The present invention relates to an axial flow fan, and more particularly, to an axial flow fan capable of promoting structural stability so as to decrease deformation and unbalance of a blade and accomplishing low noise level.
As shown in
A shroud 60 fixed to the heat exchanger is used to guide efficiently the air blown by the axial flow fan 10. The shroud 60 is formed so as to have a blowhole which is sized so that the axial flow fan 10 can be rotatably inserted therein, and support the motor 50 which is a driving source.
In the blade 30 of a conventional axial flow fan 10, as shown in
As shown in
As shown in
According to the axial flow fans 10a and 10b having the above mentioned waveform structured blades 30a and 30b respectively, an area between inflection points P1 and P2 located on a mid-chord line, which runs along middle points between the leading edge LE and the trailing edge TE, works as an area for dispersing air flow and thus prevent the air flow from being concentrated, thereby capable of increasing blowing efficiency and reducing noise compared to the axial flow fan shown in FIG. 1 and
As shown in
In addition, the distribution angle A1 of the blade can be moved by a predetermined angle in a rotational direction (+) or an opposite direction of the rotation (−) of the axial flow fan in the equiangular distribution angle, and at this time a range in which the angle can be increased or decreased is referred as a clearance angle B. In other words, it can be expressed by an equation: the distribution angle A1 of the blade=an equiangular distribution angle X the clearance angle B.
Meanwhile, U.S. Pat. No. 5,000,660 discloses an axial flow fan with a blade of an uneven structure in which curvatures from a root of the blade to a tip of the blade are different at least between two blades, and the axial flow fan is suggested for the purpose of increasing rigidity of a portion of the root of the blade and reducing noise in a portion of the tip of the blade. However, in the conventional axial flow fans with above described waveform structure, there are problems that unbalance is occurred when the axial flow fans rotate and satisfactory noise reduction effect can not be achieved if the clearance angle B is set to be excessively large.
An object of the present invention is to provide an axial flow fan capable of promoting structural stability so as to decrease deformation and unbalance of a blade and accomplishing low noise level by determining a distribution angle of the blade with an optimum clearance angle and thereby determining uneven rate of the blade.
An axial flow fan according to a preferred embodiment of the present invention includes a hub; a plurality of blades arranged radially in a circumference of the hub and having a sweeping angle of which direction changes alternately in an area between a root and a tip of the blade; and a fan band for connecting integrally the tips of the each blade; wherein when assuming that an angle between two lines which pass through a center of the hub and the middle of each root of the blade, respectively, where the adjacent two blades and the hub come into contact, is a distribution angle A1 of the blade, and an angle of an equiangular distribution angle is 360/n in the case that a number of the blades is n, the blades are arranged so that the clearance angle is in a range of 4° to 9°, while satisfying an equation: distribution angle (A1) of the blade=equiangular distribution angle±clearance angle.
According to a preferred embodiment of the present invention, it is preferable that the clearance angle is in the range of 6° to 7° In addition, it is preferable that when assuming that an angle between two lines which pass through a center of the hub and middles of each root of the blade, respectively, where the adjacent two blades and the hub come into contact is, a hub-side distribution angle of the blade, and an angle between two lines which pass through a center of the hub and middles of each tip of the two blades, respectively is a tip-side distribution angle of the blade, the hub-side distribution angle of blade and the tip-side distribution angle of blade are same.
In addition, the blade has the sweeping angle which changes gradually as it goes from the tip of the blade having a forward angle to the root of the blade having a backward angle and connected to the hub and a plurality of flow dispersing areas between the forward angle area of a side of the tip of the blade and the backward angle area of a side of the root of the blade, in which a direction of the sweeping angle is alternately reversed.
At this time, it is preferable that the blade has a leading edge extending from the tip of the blade to the root of the blade, and a direction of a sweeping angle of the leading edge changes gradually from a maximum backward angle at the root of the blade to a maximum forward angle at the tip of the blade, wherein the direction of the sweeping angle is reversed from the backward angle at a side of the root of the blade to a forward angle, then reversed to a backward angle and reversed again to a forward angle so as to be connected to a forward angle at a side of the tip of the blade. Further, it is preferable that the blade has a trailing edge extending from the tip of the blade to the root of the blade, and a changing pattern of a sweeping angle of the trailing edge is as same as that of the leading edge.
The above and other objects, features and advantages of the present invention will become apparent from the following description of preferred embodiments given in conjunction with the accompanying drawings, in which:
Hereinafter, the preferred embodiments of the present invention are described in detail with reference to accompanying drawings.
In accordance with an aspect of the present invention, when assuming that an angle between two lines L1 and L2 which pass through a center C of the hub 110 and middles C1 and C2 of each root 122 of the blade, respectively, where the adjacent two blades 120 and the hub 110 come into contact, is a distribution angle A1 of the blade, a range of an angle by which the distribution angle A1 of the blade is movable in a rotational direction (+) or an opposite direction of rotation (−) of the axial flow fan 100 is a clearance angle, and a number of the blade is n, an equiangular distribution, representing an interval by which the blades are arranged, can be defined by 360/n.
In other words, the blades 120 can be exemplary arranged in interval of 40°, an actual angular distribution of the blade 120 can be moved in the rotational direction (+) or the opposite direction of rotation (−) of the axial flow fan 100 by a predetermined angle in the range of the clearance angle. The distribution angle A1 of the blade 120 can be expressed by an equation: a distribution angle A1 of the blade=an equiangular distribution angle±a clearance angle, and the clearance angle is preferably in a range of 4° to 9° and more preferably in a range of 6° to 7°.
Further, when assuming that an angle A1r between two lines L1 and L2 which pass through center C of the hub 110 and the middle C1 and C2 of each root 122 of the blade, respectively, where the adjacent two blades 120 and the hub 110 come into contact is a hub-side distribution angle of the blade and an angle A1t between two lines L3 and L4 which pass through center C of the hub 110 and the middle C3 and C4 of each tip 124 of the two blades 120, respectively is a tip-side distribution angle of the blade, it is preferable that the hub-side distribution angle A1r of blade and the tip-side distribution angle A1t of blade are same.
In other words, the leading edge LE of the blade 120 is formed such that the direction of the sweeping angle gradually changes from backward at a side of root 122 of the blade in an order of forward, backward and forward, and finally to forward at a side of the tip 124 of the blade between a backward area of the side of the root 122 of the blade 120 and a forward area of the side of the tip 124 of the blade 120.
Further, as shown, the trailing edge TE of the blade 120 is also formed as same pattern as the leading edge LE, that is, such that the direction of the sweeping angle gradually changes from backward at a side of root 122 of the blade in an order of forward, backward and forward, and finally to forward at a side of the tip 124 of the blade between the backward area of the side of the root 122 of the blade 120 and the forward area of the side of the tip 124 of the blade 120.
As described above, the flow dispersing area D forms two flow concentrating parts S1 and S2 at which flows are concentrated to a side of the trailing edge TE and thus acts to lessen greatly concentration of the flow, thereby increasing a blowing efficiency relative to power consumption and greatly reducing noise generation.
In the graphs of
Table 1 lists data of variation in overall noise according to the clearance angle and
In the above table 1 and
With the above described axial flow fan according to the present invention, it is capable of promoting silence operation of an apparatus which employs an axial flow fan as noise can be greatly reduced compared to the conventional axial flow fan by determining the distribution angle of the blade 120 with an optimum clearance angle. Further, blowing efficiency and noise reduction effect can be much increased by adjusting the clearance angle as well as forming the flow dispersing area on the blade.
In addition, as the axial flow fan according to the present invention can generate much air flow rate even in low rpm compared to the conventional one, it is capable of promoting structural stability and thus increasing durability of the axial fan.
Number | Date | Country | Kind |
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10-2006-0010535 | Feb 2006 | KR | national |
10-2007-0001552 | Jan 2007 | KR | national |
The present application is based on, and claims priority from, KR Application Number 10-2006-0010535, filed Feb. 3, 2006; KR Application Number 10-2007-0001552, filed Jan. 5, 2007; and PCT Application Number PCT/KR2007/000234, filed Jan. 15, 2007, the disclosures of which are hereby incorporated by reference herein in their entireties.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/KR2007/000234 | 1/15/2007 | WO | 00 | 9/20/2011 |