TECHNICAL FIELD
[0001] The present invention relates to a blower and a vacuum cleaner.
BACKGROUND ART
[0002] For example, Japanese Laid-Open Patent Publication No.
2002-156128 discloses a conventional blower. A turbofan disclosed in Japanese Laid-open Patent
Publication No.
2002-156128 includes a casing, a motor, a base plate, a blade, and a shroud. The base plate,
the blade, and the shroud are accommodated in the casing. A plurality of blades are
circumferentially arranged. The shroud connects ends of the plurality of blades. The
plurality of blades are arranged on a circumference of the base plate.
[0003] The casing includes an intake-side end, a straight portion, and an inclined step.
An inner diameter of an intake-side end is equal to or larger than an outer diameter
of the base plate.
[0004] Air is discharged from a turbofan center portion to an outer circumferential direction.
It is claimed that a noise of the turbofan is reduced because the shroud has the above
characteristics.
CITATION LIST
PATENT LITERATURE
[0005] Patent Literature 1: Japanese Laid-Open Patent Publication No.
2002-156128
SUMMARY OF INVENTION
TECHNICAL PROBLEM
[0006] However, in the turbofan disclosed in Japanese Laid-Open Patent Publication No.
2002-156128, a part of the air discharged to a radial outside of the blade flows backward from
a gap between the shroud and the casing to a radial inside. At this point, turbulence
is generated in an airflow passage in the casing, or air resistance is generated by
a flowing-back airflow to degrade blowing efficiency of the blower.
[0007] An object of the present invention is to provide a blower capable of preventing the
generation of the turbulence in the airflow passage of a duct, and improving blowing
efficiency by preventing the airflow from flowing backward to the radial inside. In
addition, another object of the present invention is to provide a vacuum cleaner including
the blower capable of improving the blowing efficiency.
SOLUTION TO PROBLEM
[0008] According to an exemplary embodiment of the present invention, a blower includes:
an impeller rotatable about a central axis extending in a vertical direction; a motor
that is positioned on a lower side of the impeller and rotates the impeller about
the central axis; and a duct including an airflow passage in an inner space, a suction
port through which a fluid flows in the inner space, and an air outlet through which
the fluid is discharged from the inner space, the impeller being accommodated in the
duct. The impeller includes: a plurality of blades arranged in a circumferential direction;
a shroud that has an annular shape, connects upper portions of the plurality of blades,
and includes an opening located opposite the suction port in an axial direction; and
a base plate that connects lower portions of the plurality of blades and extends in
a radial direction, the duct includes a cover covering at least a part of the blade
and an upper portion of the shroud, an inner diameter of the shroud is equal to or
larger than an outer diameter of the base plate, and the cover includes a first projection
that projects axially downward from a bottom surface of the cover and is disposed
on a radial inside of an inner circumferential surface of the shroud.
ADVANTAGEOUS EFFECTS OF INVENTION
[0009] An exemplary embodiment of the present invention can provide the blower capable of
improving the blowing efficiency. Additionally, an exemplary embodiment of the present
invention can provide the vacuum cleaner including the blower.
BRIEF DESCRIPTION OF DRAWINGS
[0010]
Fig. 1 is a sectional view illustrating a cleaning robot according to an embodiment
of the present invention.
Fig. 2 is a perspective view illustrating a blower of the embodiment of the present
invention.
Fig. 3 is a longitudinal sectional view illustrating the blower of the embodiment
of the present invention.
Fig. 4 is a perspective view illustrating an impeller of the embodiment of the present
invention when the impeller is viewed from above.
Fig. 5 is a plan view illustrating the impeller of the embodiment of the present invention.
Fig. 6 is a side sectional view illustrating the impeller of the embodiment of the
present invention.
Fig. 7 is an enlarged longitudinal sectional view illustrating a part of the blower
of the embodiment of the present invention.
Fig. 8 is an enlarged longitudinal sectional view illustrating a part of the blower
of the embodiment of the present invention.
Fig. 9 is an enlarged longitudinal sectional view illustrating a part of a blower
according to a modification of the embodiment of the present invention.
Fig. 10 is an enlarged longitudinal sectional view illustrating a vicinity of a shroud
in the blower of the modification of the embodiment of the present invention.
Fig. 11 is an enlarged longitudinal sectional view illustrating the vicinity of the
shroud in the blower of the modification of the embodiment of the present invention.
DESCRIPTION OF EMBODIMENT
[0011] Hereinafter, an exemplary embodiment of the present invention will be described with
reference to the drawings. Note that, in the following description, an extending direction
of a central axis A of a blower 1 in Fig. 3 is simply referred to as an "axial direction",
and a radial direction and a circumferential direction about the central axis A of
the blower 1 are simply referred to as a "radial direction" and a "circumferential
direction". Similarly, with respect to an impeller 20 in Figs. 4 to 6, directions
matched with the axial direction, the radial direction, and the circumferential direction
of the blower 1 in a state where the impeller 20 is incorporated in the blower 1 are
simply referred to as the "axial direction", the "radial direction", and the "circumferential
direction". Note that, a vertical direction is simply used for the description, but
does not limit an actual positional relationship and a direction.
<1. Configuration of vacuum cleaner>
[0012] A blower according to an exemplary embodiment of the present invention will be described.
Fig. 1 is a sectional view of a cleaning robot 100 according to an exemplary embodiment
of the present invention. As illustrated in Fig. 1, the blower 1 is mounted on the
cleaning robot (vacuum cleaner) 100 to serve as suction means.
[0013] The cleaning robot 100 sucks air containing dust on a floor surface F while self-propelling
the floor surface F at an installed place, and exhausts the air from which the dust
is removed, thereby cleaning the floor surface F. The cleaning robot 100 includes
a disc-shaped chassis 101 and includes, in the disc-shaped chassis 101, a suction
passage 104, a dust container 105, a filter 106, an exhaust passage 107, and the blower
1. A driving wheel 109 and a front wheels 110 are provided on a bottom surface of
the chassis 101.
[0014] The chassis 101 includes an inlet port 103 in a center of the bottom surface and
an exhaust port 108 at the side surface. By driving the blower 1, the cleaning robot
100 sucks the air including the dust on the floor surface F from the inlet port 103
while self-propelling. The air containing the dust sucked into the chassis 101 from
the inlet port 103 passes through the suction passage 104, and flows into the dust
container 105. The airflow flowing in the dust container 105 passes through the filter
106, and is sucked in the blower 1 through the exhaust passage 107. The air sucked
by the blower 1 is exhausted diagonally upward rearward from the exhaust port 108.
At this point, the dust contained in the airflow in the dust container 105 is caught
by the filter 106, and dust D is accumulated in the dust container 105.
<2. Configuration of blower>
[0015] Fig. 2 is a perspective view illustrating the blower 1 of the embodiment of the present
invention. In addition, Fig. 3 is a longitudinal sectional view illustrating the blower
1 of the embodiment of the present invention. As illustrated in Figs. 2 and 3, the
blower 1 includes the impeller 20, a motor 30, and a duct 10. The impeller 20 is accommodated
in an internal space of the duct 10. The motor 30 is located below the impeller 20,
and rotates the impeller 20 about the central axis A.
[0016] The impeller 20 is connected to a shaft (not illustrated) extending in an axial direction
from the motor 30, and supported so as to be rotatable about the central axis A. That
is, the impeller 20 is rotatable about the central axis A extending in the vertical
direction. A control board 40 is disposed on a lower side of the motor 30 in the axial
direction, and controls the motor 30.
<3. Configuration of duct>
[0017] The duct 10 includes an airflow passage 13 in the inner space thereof, a suction
port 11 through which a fluid flows in the inner space, and an air outlet 12 through
which the fluid is discharged from the inner space. The impeller 20 is accommodated
in the duct 10. The duct 10 is constructed with a cover 14, a circumferential wall
15, and a motor housing 16, and the airflow passage 13 is formed in the internal space
surrounded by these components. More particularly, the duct 10 includes the cover
14 covering at least a part of a blade 23 and an upper portion of a shroud 22. The
cover 14 covers the upper portion of the impeller 20, and is formed into an annular
shape as seen in axial plan view. An outer diameter of the cover 14 is larger than
an outer diameter of the impeller 20. Note that, in the embodiment, the duct 10 is
constructed with a member including the cover 14 and a part of the circumferential
wall 15 and a member including a part of the circumferential wall 15 and the motor
housing 16. Consequently, the duct 10 can be constructed at low cost because the two
members can be molded as separate resin members.
[0018] A cylindrical portion 14a extending upward in the axial direction is provided at
the central portion of the cover 14. The circular suction port 11 is formed in the
cylindrical portion 14a as seen in axial plan view. The suction port 11 is disposed
opposite an opening 22a of the shroud 22 (to be described later) in the axial direction,
and gas (fluid) flows into the internal space of the duct 10 from the outside through
the suction port 11.
[0019] The circumferential wall 15 covers the impeller 20 from the lateral side, extends
downward in the axial direction from an outer circumference of the cover 14, and is
formed into a cylindrical shape. In addition, a nozzle 15a extending to the radial
outside is provided in the circumferential wall 15, and the air outlet 12 through
which the gas (fluid) is discharged from the internal space of the duct 10 is formed
in the nozzle 15a.
[0020] The motor housing 16 is located on a lower side in the axial direction of the impeller
20. More particularly, the blower 1 further includes the motor housing 16 located
below a base plate 21 (to be described later). A top surface of the motor housing
16 spreads radially, extends to the lower end of the circumferential wall 15, and
is connected to the circumferential wall 15. In addition, the circumferential surface
of the motor housing 16 is formed in a cylindrical shape extending axially downward
from the outer circumference of the circumferential wall 15, and the motor 30 and
the control board 40 are accommodated in the motor housing 16.
[0021] An annular recess 16a recessed downward on the radial outside of the impeller 20
is formed on the top surface of the motor housing 16. The airflow passage 13 including
an annular region on the radial outside of the impeller 20 is formed between the suction
port 11 and the air outlet 12 by the circumferential wall 15, the recess 16a, and
the cover 14.
<4. Configuration of impeller>
[0022] Fig. 4 is a perspective view illustrating the impeller 20 of the embodiment of the
present invention when the impeller 20 is viewed from above, and Fig. 5 is a plan
view illustrating the impeller 20 of the embodiment of the present invention. In addition,
Fig. 6 is a side sectional view illustrating the impeller 20 of the embodiment of
the present invention.
[0023] As illustrated in Figs. 4 to 6, the impeller 20 includes a plurality of blades 23,
the annular shroud 22, and the base plate 21. The blade 23 is interposed between the
base plate 21 and the shroud 22. The plurality of blades 23 are circumferentially
arranged.
[0024] The shroud 22 has an annular shape connecting the upper portions of the plurality
of blades 23, and has the opening 22a located opposite the suction port 11 in the
axial direction. More particularly, the shroud 22 is formed into the annular shape
by connecting upper portions of the plurality of blades 23, and the opening 22a for
taking the gas is formed in a central portion of the shroud 22. The opening 22a has
a circular shape as seen in axial plan view.
[0025] The base plate 21 connects the lower portions of the plurality of blades 23, and
spreads in the radial direction. The base plate 21 is formed into a disc shape. The
base plate 21 has a base plate protrusion 21a protruding downward from the bottom
surface of the base plate 21. More particularly, the base plate protrusion 21a protrudes
from the radial outer edge of the bottom surface of the base plate 21, and is formed
into the annular shape (see Fig. 6).
[0026] The blade 23 includes a first blade 23a and a second blade 23b, which have different
radial lengths, and the first blades 23a and the second blades 23b are alternately
arranged in the circumferential direction. The first blade 23a and the second blade
23b are a plate-shaped member, which rises in the axial direction and extends from
the radial inside to the outside. The radially inner end of the first blade 23a is
located on the radial inside of the radially inner end of the second blade 23b, and
the first blade 23a is longer than the second blade 23b in the radial direction.
[0027] In addition, in the case that the impeller 20 is rotated counterclockwise as seen
in axial plan view from above, the first blade 23a and the second blade 23b are curved
such that the radially outer end is inclined on a rear side in the rotational direction
with respect to the radial inner end, and such that the rear side in the rotation
direction is recessed (see Fig. 5). In addition, a distance between the first blade
23a and the second blade 23b increases toward the radial outside.
[0028] In addition, the radially outer ends 24a, 24b of the first blade 23a and the second
blade 23b extend to the radial outside of the outer circumference of the base plate
21 (see Fig. 4). That is, the radially outer ends 24a, 24b of the blade 23 extend
to the radial outside of the outer circumference of the base plate 21. In addition,
the radially inner ends of the first blade 23a and the second blade 23b extend to
the radial inside of the suction port 11 (see Fig. 3). That is, the radially inner
end of the blade 23 extends to the radial inside of the suction port 11. Consequently,
the blade 23 can be formed large in the radial direction, and an amount of air generated
by the rotation of the impeller 20 can be increased. The outer circumference of the
base plate 21 may have another shape, for example, a part of a member from a circumferential
outer edge may be notched radially inward.
[0029] The upper ends of the first blade 23a and the second blade 23b have protrusions
25a, 25b that protrude upward in the axial direction (see Fig. 6). The protrusions
25a, 25b are located on the radial inside of the opening 22a while aligned on an identical
circle, and protrude upward from the upper end of the shroud 22.
[0030] In addition, the upper ends of the first blade 23a and the second blade 23b include
inclined surfaces 26a, 26b extending downward from the protrusions 25a, 25b toward
the radial inside and inclined surfaces 27a, 27b extending downward from the protrusions
25a, 25b toward the radial outside, respectively.
[0031] In addition, in the inclined surfaces 27a, 27b, protrusions 28a, 28b protruding axially
upward are formed on the radial outside of the opening 22a of the shroud 22, and the
upper ends of the protrusions 28a, 28b extend to the bottom surface of the shroud
22 and is connected to the shroud 22. That is, the blade 23 includes the protrusions
28a, 28b protruding axially upward on the radial outside of a first projection 17
(see Fig. 7) (to be described later). Consequently, the blade 23 can axially be formed
larger on the radial outside of the opening 22a, and the amount of air generated by
the rotation of the impeller 20 can be increased.
[0032] The base plate 21, the shroud 22, and the blade 23 are formed by an identical resin
molding product made of an identical material, and an inner diameter D2 of the shroud
22 is formed equal to an outer diameter D1 of the base plate 21 (see Fig. 6).
[0033] Consequently, in forming the impeller 20 straddling the base plate 21 and the shroud
22, upper and lower dies can be pulled out onto the upper side and the lower side
in the axial direction, respectively, while mutual interference between the upper
and lower dies is prevented. Thus, the impeller 20 can integrally be molded using
the die, and mass productivity of the impeller 20 can be improved. Note that, even
in the case that the inner diameter D2 of the shroud 22 is formed larger than the
outer diameter D1 of the base plate 21, the impeller 20 can integrally be molded using
the die.
<5. Relationship between duct and impeller>
[0034] Figs. 7 and 8 are enlarged longitudinal sectional views illustrating a part of the
blower 1 of the embodiment of the present invention, and illustrate a relationship
between the duct 10 and the impeller 20. In addition, as illustrated in Fig. 7, the
shroud 22 includes an inner circumferential surface 22b constituting the opening 22a.
The cover 14 includes the first projection 17, which projects axially downward from
the bottom surface of the cover 14 and is disposed on the radial inside of the inner
circumferential surface 22b of the shroud 22. The outer circumferential surface of
the first projection 17 is radially opposed to the inner circumferential surface 22b
of the shroud 22. Note that, the outer circumferential surface of the first projection
17 and the inner circumferential surface 22b of the shroud 22 are not necessarily
opposed to each other on the circumferential surface. That is, the outer surface of
the first projection 17 may radially be opposed to the inner surface 22b of the shroud
22. Note that, the shapes of the outer surface of the first projection 17 and the
inner surface 22b of the shroud 22 are not limited to the circumferential surface.
For example, in the outer surface of the first projection 17 and the inner surface
22b of the shroud 22, irregularities may be formed on a part of the circumferential
surface.
[0035] The first projection 17 blocks the flow path of the air R1 that flows backward onto
the radial inside from the gap between the shroud 22 and the cover 14. Consequently,
a part of the air blown out onto the radial outside of the impeller 20 can be prevented
from flowing backward from the gap between the shroud 22 and the cover 14. Thus, the
degradation of the blowing efficiency can be prevented by the generation of the turbulence
or the air resistance of the flowing-back air in the airflow passage 13. In addition,
the radial gap between the outer circumferential surface of the first projection 17
and the inner circumferential surface 22b of the shroud 22 is narrower than the axial
gap between the shroud 22 and the cover 14. Thus, a flow of air R1 flowing backward
to the radial inside from the gap between the shroud 22 and the cover 14 can be blocked.
[0036] In addition, the lower end of the radially outer end of the first projection 17 extends
to the position where the height in the axial direction is substantially equal to
or lower than the height at the lower end of the inner circumferential surface 22b
of the shroud 22. Consequently, the air circulating toward the radial outside along
the bottom surface of the cover 14 is smoothly guided from the lower end of the first
projection 17 to the lower end of the inner circumferential surface 22b of the shroud
22, and blown out to the radial outside of the impeller 20 through the bottom surface
of the shroud 22. This enables the further improvement of the blowing efficiency of
the blower 1. In other words, a strike of the circulating air on the inner circumferential
surface 22b of the shroud 22 is reduced, so that the air can efficiently be blown
out onto the radial outside.
[0037] Note that, as illustrated in Fig. 8, the protrusions 28a, 28b (not illustrated in
Fig. 7, see Fig. 4) of the first blade 23a and the second blade 23b are connected
to the bottom surface of the shroud 22 on the radial outside with respect to the first
projection 17, and the first projection 17 is vertically opposed to the inclined surfaces
27a, 27b. Consequently, assuming that a region of the first blade 23a and the second
blade 23b located on the radial outside of the first projection 17 is a blade first
region L1, and that a region vertically opposed to the first projection 17 is a blade
second region L2, the upper end of the blade first region L1 is located above the
upper end at the radially outer end of the blade second region L2 in the upper ends
of the first blade 23a and the second blade 23b.
[0038] That is, the blade 23 includes the blade first region L1 located on the radial outside
of the first projection 17 and the blade second region L2 vertically opposed to the
first projection 17, and the upper end of the blade first region L1 is located above
the upper end at the radially outer end of the blade second region L2. Thus, even
if the impeller 20 vibrates vertically during the rotation, the first blade 23a and
the second blade 23b can be prevented from contacting with the first projection 17.
[0039] In addition, referring to Fig. 7, an annular groove 16b, which is axially opposed
to the base plate protrusion 21a protruding from the outer circumference of the bottom
surface of the base plate 21, is provided on the top surface of the motor housing
16. A radial width of the groove 16b is larger than that of the base plate protrusion
21a. The axial gap between the bottom surface of the base plate 21 and the top surface
of the motor housing 16 can be narrowed by disposing the base plate protrusion 21a
close to the groove 16b.
[0040] Consequently, a part of the air blown out onto the radial outside of the impeller
20 can be prevented from flowing backward from the gap between the bottom surface
of the base plate 21 and the top surface of the motor housing 16, and the degradation
of the blowing efficiency due to the generation of the turbulence or the air resistance
of the flowing-back air in the airflow passage 13 can be prevented.
[0041] In addition, the axial gap between the lower end of the base plate protrusion 21a
and the top surface of the motor housing 16 is narrower than the axial gap between
the bottom surface of the base plate 21 and the top surface of the motor housing 16.
Thus, a part of the air blown out onto the radial outside of the impeller 20 can be
prevented from flowing in the gap between the bottom surface of the base plate 21
and the top surface of the motor housing 16 to flow backward onto the radial inside.
[0042] Note that, the base plate protrusion 21a may be formed at a position other than the
radially outer edge of the base plate 21. For example, on the bottom surface of the
base plate 21, the base plate protrusion 21a may be formed at a position inside the
radially outer edge. Even in this case, a part of the air blown out onto the radial
outside of the impeller 20 can be prevented from flowing in the gap between the bottom
surface of the base plate 21 and the top surface of the motor housing 16 as air R2
to flow backward onto the radial inside.
<6. Drive of blower>
[0043] When the motor 30 is driven, the impeller 20 rotates about the central axis A. Consequently,
the air is taken in the duct 10 through the suction port 11. The air taken in the
duct 10 is accelerated toward the radial outside by the impeller 20. The air accelerated
toward the radial outside passes between the shroud 22 and the base plate 21, and
is blown out to the radial outside of the impeller 20. The air blown out to the radial
outside of the impeller 20 is discharged from the air outlet 12 to the outside of
the duct 10 through the airflow passage 13 formed in the circumferential direction
in the duct 10.
<7. Modification>
[0044] Fig. 9 is an enlarged longitudinal sectional view illustrating a part of a blower
1 according to a modification of the exemplary embodiment of the present invention.
The second projection 18 projecting downward in the axial direction may be provided
on the bottom surface of the cover 14. The inner circumferential surface of the second
projection 18 is radially opposed to the outer circumferential surface of the shroud
22.
[0045] The second projection 18 blocks the airflow flowing in a gap between the shroud 22
and the cover 14. Consequently, a part of the air blown out onto the radial outside
of the impeller 20 can be prevented from flowing in the gap between the shroud 22
and the cover 14, and the generation of the turbulence or the backward flow in the
airflow passage 13 can be prevented. Note that, although both of the first projection
17 and the second projection 18 may be provided, the degradation of the blowing efficiency
due to the generation of the turbulence or the air resistance of flowing-back air
in the airflow passage 13 can be prevented even if only one of the first projection
17 and the second projection 18 is provided. In addition, the radial gap between the
inner circumferential surface of the second projection 18 and the outer circumferential
surface of the shroud 22 is narrower than the axial gap between the shroud 22 and
the cover 14. Thus, the flow of air flowing backward to the radial inside from the
gap between the shroud 22 and the cover 14 can be blocked.
[0046] Fig. 10 is an enlarged longitudinal sectional view illustrating a vicinity of the
shroud 22 in the blower 1 of the modification of the exemplary embodiment of the present
invention. The inner circumferential surface 22b of the shroud 22 includes a first
inner circumferential surface 221 and a second inner circumferential surface 222,
and the first inner circumferential surface 221 is disposed axially above the second
inner circumferential surface 222. The first inner circumferential surface 221 is
formed in parallel to the axial direction, and the second inner circumferential surface
222 is inclined with respect to the axial direction so as to be away from the central
axis A toward the lower side in axial direction, and projectively curved toward the
radial inside. In addition, the first inner circumferential surface 221 and the second
inner circumferential surface 222 are connected to each other while a curved portion
223 projectively curved toward the radial inside is interposed therebetween. That
is, the lower end of the first inner circumferential surface 221 and the upper end
of the second inner circumferential surface 222 are smoothly connected to each other.
[0047] That is, the radial gap between the outer circumferential surface of the first projection
17 and the inner circumferential surface 22b of the shroud 22 is formed wider in the
axial lower side than the axial upper side.
[0048] Consequently, even if the impeller 20 vibrates vertically during the rotation and
even if the lower end of the inner circumferential surface 22b of the shroud 22 is
axially lowered lower than the lower end of the radially outer end of the first projection
17, the air circulating toward the radial outside along the bottom surface of the
cover 14 is smoothly guided from the lower end of the first projection 17 onto the
radial outside along the second inner circumferential surface 222. Thus, reduction
of the blowing efficiency of the blower 1 can be prevented even if the impeller 20
vibrates vertically during the rotation.
[0049] The first inner circumferential surface 221 and the second inner circumferential
surface 222 are connected to each other while the curved portion 223 projectively
curved toward the radial inside is interposed therebetween, and the second inner circumferential
surface 222 is projectively curved toward the radial inside, which allows the air
circulating along the inner circumferential surface 22b of the shroud 22 to be smoothly
guided onto the radial outside. Consequently, the reduction in the blowing efficiency
of the blower 1 can further be prevented. As used herein, the expression "connected
to each other with the curved portion 223 interposed therebetween" means that the
lower end of the first inner circumferential surface 221 and the upper end of the
second inner circumferential surface 222 are smoothly connected to each other.
[0050] In addition, when the inner circumferential surface 22b of the shroud 22 includes
the first inner circumferential surface 221 formed in parallel to the axial direction,
a vertical thickness of the shroud 22 is secured by a predetermined width from the
upper end of the inner circumferential surface 22b, so that the reduction in rigidity
of the shroud 22 can be prevented.
[0051] Note that, Fig. 11 is an enlarged longitudinal sectional view illustrating the vicinity
of the shroud 22 of the blower 1 according to the modification of the exemplary embodiment
of the present invention. As illustrated in Fig. 11, the plane parallel to the axial
direction may be omitted in the inner circumferential surface 22b of the shroud 22.
In this case, the entire inner circumferential surface 22b is constructed with the
second inner circumferential surface 222. With this configuration, even if the impeller
20 vibrates vertically during the rotation, the reduction of the blowing efficiency
of the blower 1 can further be prevented.
[0052] Note that, in Figs. 10 and 11, the second inner circumferential surface 222 is projectively
curved toward the radial inside. Alternatively, the second inner circumferential surface
222 may be formed by a conical surface that is not curved but inclined with respect
to the axial direction so as to be away from the central axis A toward the lower side
in axial direction.
[0053] According to the embodiment, the inner diameter of the shroud 22 is formed equal
to or larger than the outer diameter of the base plate 21, so that the upper and lower
dies can be pulled out onto the upper side and the lower side in the axial direction,
respectively, while the mutual interference between the upper and lower dies is prevented.
Thus, the impeller 20 can integrally be molded using the die, and the mass productivity
of the impeller 20 can be improved.
[0054] In addition, the first projection 17 projects axially downward from the bottom surface
of the cover 14, and the first projection 17 is disposed on the radial inside of the
inner circumferential surface of the shroud 22. This enables the first projection
17 to block the passage of the air flowing backward onto the radial inside due to
the air flowing in the gap between the shroud 22 and the cover 14. Consequently, a
part of the air blown out to the radial outside of the impeller 20 is prevented from
flowing in the gap between the shroud 22 and the cover 14, and the degradation of
the blowing efficiency due to the generation of the turbulence or the air resistance
of the flowing-back air in the airflow passage 13 can be prevented.
[0055] In addition, the outer circumferential surface of the first projection 17 is radially
opposed to the inner circumferential surface of the shroud 22. Consequently, the radial
inside of the gap between the shroud 22 and the cover 14 is closed by the first projection
17, and the degradation of the blowing efficiency due to the generation of the turbulence
or the air resistance of the flowing-back air in the airflow passage 13 can be prevented.
Note that, in the embodiment, the radial gap between the outer circumferential surface
of the first projection 17 and the inner circumferential surface of the shroud 22
is kept constant in the axial direction. However, the radial gap between the outer
circumferential surface of the first projection 17 and the inner circumferential surface
of the shroud 22 may not be kept constant in the axial direction. For example, at
least one of the outer circumferential surface of the first projection 17 and the
inner circumferential surface of the shroud 22 may be curved.
[0056] The provision of the second projection 18, which projects axially downward from the
bottom surface of the cover 14 and is opposed to the outer circumferential surface
of the shroud 22, allows the second projection 18 to block the air flowing in the
gap between the shroud 22 and the cover 14. Consequently, a part of the air blown
out onto the radial outside of the impeller 20 is prevented from flowing in the gap
between the shroud 22 and the cover 14, and the degradation of the blowing efficiency
due to the generation of the turbulence or the air resistance of the flowing-back
air in the airflow passage 13 can be prevented.
[0057] Assuming that the region of the blade 23 located on the radial outside of the first
projection 17 is the blade first region, and that the region vertically opposed to
the first projection 17 is the blade second region, the upper end of the blade first
region is located above the upper end at the radially outer end of the blade second
region in the upper end of the blade 23. Thus, even if the impeller 20 vibrates vertically
during the rotation, the upper end of the blade 23 can be prevented from contacting
with the first projection 17. The blade 23 can axially be formed larger on the radial
outside of the first projection 17, and the amount of air generated by the rotation
of the impeller 20 can be increased.
[0058] The lower end of the inner circumferential surface 22b of the shroud 22 and the
lower end of the radially outer end of the first projection 17 have the substantially
identical height in the axial direction. Consequently, the air circulating toward
the radial outside along the bottom surface of the cover 14 is smoothly guided from
the lower end of the first projection 17 to the lower end of the inner circumferential
surface 22b of the shroud 22, and blown out to the radial outside of the impeller
20 through the bottom surface of the shroud 22. Thus, the blowing efficiency can further
be improved by reducing the air resistance of the first projection 17.
[0059] Note that, the lower end of the inner circumferential surface 22b of the shroud 22
may axially be located above the lower end of the radially outer end of the first
projection 17. Even in this case, the air circulating toward the radial outside along
the bottom surface of the cover 14 is smoothly guided from the lower end of the first
projection 17 to the lower end of the inner circumferential surface 22b of the shroud
22, so that the blowing efficiency of the blower 1 can be improved. In this configuration,
the radial gap between the inner circumferential surface 22b of the shroud 22 and
the radially outer end of the first projection 17 is also narrowed, so that a part
of the air blown out onto the radial outside of the impeller 20 can be prevented from
flowing backward from the gap between the shroud 22 and the cover 14.
[0060] The radially outer end of the blade 23 extends to the radial outside of the outer
circumference of the base plate 21, and the radially inner end of the blade 23 extends
to the radial inside of the suction port 11, so that the blade 23 can radially be
formed larger to increase the amount of air generated by the rotation of the impeller
20.
[0061] The axial gap between the lower end of the base plate protrusion 21a and the top
surface of the motor housing 16 is narrower than the axial gap between the bottom
surface of the base plate 21 and the top surface of the motor housing 16, so that
the base plate protrusion 21a blocks the airflow flowing in the axial gap between
the bottom surface of the base plate 21 and the top surface of the motor housing 16.
Consequently, a part of the air blown out onto the radial outside of the impeller
20 can be prevented from flowing in the gap between the bottom surface of the base
plate 21 and the top surface of the motor housing 16, and the degradation of the blowing
efficiency due to the generation of the turbulence or the air resistance of the flowing-back
air in the airflow passage 13 can be prevented.
[0062] The base plate protrusion 21a is located on the radially outer edge of the base plate
21. The groove 16b vertically opposed to the base plate protrusion 21a is provided
on the top surface of the motor housing 16. The groove 16b is larger than the base
plate protrusion 21a in the radial width. That is, the groove 16b is formed on the
top surface of the motor housing 16. The groove 16b is vertically opposed to the base
plate protrusion 21a and has the radial width larger than a radial width of the base
plate protrusion 21a. Thus, the base plate protrusion 21a is disposed close to the
groove 16b, so that the axial gap between the bottom surface of the base plate 21
and the top surface of the motor housing 16 can further be narrowed. Therefore, the
part of the air flowing in the gap between the bottom surface of the base plate 21
and the top surface of the motor housing 16 can further be prevented.
[0063] The above embodiment and modifications are merely examples of the present invention.
The configurations of the embodiment and modifications may appropriately be changed
without departing from the technical idea of the present invention. In addition, the
embodiment and the plurality of modifications may be may be implemented in combination
within a feasible range.
[0064] Furthermore, the blower 1 of the present invention is mounted on the cleaning robot
100 as illustrated in Fig. 1. Note that, the blower 1 may be mounted on not only the
cleaning robot 100 but also vacuum cleaners such as a handy cleaner. Consequently,
the vacuum cleaner having the high blowing efficiency can be constructed. The blower
1 may also be mounted on an apparatus other than the vacuum cleaner. For example,
the blower 1 of the present invention may be mounted on an electronic device such
as a personal computer for the purpose of internal cooling. The blower 1 of the present
invention may also be mounted on various other office automation instruments, medical
instruments, household electrical appliances, or transport instruments.
[0065] In addition, the detailed configuration of the blower 1 may be different from the
above embodiment and modifications. Furthermore, each element appearing in the embodiment
and the modifications may appropriately be combined within a range in which inconsistency
is not generated.
INDUSTRIAL APPLICABILITY
[0066] For example, the blower of the present invention having the high blowing efficiency
is suitable for the vacuum cleaner. Note that, the blower of the present invention
can also be used for other electronic devices.
REFERENCE SIGNS LIST
[0067]
- 1
- blower
- 10
- duct
- 11
- suction port
- 12
- air outlet
- 13
- airflow passage
- 14
- cover
- 14a
- cylindrical portion
- 15
- circumferential wall
- 15a
- nozzle
- 16
- motor housing
- 16a
- recess
- 16b
- groove
- 17
- first projection
- 18
- second projection
- 20
- impeller
- 21
- base plate
- 21a
- base plate protrusion
- 22
- shroud
- 22a
- opening
- 22b
- inner circumferential surface
- 23
- blade
- 23a
- first blade
- 23b
- second blade
- 24a, 24b
- radially outer end
- 25a, 25b
- protrusion
- 26a, 26b
- inclined surface
- 27a, 27b
- inclined surface
- 30
- motor
- 40
- control board
- 100
- cleaning robot
- 101
- chassis
- 103
- inlet port
- 104
- suction passage
- 105
- dust container
- 106
- filter
- 107
- exhaust passage
- 108
- exhaust port
- 109
- driving wheel
- 110
- front wheel
- 221
- first inner circumferential surface
- 222
- second inner circumferential surface
- 223
- curved portion
- A
- central axis
- D
- dust
- D1
- outer diameter
- D2
- inner diameter
- F
- floor
- R1
- air
- R2
- air
- L1
- blade first region
- L2
- blade second region
1. A blower comprising:
an impeller rotatable about a central axis extending in a vertical direction;
a motor that is positioned on a lower side of the impeller and rotates the impeller
about the central axis; and
a duct including an airflow passage in an inner space, a suction port through which
a fluid flows in the inner space, and an air outlet through which the fluid is discharged
from the inner space, the impeller being accommodated in the duct,
wherein
the impeller includes:
a plurality of blades arranged in a circumferential direction;
a shroud that has an annular shape, connects upper portions of the plurality of blades,
and includes an opening located opposite the suction port in an axial direction; and
a base plate that connects lower portions of the plurality of blades and extends in
a radial direction,
the duct includes a cover covering at least a part of the blade and an upper portion
of the shroud,
an inner diameter of the shroud is equal to or larger than an outer diameter of the
base plate, and
the cover includes a first projection that projects axially downward from a bottom
surface of the cover and is disposed on a radial inside of an inner circumferential
surface of the shroud.
2. The blower according to claim 1, wherein an outer circumferential surface of the first
projection is radially opposed to the inner circumferential surface of the shroud.
3. The blower according to claim 2, wherein a lower side in the axial direction is wider
than an upper side in the axial direction in a radial gap between the outer circumferential
surface of the first projection and the inner circumferential surface of the shroud.
4. The blower according to any one of claims 1 to 3, wherein
the blade includes:
a blade first region located on a radial outside of the first projection; and
a blade second region vertically opposed to the first projection, and
an upper end of the blade first region is located above an upper end at a radially
outer end of the blade second region.
5. The blower according to any one of claims 1 to 4, wherein the blade includes a protrusion
that protrudes axially upward on the radial outside of the first projection.
6. The blower according to any one of claims 1 to 5, wherein a lower end of the inner
circumferential surface of the shroud and a lower end of a radially outer end of the
first projection have a substantially identical height in the axial direction.
7. The blower according to any one of claims 1 to 6, wherein a radially outer end of
the blade extends to the radial outside of an outer circumference of the base plate.
8. The blower according to any one of claims 1 to 7, wherein the radially inner end of
the blade extends to the radial inside of the suction port.
9. The blower according to any one of claims 1 to 8, further comprising a motor housing
located below the base plate,
wherein
the base plate includes a base plate protrusion protruding downward from a bottom
surface of the base plate, and
an axial gap between the lower end of the base plate protrusion and a top surface
of the motor housing is narrower than an axial gap between the bottom surface of the
base plate and the top surface of the motor housing.
10. The blower according to claim 9, wherein
the base plate protrusion is located at a radially outer edge of the base plate, and
a groove is formed on the top surface of the motor housing, is vertically opposed
to the base plate protrusion, and has a radial width larger than a radial width of
the base plate protrusion.
11. A vacuum cleaner comprising the blower according to any one of claims 1 to 10.