Patent Grant
10480526
This application is a U.S. national stage application of PCT/JP2015/080884 filed on Nov. 2, 2015, the contents of which are incorporated herein by reference.
The present invention relates to an axial flow fan including a plurality of blades, and an air-conditioning apparatus including the axial flow fan.
An existing axial flow fan includes a plurality of blades along the circumferential surface of a cylindrical boss, and forces a fluid to move by the blades being rotated by rotary force provided to the boss. In the axial flow fan, the fluid present between the blades collides against the surfaces of the blades by rotation of the blades. At each surface against which the fluid collides, the pressure increases and pushes out and moves the fluid in the direction of the rotation axis about which the blades rotate.
In such an axial flow fan, to achieve a decrease in noise and an increase in efficiency, there is an example in which a backward-tilted blade that is tilted toward downstream relative to the flowflow direction of the fluid in a blade cross-section, in a radial direction, passing through the rotation axis of the blade, is used. In addition, there is an example in which an outer circumference reflexed portion (winglet) is formed in the neighborhood of the outer circumferential edge of a blade so as to be reflexed toward upstream relative to the flow direction of the fluid (see Patent Literature 1).
Patent Literature 1: Japanese Unexamined Patent Application Publication No. 2015-34503
In such an existing axial flow fan, an air current flows at the outer circumferential edge side of the blade from a pressure surface of the blade to a suction surface of the blade, thereby generating a spiral blade edge eddy. The blade edge eddy is formed at a distance from the suction surface of the blade. Accordingly, there is a problem in that the inflow air current flowing in from the leading edge of the blade collides against the blade edge eddy formed at the suction surface of the blade, whereby the air sending efficiency of the axial flow fan decreases, and noise is generated, for example.
The present invention has been made to solve such a problem of the axial flow fan, and an object of the present invention is to provide: an axial flow fan that inhibits an inflow air current flowing in from a leading edge of a blade from colliding against a blade edge eddy formed at a suction surface side of the blade and that achieves a decrease in noise and an increase in efficiency by causing the inflow air current to smoothly flow on the blade edge eddy; and an air-conditioning apparatus including the axial flow fan.
An axial flow fan according to an embodiment of the present invention includes a plurality of blades, each of the blades including a leading edge formed in front in a direction of rotation of the axial flow fan, an inner circumferential edge formed at an inner circumference of the blades, and an outer circumferential edge formed at an outer circumference of the blades, the outer circumferential edge being located at downstream in a flow direction of a fluid, forced to move by the axial flow fan, than the inner circumferential edge, the blade being reflexed toward upstream of the fluid at a portion adjacent to the outer circumferential edge, and having a local angle-decrease section having a blade inlet angle at the leading edge decreasing from neighborhood, the local angle-decrease section being formed at a side of the leading edge and being located closer to the outer circumferential edge than to the inner circumferential edge.
In the axial flow fan according to the example of the present invention, by providing the local angle-decrease section having the blade inlet angle α decreasing from neighborhood, the local angle-decrease section being formed at the side of the blade and located closer to the outer circumferential edge at which there is influence of a blade edge eddy, a main air current flowing in from the leading edge of the blade stably flows on the blade edge eddy, whereby it is possible to achieve a decrease in noise and an increase in efficiency of the axial flow fan.
<Entire Configuration of Axial Flow Fan>
First, the entire configuration of an axial flow fan 100 according to Embodiment 1 will be described.
As shown in
Each blade 2 is formed so as to be surrounded by: a leading edge 21 located in front in a direction of rotation RT; a trailing edge 22 located in back in the direction of rotation RT; an outer circumferential edge 23 forming an outer periphery; and an inner circumferential edge 24 forming an inner periphery.
As shown in
Similarly, as shown in
The outer circumferential edge 23 is formed so as to connect the outer end of the leading edge 21 to the outer end of the trailing edge 22 and is located substantially on a circumference having a center at the rotation axis RC. The blade chord length of the blade 2 is the longest in the neighborhood of the outer circumferential edge 23.
Each blade 2 is formed so as to be tilted at a predetermined angle relative to the rotation axis RC. Each blade 2 presses a fluid present between the blades 2, with a blade surface thereof, with rotation of the axial flow fan 100, to force the fluid to flow in a flow direction F1 of the fluid. At this time, the surface that presses the fluid to increase the pressure, of the blade surfaces, is referred to as pressure surface 2a, and the surface that is a back surface of the pressure surface 2a and on which the pressure decreases is referred to as suction surface 2b (see
The blade 2 of the axial flow fan 100 according to Embodiment 1 is formed as a backward-tilted blade that is tilted toward downstream relative to the flow direction F1 of the fluid in the radial direction of the blade 2 in a cross-sectional shape of the blade 2 as shown in
<Configuration of Leading Edge 21 at Inner Circumferential Edge 24 Side>
Next, a mount angle of the leading edge 21 at the inner circumferential edge 24 side of the blade 2 will be described with reference to a blade chord direction cross-sectional view shown in
The tangent line to the suction surface 2b at the leading edge 21 of the blade 2 is referred to as leading edge tangent line 21a, a straight line parallel to the rotation axis RC is referred to as axial imaginary line RC′, and the angle formed by the leading edge tangent line 21a and the axial virtual line RC′ is referred to as blade inlet angle α. In addition, the blade inlet angle α at an inner circumferential side leading edge 11 that is the inner circumferential edge 24 side of the leading edge 21 is particularly referred to as blade inlet angle α1. In addition, the angle formed by an inflow air current F2 and the axial virtual line RC′ is referred to as inflow angle β.
In this case, as shown in
<Configuration of Leading Edge 21 at Outer Circumferential Edge 23 Side>
Next, a mount angle of the leading edge 21 at the outer circumferential edge 23 side of the blade 2 will be described with reference to a blade chord direction cross-sectional view shown in
Similarly to the cross-sectional view at the inner circumferential edge 24 side of the blade 2 in
In this case, the blade inlet angle α2 of the leading edge 21 at the outer circumferential edge 23 side of the blade 2 is set so as to be smaller than the blade inlet angle α1 of the leading edge 21 at the inner circumferential edge 24 side of the blade 2. A region where the leading edge 21 is formed at the blade inlet angle α2 is defined as local angle-decrease section 10. The boundary between the blade inlet angle α1 of the inner circumferential side leading edge 11 of the blade 2 and the blade inlet angle α2 in the local angle-decrease section 10 is set, for example, at an intermediate position in the radial length of the blade 2 shown in
As described above, each blade 2 is shaped as a backward-tilted blade that is tilted toward downstream relative to the flow direction F1 of the fluid as coming closer to the outer circumferential edge 23, and the outer circumference reflexed portion 26 is formed in the neighborhood of the outer circumferential edge 23 so as to be reflexed toward upstream relative to the flow direction F1.
Accordingly, the flow rate or the magnitude of the eddy diameter of the blade edge eddy 3 is reduced as compared to that in the case where the blade 2 is shaped as a forward-tilted blade, and an air current smoothly flows in from the pressure surface 2a of the blade 2 to the suction surface 2b of the blade 2 due to the outer circumference reflexed portion 26, to generate the spiral blade edge eddy 3 as shown in
Due to such a configuration of the blade 2, the blade edge eddy 3 is stably formed, and is also formed at a distance from the suction surface 2b of the blade 2. Therefore, pressure fluctuations on the suction surface 2b of the blade 2 are reduced, so that it is possible to achieve a decrease in noise and a reduction in power consumption of the axial flow fan 100.
As described above, since the blade 2 is shaped as a backward-tilted blade and has the outer circumference reflexed portion 26, the blade edge eddy 3 is formed at a distance from the suction surface 2b of the blade 2, and thus it is possible to achieve a decrease in noise and a reduction in power consumption of the axial flow fan 100. A main air current F3′ flowing in from the leading edge 21 of the blade 2 flows beyond the blade edge eddy 3 as shown in
Accordingly, the inflow angle β of the inflow air current F2 flowing in from the leading edge 21 and the blade inlet angle α2 of the leading edge 21 become hard to be equal to each other due to influence of the blade edge eddy 3 formed at a distance from the suction surface 2b of the blade 2. The angle formed by the axial virtual line RC′ and an inflow direction 21a′ of the main air current F3′ at the leading edge 21 of the blade 2 is referred to as main air current angle α′.
Thus, by providing the local angle-decrease section 10 having the blade inlet angle α2 decreasing from neighborhood so as to be smaller than the blade inlet angle α1 of the inner circumferential side leading edge 11, the local angle-decrease section 10 being formed at the side of the blade 2 and located closer to the outer circumferential edge 23 at which there is influence of the blade edge eddy 3, it is possible to make the main air current angle α′ and the inflow angle β substantially equal to each other as shown in
In Embodiment 1, the example has been described in which the blade inlet angle α2 of the leading edge 21 at the outer circumferential edge 23 side of the blade 2 is formed so as to be smaller than the blade inlet angle α1 of the leading edge 21 at the inner circumferential edge 24 side of the blade 2. Embodiment 2 is different from Embodiment 1 in that the shape of the local angle-decrease section 10 having the blade inlet angle α2 is specified. The other basic configuration of the axial flow fan 100 is the same as in Embodiment 1, and thus the description thereof is omitted.
Change of the blade inlet angle α of the leading edge 21 of the blade 2 according to Embodiment 2 in the radial direction will be described with reference to
On the horizontal axis, a radial direction ratio P=(R−Rb)/(Rt−Rb) is used as a parameter indicating a target position for the blade inlet angle α. Here, each variable is as follows.
R: radial length from the rotation axis RC to a target position for the blade inlet angle α.
Rb: radial length of the boss portion 1 represented by the distance from the rotation axis RC to the outer circumferential surface of the boss portion 1.
Rt: maximum radial length from the rotation axis RC to the outer circumferential edge 23 of the blade 2.
The blade inlet angle α increases as the radial direction ratio P=(R−Rb)/(Rt−Rb) moves and increases from the inner circumferential edge 24 of the blade 2 (the outer circumferential surface of the boss portion 1), at which the radial direction ratio P=(R−Rb)/(Rt−Rb) is P=0 (R=Rb), toward the outer circumferential edge 23.
When a curve of the blade inlet angle α at this time is obtained as a function of the radial direction ratio P, the curve of blade inlet angle α is represented, for example, as the following equation (1).
[Math. 1]
α=A*P3−B*P2+C*P+D (1)
A to D are positive coefficients.
The blade inlet angle α has the local angle-decrease section 10 in which the value of the blade inlet angle α decreases from neighborhood, at the outer circumferential edge 23 of the blade 2 at which the radial direction ratio P=(R−Rb)/(Rt−Rb) is P=1.0 (R=Rt).
The local angle-decrease section 10 is formed as a section of the radial direction ratio P in which the blade inlet angle α is away downward from the curve of the above equation (1) as shown in
Thus, the local angle-decrease section 10 has a first point of intersection A at one end side thereof and a second point of intersection C at the other end side thereof, as a point away downward from the curve of the equation (1). At this time, at the first point of intersection A, the blade inlet angle α=αR1, and the radial length R is R1 as shown in
In addition, the local angle-decrease section 10 has a minimum point B at which the blade inlet angle α decreasing from the blade inlet angle α=αR1 at the first point of intersection A toward the outer circumferential edge 23 changes to increase again. At this time, at the minimum point B, the blade inlet angle α=αRs, and the radial length R is Rs as shown in
Then, the local angle-decrease section 10 has the second point of intersection C at which the blade inlet angle α increasing from the blade inlet angle α=αRs at the minimum point B intersects the curve of the equation (1) again. At this time, at the second point of intersection C, the blade inlet angle α=αR2, and the radial length R is R2 as shown in
The local angle-decrease section 10 also has an intermediate point D at which the radial length R=Rm that is the intermediate between R1 and R2.
Thus, the local angle-decrease section 10 is formed at the leading edge 21 of the blade 2 so as to start from the radial length R=R1 at the first point of intersection A, pass through the radial length R=Rs at the minimum point B, and reach the radial length R=R2 at the second point of intersection C. That is, the local angle-decrease section 10 is formed with the first point of intersection A and the second point of intersection C as both ends thereof.
The local angle-decrease section 10 of the blade inlet angle α according to Modification 2 of Embodiment 2 is formed such that the radial length R=Rs at the minimum point B is shorter than the radial length R=Rm at the intermediate point D and the minimum point B is located closer to the inner circumferential edge 24 than the intermediate point D, as shown in
The advantageous effects achieved by the above-described configuration will be described with reference to
As shown in
Accordingly, as shown in
Here, since the blade 2 according to Embodiment 2 is a backward-tilted blade, the position of a perpendicular line from the center 3a of the blade edge eddy 3 to the suction surface 2b at which position the eddy diameter of the blade edge eddy 3 becomes a maximum value Lmax, is geometrically closer to the inner circumferential edge 24 than the position at which the radial length R=Rm.
That is, by making the blade inlet angle α have a minimum at the radial length R=Rs that is smaller than the radial length R=Rm at the intermediate point D, the position at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax and the position at which the blade inlet angle α has the minimum substantially coincide with each other.
Therefore, even at the radial length R of the blade 2 at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax, it is possible to make the main air current angle α′ and the inflow angle β shown in
<Modification 1 of Embodiment 2>
In the axial flow fan 100 according to Embodiment 2, the curve of the blade inlet angle α is represented as a function of the radial direction ratio P by the above equation (1) in which the blade inlet angle α also increases as the radial direction ratio P increases. In the axial flow fan 100 according to Modification 1, the curve of the blade inlet angle α is formed by the following equation (2) in which the blade inlet angle α decreases as the radial direction ratio P increases. The other configuration of the axial flow fan 100 is the same as in Embodiment 2.
[Math. 2]
α=−E*P3+F*P2−G*P+H (2)
E to H are positive coefficients.
The curve of the equation (2) indicating change of the blade inlet angle α is formed such that the blade inlet angle α decreases as the radial direction ratio P increases as shown in
Similarly to Embodiment 2, the blade inlet angle α has a local angle-decrease section 10 in which the value of the blade inlet angle α decreases from neighborhood, at the outer circumferential edge 23 of the blade 2 at which the radial direction ratio P is P=1.0 (R=Rt).
The local angle-decrease section 10 is formed as a section of the radial direction ratio P in which the blade inlet angle α is away downward from the curve of the above equation (2) as shown in
Thus, the local angle-decrease section 10 has a first point of intersection A at one end side thereof and a second point of intersection C at the other end side thereof, as a point away downward from the curve of the equation (2). At this time, at the first point of intersection A, the blade inlet angle α=αR1, and the radial length R is R1 as shown in
In addition, the local angle-decrease section 10 has a minimum point B at which the blade inlet angle α decreasing from the blade inlet angle α=αR1 at the first point of intersection A toward the outer circumferential edge 23 changes to increase again. At this time, at the minimum point B, the blade inlet angle α=αRs, and the radial length R is Rs as shown in
Then, the local angle-decrease section 10 has the second point of intersection C at which the blade inlet angle α increasing from the blade inlet angle α=αRs at the minimum point B intersects the curve of the equation (2) again. At this time, at the second point of intersection C, the blade inlet angle α=αR2, and the radial length R is R2 as shown in
The local angle-decrease section 10 also has an intermediate point D at which the radial length R=Rm that is the intermediate between R1 and R2.
Thus, the local angle-decrease section 10 is formed at the leading edge 21 of the blade 2 so as to start from the radial length R=R1 at the first point of intersection A, pass through the radial length R=Rs at the minimum point B, and reach the radial length R=R2 at the second point of intersection C. That is, the local angle-decrease section 10 is formed with the first point of intersection A and the second point of intersection C as both ends thereof.
The local angle-decrease section 10 of the blade inlet angle α according to Modification 2 of Embodiment 2 is formed such that the radial length R=Rs at the minimum point B is shorter than the radial length R=Rm at the intermediate point D and the minimum point B is located closer to the inner circumferential edge 24 than the intermediate point D, as shown in
The advantageous effects of the axial flow fan 100 according to Modification 1 of Embodiment 2 are the same as the advantageous effects of the axial flow fan 100 according to Embodiment 2.
That is, by making the blade inlet angle α have a minimum at the radial length R=Rs that is smaller than the radial length R=Rm at the intermediate point D, the position at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax and the position at which the blade inlet angle α has the minimum substantially coincide with each other.
Therefore, even at the radial length R of the blade 2 at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax, it is possible to make the main air current angle α′ and the inflow angle β shown in
<Modification 2 of Embodiment 2>
Modification 2 is different from Embodiment 2 and Modification 1 thereof in that: in the axial flow fan 100 according to Embodiment 2 and Modification 1 thereof, both ends of the local angle-decrease section 10 are defined as the points of intersection of the curves of the equation (1) and the equation (2); and in the axial flow fan 100 according to Modification 2, both ends of the local angle-decrease section 10 are defined as two maximum points on a curve. The other configuration of the axial flow fan 100 is the same as in Embodiment 2.
The local angle-decrease section 10 according to Modification 2 has a first maximum point Am at which the blade inlet angle α continuously increasing from the inner circumferential edge 24 of the blade 2 (the outer circumferential surface of the boss portion 1) at which the radial direction ratio P=(R−Rb)/(Rt−Rb) is P=0 (R=Rb) changes to decrease as shown in
In addition, the local angle-decrease section 10 has a minimum point B at which the blade inlet angle α decreasing from the first maximum point Am changes to increase again. At this time, at the minimum point B, the blade inlet angle α=αRs, and the radial length R is Rs.
Then, the local angle-decrease section 10 has a second maximum point Cm that is a point at which the blade inlet angle α increasing from the minimum point B changes to decrease again. At this time, at the second maximum point Cm, the blade inlet angle α=αR2m, and the radial length R is R2.
The local angle-decrease section 10 also has an intermediate point D at which the radial length R=Rm that is the intermediate between R1 and R2.
Thus, the local angle-decrease section 10 is formed at the leading edge 21 of the blade 2 so as to start from the radial length R=R1 at the first maximum point Am, pass through the radial length R=Rs at the minimum point B, and reach the radial length R=R2 at the second maximum point Cm. That is, the local angle-decrease section 10 is formed with the first maximum point Am and the second maximum point Cm as both ends thereof.
The local angle-decrease section 10 of the blade inlet angle α according to Modification 2 of Embodiment 2 is formed such that the radial length R=Rs at the minimum point B is shorter than the radial length R=Rm at the intermediate point D and the minimum point B is located closer to the inner circumferential edge 24 than the intermediate point D, as shown in
The advantageous effects of the axial flow fan 100 according to Modification 2 of Embodiment 2 are the same as the advantageous effects of the axial flow fan 100 according to Embodiment 2.
That is, by making the blade inlet angle α have a minimum at the radial length R=Rs that is smaller than the radial length R=Rm at the intermediate point D, the position at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax and the position at which the blade inlet angle α has the minimum substantially coincide with each other.
Therefore, even at the radial length R of the blade 2 at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax, it is possible to make the main air current angle α′ and the inflow angle β shown in
Embodiment 3 is different from Embodiment 2 in that in the axial flow fan 100 according to Embodiment 2, the local angle-decrease section 10 of the blade 2 is specified to have the minimum point B, but in Embodiment 3, the position, in the radial direction, of the minimum point B is specified. The other basic configuration of the axial flow fan 100 is the same as in Embodiments 1 and 2, and thus the description thereof is omitted.
In the local angle-decrease section 10 formed at the leading edge 21 of the blade 2, the radial length Rs at the minimum point B at which the blade inlet angle α is at its minimum is set so as to satisfy 0.1<(Rt−Rs)/(Rt−Rb)<0.5 when a radial length of the boss portion 1 represented by the distance from the rotation axis RC to the outer circumferential surface of the boss portion 1 is denoted by Rb and the maximum radial length from the rotation axis RC to the outer circumferential edge 23 of the blade 2 is denoted by Rt.
In the axial flow fan 100 according to Embodiment 3, since the radial length Rs at the minimum point B at which the blade inlet angle α of the leading edge 21 is at its minimum is set so as to satisfy 0.1<(Rt−Rs)/(Rt−Rb)<0.5, the range of the local angle-decrease section 10 in which the blade inlet angle α decreases substantially coincides with the position at which the blade edge eddy 3 occurs.
Therefore, it is possible to make the main air current angle α′ of the main air current F3′ and the inflow angle β of the blade 2 shown in
The axial flow fan 100 according to Embodiment 4 is different from the axial flow fan 100 according to Embodiments 1 to 3 in that the blade cross-section of the axial flow fan 100 according to Embodiments 1 to 3 is specified. The other configuration is the same as that of the axial flow fan 100 according to Embodiments 1 to 3, and thus the description thereof is omitted.
As shown in
The tangent line to the suction surface 2b at the leading edge 21 of the blade 2 is referred to as leading edge tangent line 21a, a straight line parallel to the rotation axis RC is referred to as axial virtual line RC′, and the angle formed by the leading edge tangent line 21a and the axial virtual line RC′ is referred to as blade inlet angle α.
The angle formed by the axial virtual line RC′ and a blade chord 27 connecting the leading edge 21 and the trailing edge 22 is referred to as stagger angle γ.
Furthermore, the acute angle at the point of intersection of the leading edge tangent line 21a to the suction surface 2b at the leading edge 21 of the blade 2 and a trailing edge tangent line 22a to the suction surface 2b at the trailing edge 22 is referred to as camber angle θc.
In this case, the blade inlet angle α of the blade 2 according to Embodiment 4 is set so as to satisfy α=γ+θc/2.
Since the blade 2 of the axial flow fan 100 according to Embodiment 4 has an arc cross-sectional shape in which the blade inlet angle α satisfies α=γ+θc/2 as described above, the surface of the blade 2 becomes smooth, so that the blade edge eddy 3 generated at the suction surface 2b of the blade 2 becomes stable. Accordingly, as shown in
It is possible to combine the respective configurations of the axial flow fans 100 according to Embodiments 1 to 4 described above. Due to the synergetic effects of these configurations, as shown in
(Application to Air-Conditioning Apparatus)
It is possible to use the axial flow fan 100 according to Embodiments 1 to 4 described above, for example, as an air-sending device that sends air for heat exchange to an indoor heat exchanger or an outdoor heat exchanger of an air-conditioning apparatus.
The air-conditioning apparatus includes a refrigeration cycle device 50 shown in
By using the axial flow fan 100 according to Embodiments 1 to 4 in such an air-conditioning apparatus, the air-sending efficiency of the condenser fan 52a or the evaporator fan 53a improves, so that it is possible to improve the cooling/heating performance of the air-conditioning apparatus.
It is also possible to use the axial flow fan 100 according to Embodiments 1 to 4 described above, as a ventilator, an electric fan, or the like. In addition, it is possible to use the axial flow fan 100 as an air-sending device that sends a fluid such as air.
By using the axial flow fan 100 according to Embodiments 1 to 4 as such a device, it is possible to achieve a decrease in noise and improvement of the air-sending efficiency of the air-sending device.
The axial flow fan 100 according to Embodiments 1 to 4 is
(1) an axial flow fan including a plurality of blades 2, each of the blades 2 including: a leading edge 21 formed in front in a direction of rotation RT of the axial flow fan; an inner circumferential edge 24 formed at an inner circumference of the blades 2; and an outer circumferential edge 23 formed at an outer circumference of the blades 2, the outer circumferential edge 23 being located in more downstream in a flow direction of a fluid, forced to flow by the axial flow fan, than the inner circumferential edge 24, the blade 2 being reflexed toward upstream of the flow direction at a portion adjacent to the outer circumferential edge 23, and having a local angle-decrease section 10 having a blade inlet angle α at the leading edge 21 decreasing from neighborhood, the local angle-decrease section 10 being formed at a side of the leading edge 21 and being located closer to the outer circumferential edge 23 than to the inner circumferential edge 24.
Thus, by providing the local angle-decrease section 10 having the blade inlet angle α decreasing from neighborhood so as to be smaller than the blade inlet angle α of the inner circumferential side leading edge 11, the local angle-decrease section 10 being formed at the side of the blade 2 and located closer to the outer circumferential edge 23 at which there is influence of the blade edge eddy 3, it is possible to make the main air current angle α′ and the inflow angle β substantially equal to each other as shown in
(2) In the axial flow fan 100 described in (1), the local angle-decrease section 10 has, at the leading edge 21 of the local angle-decrease section 10, the minimum point B at which the blade inlet angle α has a minimum.
Thus, the position at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax and the position at which the blade inlet angle α has the minimum substantially coincide with each other.
Therefore, even at the radial length R of the blade 2 at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax, it is possible to make the main air current angle α′ and the inflow angle β shown in
(3) In the axial flow fan 100 described in (2), the local angle-decrease section 10 has the intermediate point D located at an intermediate position between both ends of the local angle-decrease section 10, and the minimum point B is formed on a rotation axis RC side of the intermediate point D.
That is, by making the blade inlet angle α have a minimum at the radial length R=Rs that is smaller than the radial length R=Rm at the intermediate point D, the position at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax and the position at which the blade inlet angle α has the minimum substantially coincide with each other.
Therefore, even at the radial length R of the blade 2 at which the eddy diameter of the blade edge eddy 3 is the maximum value Lmax, it is possible to make the main air current angle α′ and the inflow angle β shown in
(4) In the axial flow fan 100 described in (2), the axial flow fan 100 includes the cylindrical boss portion 1 around the rotation axis RC, and the radial length Rs that is the distance between the rotation axis RC and the minimum point B satisfies 0.1<(Rt−Rs)/(Rt−Rb)<0.5 when: the radial length that is the distance from the rotation axis RC to the outer circumferential surface of the boss portion 1 is denoted by Rb; and the maximum radial length from the rotation axis RC to the outer circumferential edge 23 is denoted by Rt.
Thus, the range of the local angle-decrease section 10 in which the blade inlet angle α decreases substantially coincides with the position at which the blade edge eddy 3 occurs.
Therefore, it is possible to make the main air current angle α′ of the main air current F3′ and the inflow angle β of the blade 2 shown in
(5) In the axial flow fan 100 described in (1) to (4), the local angle-decrease section 10 is formed within half the length at the outer circumferential edge 23 side, of the radial length of the leading edge 21, and the blade inlet angle α of the local angle-decrease section 10 is formed as a value smaller than the blade inlet angle α at the inner circumference side relative to the local angle-decrease section 10.
Thus, by providing the local angle-decrease section 10 having the blade inlet angle α decreasing from neighborhood so as to be smaller than the blade inlet angle α of the inner circumferential side leading edge 11, the local angle-decrease section 10 being formed at the side of the blade 2 and located closer to the outer circumferential edge 23 at which there is influence of the blade edge eddy 3, it is possible to make the main air current angle α′ and the inflow angle β substantially equal to each other as shown in
(6) In the axial flow fan 100 described in (1) to (5), the plurality of blades 2 each have an arc cross-sectional shape in a blade chord direction.
(7) In the axial flow fan 100 described in (6), the blade inlet angle α satisfies α=γ+θc/2 when: the angle formed by the rotation axis RC and the blade chord 27 connecting the leading edge 21 and the trailing edge 22 formed in back in the direction of rotation is referred to as stagger angle γ; and the acute angle at the point of intersection of a tangent line at the leading edge 21 and a tangent line at the trailing edge 22 is referred to as camber angle θc.
Thus, the surface of the blade 2 becomes smooth, so that the blade edge eddy 3 generated at the suction surface 2b of the blade 2 becomes stable. Accordingly, as shown in
(8) The axial flow fan 100 described in (1) to (7) is applied to an air-conditioning apparatus.
In this case, the air-sending efficiency of the condenser fan 52a or the evaporator fan 53a improves, so that it is possible to improve the cooling/heating performance of the air-conditioning apparatus.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/JP2015/080884 | 11/2/2015 | WO | 00 |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2017/077564 | 5/11/2017 | WO | A |
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| 20040253103 | Iwase | Dec 2004 | A1 |
| 20130101420 | Nakashima et al. | Apr 2013 | A1 |
| 20150044058 | Hamada et al. | Feb 2015 | A1 |
| 20160348699 | Arai | Dec 2016 | A1 |
| Number | Date | Country |
|---|---|---|
| 2004-332674 | Nov 2004 | JP |
| 2008-121552 | May 2008 | JP |
| 2015-034503 | Feb 2015 | JP |
| 2011141964 | Nov 2011 | WO |
| 2014142225 | Sep 2014 | WO |
| 2015121989 | Aug 2015 | WO |
| Entry |
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| International Search Report of the International Searching Authority dated Feb. 9, 2016 for the corresponding international application No. PCT/JP2015/080884 (and English translation). |
| Number | Date | Country | |
|---|---|---|---|
| 20180238344 A1 | Aug 2018 | US |
