BACKGROUND OF THE INVENTION
Field of the Invention
[0001] The present invention relates to a propeller fan and a heat source unit provided
with the propeller fan.
Description of the Related Art
[0002] Conventionally, a propeller fan has been used as a fan of a variety of heat source
units such as an outdoor unit of an air conditioner, a heat source machine for a water
heater with a heat pump, and an outdoor unit of a refrigerating (freezing) machine.
A known example of such a conventional propeller fan is described in Patent Document
1 (Japanese Patent Laid-Open No.
2005-140081).
[0003] The conventional propeller is formed with substantially circular-arc shaped recesses
at a blade rear edge portion as air blow-out portion during the rotation of the fan,
and the circular-arc shaped recesses are recessed in direction opposite to an air
blowing direction, thereby suppressing the generation of the trailing vortices from
the blades to reduce noise which will be generated at the time of blowing air.
[0004] Such a conventional propeller fan, however, has arc-shaped recess portions which
have the same shape and size in a plurality of blades, and accordingly, peak frequencies
of blade pitch sound generated by trailing vortices of the respective blades are in
consonance with each other, which unfortunately does not effectively reduce the blowing
air noise, thus being inconvenient.
SUMMARY OF THE INVENTION
[0005] The present invention was conceived in consideration of the above conventional circumstances,
and an object thereof is to provide a propeller fan capable of improving the reduction
in blowing (or blown) air noise and also provide a heat source unit including such
propeller fan.
[0006] The above and other objects can be achieved according to the present invention by
providing, in one aspect, a propeller fan having a plurality of blades fixed to a
hub on a rotation axis of the fan, wherein each of the blades has a recess portion
formed in a blade rear edge section as air blow-out portion during rotation of the
fan, the recess portions of the respective blades being recessed in a direction opposite
to air blow-out direction and being different in size.
[0007] In a preferred embodiment of the above aspect, It may be desired that the recess
portions of the blades are formed such that perpendicular lines drawn from line segments
joining inner endpoints and outer endpoints of the blade rear edge sections to deepest
points of the recess portions are different from each other in lengths thereof.
[0008] It may be also desired that the recess portions are formed such that a length of
the line segments "a" and lengths of the perpendicular lines "b" of the blades satisfy
relationship of "0.1a ≤ b ≤ 0.5a" and the lengths "b" in the blades are different
from each other.
[0009] It may be also preferred that a number of the blades is three, and the lengths of
the perpendicular lines b1, b2 and b3 of the blades are determined so as to satisfy:
"b1 ≤ b2 < b3", "0.1a ≤ b1 ≤ 0.35a", "0.15a ≤ b2 ≤ 0.4a", and "0.2a ≤ b3 ≤ 0.5a."
[0010] In another aspect of the present invention, there is also provided a heat source
unit comprising: a unit housing; a propeller fan of the structures mentioned above
and housed in the unit housing; an outdoor heat exchanger housed in the unit housing
through which the propeller fan blows air; and a fan motor mounted to the unit housing
for driving the propeller fan.
[0011] According to the propeller fan of the structures mentioned above, blown or blowing
air noise can be effectively reduced, and by taking particular size or dimensions
of the recess portions formed to the fan blades, the above effects can be further
improved. The heat source unit as outdoor unit of an air conditioner, for example,
provided with the above propeller fan can attain the same or like effects as mentioned
above.
[0012] The nature and further characteristic features of the present invention will be made
clearer from the following descriptions made with reference to the accompanying drawings.
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] In the accompanying drawings
Fig. 1 is a front view illustrating a propeller fan according to an embodiment of
the present invention;
Fig. 2 is a perspective view illustrating the propeller fan in Fig. 1;
Fig. 3 is a view illustrating a blade rear edge section, in an enlarged scale, of
the propeller fan in Fig. 1;
Fig. 4 is a table of experimental data on air blowing performance of the three-bladed
propeller fan illustrated in Fig. 1;
Fig. 5 is a graph illustrating the relative relationship between dimensions of blade
rear edge recess portions and blowing air noises in the experimental data shown in
Fig. 4; and
Fig. 6 is a schematic cross-sectional view illustrating a heat source unit, according
to another embodiment of the present invention, including the three-bladed propeller
fan in Fig. 1.
DESCRIPTION OF THE PREFERRED EMBODIMENT
[0014] Embodiments of the present invention will be described in detail hereunder with reference
to the accompanying drawings. Further, it is to be noted that the same or corresponding
components or parts are denoted by adding the same reference numerals throughout the
drawings.
(First Embodiment)
[0015] Fig. 1 is a front view illustrating a propeller fan according to a first embodiment,
and Fig. 2 is a perspective view thereof.
[0016] A propeller fan 1 is entirely made of plastic compounded of glass fiber and ASG (Acrylonitrile
Styrene Glass) resin, for example, and three blades 4, 5 and 6 having similar shapes
are circumferentially installed at substantially regular intervals to a hub 3 on a
fan rotation shaft 2 (i.e., rotation axis of a fan motor, not shown), as illustrated
in Figs. 1 and 2. Each of the blades 4, 5 and 6 has substantially arc-shaped (arcuate)
blade rear edge recess portions 4b, 5b and 6b, respectively, in blade rear edge sections
4a, 5a and 6a (the term "rear edge" is used herein in the fan rotating direction as
shown with a black arrow in Fig. 1). The portions 4b, 5b and 6b are recessed in direction
opposite to air flow denoted by a white arrow in Fig. 1.
[0017] The arcuate recess portions 4b, 5b and 6b formed to the respective blades are different
from each other in size. Specifically, if perpendicular lines b1, b2 and b3 are drawn
from line segments "a" joining inner endpoints P and outer endpoints Q to deepest
points 4R, 5R and 6R of the respective recess portions 4b, 5b and 6b, the lengths
of these perpendicular lines b1, b2 and b3 (depths of the recess portions 4b to 6b)
are not smaller than 0.1a and not greater than 0.5a (0.1a ≤ b1, b2, b3 ≤ 0.5a), and
"b1 < b2 < b3".
[0018] That is, different lengths of the perpendicular lines b1, b2 and b3 lead to different
sizes of the recess portions 4b, 5b and 6b.
[0019] Furthermore, in the present embodiment, the recess portions 4b, 5b and 6b are formed
so that the lengths of the perpendiculars b1, b2 and b3 and the length of line segments
"a" satisfy the following relationship: "0.1a ≤ b1 ≤ 0.35a", "0.15a ≤ b2 ≤ 0.4a",
and "0.2a ≤ b3 ≤ 0.5a". Further, the line segments "a" in the blades 4, 5 and 6 have
the same length.
[0020] According to the present embodiment of the characters mentioned above, since the
difference in the lengths of the perpendicular lines b1, b2 and b3 in the recess portions
4b, 5b and 6b of the three fan blade also lead to the difference in sizes of the recess
portions 4b, 5b and 6b as previously described, the peak frequencies and phases of
blade sound generated by trailing vortices from the blades 4, 5 and 6 during the rotation
of the fan can be shifted to suppress consonance, and thereby the reduction in blowing
(blown) air noise can be improved.
[0021] Fig. 4 shows experimental data on air blowing performance of the propeller fan 1
illustrated in Fig. 1.
[0022] In the experiment, first to sixth test models #1 to #6 were prepared, which test
models each include its own propeller fan 1 of a required size, such as a diameter
of 420 mm. The dimensions of the perpendicular lines b1, b2 and b3 indicating the
depths of the recess portions 4b, 5b and 6b, respectively, varied within a range from
0.1a to 0.5a (0.1a ≤ b1, b2, b3 ≤ 0.5a) to satisfy the relationship "0.1a ≤ b1 ≤ 0.35a",
"0.15a ≤ b2 ≤ 0.4a", and "0.2a ≤ b3 ≤ 0.5a".
[0023] These six test models #1 to #6 were then operated at 800 rpm with an amount of air
being 2080 m
3/h, and a blown air noise value (dB(A)) was measured at a position being 1 m (1 meter)
apart from each fan in the air blowing direction.
[0024] Further, in this experiment, a three-bladed propeller fan, that is a conventional
model, was also prepared. The three recess portions 4b to 6b of the fan were the same
in depth (b1, b2, b3 : 0.2a), shape, and size. The model was operated under the same
condition as that of the first embodiment and a blown air noise value (dB(A)) and
the like were also shown in Fig. 4 as conventional fan in the table.
[0025] Fig. 5 shows the values of air noise blown from the propeller fan 1 of the present
embodiment and the conventional model shown in Fig. 4, and in Fig. 5, a curve Na represents
the one of the present embodiment and a substantially straight line Nb represents
the conventional model fan.
[0026] Fig. 5 also shows relationship between dimension ratios of the perpendiculars b1,
b2, and b3 (b1 : b2 : b3) denoting the depths of the recess portions 4b, 5b, and 6b,
respectively, and the noise values dB(A) during the rotation of the fans. A smallest
value of blown air noise, 46 dB, was given when a dimension ratio of the perpendiculars
b1, b2, and b3 was "0.2a : 0.23a : 0.26a." In other words, the test model #3, whose
b1 was 0.2a, b2 was 0.23a, and b3 was 0.26a, resulted in the smallest value of blown
air noise. On the other hand, the conventional model fan resulted in a constant noise
value of about 47.2 dB(A).
[0027] As the lengths of the perpendicular lines b1, b2 and b3 were gradually decreased
or increased from the minimum value of the blown air noise, a value of the blown air
noise gradually increases.
[0028] However, if the lengths of the perpendicular lines b1, b2 and b3 satisfy the following
relationship of "b1 < b2 < b3", "0.1a ≤ b1 ≤ 0.35a", "0.15a ≤ b2 ≤ 0.4a", and "0.2a
≤ b3 ≤ 0.5a", the blown air noise does not become greater than about 46.9 dB(A), and
hence, the noise is smaller than the noise value Nb, about 47.2 dB(A), of the conventional
model denoted by the substantially straight line shown in Fig. 5. In addition, an
input power of the motor is also smaller than that of the conventional model as illustrated
in Fig. 4, thereby also improving the motor efficiency. Accordingly, it is considered
to be preferable that the range of the perpendicular lines is set as mentioned above.
(Second Embodiment)
[0029] Fig. 6 is a schematic cross-sectional view illustrating an outdoor unit 11 of an
air conditioner as a heat source unit according to the present second embodiment provided
with the propeller fan of the structure mentioned above.
[0030] The outdoor unit 11 of the air conditioner has an outdoor heat exchanger 13 having
a planar L-shape, the propeller fan 1 according to the first embodiment, a compressor
14, a four-way valve 15 and a controller 16 such as an inverter in a unit housing
12.
[0031] In Fig. 6, reference numeral 17 denotes a partition plate separating a space inside
the outdoor unit 1 into a space for the propeller fan 1 and the outdoor heat exchanger
13, and a space for the compressor 14. Reference numeral 18 denotes a support member
supporting a fan motor 19 that drives the propeller fan 1.
[0032] Since the outdoor unit 11 includes the propeller fan 1, which can improve the reduction
in noise of the blown air as described with reference to the above first embodiment,
the outdoor unit 11 can achieve the improved reduction in the blown air noise.
[0033] It is to be noted that although the present invention was explained hereinbefore
with reference to the some embodiments, the present invention is not limited to such
embodiments, and many other changes and modifications or alternations, particularly,
in type, size, shape or like, may be made without departing from the sprits or scopes
of the appended claims.
[0034] It is explicitly stated that all features disclosed in the description and/or the
claims are intended to be disclosed separately and independently from each other for
the purpose of original disclosure as well as for the purpose of restricting the claimed
invention independent of the composition of the features in the embodiments and/or
the claims. It is explicitly stated that all value ranges or indications of groups
of entities disclose every possible intermediate value or intermediate entity for
the purpose of original disclosure as well as for the purpose of restricting the claimed
invention, in particular as limits of value ranges.
1. A propeller fan (1) having a plurality of blades (4, 5, 6) fixed to a hub (3) on a
rotation axis (2) of the fan (1),
wherein each of the blades (4, 5, 6) has a recess portion (4b, 5b, 6b) formed in a
blade rear edge section (4a, 5a, 6a) as air blow-out portion during rotation of the
fan (1), the recess portions (4b, 5b, 6b) of the respective blades (4, 5, 6) being
recessed in a direction opposite to air blow-out direction and being different in
size.
2. The propeller fan (1) according to claim 1, wherein the recess portions (4b, 5b, 6b)
of the blades (4, 5, 6) are formed such that perpendicular lines (b1, b2, b3) drawn
from line segments (a) joining inner endpoints (P) and outer endpoints (Q) of the
blade rear edge sections (4a, 5a, 6a) to deepest points (4R, 5R, 6R) of the recess
portions (4b, 5b, 6b) are different from each other in lengths thereof.
3. The propeller fan (3) according to claim 1 or 2, wherein the recess portions (4b,
5b, 6b) are formed such that a length of the line segments "a" and lengths of the
perpendicular lines "b" of the blades (4, 5, 6) satisfy relationship of "0.1a ≤ b
≤ 0.5a" and the lengths "b" in the blades (4, 5, 6) are different from each other.
4. The propeller fan (1) according to any one of claims 1 to 3, wherein a number of the
blades (4, 5, 6) is three, and the lengths of the perpendicular lines b1, b2 and b3
of the blades (4, 5, 6) are determined so as to satisfy: "b1 < b2 < b3", "0.1a ≤ b1
≤ 0.35a", "0.15a ≤ b2 ≤ 0.4a", and "0.2a ≤ b3 ≤ 0.5a".
5. A heat source unit (11)comprising:
a unit housing (12);
a propeller fan (1) according to any one of claims 1 to 4 housed in the unit housing
(12);
an outdoor heat exchanger (13) housed in the unit housing (12) through which the propeller
fan (1) blows air;
a fan motor (19) mounted to the unit housing (12) for driving the propeller fan (1).