Patent Grant
11873833
This application is a U.S. national stage application of PCT/JP2020/033229 filed on Sep. 2, 2020, the contents of which are incorporated herein by reference.
The present disclosure relates to an axial-flow fan and to an outdoor unit for an air-conditioning apparatus including an axial-flow fan.
Some axial-flow fan includes a plurality of vanes arranged around the peripheral face of a cylindrical boss. The vanes are rotated by a turning force applied to the boss and thus delivers fluid. In the axial-flow fan, when the vanes rotate, fluid that is present between the vanes collide with the surfaces of the vanes. The pressure on the surfaces with which the fluid collides increases and pushes the fluid in the direction of the axis of rotation of the vanes.
One of such axial-flow fans having proposed includes blades each shaped such that the center camber line in a section of the blade that is taken along a cylindrical plane centered at the rotation axis of the fan includes a linear portion located close to the leading edge of the blade, and a curved portion located close to the trailing edge of the blade (see Patent Literature 1, for example). The linear portion extends in substantially the same direction as the direction of the collisionless flow of incoming gas toward the blade surface. The curved portion extends in such a manner as to make the linear portion continuous with the direction of the flow of gas flowing out from the blade surface. In the axial-flow fan disclosed by Patent Literature 1 including the linear portion and the curved portion shaped as above, the direction of the tangent to the leading edge of the blade substantially coincides with the direction of the collisionless flow of incoming gas substantially over the entirety in the radial direction about the rotation axis. Accordingly, in the axial-flow fan disclosed by Patent Literature 1, the incoming gas received at the leading edge of the blade flows along the linear portion and is guided to the curved portion. Therefore, an almost ideal flow with no loss is considered to be generated.
Patent Literature 1: Japanese Unexamined Patent Application Publication No. 9-144697
In the axial-flow fan disclosed by Patent Literature 1, however, the vane load is not adjusted in the radial direction. Specifically, the vane load to be borne at the inner circumference of the axial-flow fan is not satisfactorily increased relative to the vane load to be borne at the outer circumference of the axial-flow fan. Therefore, the airflow on the vane surface tends to travel toward the outer circumference of the axial-flow fan under the influence of elements such as a partition provided in the outdoor unit. Such an airflow flowing out from the axial-flow fan produces a wind-speed distribution in the radial direction in which maximal possible values concentratedly appear at or near the outermost circumference, and the concentrated air collides with structures including a fan grille that are located downstream of the axial-flow fan. Consequently, increased noise is generated in the outdoor unit of the air-conditioning apparatus.
The present disclosure is to solve the above problem and to provide an axial-flow fan and an outdoor unit for an air-conditioning apparatus each configured to reduce noise that tends to be generated by air blown out when the axial-flow fan is in operation.
An axial-flow fan according to an embodiment of the present disclosure is an axial-flow fan to be included in an outdoor unit for an air-conditioning apparatus. The axial-flow fan includes a hub that is to be rotated and defines a rotation axis, and a vane provided on a circumference of the hub. The vane includes a leading edge forming an edge located forward in a rotating direction, a trailing edge forming an edge located backward in the rotating direction, an outer circumferential edge forming an edge at an outer circumference of the vane, and an inner circumferential edge connected to the hub and forming an edge at an inner circumference that is further inside than an outermost circumference of the vane. In a section of the vane that is along an axial direction of the rotation axis and along a circumferential direction of the axial-flow fan, in a case in which an angle formed between a virtual line intersecting the trailing edge and being parallel to the rotation axis and a virtual line representing a direction in which the trailing edge faces is defined as an outlet angle of the vane, a first diagram is set in which a horizontal axis represents a distance on the trailing edge in a radial direction of the axial-flow fan from the inner circumferential edge to the outer circumferential edge while a vertical axis represents a size of the outlet angle, and a relationship between the size of the outlet angle and the distance on the trailing edge in the radial direction from the inner circumferential edge is represented as a first line chart, the vane is shaped such that the first line chart in the first diagram includes a downward convex portion that is convex further downward than a first virtual line chart, the first virtual line chart being a linear line connecting a point representing a size of the outlet angle formed at a point of the trailing edge that is at the inner circumferential edge and a point representing a size of the outlet angle formed at a point of the trailing edge that is at the outer circumferential edge.
An outdoor unit for an air-conditioning apparatus according to another embodiment of the present disclosure includes a housing including a wall having an air outlet, the axial-flow fan configured as above that is housed in the housing, and a bell mouth provided at the air outlet and surrounding an outer circumference of the axial-flow fan.
According to an embodiment of the present disclosure, the axial-flow fan and the outdoor unit for an air-conditioning apparatus each include the vane shaped such that the first line chart includes the downward convex portion that is convex further downward than the first virtual line chart. When the downward convex portion is provided, the vane having such a portion includes, at the inner circumference of the vane, a part where the outlet angle is smaller, with the presence of the downward convex portion, than in a vane that forms the first virtual line chart. Accordingly, the vane load to be borne is increased at the part forming the downward convex portion. Therefore, in the axial-flow fan including the downward convex portion, the vane load to be borne at the inner circumference is increased satisfactorily relative to the vane load to be borne at the outer circumference, whereby the airflow on the vane surface is induced toward the inner circumference. Thus, the air blown from the axial-flow fan produces a wind-speed distribution that is even in the radial direction. Consequently, the axial-flow fan that is set in the outdoor unit generates reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan.
Elements of an air-conditioning apparatus 70, including an outdoor unit 50, according to each of the embodiments will be described below with reference to the drawings. In the drawings, including
[Air-Conditioning Apparatus 70]
[Outdoor Unit 50]
The outdoor unit 50 includes a housing 51, which serves as an outer shell of the outdoor unit 50. As illustrated in
The lateral wall 51a of the housing 51 has openings 51a1, through which air on the outside is taken in. The rear wall 51d of the housing 51 has openings (not illustrated), through which air on the outside is taken in. The front wall 51b of the housing 51 has the air outlet 53, which serves as an opening through which air on the inside of the housing 51 is blown to the outside.
The air outlet 53 is covered by the fan grille 54. Therefore, any matter outside the housing 51 of the outdoor unit 50 is prevented from coming into contact with an axial-flow fan 100, whereby safety is ensured. In
The bars 54a each have a plate shape extending between the lateral wall 51a and the lateral wall 51c. The plurality of bars 54a of the fan grille 54 are vertically spaced apart from one another. When the axial-flow fan 100 is in operation, air to be exhausted from the inside of the outdoor unit 50 to the outside passes through the gaps between the adjacent bars 54a of the fan grille 54.
As illustrated in
The axial-flow fan 100 is connected to the motor 61 at the rotary shaft 62. The motor 61 is a drive source provided closer to the rear wall 51d than the axial-flow fan 100 and drives the axial-flow fan 100 to rotate. The motor 61 provides a driving force to the axial-flow fan 100. The motor 61 is attached to a motor support 69. The motor support 69 is located between the motor 61 and a heat exchanger 68.
When the axial-flow fan 100 rotates, air is taken into the outdoor unit 50 through the lateral face and the rear face of the housing 51 and passes through the heat exchanger 68, whereby heat is exchanged between the air passing through the heat exchanger 68 and refrigerant flowing inside the heat exchanger 68.
The inside of the housing 51 is divided by a partition 51g, which forms a wall, into a fan chamber 56 and a machine chamber 57. The axial-flow fan 100 is set in the fan chamber 56. The compressor 64 and other relevant devices are set in the machine chamber 57. The fan chamber 56 is a space enclosed by the lateral wall 51a, the partition 51g, the front wall 51b, the top plate 51e, and the bottom plate 51f. The machine chamber 57 is a space enclosed by the lateral wall 51c, the partition 51g, the front wall 51b, the rear wall 51d, the top plate 51e, and the bottom plate 51f. The lateral wall 51a is located across the axial-flow fan 100 from the partition 51g. The top plate 51e is located across the axial-flow fan 100 from the bottom plate 51f.
The heat exchanger 68 located at the inlet region of the axial-flow fan 100 in the housing 51 includes a plurality of fins arranged side by side such that the planar faces of the fins extend parallel to one another, and heat-transfer tubes extending through the fins in the direction in which the fins are arranged parallel to one another. The refrigerant that circulates through the refrigerant circuit 71 flows inside the heat-transfer tubes. In the heat exchanger 68, the plurality of heat-transfer tubes are arranged in the vertical direction and each have an L shape extending along the lateral wall 51a and the rear wall 51d of the housing 51.
The shape of the heat exchanger 68 is not limited to the above shape. For example, the heat exchanger 68 may have a substantially I shape extending along the inner rear face of the fan chamber 56 that is partially defined by the rear wall 51d. The heat exchanger 68 may alternatively be what is called a finless heat exchanger, which includes no fins through which heat-transfer tubes would extend. The heat exchanger 68 serves as the evaporator 73 in the heating operation and as the condenser 72 in the cooling operation.
The heat exchanger 68 of the outdoor unit 50 is connected to the compressor 64 by a pipe and any other relevant element and is further connected to an indoor heat exchanger (not illustrate), the expansion valve 74, and other relevant devices, whereby the refrigerant circuit 71 of the air-conditioning apparatus 70 is established. The heat exchanger 68 of the outdoor unit 50 serves as the condenser 72 or the evaporator 73 illustrated in
As illustrated in
In the axial direction of the rotation axis RS, one end of the bell mouth 63 is connected to the front wall 51b of the outdoor unit 50 in such a manner as to surround the circumference of the air outlet 53. The bell mouth 63 is, but not necessarily need to be, integrally formed on the front wall 51b. The bell mouth 63 may alternatively be prepared separately from the front wall 51b in such a manner as to be connected to the front wall 51b. In the outdoor unit 50 including the bell mouth 63, an air passage provided between the inlet region and the outlet region of the bell mouth 63 serves as an air duct in the vicinity of the air outlet 53. That is, the air duct in the vicinity of the air outlet 53 is separated from the other space in the fan chamber 56 by the bell mouth 63.
[Axial-Flow Fan 100]
With reference to
A region further rear than the plane of the page of
As illustrated in
(Hub 10)
The hub 10 is connected to the rotary shaft of a drive source such as a motor (not illustrated). The hub 10 may have, for example, a cylindrical shape or a plate shape. The shape of the hub 10 is not limited, as long as the hub 10 is connected to the rotary shaft of the drive source as described above.
The hub 10 is to be rotated by the motor (not illustrated) or any other drive source and defines the rotation axis RA. The hub 10 rotates about the rotation axis RA. The rotating direction DR of the axial-flow fan 100 is counterclockwise as represented by the arrow in
(Vane 20)
The vanes 20 are provided on the circumference of the hub 10 and each extend in the radial direction from the hub 10 toward the outside. The plurality of vanes 20 are arranged in such a manner as to spread radially outward from the hub 10. The plurality of vanes 20 are spaced apart from one another in the circumferential direction CD. Embodiment 1 relates to an exemplary axial-flow fan 100 that includes three vanes 20. However, the number of vanes 20 is not limited to three.
Each vane 20 has a leading edge 21, a trailing edge 22, an outer circumferential edge 23, and an inner circumferential edge 24. The leading edge 21 forms an edge of the vane 20 that is located forward in the rotating direction DR. That is, the leading edge 21 is located further forward than the trailing edge 22 in the rotating direction DR. The leading edge 21 is located upstream of the trailing edge 22 in the direction of the flow of the fluid that is to be generated.
The trailing edge 22 forms an edge of the vane 20 that is located backward in the rotating direction DR. That is, the trailing edge 22 is located further backward than the leading edge 21 in the rotating direction DR. The trailing edge 22 is located downstream of the leading edge 21 in the direction of the flow of the fluid that is to be generated. In the axial-flow fan 100, the leading edge 21 forms a vane end that faces in the rotating direction DR of the axial-flow fan 100, and the trailing edge 22 forms a vane end located opposite the leading edge 21 in the rotating direction DR.
The outer circumferential edge 23 forms an edge at the outer circumference (Y2 side) of the vane 20. The outer circumferential edge 23 extends forward and backward in the rotating direction DR and connects the outermost circumferential point of the leading edge 21 and the outermost circumferential point of the trailing edge 22. The outer circumferential edge 23 forms an end of the axial-flow fan 100 that is at the outer circumference in the radial direction (Y-axis direction).
The outer circumferential edge 23 forms an arc when seen in a direction parallel to the rotation axis RA. The shape of the outer circumferential edge 23 is not limited to an arc when seen in the direction parallel to the rotation axis RA. When seen in the direction parallel to the rotation axis RA, the outer circumferential edge 23 is longer than the inner circumferential edge 24 in the circumferential direction CD. The relationship between the lengths of the outer circumferential edge 23 and the inner circumferential edge 24 in the circumferential direction CD is not limited to the above. The outer circumferential edge 23 and the inner circumferential edge 24 may have the same length, or the inner circumferential edge 24 may be longer than the outer circumferential edge 23.
The inner circumferential edge 24 forms an edge at the inner circumference (Y1 side), which is further inside than the outermost circumference of the vane 20. The inner circumferential edge 24 extends forward and backward in the rotating direction DR and connects the innermost circumferential point of the leading edge 21 and the innermost circumferential point of the trailing edge 22. The inner circumferential edge 24 forms an end of the axial-flow fan 100 that is at the inner circumference in the radial direction (Y-axis direction).
The inner circumferential edge 24 forms an arc when seen in the direction parallel to the rotation axis RA. The shape of the inner circumferential edge 24 is not limited to an arc when seen in the direction parallel to the rotation axis RA. The inner circumferential edge 24 of the vane 20 is connected to the hub 10 in any manner such as by being integrally formed on the hub 10. For example, the inner circumferential edge 24 of the vane 20 is integrally formed on the outer circumferential wall of the cylindrical hub 10.
The vanes 20 are each inclined to a plane perpendicular to the rotation axis RA. When the axial-flow fan 100 rotates, the vanes 20 deliver the fluid by pushing the fluid that is present between the vanes 20 at relevant surfaces of the vanes 20. One of the surfaces of each vane at which the fluid is pushed and therefore bears an increased pressure is referred to as a pressure surface 25, and a surface of each vane that is opposite the pressure surface 25 and at which the pressure decreases is referred to as a suction surface 26. In the direction of the flow of the fluid, the upstream surface of the vane 20 is the suction surface 26, and the downstream surface of the vane 20 is the pressure surface 25. In
In the plan view of the vane 20 seen in the direction parallel to the axial direction of the rotation axis RS as illustrated in
As illustrated in
In the vane section WS illustrated in
In the vane section WS of the vane 20 that forms the outlet angle θS, the pressure surface 25 of the vane 20 is more upright from the rotating direction DR, that is, the pressure surface 25 forms an angle more approximate to the right angle to the rotating direction DR, than in the vane section WS of the vane 20 that forms the outlet angle θL. This means that a part of the vane 20 that forms the outlet angle θS is to bear a greater vane load than a part of the vane 20 that forms the outlet angle θL.
In contrast, in the vane section WS of the vane 20 that forms the outlet angle θL, the pressure surface 25 of the vane 20 is more inclined toward the rotating direction DR, that is, the pressure surface 25 forms an angle more approximate to the parallel angle to the rotating direction DR, than in the vane section WS of the vane 20 that forms the outlet angle θS. This means that a part of the vane 20 that forms the outlet angle θL is to bear a smaller vane load than a part of the vane 20 that forms the outlet angle θS.
In
In
As illustrated in
The outdoor unit 50L according to Comparative Example exhibits the relationship illustrated in
The air blown from the axial-flow fan 100L exhibits a wind-speed distribution WL in the radial direction in which points of highest wind speed concentratedly appear at or near the outermost circumference of the axial-flow fan 100L. In other words, the speed of the wind generated by the axial-flow fan 100L is lower at the inner circumference and higher at the outer circumference. Therefore, in the outdoor unit 50L according to Comparative Example, the airflow concentrated at or near the outermost circumference of the axial-flow fan 100L collides with structures including the fan grille that are located downstream of the outer circumference of the axial-flow fan 100L, thereby increasing the noise.
The point P1 representing the size of the outlet angle θ formed at a point of the trailing edge 22 that is at the inner circumferential edge 24 is the point at the innermost circumferential point of the trailing edge 22. The point P2 representing the size of the outlet angle θ formed at a point of the trailing edge 22 that is at the outer circumferential edge 23 is the point at the innermost circumferential point of the trailing edge 22. That is, the outlet angle θ at the point P1 is the outlet angle θ at the innermost circumferential point of the trailing edge 22. Furthermore, the outlet angle θ at the point P2 is the outlet angle θ at the outermost circumferential point of the trailing edge 22.
As with the case of the axial-flow fan 100L according to Comparative Example described above, the first virtual line chart VL has a linear shape representing that the outlet angle θ increases at a constant rate from the inner circumferential edge 24 to the outer circumferential edge 23.
As illustrated in
The downward convex portion UD is located closer to the inner circumference than the outer circumferential edge 23. It is further effective that the downward convex portion UD is located closer to the inner circumference than the center position, CL of the vane 20 in the radial direction of the axial-flow fan 100. The downward convex portion UD may be located at the center position CL of the vane 20.
The vane 20 of the axial-flow fan 100 includes, in the first line chart L, a first linear portion LI, which extends linearly between the inner circumferential edge 24 and the downward convex portion UD. The vane 20 of the axial-flow fan 100 further includes, in the first line chart L, a second linear portion LO, which extends linearly between the outer circumferential edge 23 and the downward convex portion UD.
The downward convex portion UD may include a linear portion that has a gentle inclination to the first linear portion LI and is continuous with the first linear portion LI. In other words, the downward convex portion UD may be shaped such that the above-described linear portion D2 illustrated in
Here, a part of the trailing edge 22 that forms the first linear portion LI of the first line chart L is defined as a first region 22a, a part of the trailing edge 22 that forms the downward convex portion UD of the first line chart L is defined as the second region 22b, and a part that forms the second linear portion LO of the first line chart L is defined as a second region 22b. As illustrated in
In the vane section WS1 of the vane 20 that forms the outlet angle θ1, the pressure surface 25 of the vane 20 is more upright from the rotating direction DR, that is, the pressure surface 25 forms an angle more approximate to the right angle to the rotating direction DR, than in the vane section WS3 of the vane 20 that forms the outlet angle θ3. This means that a part of the vane 20 that forms the outlet angle θ1 is to bear a greater vane load than a part of the vane 20 that forms the outlet angle θ3.
In contrast, in the vane section WS3 of the vane 20 that forms the outlet angle θ3, the pressure surface 25 of the vane 20 is more inclined toward the rotating direction DR, that is, the pressure surface 25 forms an angle more approximate to the parallel angle to the rotating direction DR, than in the vane section WS1 of the vane 20 that forms the outlet angle θ1. This means that a part of the vane 20 that forms the outlet angle θ3 is to bear a smaller vane load than a part of the vane 20 that forms the outlet angle θ1.
Accordingly, in view of the outlet angle θ, the axial-flow fan 100 is shaped such that the vane load to be borne is greater at a region that is divided by the downward convex portion UD and is close to the inner circumference than at a region that is divided by the downward convex portion UD and is close to the outer circumference. In other words, in the vane 20 as a whole, the axial-flow fan 100 is shaped such that the outlet angle θ formed at the trailing edge 22 is smaller at the region close to the inner circumferential edge 24 than at the region close to the outer circumferential edge 23.
Furthermore, in each of the first region 22a and the third region 22c, the axial-flow fan 100 is shaped such that the outlet angle θ increases from a region close to the inner circumference toward a region close to the outer circumference. More specifically, in the axial-flow fan 100, the first region 22a forms the outlet angle θS at the innermost of the first region 22a, and the outlet angle θL at the outermost of the first region 22a.
Likewise, in the axial-flow fan 100, the third region 22c forms the outlet angle θS at the innermost of the third region 22c and the outlet angle θL at the outermost of the third region 22c. Furthermore, in the axial-flow fan 100 as a whole, the first region 22a located at the inner circumference of the axial-flow fan 100 forms the outlet angle θS, while the third region 22c located at the outer circumference of the axial-flow fan 100 forms the outlet angle θL.
In the vane section WS2 of the vane 20 that forms the outlet angle θ2, the pressure surface 25 of the vane 20 is more upright from the rotating direction DR, that is, the pressure surface 25 forms an angle more approximate to the right angle to the rotating direction DR, than in the vane section WS3 of the vane 20 that forms the outlet angle θ3. This means that a part of the vane 20 that forms the outlet angle θ2 is to bear a greater vane load than a part of the vane 20 that forms the outlet angle θ3.
In contrast, in the vane section WS3 of the vane 20 that forms the outlet angle θ3, the pressure surface 25 of the vane 20 is more inclined toward the rotating direction DR, that is, the pressure surface 25 forms an angle more approximate to the parallel angle to the rotating direction DR, than in the vane section WS2 of the vane 20 that forms the outlet angle θ2. This means that a part of the vane 20 that forms the outlet angle θ3 is to bear a smaller vane load than a part of the vane 20 that forms the outlet angle θ2.
The outlet angle θ2 formed at the second region 22b includes a part that is equal to or smaller than the outlet angle θ1 formed at the first region 22a (outlet angle θ2≤outlet angle θ1).
Here, a case where the outlet angle θ2 formed at the second region 22b of the vane 20 is smaller than the outlet angle θ1 formed at the first region 22a will be discussed. In the vane section WS2 of the vane 20 that forms the outlet angle θ2, the pressure surface 25 of the vane 20 is more upright from the rotating direction DR, that is, the pressure surface 25 forms an angle more approximate to the right angle to the rotating direction DR, than in the vane section WS1 of the vane 20 that forms the outlet angle θ1. This means that a part of the vane 20 where the outlet angle θ2 formed at the second region 22b is smaller than the outlet angle θ1 formed at the first region 22a is to bear a greater vane load than a part of the vane 20 where the outlet angle θ1 is formed in the foregoing part.
Furthermore, as described above, the outlet angle θ2 formed at the second region 22b includes a part that is equal to or smaller than the outlet angle θ1 formed at the first region 22a (outlet angle θ2≤outlet angle θ1). In this part, the pressure surface 25 of the vane 20 is more upright, that is, the pressure surface 25 forms an angle more approximate to the right angle to the rotating direction DR, than in the vane 20L that forms the first virtual line chart VL. Therefore, when the outlet angle θ2 formed at the second region 22b includes a part that is equal to or smaller than the outlet angle θ1 formed at the first region 22a, that is, when the downward convex portion UD is provided, the vane 20 including such a region is to bear a greater vane load than the vane 20L that forms the first virtual line chart VL.
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
In the outdoor unit 50L according to Comparative Example, such a vane load is not adjusted in the radial direction of the axial-flow fan 100L. Consequently, the vane load borne at the inner circumference of the axial-flow fan 100L is not satisfactorily increased relative to the vane load at the outer circumference of the axial-flow fan 100L. Therefore, in the outdoor unit 50L according to Comparative Example, the airflow concentrated at or near the outermost circumference of the axial-flow fan 100L collides with structures including the fan grille that are located downstream of the outer circumference of the axial-flow fan 100L, thereby increasing the noise.
In view of the above, the axial-flow fan 100 according to Embodiment 1 includes the vanes 20 each shaped such that the first line chart L includes the downward convex portion UD that is convex further downward than the first virtual line chart VL. When the downward convex portion UD is provided, the vane 20 having such a region includes a part where the outlet angle θ formed at the vane 20 is smaller, with the presence of the downward convex portion UD, than in the vane 20L that forms the first virtual line chart VL. Accordingly, the vane load to be borne is increased at the part forming the downward convex portion UD.
Therefore, in the axial-flow fan 100, the vane load to be borne at the inner circumference is increased satisfactorily relative to the vane load to be borne at the outer circumference, whereby the airflow on the vane surface is induced toward the inner circumference. Thus, the air blown from the axial-flow fan 100 produces a wind-speed distribution that is even in the radial direction. Consequently, the axial-flow fan 100 that is set in the outdoor unit 50 generates reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan 100. Furthermore, in the outdoor unit 50, the even wind-speed distribution of the air blown from the axial-flow fan 100 reduces the resistance caused by the collision with the fan grille 54. Accordingly, the load to be borne by the axial-flow fan 100 of the outdoor unit 50 is reduced, and the fan input is reduced.
The downward convex portion UD is located closer to the inner circumference than the center position CL of the vane 20 in the radial direction of the axial-flow fan 100. With the downward convex portion UD located at such a position, the airflow on the vane surface is induced toward the inner circumference even when the airflow on the vane surface significantly gather toward the outer circumference. Therefore, the air blown from the axial-flow fan 100 produces a wind-speed distribution that is even in the radial direction.
The vane 20 further includes, in the first line chart L, the first linear portion LI that extends linearly between the inner circumferential edge 24 and the downward convex portion UD. The vane 20 further includes, in the first line chart L, the second linear portion LO that extends linearly between the outer circumferential edge 23 and the downward convex portion UD. The presence of such portions in the vane 20 make the vane load different between that borne by the downward convex portion UD and that borne by the first linear portion LI or the second linear portion LO.
Furthermore, the downward convex portion UD includes a linear portion D2 that has a gentle inclination to the first linear portion LI and that is continuous with the first linear portion LI. The vane 20 including such a portion has the minimal possible point DN, thereby including a part where the outlet angle θ of the vane 20 is smaller than in the vane 20L forming the first virtual line chart VL. In such a configuration, the vane load increases particularly at the peak 22b1 of the vane 20 where the minimal possible point DN is defined.
Therefore, in the axial-flow fan 100, the vane load to be borne at the inner circumference is increased satisfactorily relative to the vane load to be borne at the outer circumference, whereby the airflow on the vane surface is induced toward the inner circumference. Thus, the air blown from the axial-flow fan 100 produces a wind-speed distribution that is even in the radial direction. Consequently, the axial-flow fan 100 that is set in the outdoor unit 50 generates reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan 100. Furthermore, as described above, the fan input is reduced.
The downward convex portion UD has the minimal possible point DN where the outlet angle θ is minimal possible. The vane 20 having the minimal possible point DN includes a part where the outlet angle θ is smaller than in the vane 20L forming the first virtual line chart VL. In such a configuration, the vane load increases particularly in the vane 20 having the minimal possible point DN and at the peak 22b1.
Therefore, in the axial-flow fan 100, the vane load to be borne at the inner circumference is increased satisfactorily relative to the vane load to be borne at the outer circumference, whereby the airflow on the vane surface is induced toward the inner circumference. Thus, the air blown from the axial-flow fan 100 produces a wind-speed distribution that is even in the radial direction. Consequently, the axial-flow fan 100 that is set in the outdoor unit 50 generates reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan 100. Furthermore, as described above, the fan input is reduced.
The outdoor unit 50 of the air-conditioning apparatus 70 includes the axial-flow fan 100 and therefore exerts the above advantageous effects of the axial-flow fan 100.
In the vane section WS illustrated in
In the vane section WS of the vane 20 that forms the inlet angle αS, the pressure surface 25 of the vane 20 is more upright from the rotating direction DR, that is, the pressure surface 25 forms an angle more approximate to the right angle to the rotating direction DR, than in the vane section WS of the vane 20 that forms the inlet angle αL. This means that a part of the vane 20 that forms the inlet angle αS is to bear a greater vane load than a part of the vane 20 that forms the inlet angle αL.
In contrast, in the vane section WS of the vane 20 that forms the inlet angle αL, the pressure surface 25 of the vane 20 is more inclined toward the rotating direction DR, that is, the pressure surface 25 forms an angle more approximate to the parallel angle to the rotating direction DR, than in the vane section WS of the vane 20 that forms the inlet angle αS. This means that a part of the vane 20 that forms the inlet angle αL is to bear a smaller vane load than a part of the vane 20 that forms the inlet angle αS.
The second line chart L2 is a linear line connecting a point Q1 and a point Q2. The point Q1 represents the size of the inlet angle α formed at a point of the leading edge 21 of the axial-flow fan 100 that is at the inner circumferential edge 24. The point Q2 represents the size of the inlet angle α formed at a point of the leading edge 21 that is at the outer circumferential edge 23. The second virtual line chart VL2 has a linear shape representing that the inlet angle α formed at the leading edge 21 increases at a constant rate from the inner circumferential edge 24 to the outer circumferential edge 23.
The point Q1 representing the size of the inlet angle α formed at a point of the leading edge 21 that is at the inner circumferential edge 24 is the point at the innermost circumferential point of the leading edge 21. The point Q2 representing the size of the inlet angle α formed at a point of the leading edge 21 that is at the outer circumferential edge 23 is the point at the innermost circumferential point of the leading edge 21. That is, the inlet angle α at the point Q1 is the inlet angle α at the innermost circumferential point of the leading edge 21. Furthermore, the inlet angle α at the point Q2 is the inlet angle α at the outermost circumferential point of the leading edge 21.
With reference to
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
The axial-flow fan 100 includes vanes 20 in each of which the inlet angle α at the point GF in the second diagram that is at the same distance as the radial distance of the minimal possible point DN of the outlet angle θ represented in the first diagram is smaller than the inlet angle α formed at a point of the leading edge 21 that is at the outer circumferential edge 23. Therefore, the vane 20 is shaped such that the vane load to be borne by the leading-edge load-bearing point 21b forming the point GF is greater than the vane load to be borne at a point of the leading edge 21 that is at the outer circumferential edge 23.
In the axial-flow fan 100 configured as above, the vane load to be borne on the leading edge of the vane 20 is increased satisfactorily at the radial position of the peak 22b1, which forms the minimal possible point DN, relative to the vane load to be borne at the outer circumference. Therefore, in the axial-flow fan 100, compared with the case of the axial-flow fan 100 according to Embodiment 1, more airflow is induced toward the second region 22b where the trailing edge 22 has the minimal possible point DN, and the air blown from the axial-flow fan 100 therefore produces a wind-speed distribution WL that is more even in the radial direction.
Consequently, the axial-flow fan 100 that is set in the outdoor unit 50 generates reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan 100. Furthermore, as described above, the fan input is reduced. As described above, the minimal possible point DN is a point on the trailing edge 22 of the vane 20 and where the outlet angle θ is minimal possible.
The outdoor unit 50 for the air-conditioning apparatus 70 according to Embodiment 2 includes the axial-flow fan 100 and therefore exerts the above advantageous effects of the axial-flow fan 100.
A direction along the axial direction of the rotation axis RA and oriented from the leading edge 21 toward the trailing edge 22 is defined as the direction of the airflow. In
Furthermore, as illustrated in
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
Airflow is affected by the viscosity of the vane surface. Therefore, when the position of the leading edge 21 in the axial direction varies in the radial direction, air tends to flow toward a more downstream part of the leading edge 21. In this respect, since the leading-edge load-bearing point 21b is defined downstream of the leading-edge outer circumferential point 21c in the direction of the airflow, the axial-flow fan 100 exerts the viscosity of the vane surface and thus induces the airflow toward a radial position of the trailing edge 22 that is in the second region 22b. Consequently, in the axial-flow fan 100, compared with the case of the axial-flow fan 100 according to Embodiment 1, more airflow is induced toward the second region 22b where the trailing edge 22 has the minimal possible point DN, and the air blown from the axial-flow fan 100 therefore produces a wind-speed distribution WL that is more even in the radial direction.
The outdoor unit 50 for the air-conditioning apparatus 70 according to Embodiment 3 includes the axial-flow fan 100 and therefore exerts the above advantageous effects of the axial-flow fan 100.
The second diagram in
A second virtual line chart VL2, provided in the second diagram in
The second virtual line chart VL2 has a linear shape representing that the inlet angle α formed at the leading edge 21 increases at a constant rate from the inner circumferential edge 24 to the outer circumferential edge 23.
With reference to
As illustrated in
As illustrated in
The leading edge 21 includes a convex part 21r, which forms the upward convex portion UM. In the radial direction, the convex part 21r is located closer to the outer circumference of the vane 20 than the radial position of the peak 22b1 of the trailing edge 22 that forms the minimal possible point DN. In other words, the convex part 21r of the leading edge 21 that forms the upward convex portion UM is located closer to the outer circumference than the radial position of the leading-edge load-bearing point 21b formed at the point GF in the second line chart L2. The leading-edge peak 22m is located at the center position CL of the vane 20 in
The vane 20 of the axial-flow fan 100 includes, in the second line chart L2, a third linear portion LI1, which extends linearly at the leading edge 21 between the inner circumferential edge 24 and the upward convex portion UM. The upward convex portion UM has a steeper inclination than the third linear portion LI1. The vane 20 of the axial-flow fan 100 further includes, in the second line chart L2, a fourth linear portion L02, which extends linearly at the leading edge 21 between the outer circumferential edge 23 and the upward convex portion UM.
Here, a part of the leading edge 21 that forms the third linear portion LI1 of the second line chart L2 is defined as a region 21q, a part of the leading edge 21 that forms the upward convex portion UM of the second line chart L2 is defined as the convex part 21r, and a part that forms the fourth linear portion L02 of the second line chart L2 is defined as a region 21s. As illustrated in
The inlet angle α formed at the region 21q is smaller than the inlet angle α formed at the region 21s, and the inlet angle α formed at the region 21s is greater than the inlet angle α formed at the region 21q. Accordingly, in view of the inlet angle α, the axial-flow fan 100 is shaped such that the vane load to be borne is greater at a region that is divided by the upward convex portion UM and is close to the inner circumference than at a region that is divided by the upward convex portion UM and is close to the outer circumference.
Furthermore, in each of the region 21q and the region 21s, the axial-flow fan 100 is shaped such that the inlet angle α increases from a region close to the inner circumference toward a region close to the outer circumference.
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
The convex part 21r of the leading edge 21 that forms the upward convex portion UM is located, in the radial direction, closer to the outer circumference of the vane 20 than the radial position of the peak 22b1 of the trailing edge 22 that forms the minimal possible point DN. In the axial-flow fan 100 configured as above, the vane load to be borne on the leading edge is made to vary significantly in the radial direction. Thus, the airflow is induced toward a radial position of the trailing edge 22 that is in the second region 22b. Consequently, in the axial-flow fan 100, compared with the case of the axial-flow fan 100 according to Embodiment 1, more airflow is induced toward the second region 22b where the trailing edge 22 has the minimal possible point DN, and the air blown from the axial-flow fan 100 therefore produces a wind-speed distribution WL that is more even in the radial direction.
The upward convex portion UM has the maximal possible point MA where the value is maximal possible. In the axial-flow fan 100 configured as above, the vane load to be borne on the leading edge is made to vary more significantly in the radial direction. Thus, the airflow is induced toward a radial position of the trailing edge 22 that is in the second region 22b. Consequently, in the axial-flow fan 100, compared with the case of the axial-flow fan 100 according to Embodiment 1, more airflow is induced toward the second region 22b where the trailing edge 22 has the minimal possible point DN, and the air blown from the axial-flow fan 100 therefore produces a wind-speed distribution WL that is more even in the radial direction.
The outdoor unit 50 for the air-conditioning apparatus 70 according to Embodiment 4 includes the axial-flow fan 100 and therefore exerts the above advantageous effects of the axial-flow fan 100.
In the axial-flow fan 100 according to Embodiment 5, as illustrated in the first diagram in
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
When too much airflow is gathered toward the inner circumference of the axial-flow fan 100 as in the case of the axial-flow fan 100R according to Comparative Example illustrated in
In the axial-flow fan 100 according to Embodiment 5, as described above, the outlet angle θn at the minimal possible point DN in the first diagram is smaller than the outlet angle θ1 formed at a point of the trailing edge 22 that is at the inner circumferential edge 24. The outlet angle θ1 is the outlet angle at the innermost circumferential point of the trailing edge 22. In other words, the axial-flow fan 100 has a minimal possible point DN that represents an outlet angle θ that is smaller than that at the innermost circumferential point of the fan and is closer to the outer circumference in the radial direction than the innermost circumferential point of the fan.
In the axial-flow fan 100 configured as above, while the airflow at the outer circumference of the fan is induced toward the peak 22b1 forming the minimal possible point DN, the amount of airflow induced toward the hub 10 located closer to the inner circumference, which is further inside than the peak 22b1 forming the minimal possible point DN is reduced. Therefore, in the axial-flow fan 100 illustrated in
In the axial-flow fan 100 according to Embodiment 5 illustrated in
The outdoor unit 50 for the air-conditioning apparatus 70 according to Embodiment 5 includes the axial-flow fan 100 and therefore exerts the above advantageous effects of the axial-flow fan 100.
The outdoor unit 50 includes the housing 51 including the front wall 51b in which the air outlet 53 is provided, the axial-flow fan 100 according to any of Embodiments 1 to 5 that is housed in the housing 51, and the bell mouth 63 provided at the air outlet 53 and surrounding the outer circumference of the axial-flow fan 100.
The bell mouth 63 extends in the axial direction of the rotation axis RA. The bell mouth 63 includes an inlet portion 63a, a straight portion 63b, and an outlet portion 63c, which are arranged from the upstream region toward the downstream region in a first direction W1, in which the airflow generated by the axial-flow fan 100 travels from the inside of the housing 51 to the outside through the opening, 63d, of the bell mouth 63.
The inlet portion 63a has an opening diameter that is greater at its upstream portion of the airflow than at its downstream portion in the first direction W1. The straight portion 63b is shaped as a straight pipe whose opening diameter is constant in the first direction W1. The outlet portion 63c has an opening diameter that is greater at its downstream portion of the airflow than at its upstream portion in the first direction W1.
In the outdoor unit 50, the second region 22b where the trailing edge 22 has the downward convex portion UD is at such a position as to be covered by the straight portion 63b in the axial direction of the rotation axis RA. That is, the second region 22b of the axial-flow fan 100 is positioned in the opening of the straight portion 63b. The second region 22b of the axial-flow fan 100 is located between the rotation axis RA and the straight portion 63b of the bell mouth 63.
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
The straight portion 63b of the bell mouth 63 is a portion of the bell mouth 63 where the opening 63d is narrowest. Therefore, the air taken in when the axial-flow fan 100 is in operation concentrates most in the straight portion 63b among the portions of the bell mouth 63.
In the outdoor unit 50 according to Embodiment 6, the second region 22b where the trailing edge 22 has the downward convex portion UD is at such a position as to be covered by the straight portion 63b where the airflow concentrates. Accordingly, in the outdoor unit 50 according to Embodiment 6, the vane load to be borne at the inner circumference of the axial-flow fan 100 is increased more than in an outdoor unit in which the second region 22b is not at such a position as to be covered by the straight portion 63b.
The outdoor unit 50 according to Embodiment 6 includes the axial-flow fan 100 according to any of Embodiments 1 to 5. Therefore, the outdoor unit 50 according to Embodiment 6 exerts the above advantageous effects of the axial-flow fan 100.
In the outdoor unit 50 according to Embodiment 7, the second region 22b where the trailing edge 22 has the downward convex portion UD has a convex shape protruding downstream of the airflow in the axial direction of the rotation axis RA.
When the second region 22b shaped to be convex has the peak 22b1 forming the minimal possible point DN as described above, the convex second region 22b may have, for example, a substantially triangular shape forming a mountain having the peak 22b1 at the top in the axial direction. The convex second region 22b does not necessarily need to have a substantially triangular shape and may be, for example, a protrusion with an arc-shaped edge or may be substantially polygonal.
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
Airflow is affected by the viscosity of the vane surface. Therefore, when the position of the trailing edge 22 in the axial direction varies in the radial direction, air tends to flow toward a more downstream part of the trailing edge 22. Since the second region 22b having the downward convex portion UD has a convex shape protruding downstream of the airflow, the axial-flow fan 100 exerts the viscosity of the vane surface and thus induces the airflow toward the second region 22b where the trailing edge 22 has the downward convex portion UD.
Therefore, the air blown from the axial-flow fan 100 of the outdoor unit 50 according to Embodiment 7 produces a wind-speed distribution WL that is even in the radial direction. Consequently, the outdoor unit 50 generates reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan 100. Furthermore, as described above, the fan input to the axial-flow fan 100 is reduced.
The trailing edge 22 of the axial-flow fan 100 is shaped such that, at a region closer to the outer circumference than the second region 22b where the downward convex portion UD is formed, the trailing edge 22 is shifted upstream of the airflow while extending from the second region 22b where the downward convex portion is formed to the outer circumferential edge 23.
Here, a point of the trailing edge 22 that is at the outer circumferential edge 23 is defined as a trailing-edge outer circumferential point 22e. The trailing-edge outer circumferential point 22e is the outermost circumferential point of the trailing edge 22. As illustrated in
When the trailing edge 22 of the axial-flow fan 100 includes a plurality of second regions 22b as illustrated in
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
As described above, the air taken in when the axial-flow fan 100 is in operation concentrates most in the straight portion 63b among the portions of the bell mouth 63. Furthermore, in the outdoor unit 50, the greater the surface area of the part of the vane 20 that is positioned in the straight portion 63b of the bell mouth 63, the greater the vane load to be borne by this part.
The trailing edge 22 of the axial-flow fan 100 is shaped such that, at a region closer to the outer circumference than the second region 22b where the downward convex portion UD is formed, the trailing edge 22 is shifted upstream of the airflow while extending from the second region 22b where the downward convex portion is formed to the outer circumferential edge 23. In the outdoor unit 50, when the area of the part that is located at the outer circumference of the axial-flow fan 100 and is positioned in the straight portion 63b is reduced, the vane load to be borne at the outer circumference is relatively reduced, which increases the vane load to be borne by the second region 22b where the downward convex portion UD is formed.
Therefore, in the axial-flow fan 100, more airflow is induced toward the second region 22b where the downward convex portion UD is formed, and the air blown from the axial-flow fan 100 of the outdoor unit 50 according to Embodiment 8 produces a wind-speed distribution WL that is even in the radial direction. Consequently, the outdoor unit 50 generates reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan 100. Furthermore, as described above, the fan input to the axial-flow fan 100 is reduced.
In the outdoor unit 50 according to Embodiment 9, a part of the trailing edge 22 that is connected to the hub 10 is located upstream of the straight portion 63b in the direction of the airflow, that is, at such a position in the axial direction of the rotation axis RA as not to be covered by the straight portion 63b.
Here, as described above, a point of the trailing edge 22 that is at the inner circumferential edge 24 is defined as a trailing-edge inner circumferential point 22d. The trailing-edge inner circumferential point 22d is the innermost circumferential point of the trailing edge 22 and a part of the trailing edge 22 that is connected to the hub 10. That is, the trailing-edge inner circumferential point 22d is located upstream of the straight portion 63b in the direction of the airflow and at such a position in the axial direction of the rotation axis RA as not to be covered by the straight portion 63b. In other words, the trailing-edge inner circumferential point 22d the second region 22b of the axial-flow fan 100 is not positioned in the opening defined by the straight portion 63b.
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
As described in Embodiment 5, when too much airflow is gathered toward the inner circumference of the axial-flow fan 100, the airflow around the hub 10 causes turbulence TB when leaving a downstream part of the hub 10. Furthermore, as described in Embodiment 8, the air taken in when the axial-flow fan 100 is in operation concentrates most in the straight portion 63b among the portions of the bell mouth 63. Furthermore, in the outdoor unit 50, the greater the surface area of the part of the vane 20 that is positioned in the straight portion 63b of the bell mouth 63, the greater the vane load to be borne by this part.
In the outdoor unit 50 according to Embodiment 9, as described above, the part of the trailing edge 22 that is connected to the hub 10 is located upstream of the straight portion 63b in the direction of the airflow, that is, at such a position in the axial direction of the rotation axis RA as not to be covered by the straight portion 63b. In the outdoor unit 50, since the innermost circumferential point of the trailing edge 22 is not covered by the straight portion 63b, the vane load to be borne by the innermost circumferential point is relatively reduced, whereby the vane load to be borne by the second region 22b where the downward convex portion UD is formed is increased.
In the axial-flow fan 100 configured as above, while the airflow at the outer circumference of the axial-flow fan 100 is induced toward the second region 22b where the downward convex portion UD is formed, the amount of airflow induced toward the hub 10 located closer to the inner circumference than the second region 22b is reduced. Therefore, in the axial-flow fan 100, turbulence TB that tends to occur when the airflow around the hub 10 leaves a downstream part of the hub 10 is controlled. Consequently, in the outdoor unit 50, the generation of noise due to turbulence TB is controlled, and the increase in the fan input due to turbulence TB is controlled.
As described in Embodiment 1, the motor 61 is attached to the motor support 69. The motor support 69 supports the motor 61, which is configured to rotate the hub 10. The motor support 69 extends in the vertical direction of the outdoor unit 50. The motor support 69 has, for example, a plate shape or a columnar shape.
The motor support 69 is configured such that at least a part of the motor support 69 is located further outside than the motor 61 in the radial direction about the rotation axis RA. Furthermore, at least a part of the motor support 69 overlaps each of the vanes 20 of the axial-flow fan 100 in the axial direction of the rotation axis RA.
In the direction of the airflow generated in the housing 51 by the axial-flow fan 100, the motor support 69 is located upstream of the vanes 20, and the vanes 20 are located downstream of the motor support 69.
In the top view of the outdoor unit 50 as illustrated in
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
In the outdoor unit 50, as described above, the second region 22b where the trailing edge 22 has the downward convex portion UD is located at such a position as to overlap the motor support 69 in the axial direction. In the outdoor unit 50, since the second region 22b overlaps the motor support 69, the airflow is made to flow into the radial area AL of each of the vanes 20 that is located downstream of the motor support 69, whereby the occurrence of turbulence TB is controlled. Consequently, in the outdoor unit 50, the generation of noise due to turbulence TB is controlled, and the increase in the fan input due to turbulence TB is controlled.
As described in Embodiment 1, the outdoor unit 50 includes the fan grille 54 at the air outlet 53 to prevent the insertion of hand fingers of any person into the housing 51. The fan grille 54 includes, among bars, a plurality of bars 54a that each extend in the horizontal direction and are arranged in the vertical direction. The fan grille 54 is located downstream of the axial-flow fan 100 in the direction of the airflow.
In the front view of the outdoor unit 50 as illustrated in
In the front view of the outdoor unit 50, when the vanes 20 rotate and the trailing edge 22 of each of the vanes 20 passes by any of the bars 54a of the fan grille 54, the trailing-edge outer circumferential point 22e that is the outermost circumferential point of the trailing edge 22 passes by the bar 54a of the fan grille 54 earlier than the second region 22b.
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
In a typical outdoor unit, in front view, when the trailing edge 22 of the vane 20 passes by the bar 54a of the fan grille 54, the airflow flowing out from the trailing edge 22 collides with the bar 54a of the fan grille 54, whereby a great resistance is generated on the vane 20.
Since a great resistance is generated at the trailing edge 22 passing by the bar 54a of the fan grille 54, as illustrated in
In the outdoor unit 50, the preceding region 22g that passes by the bar 54a of the fan grille 54 earlier than the second region 22b is provided at a region closer to the outer circumference than the second region 22b. That is, when the axial-flow fan 100 is in operation, a part at a region closer to the outer circumference than the second region 22b receives the resistance of the air earlier than the second region 22b. Therefore, the air taken into the outdoor unit 50 flows into the second region 22b, whereby the air blown from the axial-flow fan 100 produces a wind-speed distribution that is even in the radial direction. Consequently, the outdoor unit 50 generates reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan 100. Furthermore, as described above, the fan input is reduced.
In the outdoor unit 50, the second region 22b where the trailing edge 22 has the downward convex portion UD has a convex shape protruding in the direction opposite to the rotating direction DR of the vane 20. The axial-flow fan 100 configured as above exerts the viscosity of the vane surface and thus induces the airflow toward the second region 22b where the trailing edge 22 has the downward convex portion UD. Therefore, the air blown from the axial-flow fan 100 of the outdoor unit 50 produces a wind-speed distribution WL that is even in the radial direction. Consequently, the outdoor unit 50 generates reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan 100. Furthermore, the fan input to the axial-flow fan 100 is reduced.
In view of the outlet angle θ, the axial-flow fan 100 according to Embodiment 1 is shaped such that the vane load to be borne is greater at a region that is divided by the downward convex portion UD and is close to the inner circumference than at a region that is divided by the downward convex portion UD and is close to the outer circumference. In contrast, the axial-flow fan 100 according to Embodiment 12 is shaped in view of the outlet angle θ such that the vane load to be borne is greater at a region that is divided by the downward convex portion UD and is close to the outer circumference than at a region that is divided by the downward convex portion UD and is close to the inner circumference. In other words, in the vane 20 as a whole, the axial-flow fan 100 according to Embodiment 12 is shaped such that the outlet angle θ formed at the trailing edge 22 is smaller at the region close to the outer circumferential edge 23 than at the region close to the inner circumferential edge 24. The axial-flow fan 100 may include such vanes 20 each forming the outlet angle θ described in Embodiment 12.
The axial-flow fan 100 according to Embodiment 12 includes vanes 20 each forming the first line chart L illustrated in the first diagram in
[Operational Effects of Axial-Flow Fan 100 and Outdoor Unit 50]
In the axial-flow fan 100 including the vanes 20 each including the downward convex portion, the vane load to be borne at the inner circumference is increased satisfactorily relative to the vane load to be borne at the outer circumference. Accordingly, the airflow on the vane surface is induced toward the inner circumference. Therefore, the air blown from the axial-flow fan 100 produces a wind-speed distribution that is even in the radial direction. Consequently, the axial-flow fan 100 and the outdoor unit 50 each generate reduced noise that tends to occur at the collision with structures including the fan grille that are located downstream of the axial-flow fan 100. Furthermore, the fan input is reduced.
The configurations according to the embodiments described above are only exemplary and may be combined in any manner. The configurations according to the embodiments described above may be combined with any of other known technologies and may be partly changed or omitted without departing from the essence.
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/JP2020/033229 | 9/2/2020 | WO |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2022/049665 | 3/10/2022 | WO | A |
| Number | Name | Date | Kind |
|---|---|---|---|
| 20070258822 | Spaggiari | Nov 2007 | A1 |
| 20150240645 | Yokose et al. | Aug 2015 | A1 |
| Number | Date | Country |
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| 106151105 | Nov 2016 | CN |
| H08-165999 | Jun 1996 | JP |
| H09-144697 | Jun 1997 | JP |
| 2007-113474 | May 2007 | JP |
| 2014-058902 | Apr 2014 | JP |
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| 201480970 | May 2014 | JP |
| 6373439 | Aug 2018 | JP |
| Entry |
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| International Search Report of the International Searching Authority dated Oct. 20, 2020 for the corresponding international application No. PCT/JP2020/033229 (and English translation). |
| Extended European Search Report dated Sep. 18, 2023 issued in corresponding European patent application No. 20952405.7. |
| Number | Date | Country | |
|---|---|---|---|
| 20230235750 A1 | Jul 2023 | US |
