BACKGROUND OF THE INVENTION
[0001] The present invention relates to a yarn cooler configured to cool yarns spun out
downward from a spinneret.
[0002] There have been known yarn coolers each configured to cool yarns spun out from a
spinneret, such as a yarn cooler disclosed in Patent Literature 1 (Japanese Unexamined
Patent Publication No.
2008-231607) . In this yarn cooler, a buffer chamber in which cooling air flows upward is formed
around a cylindrical member structuring a peripheral wall of a yarn running space,
and yarns are cooled by the cooling air entering from the buffer chamber to the yarn
running space. Now, if there is a time variation in the flow of the cooling air entering
into the yarn running space, unevenness in terms of cooling may be caused in the yarns,
leading to deterioration in quality of the yarns. In this regard, it is important
to restrain the time variation in the flow of the cooling air. To deal with this,
Patent Literature 1 discloses that one or more porous plates (flow adjustment members)
are provided in the buffer chamber. Particularly in FIG. 3 (2), there is disclosed
a multiple-stage configuration in which a plurality of porous plates are provided.
SUMMARY OF THE INVENTION
[0003] However, Patent Literature 1 totally fails to disclose how the porous plates are
designed in terms of their properties in such a multiple-plate configuration where
the plurality of porous plates are provided. Further, the above literature merely
describes the advantageous effect brought about by the multiple-plate configuration
as follows: even though the porosity of the porous plates is somewhat increased, the
effect of flow adjustment is substantially equivalent to that in a single-plate configuration
where a single porous plate is provided; and thus clogging in the porous plates is
prevented. That is to say, the technique of the Patent Literature 1 is not intended
to actively improve the effect of flow adjustment by the multiple-plate configuration,
as compared to that in the single-plate configuration.
[0004] An object of the present invention is to actively improve the effect of flow adjustment
in a yarn cooler including a plurality of porous plates, as compared with the configuration
of a single porous plate, and to effectively restrain a time variation in the flow
of cooling air entering into a yarn running space.
[0005] To achieve the above obj ect, the present invention provides a yarn cooler configured
to cool a yarn spun out downward from a spinneret, the yarn cooler including: a cooling
cylinder provided below the spinneret to be opposed to the spinneret, the cooling
cylinder including therein a yarn running space through which the yarn is runnable,
an upper peripheral wall of the yarn running space forming a flow adjustment section
configured to adjust the flow of cooling air entering into the yarn running space
while a lower peripheral wall of the yarn running space forming a impassable section
configured to prevent the cooling air from entering into the yarn running space; an
accommodation box accommodating the cooling cylinder, to which box the cooling air
is supplied through a supply portion provided at a lower portion of the accommodation
box; a first porous plate disposed in a supply passage where the cooling air supplied
through the supply portion flows upward along the impassable section, the first porous
plate being configured to adjust the flow of the cooling air; and a second porous
plate disposed above and apart from the first porous plate in the supply passage,
the second porous plate being configured to further adjust the flow of the cooling
air having been adjusted by the first porous plate, wherein the thickness ratio of
the second porous plate is smaller than the thickness ratio of the first porous plate.
[0006] In this arrangement, the flow of the cooling air supplied through the supply portion
of the accommodation box is first adjusted by the first porous plate and then adjusted
by the second porous plate, and thereafter, the flow of the cooling air enters into
the yarn running space through the flow adjustment section of the cooling cylinder.
By designing the porous plates so that the thickness ratio of the second porous plate
is smaller than the thickness ratio of the first porous plate, the directions of the
flow of the cooling air and the flow rates of the cooling air are uniformized, and
thereby the time variation in the flow of the cooling air entering into the yarn running
space is effectively restrained. This will be detailed later.
[0007] Further, in the present invention, it is preferable that the thickness ratio of the
first porous plate is not less than 0.7 and not more than 1.6, and it is more preferable
that the thickness ratio of the first porous plate is not less than 0.8 and not more
than 1.2.
[0008] As will be described later, by designing the thickness ratio of the first porous
plate as above, the directions of the flow of the cooling air having passed through
the first porous plate are paralleled to an upward direction more successfully, and
this further promotes the uniformity in the directions of the flow and the flow rates
of the cooling air having passed through the second porous plate finally.
[0009] In addition, it is preferable that the average porosity of the second porous plate
is equal to or larger than the average porosity of the first porous plate.
[0010] If the pressure loss (fluid resistance) in the second porous plate is larger than
the pressure loss in the first porous plate, it is difficult for the cooling air having
passed through the first porous plate to smoothly pass through the second porous plate,
which may hinder the flow of the cooling air. For this reason, the average porosity
of the second porous plate is designed to be equal to or larger than the average porosity
of the first porous plate. This limits the pressure loss in the second porous plate
to a predetermined value or less, to ensure the smooth flow of the cooling air.
[0011] Furthermore, it is preferable that the distance between the first porous plate and
the second porous plate is not less than 20 mm and not more than 80 mm.
[0012] If the distance between the first porous plate and the second porous plate is too
large, the flow of the cooling air, the directions of which have been adjusted by
the first porous plate to be parallel to the upward direction, may be disturbed before
reaching the second porous plate. Meanwhile, if the distance between the first porous
plate and the second porous plate is too small, the flow of the cooling air passing
through the first porous plate is likely to be affected by the second porous plate,
and this may cause unsuccessful flow adjustment by the first porous plate. Thus, by
defining the distance between the first porous plate and the second porous plate as
being not less than 20 mm and not more than 80 mm, the effect of the flow adjustment
brought about by the use of the first porous plate and the second porous plate is
reliably improved.
[0013] Furthermore, it is preferable that a plurality of the cooling cylinders are accommodated
in the accommodation box.
[0014] In this arrangement, when sets of yarns are respectively spun out from a plurality
of spinnerets, the sets of the yarns are simultaneously cooled in the respective cooling
cylinders. When the plurality of cooling cylinders are disposed in the accommodation
box, the variation in the flow of the cooling air among the different cooling cylinders
tends to be larger because the spaces around the cooling cylinders are different in
shape from one another. In this regard, with the present invention, such a variation
is able to be decreased well.
[0015] In the present invention, by designing the thickness ratio of the second porous plate
to be smaller than the thickness ratio of the first porous plate, the effect of flow
adjustment is actively improved as compared with the configuration of the single porous
plate, and the time variation in the flow of the cooling air entering into the yarn
running space is effectively restrained.
BRIEF DESCRIPTION OF THE DRAWINGS
[0016]
FIG. 1 is a partial cross section of a melt spinning device including a yarn cooler
of the present invention.
FIG. 2 is a cross section taken along II-II in FIG. 1.
FIG. 3 is a schematic diagram of an analytical model.
FIG. 4 is a vector diagram showing the flow of the cooling air obtained through analysis.
FIG. 5 is a schematic diagram of an analytical model.
FIG. 6 is a vector diagram showing the flow of cooling air obtained through analysis.
FIG. 7 is a cross section schematically showing the flow of the cooling air.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0017] The following will describe an embodiment of a yarn cooler of the present invention.
[Melt spinning device]
[0018] FIG. 1 is a partial cross section of a melt spinning device including the yarn cooler
of the present invention. FIG. 2 is a cross section taken along II-II in FIG. 1. As
shown in FIG. 1, a melt spinning device 1 includes a spinning beam 2, a yarn cooler
3, oiling devices 4, and the like. The spinning beam 2 is provided with a plurality
of pack housings 11. In each pack housing 11, a spinning pack 12 is disposed. The
spinning pack 12 stores therein molten material to be formed into yarns Y, such as
molten polyester. A spinneret 13 is provided at a lower end portion of each spinning
pack 12. The molten material stored in the spinning pack 12 is spun out downward as
the yarns Y from a plurality of through holes (not illustrated) formed in the spinneret
13. It should be noted that the spinnerets 13 are arranged in a staggered arrangement
in two rows each extending in a left-right direction, in the same manner as cooling
cylinders 31 which will be described later (see FIG. 2).
[0019] The yarn cooler 3 is disposed below the spinning beam 2. The yarn cooler 3 is configured
to cool the yarns Y, which are spun out downward from the spinnerets 13 in the spinning
beam 2, by cooling air supplied through a duct 5. The oiling devices 4 are disposed
below the yarn cooler 3. The oiling devices 4 are configured to apply oil to the yarns
Y cooled by the yarn cooler 3. The yarns Y to which oil has been applied by the oiling
devices 4 are wound onto bobbins by an unillustrated winding device which is disposed
below the oiling devices 4.
[Yarn cooler]
[0020] The yarn cooler 3 is configured to cool the yarns Y by the cooling air supplied through
the duct 5. The yarn cooler 3 includes a substantially rectangular-parallelepiped
accommodation box 30 which accommodates the plurality of cooling cylinders 31. The
accommodation box 30 is provided with a supply portion 30a at its lower back end portion.
The supply portion 30a is connected with the duct 5, and the cooling air supplied
through the duct 5 flows into the accommodation box 30 via the supply portion 30a.
[0021] As shown in FIG. 2, the cooling cylinders 31 are arranged in a staggered arrangement
in two rows each extending in the left-right direction. The staggered arrangement
of the cooling cylinders 31 (and the spinnerets 13) enables the cooling cylinders
31 to be arranged densely, to improve the production efficiency of the yarns Y. The
supply portion 30a is provided to cover the entire length of the accommodation box
30 in the left-right direction, which is a lined-up direction in which the cooling
cylinders 31 are lined up in each row. This structure enables the cooling air to be
supplied substantially uniformly to the cooling cylinders 31 lined up in the lined
up direction.
[0022] Description continues referring back to FIG. 1. Each cooling cylinder 31 has a substantially
cylindrical shape, and is disposed below the corresponding spinneret 13 so as to be
opposed to the spinneret 13. Each cooling cylinder 31 penetrates the accommodation
box 30 in an up-down direction. The inside of each cooling cylinder 31 is a yarn running
space 32 extending in the up-down direction. The yarns Y spun out from the spinneret
13 run downward in the yarn running space 32. A peripheral wall of the yarn running
space 32, i.e., a cylinder body of the cooling cylinder 31 is structured so that its
upper portion forms a flow adjustment section 33, while its lower portion forms an
impassable section 34.
[0023] The flow adjustment section 33 is structured to include a first flow adjustment member
33a and a second flow adjustment member 33b provided inside the flow adjustment member
33a. The first flow adjustment member 33a is formed by perforated metal, for example.
The first flow adjustment member 33a is configured to adjust the flow so that the
flow of the cooling air enters into the yarn running space 32 substantially horizontally.
The second flow adjustment member 33b is formed by multi-layer metal wire mesh, for
example. The second flow adjustment member 33b is configured to uniformize the flow
of the cooling air entering into the yarn running space 32. The impassable section
34 is made of material through which the cooling air is impassable, so that the cooling
air does not enter into the yarn running space 32 through the impassable section 34.
[0024] The cooling air entering through the supply portion 30a to the accommodation box
30 flows along the cooling cylinders 31, through a portion of the space in the accommodation
box 30 in which portion no cooling cylinder 31 is disposed (this portion is hereinafter
referred to as a "supply passage 35"). Finally, the cooling air passes through the
flow adjustment section 33 of each cooling cylinder 31 and then enters into the yarn
running space 32 (see arrows in FIG. 7) . If the cooling air enters into the yarn
running space 32 without sufficient flow adjustment, there may be caused a time variation
in the flow of the cooling air, possibly leading to unevenness in the yarns Y in terms
of cooling. In view of the above, in the yarn cooler 3, a first porous plate 36 and
a second porous plate 37 are provided at a portion of the supply passage 35 which
is around the impassable sections 34 , i.e., at the portion where the cooling air
flows upward along the impassable sections 34. With this arrangement, the flow adjustment
of the cooling air is effectively performed.
[0025] It should be noted that the supply passage 35 is actually a single space as shown
in FIG. 2. In the cross section of FIG. 1, the supply passage 35 is illustrated as
if it is divided. For the sake of convenience, the reference sign is given to each
of the divided parts of the supply passage in FIG. 1, though the supply passage is
a single space. The same applies to FIG. 3, FIG. 5, and FIG. 7.
[0026] The first porous plate 36 is disposed substantially horizontally to be substantially
level with an upper end of the supply portion 30a. The first porous plate 36 is formed
by perforated metal, for example. The second porous plate 37 is disposed, not less
than 20 mm and not more than 80 mm above the first porous plate 36. The second porous
plate 37 is disposed substantially horizontally to be substantially level with upper
ends of the impassable sections 34. Similarly to the first porous plate 36, the second
porous plate 37 is also formed by perforated metal, for example. In the present embodiment,
the first and second porous plates 36 and 37 are designed so that the thickness ratio
of the second porous plate 37 is smaller than the thickness ratio of the first porous
plate 36. This will be detailed later.
[Study on porous plates]
[0027] The present inventors conducted fluid analysis for wholehearted consideration on
how the effect of flow adjustment can be improved in the configuration of multiple
porous plates. FIG. 3 is a schematic diagram of an analytical model. The detailed
dimensions are indicated in FIG. 3. Analysis was conducted for 6 cases shown in Table
1 under the condition that: the cooling air enters from the supply portion 30a at
a flow rate of 0.437 m
3/min; and an upper end of the supply passage 35 is open to the atmosphere. Table 1
shows the dispersion in the in-plane velocity of the cooling air having passed through
the last porous plate (i.e. , the second porous plate 37 in each of Cases A to E,
or the first porous plate 36 in Case F) . Further, FIG. 4 is a vector diagram showing
the flow of the cooling air obtained through the analysis. Note that "porosity" used
herein means an average porosity on the entire surface of the porous plate, i.e.,
the ratio of the total sum of the areas of all the holes to the entire area of the
porous plate (the holes may be arranged regularly or irregularly). Further, "thickness
ratio" used herein means the ratio of the thickness of the plate to the diameter of
the hole.
[Table 1]
| |
Case A |
Case B |
Case C |
| First porous plate |
Second porous plate |
First porous plate |
Second porous plate |
First porous plate |
Second porous plate |
| Plate thickness t [mm] |
1.6 |
0.8 |
1.6 |
1.6 |
0.8 |
1.6 |
| Hole diameter d [mm] |
2 |
2 |
2 |
2 |
2 |
2 |
| Thickness ratio t/d [-] |
0.8 |
0.4 |
0.8 |
0.8 |
0.4 |
0.8 |
| Porosity [%] |
29.6 |
49.7 |
29.6 |
29.6 |
49.7 |
29.6 |
| Dispersion in in-plane velocity (standard deviation) at 1 mm above the last porous
plate |
1.91284 |
3.04940 |
3.08742 |
| Dispersion in in-plane velocity (standard deviation) at 5 mm above the last porous
plate |
0.59582 |
0.97709 |
1.10766 |
| Dispersion in in-plane velocity (standard deviation) at 10 mm above the last porous
plate |
0.48911 |
0.80593 |
0.91697 |
| |
Case D |
Case E |
Case F |
| First porous plate |
Second porous plate |
First porous plate |
Second porous plate |
First porous plate |
Second porous plate |
| Plate thickness t [mm] |
0.8 |
0.4 |
1.6 |
0.8 |
1.6 |
- |
| Hole diameter d [mm] |
2 |
2 |
2 |
2 |
2 |
- |
| Thickness ratio t/d [-] |
0.4 |
0.2 |
0.8 |
0.4 |
0.8 |
- |
| Porosity [%] |
29.6 |
49.7 |
49.7 |
49.7 |
29.6 |
- |
| Dispersion in in-plane velocity (standard deviation) at 1 mm above the last porous
plate |
2.04426 |
1.88220 |
3.31466 |
| Dispersion in in-plane velocity (standard deviation) at 5 mm above the last porous
plate |
0.76864 |
0.61748 |
1.23981 |
| Variation in in-plane velocity (standard deviation) at 10 mm above the last porous
plate |
0.66238 |
0.60356 |
1.03116 |
[0028] The dispersion in velocity is improved in each of Cases A to E where both the first
porous plate 36 and the second porous plate 37 are provided, as compared to Case F
where the single porous plate is provided. This shows that the effect of the flow
adjustment is improved by providing the plurality of porous plates. However, in Cases
B and C, the dispersion in velocity is just a little improved as compared with Case
F, and in addition, there were observed relatively larger swirls in the flow of the
cooling air having passed through the second porous plate 37, as can be clearly seen
in FIG. 4. Meanwhile, in Cases A, D, and E, the dispersion in velocity is significantly
improved as compared to Case F. Further, no noticeable swirl was found in the flow
of the cooling air having passed through the second porous plate 37 in FIG. 4.
[0029] Among Cases A, D, and E, in which the improvement is larger, there is a common condition:
the thickness ratio of the second porous plate 37 is smaller than the thickness ratio
of the first porous plate 36. Meanwhile, in Cases B and C in which the improvement
is smaller, the thickness ratio of the second porous plate 37 is equal to or larger
than the thickness ratio of the first porous plate 36. Based on the above finding,
the present inventors arrives at the consideration that: when the thickness ratio
of the second porous plate 37 is designed to be smaller than the thickness ratio of
the first porous plate 36, the directions of the flow of the cooling air are first
paralleled to the upward direction to some extent by the first porous plate 36, and
then the flow rates of the cooling air is uniformized by the second porous plate 37,
and thereby the effect of the flow adjustment is actively improved.
[0030] The present inventors further examined an optimum range of the thickness ratio of
the first porous plate 36 through fluid analysis, in order to improve the effect of
paralleling the directions of the flow of the cooling air to the upward direction
by the first porous plate 36. FIG. 5 is a schematic diagram of an analytical model.
The detailed dimensions are indicated in FIG. 5. Analysis was conducted for 5 cases
shown in Table 2 under the condition that: the cooling air enters from the supply
portion 30a at a flow rate of 0.437 m
3/min; and the upper end of the supply passage 35 is open to the atmosphere. Note that
how well the directions of the flow of the cooling air are paralleled to the upward
direction by the first porous plate 36 is influenced mainly by the thickness ratio,
and little by the porosity.
[Table 2]
| |
Case 1 |
Case 2 |
Case 3 |
Case 4 |
Case 5 |
| Plate thickness t [mm] |
0.8 |
1.4 |
1.6 |
2.3 |
3.2 |
| Hole diameter d [mm] |
2 |
2 |
2 |
2 |
2 |
| Thickness ratio t/d [-] |
0.4 |
0.7 |
0.8 |
1.15 |
1.6 |
| Porosity [%] |
29.6 |
29.6 |
29.6 |
29.6 |
29.6 |
[0031] FIG. 6 is a vector diagram showing the flow of the cooling air obtained through the
analysis. In Case 1 (the thickness ratio is 0.4), the flow of the cooling air, which
has flowed from the right to the left in this figure and passed through the first
porous plate 36, still considerably has a leftward velocity component. That is, the
effect of paralleling the directions of the flow of the cooling air to the upward
direction is relatively smaller. Meanwhile, in Cases 2 to 5 (the thickness ratio is
0.7 to 1.6), the cooling air having passed through the first porous plate 36 flows
in the upward direction substantially well, though in some of the cases, the flow
of the cooling air having passed through the first porous plate 36 still has a leftward
velocity component a little. Particularly in Cases 3 to 5 where the thickness ratio
of the first porous plate 36 is not less than 0.8, the effect of the flow adjustment
was significant.
[0032] The above result shows that when the thickness ratio of the first porous plate 36
is not less than 0.7 (more preferably not less than 0.8) and not more than 1.6, the
effect of adjusting the flow of the cooling air to the upward direction by the first
porous plate 36 is enhanced, and finally the effect of adjusting the flow of the cooling
air having passed through the second porous plate 37 is further enhanced. This finding
conforms to the fact that among Cases A, D, and E of Table 1 in each of which the
effect of the flow adjustment is larger, the dispersion in velocity is significantly
reduced particularly in Cases A and E in each of which the thickness ratio of the
first porous plate 36 is not less than 0.7 and not more then 1.6.
[0033] FIG. 7 is a cross section schematically showing the flow of the cooling air. The
flow of the cooling air is schematically illustrated with bold arrows. First, the
directions of the flow of the cooling air supplied from the supply portion 30a to
the supply passage 35 are substantially paralleled by the first porous plate 36 to
the upward direction. As described above, this effect is particularly significant
when the thickness ratio of the first porous plate 36 is not less than 0.7 (more preferably
not less than 0.8) and not more than 1.6. Further, by designing the porous plates
so that the thickness ratio of the second porous plate 37 is smaller than the thickness
ratio of the first porous plate 36, the flow rates of the cooling air, the directions
of which have been paralleled to the upward direction by the first porous plate 36,
are uniformized successfully by the second porous plate 37. As a result, uniformity
is achieved with respect to both the direction and flow rate of the cooling air having
passed through the second porous plate 37, and this restrains the time variation in
the flow of the cooling air entering into the yarn running space 32. Consequently,
unevenness in the yarns Y in terms of cooling is restrained, and the yarns Y having
good quality are provided.
[0034] Finally, the inventors examined how much the physical properties of the yarns Y are
actually improved, as compared with the configuration of the single porous plate,
when the porous plates are provided and designed so that the thickness ratio of the
second porous plate 37 is smaller than the thickness ratio of the first porous plate
36. Table 3 shows its result. It should be noted that CV% stands for the coefficient
of variation (CV) expressed in percentage, and indicates the degree of dispersion
in values of physical properties. In this test, dispersion in values were obtained,
for elongation, strength, U%, and thermal stress of the yarns Y. Note that U% is a
percentage representing the degree of unevenness in yarns (USTER coefficient) measured
using an USTER yarn unevenness tester produced by Zellweger Uster.
[Table 3]
| |
Single porous plate |
Two porous plates |
| First porous plate |
Second porous plate |
First porous plate |
Second porous plate |
| Plate thickness t [mm] |
1.6 |
- |
1.6 |
1 |
| Hole diameter d [mm] |
2 |
- |
2 |
2 |
| Thickness ratio t/d [-] |
0.8 |
- |
0.8 |
0.5 |
| Porosity [%] |
29.6 |
- |
29.6 |
29.6 |
| Strength CV% |
3.12 |
2.06 |
| Elongation CV% |
3.16 |
1.93 |
| U% CVm (hi) |
0.41 |
0.32 |
| Thermal stress CV% |
1.72 |
1.57 |
[0035] As shown in Table 3, by designing the porous plates so that the thickness ratio of
the second porous plate 37 is smaller than the thickness ratio of the first porous
plate 36, the dispersion in each physical property of the yarns Y is decreased, and
the quality of the yarns Y is improved. This confirms that, by improving the effect
of the flow adjustment of the cooling air by the first porous plate 36 and the second
porous plate 37, the time variation in the flow of the cooling air entering into each
yarn running space 32 is restrained, and finally the quality of the yarns Y is reliably
improved.
[Advantageous Effects]
[0036] By designing the porous plates so that the thickness ratio of the second porous plate
37 is smaller than the thickness ratio of the first porous plate 36 as is in the present
embodiment, uniformity is achieved with respect to the direction of the flow of the
cooling air and the flow rate of the cooling air, and thereby the time variation in
the flow of the cooling air entering into each yarn running space 32 is effectively
restrained. Further, by designing the thickness ratio of the first porous plate 36
to be not less than 0.7 and not more than 1.6, the effect of paralleling the directions
of the flow of the cooling air to the upward direction by the first porous plate 36
is improved, and the effect of the flow adjustment as a whole is further improved.
[0037] As a porous plate, perforated metal, which is a metal plate processed through punch
press, is often used. For this reason, if the thickness ratio (thickness) of the porous
plate is too large, the punch press process is difficult, and there is a possibility
that the intended porous plate cannot be prepared. Thus, in the present embodiment,
the upper limit of the thickness ratio of the first porous plate 36 is defined as
1.2, to easily produce the first porous plate 36 and the second porous plate 37 by
punch press. In addition, by designing the thickness ratio of the first porous plate
36 to be not less than 0.8, as described above, the effect of the flow adjustment
is further improved. Thus, it is more preferable that the thickness ratio of the first
porous plate 36 is not less than 0.8 and not more than 1.2.
[0038] Further, in the present embodiment, it is preferable that the porosity of the second
porous plate 37 is equal to or larger than the porosity of the first porous plate
36. If the pressure loss (fluid resistance) in the second porous plate 37 is larger
than the pressure loss in the first porous plate 36, it is difficult for the cooling
air having passed through the first porous plate 36 to smoothly pass through the second
porous plate 37, which may hinder the flow of the cooling air. For this reason, the
porosity of the second porous plate 37 is designed to be equal to or larger than the
porosity of the first porous plate 36. This prevents the pressure loss in the second
porous plate 37 from exceeding a predetermined value, to ensure the smooth flow of
the cooling air. This is consistent with the fact that the porosity of the second
porous plate 37 is equal to or larger than the porosity of the first porous plate
36 in each of Cases A, D, and E in Table 1, in each of which the effect of the flow
adjustment was significant.
[0039] Furthermore, as is in the present embodiment, it is preferable that the distance
between the first porous plate 36 and the second porous plate 37 is not less than
20 mm and not more than 80 mm. If the distance between the first porous plate 36 and
the second porous plate 37 is too large, the flow of the cooling air, the directions
of which have been adjusted by the first porous plate 36 to be parallel to the upward
direction, may be disturbed before reaching the second porous plate 37. Meanwhile,
if the distance between the first porous plate 36 and the second porous plate 37 is
too small, the flow of the cooling air passing through the first porous plate 36 is
likely to be affected by the second porous plate 37, and this may cause unsuccessful
flow adjustment by the first porous plate 36. Thus, by defining the distance between
the first porous plate 36 and the second porous plate 37 as being not less than 20
mm and not more than 80 mm, the effect of the flow adjustment brought about by the
use of the first porous plate 36 and the second porous plate 37 is reliably improved.
[0040] Moreover, as is in the present embodiment, it is preferable that the plurality of
cooling cylinders 31 are accommodated in the accommodation box 30. In this arrangement,
when sets of yarns Y are respectively spun out from the spinnerets 13, the sets of
the yarns Y are simultaneously cooled in the respective cooling cylinders 31. When
the plurality of cooling cylinders 31 are disposed in the accommodation box 30, the
variation in the flow of the cooling air among the different cooling cylinders 31
tends to be larger because the spaces around the cooling cylinder 31 are different
in shape from one another. In this regard, according to the present embodiment, such
a variation is able to be decreased well.
[Other embodiments]
[0041] The present invention is not limited to the embodiment above. Combinations of components
of the above embodiment, and various modifications and variations are possible within
the scope of the spirit of the invention.
[0042] For example, while the above-described embodiment describes the yarn cooler 3 including
the plurality of cooling cylinders 31 disposed in the accommodation box 30, it is
not essential that the number of the cooling cylinders 31 in the accommodation box
30 is two or more.
[0043] Further, while the cooling cylinders 31 are arranged in a staggered arrangement in
two rows each extending in the left-right direction in the above-described embodiment,
the manner of arrangement of the cooling cylinders 31 is not limited to this. For
example, the cooling cylinders 31 may be aligned in a single row extending in the
left-right direction, or may be arranged in multiple rows in an arrangement manner
other than the staggered arrangement.