Jia-Kun Chen1, Rong Fung Huang. 1. Graduate Institute of Applied Science and Technology, National Taiwan University of Science and Technology, Taiwan.
Abstract
A novel design of range hood, which was termed the inclined quad-vortex (IQV) range hood, was examined for its flow and containment leakage characteristics under the influence of a plate sweeping across the hood face. A flow visualization technique was used to unveil the flow behavior. Three characteristic flow modes were observed: convex, straight, and concave modes. A tracer gas detection method using sulfur hexafluoride (SF6) was employed to measure the containment leakage levels. The results were compared with the test data reported previously in the literature for a conventional range hood and an inclined air curtain (IAC) range hood. The leakage SF6 concentration of the IQV range hood under the influence of the plate sweeping was 0.039 ppm at a suction flow rate of 9.4 m(3)/min. The leakage concentration of the conventional range hood was 0.768 ppm at a suction flow rate of 15.0 m(3)/min. For the IAC range hood, the leakage concentration was 0.326 ppm at a suction flow rate of 10.9 m(3)/min. The IQV range hood presented a significantly lower leakage level at a smaller suction flow rate than the conventional and IAC range hoods due to its aerodynamic design for flow behavior.
A novel design of range hood, which was termed the inclined quad-vortex (IQV) range hood, was examined for its flow and containment leakage characteristics under the influence of a plate sweeping across the hood face. A flow visualization technique was used to unveil the flow behavior. Three characteristic flow modes were observed: convex, straight, and concave modes. A tracer gas detection method using sulfur hexafluoride (SF6) was employed to measure the containment leakage levels. The results were compared with the test data reported previously in the literature for a conventional range hood and an inclined air curtain (IAC) range hood. The leakage SF6 concentration of the IQV range hood under the influence of the plate sweeping was 0.039 ppm at a suction flow rate of 9.4 m(3)/min. The leakage concentration of the conventional range hood was 0.768 ppm at a suction flow rate of 15.0 m(3)/min. For the IAC range hood, the leakage concentration was 0.326 ppm at a suction flow rate of 10.9 m(3)/min. The IQV range hood presented a significantly lower leakage level at a smaller suction flow rate than the conventional and IAC range hoods due to its aerodynamic design for flow behavior.
Cooking produces air pollutants, moisture, and odors1, 2). Residential gas cooking
burners also emit air pollutants3, 4) at rates that can lead to indoor
concentrations exceeding health-based standards5). Removal of these contaminants is important for maintaining
acceptable indoor air quality in homes. When gas cooking is used in kitchens, the cooking
procedure generates various pollutants, like carbon monoxide, oxides of nitrogen (NOx), and
particulate matter (PM). Many different types of appliances are used for heating, cooking,
and supplying hot water6,7,8). Previous studies
have reported indoor air pollution from various heating systems9,10,11).Range hoods are the primary ventilation device for exhausting the contaminants produced in
kitchens. Conventional range hoods basically have one or two circular holes fitted with fans
and ducts to exhaust contaminants. Previous studies, by either measuring or modeling, have
reported the capture efficiencies of various conventional range hoods12,13,14,15). Hunt and
Ingham16) presented a mathematical model
for the air flow pattern of an exhaust ventilation hood. Abanto and Marcelo17) reported the flow field around a range
hood obtained by using a computational fluid dynamics code. Recently, Chen et
al.18) and Huang et
al.19) used the laser-assisted
flow visualization technique and SF6 (sulfur hexafluoride) tracer gas detection
method to determine the correlation between the flow field characteristics and the
containment leakage levels of the conventional range hood. They found that the leakage of
the conventional range hood is primarily induced by the inappropriate aerodynamic design of
the hood. The hood must be installed at a distance about six to eight suction opening
diameters from the counter top in order to allow for the cook’s hand movements, but this
produces an insufficient upward flow velocity at the pollutant generation altitude to carry
the fumes. Influences of cross draughts, cook presence, and cook’s movements are detrimental
to the performance of conventional range hoods. Reducing oil fume leakage levels by
increasing the suction flow rate is a straight forward method but may not be the best to
solve the problem because a drastic increase in the suction flow rate would be accompanied
by significant energy consumption and a higher noise level. Huang et
al.20, 21) represented an inclined air-curtain (IAC) range hood which
was designed by combining a suction slot installed at the hood and a plane jet arranged at
the front part of the countertop to form a backward-inclined push-pull air curtain. They
showed that the IAC range hood has higher performance than the conventional range hoods
under both the static and dynamic tests. However, the leakages were still not negligibly
small.The inclined quad-vortex (IQV) range hood has been shown to present high containment
performance due to its special aerodynamic design. In order to compare the performance
characteristics among the conventional, IAC, and IQV range hoods, we performed experimental
studies on the robustness of the IQV range hood and compared the results with the published
experimental data of the conventional and IAC hoods. The sweeping plate method, which was
referred to in the robustness test methodology for the chemical fume hood proposed by the
European Committee for Standardization22),
was used. The laser-assisted smoke flow visualization technique was used to determine the
qualitative flow behaviors and the tracer gas detection method was employed to quantify the
leakage levels of the hood.
Materials and Methods
IQV range hood and test rig
The configurations of the IQV range hood used for the experiments are shown in Fig. 1. The hood consisted of three features that are different from the conventional
range hoods. First, a suction slot (60 cm × 2 cm) was located at the bottom face of the
hood. Second, two jets provided by cross flow fans blowing down through the slots (30 cm ×
2 cm) were arranged at the bottom face of the hood. Third, two side plates (40 cm× 55 cm)
were installed at the lateral ends of the hood. The hood had a depth of 50 cm and a width
of W, which is variable from 90 cm to 120 cm. The hood was installed at a
height of 60 cm above the countertop. An air box was installed on the hood to accumulate
the air and oil fumes drawn from the suction slot and to exhaust the mixture to the
outdoors. Half circular arcs with a radius of 2.5 cm were installed at the front edges of
the hood and the side plates to guide the flow. The gap between the bottom edges of the
side plates and the countertop was 5 cm. The distance between the front edge of the
countertop and the front edges of the side plates was 10 cm.
Fig. 1.
Configurations of IQV range hood. (a) top view, (b) isometric view.
Configurations of IQV range hood. (a) top view, (b) isometric view.The countertop (128 cm in width and 60 cm in depth) had a height of 86 cm from the ground
level. Two electric heaters with hot plates on their tops were imbedded under the
countertop with 7 cm protruding upward. Circular oil pans were placed on the hot plates of
the electric heaters. The diameter and height of the oil pans were 28 cm and 6 cm,
respectively.
Flow visualization
The laser-assisted smoke flow visualization technique was used to reveal the patterns of
the oil mist in the flow. Mineral oil was poured into the oil pans and heated to 230 °C by
the hot plates. The smoke (i.e., the oil mists) was generated and rose up from the oil
pans. The diameter of the oil mist particles, measured by a particle analyzer (Model
2600C, Malvern Instrument Ltd., Malvern, Worcestershire, UK), was 1.7 ± 0.2 μm. A green
laser beam was generated from a 100 mW Nd-YAG laser. The wavelength of the laser beam was
532 nm. The laser beam was passed through a homemade laser-light expander to form a
laser-light sheet. The thickness of the laser-light sheet was about 0.5 mm. The oil mists
scattered the laser light to describe the flow pattern in the flow field of the IQV range
hood. A charge-coupled device (CCD) camera was used to record the images of the oil mists
in the plane of the laser-light sheet. The framing rate and the exposure time were 30 fps
and 1/60 s, respectively.
Robustness test
Figure 2 shows the configurations of the flat-plate sweeping experiment for the robustness
test. The sweeping plate method was based on the robustness test methodology proposed by
the European Committee for Standardization22). This method was used to simulate the walk-by motion of people
across the front face of a pollutant removing device. A rectangular flat plate was
installed upright on a traversing mechanism. The dimensions of the flat plate were 2 cm
(thickness) × 40 cm (width) × 150 cm (height). The plate moved from the right to the left
at a velocity of 1 m/s across the front area of the range hood. The distance between the
inner edge of the flat plate and the front edge of the countertop was denoted as
L. Two cases of the distance L were tested in the
study: 40 cm and 80 cm. During the experiment for L = 40 cm, as shown in
Fig. 2 (a), no mannequin was installed in
front of the countertop. For the experiment at L = 80 cm, a mannequin was
installed in front of the countertop, as shown in Fig.
2 (b). The height and shoulder width of the mannequin were 158 cm and 43 cm,
respectively. The distance between the chest of the mannequin and the front edge of the
range hood was 15 cm.
Fig. 2.
Arrangement of robustness tests. (a) L = 40 cm, (b) L = 80 cm.
Arrangement of robustness tests. (a) L = 40 cm, (b) L = 80 cm.
Tracer gas releasing and sampling
The tracer gas (SF6) was released from two home-made gas release rings (Fig. 3 (a)) that were made of copper tubes with an outer diameter of 0.4 cm. In total, 20
small holes with diameters of 0.2 cm were drilled along each gas release ring to eject
SF6 gas. A pressure gauge, a needle valve, and a rotameter calibrated with
SF6 gas were attached to a piping system to control the flow rate of
SF6. The flow rate of SF6 (QSF6)
released from each of the gas release rings was 3 L/min. The exit velocity of the
SF6 from the ejecting holes was thus about 0.8 m/s. When the experiments were
conducted, the gas release rings were placed on the hot plates of the electric heaters in
order to receive the heat and buoyancy from the hot plates.
Fig. 3.
Tracer gas releasing ring and deployments of sampling probes. (a) gas releasing ring, (b) suction probe deployment in front plane, (c) suction
probe deployment in left lateral plane, (d) sampling probe at breathing zone of a
mannequin.
Tracer gas releasing ring and deployments of sampling probes. (a) gas releasing ring, (b) suction probe deployment in front plane, (c) suction
probe deployment in left lateral plane, (d) sampling probe at breathing zone of a
mannequin.Twenty one sampling probes made of cylindrical stainless tubes were deployed in a plane
10 cm in front of the hood face (Fig. 3 (b)) and
six suction probes were deployed in the left lateral plane of the hood (Fig. 3 (c)). The length and inner diameter of the
sampling probes were 10 cm and 1.3 cm, respectively. The suction velocity at the inlet of
each sampling probe was adjusted to a low value, about 3 cm/s, in order not to
significantly disturb the flow patterns. The sampling probes were connected to the inlets
of a mixing chamber by Teflon tubes. The detector probe was affixed to the outlet of the
mixing chamber. The detection probe was connected to a Miran SapphIReTM
Portable Ambient Analyzer (Thermo Electron Corp., Franklin, Mass.) via a Teflon tube. The
Miran SapphIReTM analyzer was used to measure the concentration of the tracer
gas. The resolution of the Miran SapphIReTM analyzer used to measure the
concentration of the tracer gas SF6 was 0.001 ppm. The sampling rate was 20
readings per second.During the experiment for L = 80 cm, an additional sampling probe was
installed at the breathing zone of the mannequin. The inlet velocity of the sampling probe
was 1 m/s. The tracer gas concentration around the breathing zone of the mannequin was
independently measured—the sampled mixture was directly delivered to a Miran
SapphIReTM analyzer through a Teflon pipe without pre-mixing with the mixture
sampled by the probes shown in Fig. 3 (b) and
(c).
Results and Discussion
Flow behavior
Figure 4 shows the flow pattern revealed by oil mists in the horizontal plane
z = 20 cm. The suction velocity at the inlet of the suction slot is
Vs = 12 m/s and the blowing velocity at the exit of the
down-blowing jets is Vb = 1.9 m/s. Oil mists are concentrated
in four groups above the oil pans. In the recorded movies that are not shown here, the
motion of the oil mists clearly show four counter-rotating vortices-neighboring vortices
present a counter-rotating motion, as indicated by the arrows in Fig. 4. The oil mists are coherently contained in the rotating
vortices so that the dispersion of the oil mists toward the areas near the side plates,
rear corners, and hood face is not observed. The pressure in a vortex would be lower than
the pressure of its surrounding atmosphere due to the rotating motion of the flow23). The pressure difference increases with
an increasing the rotation rate of the vortex. By observing the movies recorded in the
study, the rotation rate of the vortices increases with the increasing the suction
velocity Vs. As the suction velocity is increased beyond about
8 m/s, the pressure difference between the core regions of the vortices and the
surrounding atmosphere becomes large enough to attract and contain the oil mists in the
vortices. The scenario in which oil mists are concentrated in four vortices, as shown in
Fig. 4, is thus observed. At the suction
velocities smaller than or equal to 8 m/s, four vortical flow motions are still observable
(although not very coherent), but some oil mists are dispersed out of the vortices.
Fig. 4.
Flow pattern in horizontal plane. z = 20 cm. Vs = 12 m/s and
Vb = 1.9 m/s.
Flow pattern in horizontal plane. z = 20 cm. Vs = 12 m/s and
Vb = 1.9 m/s.In order to better understand the vortex system induced by the IQV range hood, the hand
sketch of the topological flow pattern corresponding to Fig. 4 is analyzed and shown in Fig.
5. We obtained the topological sketch by employing the critical point theory,
developed by Lighthill24) and Perry and
Steiner25). This technique can help to
reveal features in the flow field. As shown in Fig.
5, the critical points consist of six ‘three-way saddles’
(S1′ −
S6′), four ‘four-way saddles’
(S1 − S4), and six full nodes
(N1 − N6). From the topological
point of view, the boundary layers near the leading edges of the side plates separate at
the three-way saddles S1′ and
S4′ then reattach to the downstream parts
of the side plates at the three-way saddles
S2′ and
S3′ to form the recirculation bubbles
centered at the nodes N1 and N4.
The counter-rotating vortices centered at the nodes N2,
N3, N5, and
N6 and the associated four-way saddles
S1, S2,
S3, and S4 are formed according
to the topological rule that the neighboring separatrices (or streamlines) should not go
in opposite directions. For instance, there are alleyways between neighboring vortices in
Fig. 5. In these alleyways between neighboring
vortices, the flows all go rearwards. The vortex N3 rotates
clockwise, which will induce a flow in the opposite direction in the alleyway around the
symmetry plane. A saddle point S2, therefore, must exist so
that the vortex and the flow in the alleyway can coexist. The principle of this example
applies to the whole flow field so that the complex flow field in Fig. 4 is formed. The number of nodes and saddles shown in Fig. 5 satisfies the topological rule that found by
Hunt et al26).
Fig. 5.
Topological flow pattern corresponding to Fig.
4.
Topological flow pattern corresponding to Fig.
4.Figure 6 shows the images of oil mists in the vertical planes x = 0 and
−20 cm at Vs = 8 m/s and Vb = 0.
In the symmetry plane x = 0 (Fig. 6
(a)), oil mists incline rearward as they rise toward the suction slot. Two
effects may induce the rearward inclination of oil mists—the rearward offset of the
suction slot and the Coanda effect27).
In the vertical plane across the center of the left oil pan x = −20 cm
(Fig. 6 (b)), oil mists rising from the front
edge of the left oil pan incline rearward at a large inclination angle. It is noted that
in both Fig. 6 (a) and (b), oil mists disperse
to the area around the front edge of the hood bottom face and form recirculation bubbles.
This recirculation bubble would induce a danger of oil mist diffusion and dispersion. The
oil mists contained in the recirculation bubble located near the front edge of the hood
may disperse if a cook walks by the hood face or stands in front of the hood.
Fig. 6.
Oil flow images in vertical planes. (a) x = 0, (b) x = −20 cm.
Vs = 8 m/s, Vb = 0.
Oil flow images in vertical planes. (a) x = 0, (b) x = −20 cm.
Vs = 8 m/s, Vb = 0.Figure 7 shows the images of oil mists in the vertical planes x = 0 and
−20 cm at the suction velocity Vs = 8 m/s and
Vb = 1.9 m/s. In the symmetry plane x = 0
(Fig. 7 (a)), the recirculation bubble shown
in Fig. 6 (a) disappears. In the vertical plane
x = −20 cm, as shown in Fig. 7
(b), the recirculation bubble is retracted rearward and is located behind the
down-blowing jet because the down-blowing jet forms an “air curtain” and isolates the oil
mists from dispersing outward.
Fig. 7.
Oil flow images in vertical planes. (a) x = 0, (b) x = −20 cm.
Vs = 8 m/s, Vb = 1.9
m/s.
Oil flow images in vertical planes. (a) x = 0, (b) x = −20 cm.
Vs = 8 m/s, Vb = 1.9
m/s.Figure 8 shows three characteristic flow modes appearing in the vertical plane. At
Vs = 8 m/s (Fig. 8
(a)), the rearward inclined oil mists present a convex scenario because the
suction velocity is not large enough. At the suction velocity
Vs = 10 m/s (Fig. 8
(b)), the front edge of the oil mists reveals a straight mode. At
Vs = 12 m/s (Fig. 8
(c)), the rearward inclined oil mists present the concave mode because the Coanda
effect is enhanced under this condition. The convex mode appears at
Vs ≤ 8 m/s. The straight mode is observed in the range 8
m/s12
m/s, the concave mode presents. As mentioned previously, at Vs
≤ 8 m/s we may observe four “loose” vortical flow motions in the horizontal plane with
dispersion of oil mists out of the vortices. By comparing this flow mode with the
characteristic flow modes appearing in the vertical plane shown in Fig. 8, we may conclude that operating the suction velocity in the
range Vs ≤ 8 m/s is not enough to set up a strong
rearward-inclined vortical flow structured to coherently contain the oil mists in the
vortices.
Fig. 8.
Characteristic flow modes in vertical plane. x = 0. (a) convex mode, Vs = 8 m/s;
(b) straight mode, Vs = 10 m/s; (c) concave mode,
Vs = 12 m/s. Vb = 1.9
m/s.
Characteristic flow modes in vertical plane. x = 0. (a) convex mode, Vs = 8 m/s;
(b) straight mode, Vs = 10 m/s; (c) concave mode,
Vs = 12 m/s. Vb = 1.9
m/s.
Tracer gas leakage concentrations after plate sweeping
Table 1 shows the robustness test results at L = 40 cm by using the
plate-sweeping method (Fig. 2). For comparison,
the data for the IAC and conventional range hoods were quoted from Huang et
al20, 21). The conventional range hood has a very low robustness. For
instance, operating at Qs = 10.5 m3/min, the
leakage concentration of the conventional range hood is drastically large—1.251 ppm. At
Qs = 12 m3/min, the leakage concentration of the
conventional range hood is 0.618 ppm while the IQV range hood presents a similar leakage
level of 0.601 ppm at a significantly smaller suction flow rate
Qs = 7.2 m3/min. Operating at
Qs = 9.4 m3/min, the IQV range hood presents a
negligibly small leakage concentration value of 0.039 ppm, which is only one-twentieth
that of the conventional range hood operating at Qs = 15
m3/min and one-eighth of the IAC range hood operating at
Qs = 10.9 m3/min. Apparently, the IQV range hood
presents the highest robustness and lowest energy consumption among the three types of
range hoods.
Table 1.
Robustness test results of IQV, IAC, and conventional range hoods
Vs(m/s)
Qs(m3/min)
IQV
IAC(Huang et al.21))
Conventional(Huang et al.20))
Cave (ppm)
8
5.8
0.761
10
7.2
0.601
12
8.6
0.291
13
9.4
0.039
10.5
1.251
10.9
0.326
12.0
0.618
15.0
0.768
L = 40 cm.
L = 40 cm.Table 2 shows the robustness test results at L = 80 cm. A mannequin
is standing in front of the counter for this experiment. The test data in Table 2 present negligibly small leakage
concentrations under all conditions, revealing two facts. First, the presence of the
mannequin does not induce containment leakage. According to Huang et
al.19), the presence of a
mannequin in front of the conventional range hood would induce a recirculation bubble
around the mannequin chest and therefore lead to containment leakage. The leakage
concentrations measured at the breathing zone of a mannequin standing in front of a
conventional range hood are 17.0 ppm at Qs = 10.5
m3/min and 20.5 ppm at Qs = 15 m3/min.
The leakage concentrations measured at the breathing zone of a mannequin standing in front
of an IAC range hood are 0.3 ppm at Qs = 10.1
m3/min and 0.1 ppm at Qs = 11.8 m3/min.
In Table 2, the leakage concentrations of the
IQV range hood measured at the breathing zone are all negligibly small. This can be
explained by the rearward inclination of the vortical flows. The rearward inclined
vortical flows that contain the oil mists are located far from the recirculation bubble
induced by the mannequin presence, and therefore the entrainment and dispersion effects
are weakened. Second, the plate sweeping across the back area of the mannequin does not
induce containment leakage. This happens because the wake flow induced by the plate is
generally not wide enough to reach the hood face situated at 80 cm away.
Table 2.
Robustness test results of IQV range hood at various hood width
Vs(m/s)
Qs(m3/min)
Normal probedeployment
Breathing zoneof mannequin
W (cm)
90
100
120
90
100
120
Cave (ppm)
8
5.8
<0.001
<0.001
0.002
<0.001
0.001
<0.001
10
7.2
<0.001
<0.001
<0.001
<0.001
0.002
<0.001
12
8.6
<0.001
<0.001
0.001
<0.001
0.001
<0.001
13
9.4
<0.001
<0.001
<0.001
<0.001
<0.001
0.001
L = 80 cm, W = 90~120 cm. Mannequin standing in
front of the hood.
L = 80 cm, W = 90~120 cm. Mannequin standing in
front of the hood.
Conclusions
The IQV range hood employed a narrow suction slot and two side plates to generate a flow
field containing four rearward-inclined counter rotating vortices. The counter rotating
vortical flows were formed applying topological reasoning to the flow dynamics. The boundary
layer separations occurring at the leading edges of the side plates induced two corner
vortices. The corner vortices subsequently induced two outer vortices. These two outer
vortices together with the central rearward-going flow further induced two counter rotating
inner vortices. As a result of the low pressure inside the vortical flows, the oil mists
were coherently contained in the inner and outer counter rotating vortices at the suction
velocities greater than about 8 m/s. The vortical flows rose up with spiral motions and
inclined rearward owing to the effects induced by the rearward offset of the suction slot
and Coanda effect. Three characteristic flow modes were observed: convex, straight, and
concave. The convex flow mode corresponded to a suction velocity of less than or equal to 8
m/s that the oil mists may disperse out of the counter rotating vortices. The robustness
tests performed by the sweeping plate method showed that the IQV range hood presented a
negligibly small leakage concentration value which is drastically lower than those of the
conventional and IAC range hoods. The IQV range hood presented the highest robustness and
lowest energy consumption among the three types of range hoods. This high performance may be
explained by the rearward inclination of the vortical flows created by the configurations of
the IQV range hood.