Patent Grant
11635089
This application is a U.S. national stage application of PCT/JP2016/081818 filed on Oct. 27, 2016, the contents of which are incorporated herein by reference.
The present invention relates to a so-called integrated-wing propeller fan, in which blades are each joined at leading edge thereof to a trailing edge of an adjoining blade of the blades, and an outdoor unit and a refrigeration cycle apparatus having the propeller fan.
Refrigeration cycle apparatuses perform operations, such as heating and cooling of a target space or other place, by circulating refrigerant through a refrigerant circuit. These refrigeration cycle apparatuses often include an indoor unit (indoor device) and an outdoor unit (outdoor device). The outdoor unit is provided with a propeller fan, serving as an air-sending device, having blades (propeller). By rotating the propeller fan to generate an airflow, an air-sending operation, such as cooling or heat release, is performed.
Typically, the above-described propeller fan is configured such that a plurality of blades are joined to the outer circumferential side of a cylindrical boss part, which is connected to a rotary shaft of a driving source, such as a motor. In the propeller fan having the boss part, a weight reduction is difficult because of the heavy boss part. Thus, it is difficult to promote resource saving (reduce the environmental load). In addition, there has been a problem in that it is difficult improve the air-sending efficiency of the fan because the boss part does not have an air-sending function.
To overcome such a problem, a so-called integrated-wing propeller fan having: a rotation-axis part (center of rotation) connected to a rotary shaft of a driving source, such as a motor; and a plurality of blades provided on the outer circumferential side of the rotation-axis part has been proposed, in which the adjoining blades are joined to one another at the leading edges and trailing edges thereof. This integrated-wing propeller fan is configured such that the adjoining blades are joined to one another via a continuous surface, not a boss part. Hence, in the integrated-wing propeller fan, the minimum radius of the continuous surface extending between the blades, centered at the rotation-axis part (center of rotation), is greater than the radius of the rotation-axis part. Hence, the integrated-wing propeller fan can overcome the above-described problem in the propeller fan having the boss part.
However, in the integrated-wing propeller fan, the amount of deformation of the blades during rotation is large due to insufficient strength of the blades, leading to a problem, such as a decrease in the air-sending performance. To overcome this problem, an integrated-wing propeller fan having, around the rotation-axis part, ribs for compensating for the insufficient strength of the blades has been proposed. For example, an integrated-wing propeller fan disclosed in Patent Literature 1 is configured such that the rotation-axis part projects toward a pressure-surface side of the blades. Ribs extending radially from the rotation-axis part are formed on the pressure surfaces of the blades. According to Patent Literature 1, the radially extending ribs also function as a turbo fan, thus improving the air-sending performance of the integrated-wing propeller fan.
Patent Literature 1: International Publication No. 2016/021555
The main flow of an airflow generated by an integrated-wing propeller fan when it rotates flows on the outer circumferential side of the blades. Hence, the air does not flow actively on the downstream side of the rotation-axis part and stagnates, thus generating a large separation area on the downstream side of the rotation-axis part. In the propeller fan disclosed in Patent Literature 1, it is possible to diffuse the air near the outer circumferential ends during rotation, at positions near the outer circumferential ends of the radially extending ribs formed on the pressure surfaces. Hence, in the propeller fan disclosed in Patent Literature 1, as a result of being attracted of the diffused air to the main flow, it is possible to allow the main flow to move slightly toward the inner circumferential side (rotation-axis part side). However, even the propeller fan disclosed in Patent Literature 1 has a problem in that it is impossible to generate a sufficient airflow on the downstream side of the rotation-axis part to reduce the separation area generated on the downstream side of the rotation-axis part.
The present invention has been made in view of the above-described problems, and a first object thereof is to provide an integrated-wing propeller fan in which it is possible to reduce the separation area generated on the downstream side of the rotation-axis part, compared with that in the related-art propeller fan. A second object is to provide an outdoor unit and refrigeration cycle apparatus having this propeller fan.
A propeller fan according to an embodiment of the present invention includes: a rotation-axis part that serves as a center of rotation of the propeller fan; and a plurality of blades provided on an outer circumferential side of the rotation-axis part, the plurality of blades each being joined at an leading edge of the blade to a trailing edge of an adjoining blade of the blades, the propeller fan having a first rib provided on pressure surfaces of the plurality of blades, the first rib projecting in a direction of the center of rotation of the rotation-axis part and surround the rotation-axis part, and second ribs provided on pressure surfaces of the plurality of blades, the second ribs projecting in the axial direction of the rotation-axis part and extending from the rotation-axis part toward the first rib, and wherein, of ends of the second ribs in the axial direction of the rotation-axis part, ends, distant from the pressure surfaces, of the second ribs project in a direction away from the pressure surfaces farther than an end of the first rib distant from the pressure surfaces, among the ends of the first rib in the axial direction of the rotation-axis part.
In the propeller fan according to an embodiment of the present invention, it is possible to diffuse, by means of the first ribs, the airflow generated by the rotation of the blades toward the inner circumferential side. In addition, in the propeller fan according to an embodiment of the present invention, it is possible to further diffuse, by means of the second ribs, the flow diffused by the first ribs toward the downstream side of the rotation-axis part. Hence, in the propeller fan according to an embodiment of the present invention, it is possible to generate a sufficient airflow on the downstream side of the rotation-axis part to reduce the separation area generated on the downstream side of the rotation-axis part, compared with that in the related-art propeller fan.
Embodiments of the present invention will be described below with reference to the drawings.
First, the configuration of an outdoor unit according to Embodiment 1 of the present invention will be described. In Embodiment 1, an outdoor unit of an air-conditioning apparatus, which is an example of the outdoor unit, will be described. Note that the outdoor unit according to Embodiment 1 may be, for example, an outdoor unit of a water heater, which may have the same configuration as the outdoor unit of the air-conditioning apparatus.
An outdoor unit 100 mainly includes: an outdoor unit body 1; a fan grille 2; a propeller fan 3, serving as an air-sending device; a fan motor 4; a partition plate 5; a fan chamber 6; a machine chamber 7; a heat exchanger 8; and a bell mouth 9.
The outdoor unit body 1 has, for example, a substantially rectangular-parallelepiped shape and constitutes the outer shell of the outdoor unit 100. The outdoor unit body 1 includes a first side-surface part 1a, a front-surface part 1b, a second side-surface part 1c, a back-surface part 1d, a top-surface part 1e, and a bottom-surface part 1f. The interior of the outdoor unit body 1 is sectioned into the fan chamber 6 and the machine chamber 7 by the partition plate 5. Openings, serving as air inlets 1h, through which air is taken into the outdoor unit body 1, are provided in the first side-surface part 1a and the back-surface part 1d, at portions constituting the fan chamber 6. Furthermore, an opening, serving as an air outlet 1g, through which the air is blown outside, is provided in the front-surface part 1b, at a portion constituting the fan chamber 6.
The propeller fan 3, the fan motor 4, the heat exchanger 8, and the bell mouth 9 are provided in the fan chamber 6. The heat exchanger 8 is provided in the fan chamber 6 to face the air inlets 1h provided in the first side-surface part 1a and the back-surface part 1d. Specifically, the heat exchanger 8 is formed in a substantially L shape in plan view. The heat exchanger 8 is configured as a fin-and-tube-type heat exchanger, which has a plurality of fins and heat transfer tubes, and exchanges heat with the air introduced by the propeller fan 3. The plurality of fins are arranged in parallel in the lateral direction with a predetermined distance therebetween, along the first side-surface part 1a and the back-surface part 1d. The plurality of heat transfer tubes are provided to penetrate through the plurality of fins. Specifically, the heat transfer tubes are formed in a substantially L shape in plan view. The heat transfer tubes are arranged in parallel in the top-bottom direction with a predetermined distance therebetween. Refrigerant circulating through a refrigerant circuit flows through the heat transfer tubes.
The propeller fan 3 is provided to face the air outlet 1g provided at the front-surface part 1b. Specifically, the above-described heat exchanger 8 is provided on the air-inlet side of the propeller fan 3. As will be described below, the propeller fan 3 has a rotation-axis part 30, serving as the center of rotation (see
The details of the propeller fan 3 will be described below.
The bell mouth 9 is provided to project from the periphery of the air outlet 1g provided at the front-surface part 1b toward the propeller fan 3. The bell mouth 9 is disposed to cover the outer circumferential portion of the propeller fan 3 with a predetermined distance therebetween. With this configuration, the bell mouth 9 divides the air passage near the air outlet 1g into the air-inlet side and the air-outlet side. Furthermore, the air outlet 1g provided at the front-surface part 1b is covered by the fan grille 2. The fan grille 2 prevents contact between an object or foreign matter and the propeller fan 3 for the safety. The bell mouth 9 may be formed either as an integral part of the front-surface part 1b or as a separate member.
Furthermore, a compressor 10, pipes 11, and a board box 12 are provided in the machine chamber 7. The compressor 10 constitutes a portion of the refrigerant circuit and compresses the refrigerant circulating through the refrigerant circuit. The pipes 11 include pipes that connect the compressor 10 and the heat exchanger 8. The board box 12 accommodates a control substrate 13. The control substrate 13 controls the devices, such as the compressor 10, installed in the outdoor unit 100.
Next, the configuration of the propeller fan 3 according to Embodiment 1 will be described in more detail.
The propeller fan 3 includes the rotation-axis part 30, serving as the center of rotation of the propeller fan 3, and a plurality of blades 31 (a propeller) provided on the outer circumferential side of the rotation-axis part 30. The rotation-axis part 30 has, for example, a cylindrical shape and is provided with a connection hole 30a, into which the rotary shaft 4a of the fan motor 4 is inserted and fixed, at the central portion thereof, serving as the center of rotation of the rotation-axis part 30. Although the rotation-axis part 30 projects on the pressure surface 31a side of the blades 31 in Embodiment 1, the rotation-axis part 30 does not need to project on the pressure surface 31a side of the blades 31.
Hereinbelow, the “center of rotation” means the center of rotation of the propeller fan 3, that is, the center of rotation of the rotation-axis part 30. Furthermore, the direction of the center of rotation means the direction in which the center of rotation of the rotation-axis part 30 extends, in other words, the direction in which the connection hole 30a extends.
The plurality of blades 31 are disposed at equal angles around the rotation-axis part 30 in the circumferential direction of the rotation-axis part 30. The adjoining blades 31 is joined at a leading edge 31b to a trailing edges 31c of an adjoining blade. In other words, the propeller fan 3 according to Embodiment 1 is a so-called integrated-wing propeller fan. Although the propeller fan 3 according to Embodiment 1 has three blades 31, the number of the blades 31 is not limited to three. Furthermore, the blades 31 may be disposed at different angles around the rotation-axis part 30.
Furthermore, the propeller fan 3 according to Embodiment 1 has a first rib 32 and second ribs 33 around the rotation-axis part 30. The rotation-axis part 30, the first rib 32, and the second ribs 33 constitute a hub of the propeller fan 3. The propeller fan 3 according to Embodiment 1 also has reinforcing ribs 34 and third ribs 35 to further improve at least one of the air diffusion effect and the strength. The reinforcing ribs 34 and the third ribs 35 of the propeller fan 3 may be omitted.
The first rib 32 is provided on the pressure surfaces 31a of the plurality of blades 31. Furthermore, the first rib 32 projects in the direction of the center of rotation and surrounds the rotation-axis part 30. In other words, the first rib 32 projects toward the downstream side in the airflow direction and surrounds the rotation-axis part 30. More specifically, the first rib 32 according to Embodiment 1 has three ribs 32a having arc-shaped outer circumferential surfaces as viewed in the axial direction of the rotation-axis part. In other words, the outer circumferential surfaces of the ribs 32a have a curved shape. The ribs 32a are disposed at equal angles around the rotation-axis part 30 in the circumferential direction of the rotation-axis part 30. Furthermore, the adjoining ribs 32a are joined to one another at ends thereof. Hence, the first rib 32 according to Embodiment 1 surrounds the rotation-axis part 30 such that the outer circumferential surface thereof forms a substantially triangle shape when the first rib 32 is viewed in the axial direction of the rotation-axis part. Note that the ribs 32a constituting the first rib 32 have a substantially uniform thickness between the ends thereof when viewed in the axial direction of the rotation-axis part. In other words, the first rib 32 has a substantially uniform thickness over the entire circumference. Hence, the inner circumferential surface of the first rib 32 also has a substantially triangle shape when the first rib 32 is viewed in the axial direction of the rotation-axis part. In other words, the first rib 32 surrounds the rotation-axis part 30 to form a substantially triangle shape when the first rib 32 is viewed in the axial direction of the rotation-axis part.
When the propeller fan 3 rotates, the first rib 32 diffuses the air therearound. As a result of being attracted of the diffused air to the main flow generated by the propeller fan 3, which flows on the outer circumferential side of the blades 31, it is possible to diffuse the main flow generated by the propeller fan 3 toward the inner circumferential side. In other words, it is possible to diffuse the main flow generated by the propeller fan 3 to the vicinity of the outer circumferential part of the first rib 32.
Furthermore, the third rib 35 is provided at one end of each rib 32a constituting the first rib 32 and extends along the rib 32a toward the outer circumferential side of the first rib 32. Specifically, the third ribs 35 are provided on the pressure surfaces 31a of the blades 31, and the third ribs 35 project in the direction of the center of rotation and extends from the first rib 32 toward the outer circumferential side. In other words, the third ribs 35 project toward the downstream side in the airflow direction and extends from the first rib 32 toward the outer circumferential side. By providing the third ribs 35, it is possible to further diffuse the air around the first rib 32 when the propeller fan 3 rotates, thus allowing the main flow generated by the propeller fan 3 to further diffuse toward the inner circumferential side.
Herein, the number of the ribs 32a constituting the first rib 32 is not limited to three. The ribs 32a may be disposed at different angles around the rotation-axis part 30 and may be disposed at different distances from the rotation-axis part 30. Furthermore, the ribs 32a may have different lengths when the first rib 32 is viewed in the axial direction of the rotation-axis part. The third ribs 35 provided at the ends of the ribs 32a may be omitted, and, for example, the third ribs 35 do not need to be provided at the ends of the ribs 32a, as shown in
Note that
The second ribs 33 are provided on the pressure surfaces 31a of the plurality of blades 31. The second ribs 33 project in the direction of the center of rotation and extends from the rotation-axis part 30 toward the first rib 32. In other words, the second ribs 33 project toward the downstream side in the airflow direction and extends from the rotation-axis part 30 toward the first rib 32. More specifically, in Embodiment 1, three second ribs 33 are provided. The second ribs 33 are disposed at equal angles around the rotation-axis part 30, in the circumferential direction of the rotation-axis part 30. In other words, the second ribs 33 extend substantially radially from the rotation-axis part 30.
When the propeller fan 3 rotates, the second ribs 33 diffuse the air therearound. As a result of being attracted of the diffused air to the main flow generated by the propeller fan 3, which has been diffused by the first rib 32 to the vicinity of the outer circumferential part of the first rib 32, it is possible to diffuse the main flow generated by the propeller fan 3 to the downstream side of the rotation-axis part 30. In other words, it is possible to generate a sufficient airflow on the downstream side of the rotation-axis part 30.
Furthermore, a third rib 35 is provided at the outer circumferential end of each second rib 33 and extends along the second rib 33 toward the outer circumferential side of the first rib 32. As has been described above, by providing the third ribs 35, it is possible to further diffuse the air around the first rib 32 when the propeller fan 3 rotates, thus allowing the main flow generated by the propeller fan 3 to further diffuse toward the inner circumferential side.
Herein, as shown in
The number of the second ribs 33 is not limited to three. The second ribs 33 may be disposed at different angles around the rotation-axis part 30. Furthermore, the third ribs 35 provided at the outer circumferential ends of the second ribs 33 may be omitted, and, for example, the third ribs 35 do not need to be provided at the outer circumferential ends of the second ribs 33, as shown in
Note that
The reinforcing ribs 34 may be omitted. The reinforcing ribs 34 are provided on the pressure surfaces 31a of the blades 31 when the strength of the hub constituted of the rotation-axis part 30, the first rib 32, and the second ribs 33 is to be further improved. In that case, for example, the reinforcing ribs 34 may be formed as shown in
Alternatively, for example, the reinforcing ribs 34 may be formed as shown in
Note that
Next, an air-sending operation of the outdoor unit 100 according to Embodiment 1 will be described.
As indicated by arrows in
In a related-art propeller fan, the main flow of the airflow generated when the propeller fan rotates flows on the outer circumferential side of the blades. Hence, in the related-art propeller fan, not a large part of the airflow A blown outdoors through the air outlet provided at the outdoor unit flows on the downstream side of the rotation-axis part and stagnates, thus generating a large separation area on the downstream side of the rotation-axis part. On the other hand, the propeller fan 3 according to Embodiment 1 has the above-described first rib 32 and the second ribs 33. Hence, the airflow A blown outdoors through the air outlet 1g of the outdoor unit 100 can flow on the downstream side of the rotation-axis part 30, reducing the separation area generated on the downstream side of the rotation-axis part 30, compared with that in the related-art propeller fan.
Hereinbelow, with comparison between the outdoor unit 100 having the propeller fan 3 according to Embodiment 1 and an outdoor unit having a related-art propeller fan, how the propeller fan 3 and the outdoor unit 100 according to Embodiment 1 reduce the separation area will be described. Hereinbelow, when the related-art propeller fan and outdoor unit are described, the same components as those of the propeller fan 3 and the outdoor unit 100 according to Embodiment 1 will be denoted by the same reference signs as those in the propeller fan 3 and the outdoor unit 100 according to Embodiment 1, and the explanations thereof will be omitted.
The related-art outdoor unit 500 differs from the outdoor unit 100 according to Embodiment 1 in the configuration of a propeller fan 503. More specifically, the related-art propeller fan 503 does not have the ribs (the first rib 32, the second ribs 33, the reinforcing ribs 34, and the third ribs 35) that are provided on the propeller fan 3 according to Embodiment 1. Instead of these ribs, the related-art propeller fan 503 has ribs 540. The ribs 540 are provided on the pressure surfaces 31a of the plurality of blades 31. The ribs 540 extend radially from the rotation-axis part 30 and have a shape projecting downstream in the airflow direction from the pressure surfaces 31a. The other configurations of the related-art outdoor unit 500 and the related-art propeller fan 503 are the same as those of the outdoor unit 100 and the propeller fan 3 according to Embodiment 1.
The main flow generated when the propeller fan 503 rotates flows on the outer circumferential side of the blades 31. At this time, because the propeller fan 503 has the ribs 540 extending radially from the rotation-axis part 30, the air near the outer circumferential ends of the ribs 540 are diffused. As a result of being attracted of the diffused air to the main flow, the main flow diffuses to the vicinity of the outer circumferential ends of the ribs 540. In other words, it is possible to cause the airflow A to flow to the vicinity of the outer circumferential ends of the ribs 540. However, the airflow A does not diffuse to the downstream side of the rotation-axis part 30. Hence, in the propeller fan 503, a large separation area 20 is generated on the downstream side of the rotation-axis part 30.
The main flow generated when the propeller fan 3 rotates also flows on the outer circumferential side of the blades 31. At this time, the first rib 32 of the propeller fan 3 diffuses the air therearound. As a result of being attracted of the diffused air to the main flow, it is possible to diffuse the main flow generated by the propeller fan 3 toward the inner circumferential side. In other words, it is possible to diffuse the airflow A to the vicinity of the outer circumferential part of the first rib 32. In addition, when the propeller fan 3 rotates, the second ribs 33 also diffuse the air therearound. As a result of being attracted of the diffused air to the airflow A, which has been diffused to the vicinity of the outer circumferential part of the first rib 32 by the first rib 32, it is possible to diffuse the airflow A to the downstream side of the rotation-axis part 30. In other words, it is possible to generate a sufficient amount of airflow A on the downstream side of the rotation-axis part 30. Hence, in the propeller fan 3, it is possible to make the separation area 20 generated on the downstream side of the rotation-axis part 30 sufficiently small.
As has been described above, because the propeller fan 3 according to Embodiment 1 has the first rib 32 and the second ribs 33 as described above, it is possible to make the separation area 20 generated on the downstream side of the rotation-axis part 30 sufficiently small. Hence, in the propeller fan 3 according to Embodiment 1, it is possible to suppress the creation of a vortex on the downstream side of the rotation-axis part 30. As a result, in the propeller fan 3 according to Embodiment 1, it is possible to suppress a decrease in the pressure-flow characteristics due to the creation of a vortex. Furthermore, in the propeller fan 3 according to Embodiment 1, it is possible to reduce the noise caused by the creation of a vortex.
Furthermore, the propeller fan 3 according to Embodiment 1 has the third ribs 35 extending toward the outer circumferential side of the first rib 32. Hence, in the propeller fan 3 according to Embodiment 1, it is possible to further diffuse the airflow A generated by the propeller fan 3 toward the inner circumferential side. Hence, in the propeller fan 3 according to Embodiment 1, it is possible to further suppress a decrease in the pressure-flow characteristics due to the creation of a vortex and, thus, to further reduce the noise caused by the creation of a vortex.
Furthermore, the outdoor unit 100 according to Embodiment 1 includes the above-described propeller fan 3 and the heat exchanger 8. Accordingly, in the outdoor unit 100 according to Embodiment 1, it is possible to make the separation area 20 generated on the downstream side of the rotation-axis part 30 of the propeller fan 3 sufficiently small. Hence, in the outdoor unit 100 according to Embodiment 1, it is possible to suppress the creation of a vortex on the downstream side of the rotation-axis part 30. Accordingly, it is possible to obtain the outdoor unit 100 in which a decrease in the pressure-flow characteristics due to the creation of a vortex is suppressed. Furthermore, it is possible to obtain the outdoor unit 100 in which the noise caused by the creation of a vortex is reduced.
In the propeller fan 3 according to Embodiment 1, the first rib 32 is formed of a plurality of ribs 32a having outer circumferential surfaces formed in a curved shape and having a substantially uniform thickness. In the propeller fan 3 according to Embodiment 1, the first rib 32 surrounds the rotation-axis part 30 to have a substantially polygonal shape when the first rib 32 is viewed in the axial direction of the rotation-axis part. However, the shape of the first rib 32 surrounding the rotation-axis part 30 is not limited to the shape described in Embodiment 1. For example, the first rib 32 may surround the rotation-axis part 30 in a manner described below. Note that, in Embodiment 2, components that are not specifically described have the same configurations as those in Embodiment 1, and the same functions and configurations will be described by using the same reference signs.
Also in the propeller fan 3 in which the first rib 32 is configured as shown in
Hence, also in the propeller fan 3 shown in
Comparing the propeller fan 3 shown in
Furthermore, comparing the propeller fan 3 shown in
Furthermore, the propeller fan 3 according to Embodiment 1 also has an advantage in that it can reduce the noise, compared with the propeller fan 3 shown in
Also in the propeller fan 3 having the first rib 32 configured as shown in
Hence, also in the propeller fan 3 shown in
Comparing the propeller fan 3 shown in
Furthermore, compared with the propeller fan 3 shown in
The first ribs 32 of the propeller fans 3 according to Embodiments 1 and 2 are formed of the ribs 32a having curved outer circumferential surfaces. However, the configuration is not limited thereto, and the present invention may also be implemented by forming the outer circumferential surfaces of the ribs 32a constituting the first rib 32 in a planar shape. Note that, in Embodiment 3, components that are not specifically described have the same configurations as those in Embodiment 1 or 2, and the same functions and configurations will be described by using the same reference signs.
The first rib 32 according to Embodiment 3 has a plurality of ribs 32a having linear outer circumferential surfaces when viewed in the axial direction of the rotation-axis part. In other words, the ribs 32a have planar outer circumferential surfaces. Furthermore, ends of the adjoining ribs 32a are joined to one another. Hence, the first rib 32 according to Embodiment 3 surrounds the rotation-axis part 30 such that the outer circumferential surface thereof has a polygonal shape when the first rib 32 is viewed in the axial direction of the rotation-axis part.
Also in the propeller fan 3 in which the first rib 32 is configured as described in Embodiment 3, the first rib 32 diffuses the air therearound as the propeller fan 3 rotates. Hence, it is possible to diffuse the airflow A to the vicinity of the outer circumferential part of the first rib 32. In addition, because the second ribs 33 also diffuses the air therearound, it is possible to diffuse the airflow A to the downstream side of the rotation-axis part 30. Accordingly, also in the propeller fan 3 according to Embodiment 3, it is possible to generate a sufficient amount of airflow A on the downstream side of the rotation-axis part 30 and, thus, to make the separation area 20 generated on the downstream side of the rotation-axis part 30 sufficiently small.
Hence, also in the propeller fan 3 according to Embodiment 3, similarly to those according to Embodiments 1 and 2, it is possible to suppress the creation of a vortex on the downstream side of the rotation-axis part 30. Accordingly, in the propeller fan 3 according to Embodiment 3, similarly to those according to Embodiments 1 and 2, it is possible to suppress a decrease in the pressure-flow characteristics due to the creation of a vortex and to reduce the noise caused by the creation of a vortex.
Compared with the propeller fan 3 shown in
Furthermore, compared with the propeller fan 3 shown in
In the case where the pressure generated on the upstream side or the downstream side of the propeller fan 3 in the airflow direction when the propeller fan 3 rotates increases, such as when the fins of the heat exchanger 8 are clogged with dust or dirt, a flow directed in the direction opposite to the direction of the airflow A is generated in the area on the downstream side of the rotation-axis part 30 in the direction of the airflow A. In other words, a flow of the air in the area shown as the separation area 20 in
However, in the propeller fan 3 according to Embodiments 1 to 3, the downstream ends 33a of the second ribs 33 are located on the downstream side of the downstream end 32b of the first rib 32 in the direction of the airflow A. Hence, when the propeller fan 3 rotates, the air flowing back toward the rotation-axis part 30 can be directed toward the outer circumferential side, with the portions of the second ribs 33 projecting further toward the downstream side in the direction of the airflow A than the first rib 32. As a result of this sent-out air being attracted to the airflow A, it is possible to diffuse the airflow A toward the inner circumferential side. Accordingly, in the propeller fan 3 described in Embodiments 1 to 3, it is possible to suppress the creation of a vortex on the downstream side of the rotation-axis part 30, even when the pressure generated on the upstream side or the downstream side of the propeller fan 3 in the airflow direction when the propeller fan 3 rotates increases. Accordingly, in the propeller fan 3 described in Embodiments 1 to 3, it is possible to suppress a decrease in the pressure-flow characteristics due to the creation of a vortex and to reduce the noise caused by the creation of a vortex, even when the pressure generated on the upstream side or the downstream side of the propeller fan 3 in the airflow direction when the propeller fan 3 rotates increases.
As has been described, when the creation of a vortex caused by an increase in the pressure generated on the upstream side or the downstream side of the propeller fan 3 in the airflow direction is to be suppressed, the creation of the vortex can be more effectively suppressed by providing closing ribs 36 as described below. In Embodiment 4, components that are not specifically described have the same configurations as those in any one of Embodiments 1 to 3, and the same functions and configurations will be described by using the same reference signs.
In the propeller fan 3 according to Embodiment 4, the downstream ends 33a of the second ribs 33 are located on the downstream side of the downstream end 32b of the first rib 32 in the direction of the airflow A. In other words, among the ends of the second ribs 33 in the direction of the center of rotation, the downstream ends 33a of the second ribs 33, which are distant from the pressure surfaces 31a, project in the direction away from the pressure surfaces 31a farther than the downstream end 32b of the first rib 32, which is distant from the pressure surfaces 31a, among the ends of the first rib 32 in the direction of the center of rotation.
Furthermore, the propeller fan 3 according to Embodiment 4 has the closing ribs 36 that close at least portions of spaces formed between the first rib 32 and the second ribs 33. The closing ribs 36 are disposed, for example, on a plane extending in a direction substantially perpendicular to the center of rotation from the downstream end 32b of the first rib 32. Note that
In the propeller fan 3 according to Embodiment 4, which has the closing ribs 36, when the air flowing back toward the rotation-axis part 30 as a result of an increase in the pressure generated on the upstream side or the downstream side of the propeller fan 3 in the airflow direction is to be directed toward the outer circumferential side with the second ribs 33, it is possible to prevent the air to be directed toward the outer circumferential side from colliding with the inner circumferential surface of the first rib 32, thus preventing failure to direct the air, which is to be directed toward the outer circumferential side, toward the outer circumferential side of the first rib 32. Accordingly, in the propeller fan 3 according to Embodiment 4, when the creation of a vortex caused by an increase in the pressure generated on the upstream side or the downstream side of the propeller fan 3 in the airflow direction is to be suppressed, it is possible to more effectively suppress the creation of a vortex, compared with a case where the closing ribs 36 are not provided.
In Embodiment 5, an example of a refrigeration cycle apparatus that has the propeller fan 3 described in Embodiments 1 to 4 will be described. In Embodiment 5, an example in which the refrigeration cycle apparatus is used as an air-conditioning apparatus will also be described. Note that, in Embodiment 5, components that are not specifically described have the same configurations as those in any one of Embodiments 1 to 4, and the same functions and configurations will be described by using the same reference signs.
An air-conditioning apparatus 400 includes the outdoor unit 100 and an indoor unit 200. The components of the outdoor unit 100 and the components of the indoor unit 200 are connected by refrigerant pipes, forming a refrigerant circuit through which refrigerant circulates. Note that, in the refrigerant pipes connecting the components of the outdoor unit 100 and the components of the indoor unit 200, a pipe through which gaseous refrigerant (gas refrigerant) flows is referred to as a gas pipe 301, and a pipe through which liquid refrigerant (liquid refrigerant, or in some cases, gas-liquid two-phase refrigerant) flows is referred to as a liquid pipe 302.
The outdoor unit 100 includes, for example: a compressor 10; a four-way valve 102; a heat exchanger 8, serving as an outdoor heat exchanger; the propeller fan 3; and an expansion device 105, serving as, for example, an expansion valve.
The compressor 10 compresses and discharges the refrigerant taken therein. Herein, it is desirable that the compressor 10 include an inverter device and that the capacity of the compressor 10 (the amount of refrigerant discharged unit time) can be finely changed by appropriately changing the operating frequency. Based on the instruction from the control substrate 13, the four-way valve 102 switches the direction of flow of the refrigerant according to whether the cooling operation is performed or the heating operation is performed. Note that, if the air-conditioning apparatus 400 performs only one of the cooling operation and the heating operation, the four-way valve 102 is unnecessary.
The heat exchanger 8, serving as the outdoor heat exchanger, performs heat exchange between the refrigerant and the outdoor air. For example, during the heating operation, the heat exchanger 8 serves as an evaporator and performs heat exchange between the outdoor air and a low-pressure refrigerant flowing into the outdoor unit 100 from the liquid pipe 302 and decompressed by the expansion device 105, thus evaporating the refrigerant into gas. During the cooling operation, the heat exchanger 8 serves as a condenser and performs heat exchange between the outdoor air and the refrigerant flowing therein from the four-way valve 102 side and compressed in the compressor 10, thus condensing the refrigerant into liquid. The propeller fan 3 described in Embodiments 1 to 4 above is provided near the heat exchanger 8 to guide the outdoor air to the heat exchanger 8. As described in Embodiment 1, the fan motor 4 for rotationally driving the propeller fan 3 is connected to the propeller fan 3. The fan motor 4 may also be configured such that the operating frequency thereof can be appropriately changed by using an inverter device so that the rotation speed of the propeller fan 3 can be finely changed. The expansion device 105 is provided to adjust the pressure of the refrigerant or other factor by changing the opening degree.
On the other hand, the indoor unit 200 has a load-side heat exchanger 201 and a load-side fan 202. The load-side heat exchanger 201 performs heat exchange between the refrigerant and the indoor air. For example, during the heating operation, the load-side heat exchanger 201 serves as a condenser and performs heat exchange between the indoor air and the refrigerant flowing therein from the gas pipe 301, thus condensing the refrigerant into liquid (or gas-liquid two-phase fluid) and then discharging the fluid into the liquid pipe 302. During the cooling operation, the load-side heat exchanger 201 serves as an evaporator and performs heat exchange between the indoor air and the refrigerant that has been reduced in pressure by, for example, the expansion device 105, thus allowing the refrigerant to remove heat from the air to be evaporated into gas and discharging the gas toward the gas pipe 301 side. Furthermore, the indoor unit 200 is provided with the load-side fan 202 that guides the indoor air to the load-side heat exchanger 201. The operating speed of the load-side fan 202 is set by, for example, a user. Note that the propeller fan 3 described in Embodiments 1 to 4 may of course be used as the load-side fan 202.
The air-conditioning apparatus 400 according to Embodiment 5 has a refrigerant circuit that includes the condenser (one of the heat exchanger 8 and the load-side heat exchanger 201) and the evaporator (the other of the heat exchanger 8 and the load-side heat exchanger 201). More specifically, the refrigerant circuit according to Embodiment 5 includes the compressor 10, the condenser (one of the heat exchanger 8 and the load-side heat exchanger 201), the expansion device 105, and the evaporator (the other of the heat exchanger 8 and the load-side heat exchanger 201). The air-conditioning apparatus 400 according to Embodiment 5 has the propeller fan 3 described in Embodiments 1 to 4, which serves as a fan for guiding the air to the condenser or the evaporator. Accordingly, in the air-conditioning apparatus 400 according to Embodiment 5, it is possible to make the separation area 20 generated on the downstream side of the rotation-axis part 30 of the propeller fan 3 sufficiently small. Hence, in the air-conditioning apparatus 400 according to Embodiment 5, it is possible to suppress the creation of a vortex on the downstream side of the rotation-axis part 30 of the propeller fan 3. Accordingly, it is possible to obtain the air-conditioning apparatus 400 in which a decrease in the pressure-flow characteristics due to the creation of a vortex is suppressed. Furthermore, it is possible to obtain the air-conditioning apparatus 400 in which the noise caused by the creation of a vortex is reduced.
Herein, the refrigeration cycle apparatus having the propeller fan 3 described in Embodiments 1 to 4 does not necessarily have to be used in the air-conditioning apparatus 400. For example, the refrigeration cycle apparatus having the propeller fan 3 described in Embodiments 1 to 4 may be used as any of various devices and facilities, such as a water heater, that have a refrigerant circuit and a fan for supplying the air to the heat exchanger of the refrigerant circuit.
It should be considered that the embodiments disclosed herein are examples and are not limiting in all aspects. It is intended that the scope of the present invention is defined by the claims, not by the descriptions given above, and that the scope of the present invention includes all modifications that have equivalent meaning to the claims and that are within the scope of the claims.
1 outdoor unit body, 1a first side-surface part, 1b front-surface part, 1c second side-surface part, 1d back-surface part, 1e top-surface part, 1f bottom-surface part, 1g air outlet, 1h air inlet, 2 fan grille, 3 propeller fan, 4 fan motor, 4a rotary shaft, 5 partition plate, 6 fan chamber, 7 machine chamber, 8 heat exchanger, 9 bell mouth, 10 compressor, 11 pipe, 12 board box, 13 control substrate, 20 separation area, 30 rotation-axis part, 30a connection hole, 31 blade, 31a pressure surface, 31b leading edge, 31c trailing edge, 32 first rib, 32a rib, 32b downstream-side end, 33 second rib, 33a downstream-side end, 34 reinforcing rib, 35 third rib, 36 closing rib, 100 outdoor unit, 102 four-way valve, 105 expansion device, 200 indoor unit, 201 load-side heat exchanger, 202 load-side fan, 301 gas pipe, 302 liquid pipe, 400 air-conditioning apparatus, 500 (related-art) outdoor unit, 503 (related-art) propeller fan, 540 (related-art) rib, A airflow
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/JP2016/081818 | 10/27/2016 | WO |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2018/078757 | 5/3/2018 | WO | A |
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| Number | Date | Country | |
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| 20200018321 A1 | Jan 2020 | US |
