituted alkyl groups, e.g., fluoro-alkyl groups. A number
of different molecules with different organic groups, such as
1H,1H,2H,2H-heptadecafluorodecyl (fluorodecyl POSS) and
1H,1H,2H,2H-tridecafluorooctyl (fluorooctyl POSS), have now
been synthesized. Fluorinated POSS molecules contain a very
high surface concentration of fluorine containing groups,
including -CF 2 and -CF 3 moieties. The high surface
concentration and low surface mobility of these groups, as
well as the relatively high ratio of -CF 3 groups with respect
to the CF 2 groups results in one of the most hydrophobic and
lowest surface energy materials available today. See, for
example, Owen, M. J. & Kobayashi, H. Surface active
fluorosilicone polymers. Macromol. Symp. 82, 115-123 (1994).
Blends of a moderately hydrophilic polymer, poly(methyl
methacrylate) (PMMA) and fluorodecyl POSS can be used in
various weight ratios to create materials with different
surface properties. Other polymers can be used in place of or
in combination with other polymers. By varying the mass
fraction of POSS blended with various polymers, the surface
energy of the polymer-POSS blend can be systematically
changed. See, for example, WO 2009/009185, which is
incorporated by reference in its entirety
[0057] Meshes, e.g., woven meshes, having cylindrical fibers
are commercially available over a wide range of wire radii and
spacings (as shown in FIG. 1). Woven meshes can be a suitable
material for fog harvesting structures because of their
relatively low cost (e.g., $5 to $10 per sq. ft.), wide
availability, and mechanical robustness. Their regular
geometric structure also facilitates quantitative study,
modeling, and design of their fog harvesting properties. A
comprehensive model to analyze the efficiency of water
collection (ii) using woven meshes has been described (Rivera,
J. D., Atmospheric Research 2011, 102, 335-342, which is
incorporated by reference in its entirety). The efficiency
[eta] can be represented in terms of two independent,
dimensionless variables. The first is the spacing ratio, D*.
The second, R* is the ratio of the radius of fog droplets (r
fog) to the radius of the mesh wire (R), i.e., R*=r fog/R.
[0058] The overall collection efficiency is a product of i)
the aerodynamic collection efficiency ([eta] a) and ii) the
subsequent deposition efficiency ([eta] d) (Rivera, J. D.,
Atmospheric Research 2011, 102, 335-342, which is incorporated
by reference in its entirety). Rivera argued that the
aerodynamic collection efficiency accounts for the fraction of
fog flow that is directed towards the solid portion of the
mesh. The high Reynolds number (Re>>1) flow around the
mesh ( FIG. 2A) is modeled as a linear combination of the flow
around an impermeable rigid solid (i.e., D* =1), and an
unobstructed uniform flow. FIG. 2B is an enlarged view, in
which droplets that are closer to the central axis are trapped
on the cylindrical wire, whereas droplets closer to the
periphery follow the streamline around the wire. Droplets on
the wire coalesce, and once they grow past a threshold size,
they drain under gravity. Due to the no slip and no
penetration boundary conditions at the solid surface, the wind
speed is locally reduced in the vicinity of the mesh elements.
This momentum defect is modeled in terms of a drag coefficient
for the overall structure (C D 1.18) and the aerodynamic
collection efficiency is ultimately expressed as [eta]
a=SC/(1+[square root of]{square root over (C 0/C D)}), where C
0 is the pressure drop coefficient for a cylindrical mesh
given as C 0=1.44[1.3SC+(SC/(1-SC)) <2>]. The collection
efficiency is not simply equal to the shade coefficient of the
mesh, but changes nonmonotonically with the openness of the
mesh and the aerodynamic characteristics of the flow through
the mesh. As D* increases from unity (an impermeable plate),
the aerodynamic collection efficiency ([eta] a) increases from
zero as the lateral deflection of the air stream is
diminished. Beyond a local maximum at D* crit 3.1(or
equivalently, SC 0.55), most fog droplets pass through the
void area between wires without being deflected and [eta] a
decreases.
[0059] The deposition efficiency ([eta] d) quantifies the
fraction of fog droplets that are actually deposited from the
population initially headed towards the solid wires. In their
seminal work, Langmuir and Blodgett used numerical
calculations to develop an empirical correlation for the
deposition of small particles on an infinitely long cylinder
(Langmuir I, Blodgett KB (2004) A mathematical investigation
of water droplet trajectories. Collected works of Irving
Langmuir (Pergamon Press, Oxford), which is incorporated by
reference in its entirety.); the deposition efficiency ([eta]
d St/(St+[pi]/2)) monotonically increases as the dimensionless
radius ratio R* increases, i.e. cylinders with progressively
smaller radii are more efficient collectors.
[0060] The resultant overall collection efficiency from the
two components
[0000] [mathematical formula]
[0061] is shown in FIG. 2C as a contour map in R*, D*
parameter space, assuming a wind velocity of 2 m/s and uniform
droplet size r fog 3 [mu]m (0<=St<=4). The contours
indicate that the collection efficiency of a conventional
Raschel mesh (D* 5.1, R* 0.005; [eta] 4.8%) is much lower than
that of a thinner and denser wire mesh (D* 3.5, R* 0.024;
[eta] 12%). The contour map can also be used as a design chart
for selecting an optimal mesh by choosing D* (or SC) and
maximizing R*. The chart can be employed to estimate the
maximum fog collection efficiency and evaluate the amount of
collected water expected for a specific mesh surface, if the
characteristic wind speed of the fog ([nu] 0), liquid water
content, total mesh area, and collection time are known.
[0062] In the design chart presented in FIG. 3, contours of
efficiency of aerosol harvesting ([eta]) are plotted as a
function of spacing ratio (D*) and R*. The contours correspond
to different values of r fog, shown at upper right in FIG. 3.
The efficiency increases monotonically with increasing value
of R*, i.e., decreasing size of the cylindrical strands (R).
On the contrary, the variation of [eta] with D* is not
monotonic. Instead, the efficiency goes through a maximum
value at intermediate spacing ratios, i.e., the optimal value
of D* is between about 3 and about 4. When the spacing ratio
is small (D* approaching 1), the aerosol harvesting efficiency
is close to zero. At such low spacing ratios, the mesh behaves
like an impermeable solid object: the gas, along with the
liquid droplets suspended in it, are deflected around the
mesh. As a result, very few droplets impact the mesh,
resulting in a low collection efficiency. As D* increases, the
openness of the mesh increases, and the airflow is perturbed
to a smaller extent. As a result, more droplets impact the
cylindrical strands of the mesh and the collection efficiency
increases. However, as D* increases further, less solid
material per unit projected area is available for droplets to
impact, and therefore the efficiency decreases. At still
larger value of D*, the strands of the woven mesh are far away
from each other, and most fog droplets go through the mesh
without being intercepted by the solid strands. Therefore,
there is a trade-off between the two effects, i.e., deflection
of the air stream around an impermeable blunt body at low D*,
and passage of the air stream through the mesh at high D*. As
a result, the optimal efficiency for collection of liquid
droplets is expected for a mesh with low R and intermediate
value of D* (D* 3 to 3.5).
[0063] Based on the design chart, the mesh surface with
highest efficiency for a given aerosol condition
(characterized by a particular size of the liquid droplet and
gas velocity) can be selected. Note that efficiency increases
moving from left to right on the x-axis of FIG. 3. Therefore,
for a given mesh with wire radius R, the efficiency of
collection is highest for the largest droplets (r fog).
Because the volume of a droplet is directly proportional to
the cube of its radius, mesh surfaces that are highly
effective in capturing large droplets will harvest most of the
liquid volume fraction in the aerosol.
[0064] The design chart outlined FIG. 2C can be extended to
other permeable surfaces like springs. An array of springs can
be used to capture tiny droplets of water in a moving column
of air. Springs are symmetric structures, and therefore fog
collectors made of springs will perform equally well
irrespective of the direction of fog-laden wind. The spacing
between two helical elements of a spring can be tuned by
applying a tension/compression in the vertical direction.
Therefore, the spacing ratio (D*) or shade coefficient can be
chosen based on the incoming wind velocity and other physical
properties of the system.
[0065] The theoretical collection efficiency anticipated from
this design framework for meshes can be adversely affected in
actual performance due to two issues that depend on the
surface wettability; i) convective loss of deposited droplets
(or re-entrainment; as shown schematically in FIG. 3A) and ii)
mesh clogging that modifies the local aerodynamics ( FIG. 3B).
Re-entrainment arises from aerodynamically-induced detachment
of deposited water droplets back into the air stream before
they can reach the critical volume at which gravitational
drainage dominates. As the small deposited water droplets
coalesce, the growing droplets are influenced by the
competition between aerodynamic drag forces and surface
adhesion forces. See, for example, 24. Milne A J B, Amirfazli
A (2009) Drop shedding by shear flow for hydrophilic to
super-hydrophobic surfaces. Langmuir 25:14155-14164, and
Ledesma-Aguilar R, Nistal R, Hernandez-Machado A,
Pagonabarraga I (2011) Controlled drop emission by wetting
properties in driven liquid filaments. Nat. Mater. 10:367-371,
each of which is incorporated by reference in its entirety.
When F drag>F adhesion, the droplets are re-entrained in
the fog flow, leading to a decrease in the fog collection
efficiency ( FIG. 3A).
[0066] In FIG. 3B a second problem that occurs on a mesh when
the deposited liquid volume becomes large is identified. In
the clogging region, the hysteretic wetting force pinning a
droplet in the interstices of the mesh exceeds the
gravitational draining force when the deposited water droplet
size is less than a critical volume. The void area between
mesh elements could become occluded by these pinned
(non-draining) drops, depending on the half spacing of the
mesh as discussed below. Such clogged parts of the mesh are
impermeable and obstruct the local wind, significantly
hampering the overall fog-harvesting ability of the grid. The
effective void fraction approaches zero (or D*
effective->1) as the mesh clogs and the aerodynamic
collection becomes zero.
[0067] To overcome these two challenges and to design fog
collection mesh surfaces with high efficiency in practice, the
two critical water drop radii-denoted r e and r c in FIGS. 3C,
D-that are sensitive to the physico-chemical surface
properties of the meshes are considered. In FIG. 3C, the
right-most shaded region represents the range of paramater
space where the aerodynamic drag force (which grows as F drag
[rho][nu] 0 <2>r <2> drop) exceeds the adhesion
force (which grows as F adhesion [gamma] LV (1+cos [theta]
rec)r drop); droplet re-entrainment is expected in this region
where F drag>F adhesion. A detailed force balance on a
spherical cap gives a critical droplet radius at which these
two forces balance each other:
[0000] [mathematical formula]
[0000] where [gamma] LV is the surface tension of water,
[theta]=([theta] adv+[theta] rec)/2 is the mean contact angle
of the droplet on the surface, and [theta] adv, [theta] rec
are the advancing contact angle and receding contact angle,
respectively (see below for details). A droplet with radius r
drop>r e is susceptible to re-entrainment. To reduce
re-entrainment, the slope of the adhesion force curve, which
is proportional to the work of adhesion [gamma] LV (1+cos
[theta] rec), must be increased. This can be achieved in
practice by lowering the receding contact angle [theta] rec.
[0068] As the droplets grow on the mesh, gravity has to
overcome the surface pinning force in order to shed these
collected droplets into the collecting gutter at the base of
the mesh. Balancing the the gravitational body force F grav
[rho]gr <3> drop with the hysteretic force F CAH [gamma]
LV(CAH)r drop that characterizes depinning of a liquid droplet
in the interstitial gap of a woven mesh with a simple square
weave. Setting F grav=F CAH gives a second critical radius for
'choking' or clogging of the mesh
[0000] [mathematical formula]
[0000] where B=(1-cos [theta])/sin [theta] (see below for
additional details). FIG. 3D shows that mesh-clogging as a
result of contact line pinning can be reduced (i.e. the
minimum droplet size r c that will freely drain off the mesh)
by developing surface coatings with smaller values of the
contact angle hysteresis CAH=cos [theta] rec-cos [theta] adv
[0069] For an ideal fog-collecting surface, liquid droplets
convected towards the mesh and deposited on the surface will
be drained quickly by gravity into the collecting gutter
without loss by re-entrainment to the airflow, thus refreshing
the base mesh surface for capture of new fog droplets. Design
of an improved mesh to maximize fog collection efficiency thus
involves: I) minimizing rc to avoid clogging, II) maximizing
re to reduce re-entrainment, while also III) selecting a mesh
opening near the optimal aerodynamic value of D* 3.1 and IV)
maximizing R* to the extent possible.
[0070] The surface forces controlling adhesion and hysteresis
depend upon the physico-chemical surface characteristics of
the mesh (Quere D (2008) Wetting and roughness. Annu. Rev.
Mater. Res. 38:71-99, which is incorporated by reference in
its entirety), and therefore smart engineering of suitable
coatings can enable woven meshes to collect fog with improved
efficiency. If r e>>r c can be achieved by surface
modifications, then the performance degradation associated
with both shaded regions in FIGS. 3C, 3D can be minimized.
Such a mesh surface would have both low contact angle
hysteresis (CAH<<1) and a low receding contact angle
([theta] rec->0). This material challenge can be summarized
in the surface modification design space shown in FIG. 3E. The
two important design parameters are contact angle hysteresis
(CAR) and a scaled work of adhesion (W a/[gamma] LV=1+cos
[theta] rec) that can be exploited to rank the wetting
properties of various materials for preventing clogging and
re-entrainment problems. From the expression for mesh clogging
(r c) given in eq.(3), it is clear that a coating with
extremely low hysteresis (CAH->0) will lead to a small
value of the critical mesh half spacing (denoted D crit) above
which the clogging problem does not occur.
[0071] Previously deployed fog harvesting setups used a
double-layered Raschel mesh made of polyolefin (denoted PO)
which has CAH <(PO)>=cos [theta] rec <(PO)>-cos
[theta] adv <(PO)> 0.40 (see Table 1). By contrast, a
topographically smooth surface dipcoated with a blend of 50%
POSS -50% PEMA (denoted PPD) has one of the lowest values of
contact angle hysteresis reported to date; CAH
<(PPD)>=cos [theta] rec <(PPD)>-cos [theta] adv
<(PPD)> 0.06. See, for example, Meuler A J, Chhatre S S,
Nieves A R, Mabry J M, Cohen R E, et al.(2011) Examination of
wettability and surface energy in fluorodecyl POSS/polymer
blends. Soft Matter 7:10122-10134, which is incorporated by
reference in its entirety. The critical opening size for a PPD
coated mesh D crit <(PPD)> 0.41 mm is significantly
smaller than D crit <(PO)> 1.5 mm, and therefore finer
meshes, if dipcoated with POSS-PEMA, will drain more readily
and be less susceptible to clogging.
[0072] This hysteretic drainage criterion involves differences
in the surface energies based on advancing and receding
contact angles; however, from eq. (2) it is clear that the
absolute magnitude of the receding contact angle is also
important for preventing re-entrainment and subsequent loss of
deposited droplets. The adhesive work (per unit area) required
to pull a droplet off the surface (against aerodynamic drag)
scales as W a=[gamma] LV (1+cos [theta] rec). Therefore,
'sticky' surfaces with low [theta] rec (and high W a) promote
the adhesion of droplets on solid surfaces.
[0073] The surface properties of the POSS coating can be
manipulated further by altering the deposition technique (
FIG. 3E). The CAH can be further decreased to CAH 0.01 by
spray-coating the mesh to create a re-entrant roughened
topography using POSS-PEMA (see, for example, Srinivasan S,
Chhatre S S, Mabry J M, Cohen R E, McKinley G H (2011)
Solution spraying of poly(methyl methacrylate) blends to
fabricate microtextured, superoleophobic surfaces. Polymer
52:3209-3218, which is incorporated by reference in its
entirety), but the receding contact angle increases to [theta]
rec 159[deg.]. Therefore, such spray coated meshes (denoted
PPS in FIG. 3E) are extremely clogging-resistant, but the
higher [theta] rec value reduces drop adhesion which leads to
greater re-entrainment and a lower overall collection
efficiency. A liquid impregnated textured surface or 'SLIPS
surface' (29, 30, 31) with low CAH and low [theta] rec can be
obtained by imbibing a nonvolatile oil (e.g., Krytox oil) into
the pores of the spray-coated surface (31). This
liquid-impregnated surface (denoted KO in FIG. 3E) has CAH
0.03 and [theta] rec 100[deg.], and therefore it is expected
to harvest fog better than dip-coated or spray-coated meshes.
[0074] The fog harvesting technique described was based on
physical impaction and interception of liquid droplets in a
flow. The mesh surfaces captured liquid particles. In addition
to water droplets, fog also includes a high level of humidity.
The condensation of water vapor in this humid mass represents
another source of water. Woven mesh surfaces have a large
interface available for heat transfer, and by selecting the
thermal emissivity and heat transfer properties of the mesh
surface, harvesting of droplets in fog can be supplemented by
condensation of humidity to provide additional water.
[0075] A woven mesh surface can be cooled by processes
including natural convection, infrared emission, and
artificial cooling through conduction. Materials that are
highly emissive in the infrared (such as, for example, carbon
black nanoparticles), can be used as a coating on the
permeable structures to further enhance the liquid-collecting
efficiency. Carbon nanoparticles can be coated by simply
exposing the permeable structure to an open flame; e.g.,
candle soot can be a source of carbon black nanoparticles.
Nanoparticles can also be added using layer-by-layer
deposition. Besides infrared emissivity, nanoparticles (of any
suitable material) can create structures on the micrometer
and/or nanometer scale to enhance heat transfer (e.g., by
increasing the effective surface area of the permeable
structures).
[0076] In some circumstances, it may be beneficial to provide
more than one layer of the permeable structures to increase
the efficiency of liquid collection. For example, in
high-velocity wind conditions, as in the case of inertial
Chilean fog, droplets collected on the mesh might blow away.
One more more additional meshes placed downwind of the first
structure can act as a barrier and capture such droplets. In
another example, when fog droplets are extremely small, and
the wind velocity is low, a single layered collection surface
may have limited collection efficiency. One or more additional
layers can be selected so that its capture elements (e.g.,
cylindrical wires) are aligned with the openings of the first
permeable structure. Then, by adjusting the distance between
the two mesh structures, fog collection can be optimiazed
without significantly disturbing the wind profile. Multiple
layers of mesh placed close together are likely to touch when
the wind is blowing; this contact can aid the drainage of
liquid droplets collected on the meshes.
[0077] The liquid-collecting permeable structures discussed
above involved flat or curved woven wire mesh. Three
dimensional geometries for the permeable structures are also
contemplated. Examples of such three-dimensional geometries
include helical springs, cones or inverted cone shapes,
including one or more layers of mesh surfaces to capture
omnidirectional fog/mist flow. Like a fog-well, an axially
symmetric structure can show uniform collection efficiency
regardless of direction of fog/mist flow. In addition,
convenience for collecting liquid into a container or pipe
system can be significantly enhanced by engineering the aspect
ratio and symmetry of the devices.
[0078] Apart from fog harvesting, the permeable structures can
be used in other applications as well. Such structures can be
used (1) to eliminate mist in engines and turbines or (2) to
eliminate small droplets/colloidal particles in unit
operations in chemical process industries that involve pipes
and reactors. These mist eliminators decrease pressure drops
across unit operations like distillation columns and therefore
save energy required for pumping. Demisters are used to
separate liquid droplets from air in absorbers, seawater
desalination plants, washers, sulphuric acid plants, vacuum
columns, sound absorbers, vibration dampers, distillation and
rectification plants, oil separators, evaporators, flash
vessel systems, and other equipment. Filters based on such
structures can selectively capture hazardous colloidal
emissions based on their size. The design framework allows the
construction of a size-specific "membrane" that allows
particles or liquid droplets under a certain size to pass
through, while almost completely blocking particles above a
threshold size. Further, by appropriately tuning the wetting
parameters of the surface, a membrane that selectively
collects a few liquids while letting other liquids go through
can also be constructed.
Examples
[0079] In FIG. 4, the x-axis is the ratio of fog droplet
radius to the radius of the mesh wire (r fog/R), and the
y-axis is the spacing ratio ((R+D)/R), so for a given fog
condition (fixed r fog), each positively sloped line through
the origin represents a unique mesh spacing. In FIG. 5, the
critical mesh opening size for PP (left panel) and POSS-PEMA
(right panel) are represented on the contour plots for the
expected aerodynamic efficiency of fog harvesting.
[0080] Consider a mesh with a PP material/coating with a
critical opening size of 1190 [mu]m, as shown in the left
panel of FIG. 6 ( FIG. 6A). For any point to the right of the
limiting spacing (i.e., any point in the shaded region), the
mesh is expected to clog with liquid droplets; consequently,
the mesh will never reach its predicted efficiency in
collecting droplets. The overall efficiency of fog harvesting
is the product of the two sequential processes (1) the
collection of fog droplets on mesh surfaces, and (2) the
drainage of water from the mesh to a storage tank. For points
in the shaded region, the efficiency of fog impaction might be
higher, but the drainage efficiency decreases significantly
and therefore, the overall fog harvesting efficiency will not
improve. Due to this restriction, the higher efficiency
portion of the design space cannot be fully utilized and at
best 6% efficiency can be obtained with a PP coating.
[0081] However, a POSS-PEMA coating with smaller contact angle
hysteresis (than PP) has a lower critical opening size, and
therefore, a significantly higher fraction of the design space
is free of clogging and drainage limitations. Therefore, a
mesh surface with smaller radius (smaller R) and a
correspondingly more effective value of D* could be chosen. An
appropriately chosen POSS-PEMA coated mesh will have an
expected aerodynamic efficiency of about 12-13%, as shown in
the right side of FIG. 6B.
[0082] Therefore, changing the surface chemistry from PP to
POSS-PEMA allowed the choice of a surface texture with double
the overall expected efficiency. The triangular wedge shaped
portions between the two straight lines shown in FIG. 6B was
not accessible with a PP coating, but was available if the
meshes were coated with POSS-PEMA.
[0083] With this mechanistic understanding of fog harvesting,
the model was tested with a set of woven wire meshes. The
results were compared to those obtained with a polypropylene
Raschel mesh, which has been used in the field to harvest fog.
The comparison therefore provides a good benchmark to compare
performance to actual deployments in the field. The woven wire
meshes were dip-coated in a 50% POSS-50% PEMA solution (total
solids=10 g/l) for 5 minutes, then air-dried and annealed in
an oven at 60[deg.] C. for half an hour, as shown in FIG. 7.
The mesh samples were tested using an artificially generated
fog environment, as schematically shown in FIG. 8.
[0084] Materials and Methods Preparation of Meshes. Raschel
mesh samples with 35% shade coefficient were procured from
Fogquest volunteers in Chile and were cut into 30 mm by 30 mm
pieces. To keep the Raschel mesh flat and to ensure that the
meshes are normal to the direction of fog stream, the three
edges of square planar mesh were supported by a metal wire
frame with diameter of 127 [mu]m. Sample wire meshes surfaces
were prepared by cutting commercially available wire meshes
(McMaster-Carr, Corrosion-Resistant Type 304 Stainless Steel
Woven Wire Cloth) into the same square planar shape with 30 mm
side.
[0085] Polyolefin emulant coating (denoted by PO in FIGS. 3E,
9B). It has been shown that by tuning the relative
concentration of the FluoroPOSS species and a compatible
polymer binder (eg PEMA) the wettability characteristics of a
dip-coated surface can be tuned over a wide range (see, for
example, Meuler A J, Chhatre S S, Nieves A R, Mabry J M, Cohen
R E, et al.(2011) Examination of wettability and surface
energy in fluorodecyl POSS/polymer blends. Soft Matter
7:10122-10134). To generate a coated wire mesh that closely
mimics the surface properties of the polyolefin Raschel mesh,
the as-received wire mesh was dip-coated using a 1.7 wt. %
1H,1H,2H,2H-heptadecafluorodecyl polyhedral oligomeric
silsesquioxane (fluorodecyl POSS) 98.3 wt. % poly(ethyl
methacrylate) (PEMA, Mw=515 kDa, Sigma Aldrich) solution in a
volatile hydrochlorofluorocarbon solvent (Asahiklin AK-225,
Asahi Glass Company) at a concentration of 10 mg/mL. The
meshes were dipped for 5 minutes, and then air-dried to
evaporate the solvent. Uniformity of the coating was checked
by scanning electron microscope (SEM) and by contact angle
measurements at multiple locations on the surface.
[0086] POSS-PEMA dipcoating (denoted by PPD). Mesh samples
were dip-coated using a 50 wt. % fluorodecyl POSS 50 wt. %
PEMA solution in Asahiklin at a concentration of 10 mg/mL. The
meshes were dipped for 5 minutes, and then air-dried to
evaporate the solvent, resulting in a smooth superhydrophobic
coating.
[0087] POSS-PEMA spraycoating (denoted by PPS). A 50 wt. %
fluorodecyl POSS 50 wt. % PEMA solution was prepared in
Asahiklin at a concentration of 50 mg/mL. The superhydrophobic
spray-coated meshes were prepared by spray deposition of the
polymer solution using an air spray-brush (McMaster-Carr)
using a pressurized nitrogen stream to produce a re-entrant
microtexture with very low contact angle hysteresis (see, for
example, Srinivasan S, Chhatre S S, Mabry J M, Cohen R E,
McKinley G H (2011) Solution spraying of poly(methyl
methacrylate) blends to fabricate microtextured,
superoleophobic surfaces. Polymer 52:3209-3218). A
representative micrograph of the spray-coated mesh is shown in
FIG. 12.
[0088] Liquid Impregnated surfaces (denoted by KO). The
spray-coated meshes were immersed into nonvolatile Krytox oil
([gamma] LV=17 mN/m at 25[deg.] C., [mu] 113 mPa.s at 20[deg.]
C., DuPont) using a DCAT 11 (DataPhysics Instruments)
tensiometer at a rate of 0.5 mm/min and then retracted at the
same speed. A thin film of fluorinated Krytox oil remains
imbibed into the porous spraycoated texture after the mesh is
completely withdrawn from the oil bath, resulting in a 'SLIPS'
surface with very low contact angle hysteresis (see, for
example, Quere D (2005) Non-sticking drops. Rep. Prog. Phys.
68:2495-2532; Wong T -S, Kang S H, Tang S K Y, Smythe E J,
Hatton B D, et al. (2011) Bioinspired self-repairing slippery
surfaces with pressure-stable omniphobicity. Nature
477:443-447; and Smith J D, Dhiman R, Anand S, Garduno E,
Cohen R E, et al. (In press) Droplet mobility on
lubricant-impregnated surfaces. Soft Matter).
[0089] Experimental Procedure. All fog collection experiments
were performed at a relative humidity of RH=100% and
temperature of 26.4+-0.5[deg.] C. in a controlled-humidity
glove box (environmental chamber, Electro-Tech Systems, Inc.)
to eliminate evaporation and condensation. Each sample was
positioned 10 mm in front of the end of two plastic concentric
cylinders with different diameters of 100 mm and 20 mm,
respectively. As shown in FIG. 7, fog droplets (r fog=3 [mu]m)
created from a nebulizer (Omron Compair XLT Nebulizer
Compressor Kit NE-C25, Q=16 mL/hr) were convected towards the
mesh sample by a wind stream of velocity [nu] 0 2 m/s,
generated by a speed-tunable fan (Thermaltake Mobile Fan II
External USB Cooling Fan). The concentric axis of the two
cylinders and axes of symmetry of meshes and container were
aligned to be on the same vertical plane. The mass of water
collected in the container with dimension of 50 mm by 50 mm
located 50 mm under the mesh samples was measured every hour
for Raschel meshes and every 30 minutes for wire woven meshes
to quantify the time evolution of efficiency. Once the
efficiency reached the asymptotic value, the readings from at
least three consecutive experiments were averaged to calculate
the fog collection efficiency.
[0090] The fog harvesting results are summarized in FIG. 9 and
Table 1.
[0000]
TABLE 1
Theoretical Wind Average collection
Input water Collected Measured
velocity droplet efficiency flow
rate water efficiency
[m/s] size [[mu]m] [%]
<+> [L/m <2>/day] [L/m
<2>/day] [%]
Humid chamber 2 3 5.1 317.5
6.5 1.8
experiment (single
Raschel mesh)
Humid chamber 2 3 6.2 317.5
NA NA
experiment (double
Raschel mesh)
Humid chamber 2 3 13.8 317.5
31.4 9.9
experiment (POSS-
PEMA coated wire
mesh, R = 127 [mu]m,
D* = 3.5)
Chilean Fog Condition 8 6 16.3
~77.8 0.2-10 0.25-12.8
(double Raschel mesh)
Chilean Fog Condition 8 6 21.4
~77.8 11.9 <+> 15.3 <+>
(POSS-PEMA coated
wire mesh, R = 127 [mu]m,
D* = 3.5)
<+>computed using the framework and data under lab
conditions.
<+>assuming no drainage limitations.
Lab results were translated into L/m <2>/day assuming
uniform fog harvesting for 24 hours
[0091] Guided by this framework relating surface wettability
and fog harvesting performance, a set of parametric
experiments were performed using a family of simple woven
meshes with a range of surface coatings (see below section for
details). Results were benchmarked against the canonical
Raschel mesh, using an artificially generated laboratory fog.
These results are summarized in FIG. 9 and Table 1. As shown
in Table 1, for most coating materials (cos [theta]
rec<>-1), r e>>r c, and r e does not impact the
fog collection efficiency. For a given fog condition (i.e.,
fixed r fog) the critical mesh half spacing with a given
coating to prevent the clogging and re-entrainment problems (r
c=D crit<D<r e) can be represented as a line (D*=(D/r
fog)R*+1) through the origin with positive slope D/r
fog.Therefore the high efficiency region to the right of these
lines are inaccessible due to clogging (i.e. in this region of
FIG. 9A the mesh openings are too small D<r c and the
clogged mesh grids become impermeable). A first study is of
the polyolefin Raschel mesh (with large CAH, and a critical
opening size D crit <(PO)> 1.5 mm). Because of the
clogging constraint, large portions of the design space with
the highest efficiency cannot be accessed and, at best, a
theoretical efficiency of 5% efficiency can be obtained. As
shown in FIG. 9B, the measured fog-harvesting efficiency of a
Raschel mesh (D* 5.1) was [eta] 2%, under simulated fog
conditions.
[0092] The locus of the conventional polyolefin Raschel mesh
in the design space of FIG. 9A is shown by the open diamond.
Because it lies above the critical clogging line (i.e., D
Raschel>D crit <(PO)> 1.5 mm) it is not prone to
clogging. Additional dipcoating of the Raschel mesh with a
POSS-PEMA coating therefore does not appreciably enhance its
fog collection performance (sample - shown in FIG. 9B with
[eta]=2+-0.5%). To access the regions of higher efficiency, it
is clear from these resultes that meshes with higher R* are
required. Surfaces that are dipcoated in POSS-PEMA (to achieve
smaller CAH) have a lower critical opening size D crit
<(PPD)> 0.41 mm, and therefore, a significantly higher
fraction of the design space is free of clogging and drainage
limitations. As a result, meshes that were previously unusable
with thinner fibers (higher R*) and higher shade coefficients
closer to the optimal value can now be employed for fog
harvesting. These finer meshes are predicted to have much
higher fog collection efficiencies ([eta] 12%), provided a
suitable low hysteresis coating is applied.
[0093] In FIG. 9B, the role of surface coating alone for a
particular mesh geometry is examined. The measured efficiency
increases from [eta] 2% (for a woven mesh that is dip-coated
to achieve the same surface wettability characteristics as the
polyolefin Raschel mesh) to [eta] 5% for a POSS-PEMA
dip-coated woven mesh (PPD, ?) with the same radius R 445
[mu]m and the same shade coefficient SC 0.5 (D* 3.5). However,
the fog-collecting efficiency of a sprayed texture (PPS,
[image])) and liquid-impregnated surface (KO, [image]) woven
mesh (again with the same R 445 [mu]m) do not perform as well
as the dip-coated mesh due to the predominance of
re-entrainment and clogging. Interaction with water droplets
impacting and sliding along the Krytox-impregnated 'SLIPS
surface' results in a progressive loss of the nonvolatile
impregnating liquid (see FIG. 13 for details). This leads to
increasing contact angle hysteresis and the mesh openings
start to clog. Optimization studies focused on the dip-coated
surfaces as they tend to be stable over much longer
timescales.
[0094] In FIG. 9C, the fog-collecting efficiency is plotted
against the wire radius, keeping the weave constant (D* 3.5)
with the same surface coating (dip-coated with POSS-PEMA). The
theoretical fog collecting efficiency [eta](R,D) given by the
analysis in eq. (1) above (broken line) provides a good
estimate of the observed trends. The measured efficiency
increases monotonically from 5% to 10% as the fiber radius
decreases from R 445 [mu]m to R 172 [mu]m for the first 4
meshes (?, -, -, and -) that lie in the region of the design
chart where clogging is not a limiting factor. However, the
finest mesh (R 127 [mu]m, [image]) is located inside the
hysteresis-limited region (with mesh spacing D<D crit=r c),
and clogging once again prohibits any further increase in the
efficiency. A mesh located in the clogging-prone region of the
design space still collects an appreciable amount of fog, but
its efficiency could be improved still further by reducing the
clogging constraint imposed by eq.(3) (i.e., lowering the
slope of the bounding line for D crit, via lower values of
CAH).
[0095] The maximum fog harvesting efficiency observed in the
experiments is [eta]=9.9+-0.5% (N=3) for a fine POSS-PEMA
dipcoated mesh with close to optimal weave (R 172 [mu]m, D*
3.5, CAH 0.06, -). In FIG. 9D, the time evolution of the fog
harvesting performance for the optimal mesh and the Raschel
mesh is compared over many hours. The optimized wire mesh
collects water at a faster rate and also reaches steady state
faster than the Raschel mesh. Thus, by an appropriate choice
of the surface texture and coating chemistry, the fog
harvesting efficiency for representative fog conditions ([nu]
0=2 m/s, r fog=3 [mu]m) has been enhanced approximately
five-fold.
[0096] A comparison of theoretical fog collection efficiency
across many fog conditions (see below) indicates that the fog
harvesting efficiency for the POSS-PEMA dipcoated wire mesh (R
172 [mu]m, -) is also more robust than the conventional
Raschel mesh to changes in fog conditions (1<=r fog<=40
[mu]m, <=[nu] 0<=10 m/s). As a result, fog harvesting
technology based on POSS-PEMA dipcoated woven meshes may be
deployable in many regions of the world where the size and
velocity of fog droplets are not suitable for traditional
Raschel meshes to work well. The performance of these
rapidly-draining woven meshes are less susceptible to daily or
seasonal changes of wind speed and direction, or temperature.
Optimally-engineered surfaces can work effectively in foggy
conditions for longer periods of time, and subsequently
produce much more water; even in a mild fog with droplet
radius of 3 [mu]m, wind speed of 2 m/s and liquid water
content of 0.1 g/m <3>, the optimal mesh surface (R 172
[mu]m, -) can collect approximately two liters of water
through an area of 1 m <2 >per day. Using literature
values for conditions in a typical Chilean fog environment
(see, for example, Schemenauer R S, Joe P I (1989) The
collection efficiency of a massive fog collector. Atmos. Res.
24:53-69, which is incorporated by reference in its entirety)
and the design framework described here, the amount of water
that can be collected using the optimal fog harvesting mesh
can be estimated. Typical Chilean fog conditions are
characterized by a larger droplet size and higher wind
velocity (r fog 13 [mu]m, [nu] 0 6 m/s) and in such inertial
conditions, the collection rate is predicted to be as large as
twelve liters of water through an area of 1 m <2 >per
day, assuming a liquid water content of 0.7 g/m <3>.
From such calculations it is clear that understanding the
enabling roles of surface wettability in conjunction with the
physical characteristics of the woven mesh geometry (i.e.
fiber radius and shade coefficient) expands the accessible fog
harvesting design space as well as future geographic
opportunities for deploying fog harvesting technology.
[0097] Using the literature values for conditions in a typical
fog environment in Chile, and the design framework presented
above, the amounts of water that could be collected using a
Raschel mesh and the optimal fog harvesting mesh were
predicted. The results for fog environments in Chile and the
lab were summarized in Table 1. From the last column of Table
1, it was clear that the optimal wire mesh was more efficient
in collecting fog than a double layer Raschel mesh. Also, the
Chilean fog conditions had a higher wind velocity and larger
droplet size; in other words, the fog droplets had more
inertia. In such inertial conditions, the woven mesh performed
marginally better than the Raschel mesh (about 10% better than
the best case scenario). However, under less inertial fog
conditions (like those used in the lab), the woven meshes
provided a significant advantage over the Raschel meshes. The
relative advantage of this design framework was clarified
further by comparing theoretical fog harvesting efficiencies
of the Raschel mesh with optimally chosen woven mesh under a
wide range of wind velocities and droplet radii, as plotted in
FIG. 10.
[0098] As the wind velocity and droplet size increased from
condition 1 to condition 6 (see FIG. 10), the fog became more
inertial and theoretical collection efficiencies increased
both for the Raschel mesh (indicated bars in FIG. 10) and the
woven meshes (indicated bars in FIG. 10). Under all six fog
conditions, the woven mesh was expected to perform
significantly better than the Raschel mesh. However, the main
advantage of the design framework was evident under
non-inertial (light) fog conditions, i.e., conditions 1 and 2.
The fog harvesting efficiency for the woven mesh was more
robust to changes in fog conditions, so it did not deteriorate
to the same extent as the Raschel mesh. As a result, the fog
harvesting with woven meshes can be effectively used in a more
places, e.g., where fog might not be dense enough for the
Raschel meshes to work well. Nor are fog conditions at any one
place constant; rather, they are expected to change based on
the time of the day, temperature, wind patterns, season, and
other factors. Accordingly, a permeable surface having
properties chosen for the local conditions can produce more
water than a generic surface. For example, condition 6 might
be representative of Chilean fog at the peak of the winter.
However, a woven mesh will work even when the fog is not as
thick, as in the Chilean summer, when the conditions are
similar to conditions 3 or 4. Higher efficiency at all fog
conditions will help to collect more water, at more places,
and over a longer part of the year, all of which benefits the
economics of fog harvesting.
[0099] Derivation of critical droplet radii r e and r c. Two
criteria for the critical radius of a droplet can be derived
by equating the drag force acting on a drop to the adhesion
force and secondly by equating gravitational force and pinning
force based on contact angle hysteresis. FIG. 11 shows a
schematic diagram of water droplets on a cylindrical mesh
filament (cross-sectional view) and on one grid element of a
woven mesh (top view). Both droplets are assumed to be
spherical caps with the algebraic average of contact angles
[theta]=[theta] adv+[theta] rec/2.
[0100] The first critical droplet radius r e for
re-entrainment of droplets into the airstream is a threshold
value of the liquid droplet radius at which the aerodynamic
drag force (F drag) and the surface adhesion force (F
adhesion) acting on a water droplet ( FIG. 11A) are balanced.
To calculate the critical droplet radius r e the drag force
exerted by wind on a fog droplet and the force of adhesion on
the droplet exerted by the mesh were equate. First the drag
force is obtained from the following equation,
[0000]
F drag=[1/2][rho] air[nu] 0 <2> C D A P (eq. s1-1)
[0101] where [rho] air is the density of air, [nu] 0 is the
velocity of fog stream, C D is the drag coefficient (which
typically ranges from 0.4 to 1 for a bluff body such as a
droplet at Reynolds numbers of Re~10 <3>) and A P is the
projected area normal to the direction of fog flow.
[0102] The projected area can be obtained by a simple
trigonometric formula.
[0000]
A P =r drop <2>([theta]-sin [theta] cos [theta])/sin
<2>[theta] (eq. s1-2)
[0103] where [theta] is the algebraic average of advancing and
receding contact angles ([theta] adv+[theta] rec)/2.
[0104] On the other hand, the adhesion force on the liquid
droplet is calculated in the following way-
[0000]
F adhesion =L l[gamma] LV(1+cos [theta] rec) (eq. s1-3)
[0105] where L l is the characteristic length of the droplet
(2[pi]r drop) and [gamma] LV is the surface tension of water.
Finally, by equating eqs s1-1 and s1-3 and substituting eq.
s1-2 into eq. s1-1, the following equation for the critical
radius r e is obtained.
[0000]
r e=4[pi] [gamma] LV sin <2>[theta](1+cos [theta]
rec)/[rho] air[nu] 0 <2> C D([theta]-sin [theta] cos
[theta]) (eq. s1-4)
[0106] If the droplet is not a spherical cap this will only
change the precise form of f ([theta]) in eq. s1-4, but not
the fundamental scaling or magnitude of the expression
[0000]
r e([gamma] LV/[rho] air[nu] 0 <2> C D) f([theta]).
[0107] Similar expressions have been developed by Milne and
Amirfazli for sheared droplets of water on airfoil surfaces.
See Milne A J B, Amirfazli A (2009) Drop shedding by shear
flow for hydrophilic to super-hydrophobic surfaces. Langmuir
25:14155-14164, which is incorporated by reference in its
entirety.
[0108] The critical droplet radius r c for drainage of
droplets from the mesh is found by balancing gravitational
force (F grav) and pinning force (F CAH) acting on a water
droplet that covers a single grid of the mesh ( FIG. 11) is
calculated here.
[0109] The gravitational force is expressed as-
[0000]
F grav=[rho] water gV (eq. s1-5)
[0110] where [rho] water is the density of water, g is the
constant of gravity, and V is the volume of the spherical cap
shaped water droplet. Using simple trigonometric algebra,
[0000]
V=[pi]/6 h(3 r drop <2> +h <2>) (eq. s1-6)
[0111] where h can be also expressed as h=r drop (1-cos
[theta])/sin [theta].
[0112] To calculate the critical radius of the water droplet
that causes clogging on a mesh surface, the radius of a
hemispherical droplet that covers a single square grid of mesh
(or r drop=D). In this case, the pinning force can be
expressed as
[0000]
F CAH 2 r drop[gamma] LV (cos [theta] rec-cos [theta] adv)
(eq. s1-7)
[0113] If the pinning force is smaller than the gravitational
force, the droplet will be drained off the mesh, leading to a
fresh unoccupied mesh grid for the next fog deposition cycle.
Therefore, by equating eqs. s1-5 and s1-7, the critical radius
at which clogging occurs.
[0000] [mathematical formula]
[0114] Once again, if the droplet is not a hemispherical cap
this will change the precise form of eq. s1-8 but not the
fundamental scaling r c [square root of]{square root over
([gamma]LV/[rho]waterg)}[square root of]{square root over
(CAH)}, where CAH=cos [theta] rec-cos [theta] adv.
[0115] Table 1 shows The values of the receding contact angle,
contact angle hysteresis, and critical radii r e and r c for
each surface coating, with the laboratory fog condition used
in the humidity chamber experiment ([nu] 0 2 m/s) and a
representative value of C D=0.7. For this airstream velocity,
all four of the coatings show r c<<r e. As a result of
the large values of [theta] rec (which lead to easy drop
roll-off and low adhesion forces), the POSS-PEMA spraycoating
(denoted PPS) shows a smaller value of r e than the half
spacing D of most of the woven meshes used in the fog
collection experiments, which explains the low collection
efficiency value measured experimentally (because of
re-entrainment of deposited water droplets back into the
convected air stream). The liquid-impregnated surfaces
initially exhibit a critical droplet drainage radius (r c)
that is similar to the POSS-PEMA dipcoating (denoted PPD), but
after a short period of operation this ultimately transitions
to a value that is greater than the original polyolefin
material (denoted PO). A micrograph of the POSS-PEMA
spraycoated mesh is shown FIG. 12.
[0000]
TABLE 1
[0116] Time evolution of the performance of liquid-impregnated
textured surfaces and schematic diagram of experimental setup
for fog collection efficiency measurement
[0117] Experimental details of the preparation of these
surfaces are described in the Methods section. Repeated
interaction with successive water droplets impacting and
sliding along the liquid impregnated textured mesh surface
(denoted by the label KO in FIG. 3E, 8B) results in a
progressive loss of the nonvolatile low surface tension liquid
that is impregnated into the microtecture, as shown in FIG.
13, which shows the evolution of the advancing (dark line) and
receding (light line) contact angles of water droplets on the
liquid-impregnated surfaces. The contact angles were measured
every three minutes while water droplets were released from a
height of 10 mm (corresponding to impact velocity [nu] 0.44
m/s; We 6.7) from the inclined surfaces (45[deg.]) with the
flow rate of 3.3 ml/min (corresponding to 70 impacts per
minute). This leads to a steady increase in the contact angle
hysteresis (CAH) over a period of 5 mins and the mesh openings
of the KO-impregnated mesh subsequently start to clog.