Patent Grant
12196218
This application is a U.S. national stage application of PCT/JP2019/050392 filed on Dec. 23, 2019, the contents of which are incorporated herein by reference.
The present disclosure relates to an impeller, a multi-blade fan including the impeller, and an air-conditioning apparatus including the multi-blade fan.
An existing multi-blade fan includes a volute scroll casing and an impeller that is housed in the scroll casing and is rotated around an axis (see, for example, Patent Literature 1). The impeller of the multi-blade fan of Patent Literature 1 includes a discoid main plate, an annular side plate, and blades that are arranged radially. The blades of the impeller are provided such that main blades and intermediate blades are alternately arranged, and the inside diameters of the main and intermediate blades increase from the main plate toward the side plate. Furthermore, each of the blades of the impeller is a sirocco blade (forward-swept blade) whose outlet angle is greater than or equal to 100 degrees, includes an inducer portion of a turbo blade (swept-back blade) on an inner circumferential side of the blade, and is configured such that at portion of the main blades that are closer to the main plate, the ratio of the blade inside diameter to the blade outside diameter of the main blades is lower than or equal to 0.7.
The multi-blade fan of Patent Literature 1 includes a single-suction impeller configured to suck air into the impeller from one side of the impeller in an axial direction of the impeller. On the other hand, in a double-suction impeller configured to suck air into the impeller from both sides of the impeller in an axial direction of the impeller, the flow of sucked air may vary between the both sides of the impeller, depending on the type of usage, the environment of usage, or other conditions. For example, in the case where a motor is provided on one of the both sides of the impeller, the area where air is sucked is substantially reduced, thus causing a loss.
The present disclosure is applied to solve the above problem, and relates to an impeller that is of a double-suction type and reduces a loss that would be caused in the case where the of sucked air varies between both sides of the impeller because of the type of usage, the environment of usage, or other conditions, and also relates to a multi-blade fan including the impeller, and an air-conditioning apparatus including the multi-blade fan.
An impeller according to an embodiment of the present disclosure includes: a main plate configured to be driven to rotate; an annular side plate provided opposite to the main plate; and a plurality of blades connected to the main plate and the side plate and arranged in a circumferential direction with respect to a rotation axis of the main plate. Each of the plurality of blades has an inner circumferential end located closer to the rotation axis in a radial direction from the rotation axis, an outer circumferential end located closer to an outer circumferential side than the inner circumferential end in the radial direction, a sirocco blade portion formed as a forward-swept blade portion, including the outer circumferential end, and having an outlet angle that is greater than 90 degrees, and a turbo blade portion formed as a swept-back blade portion and including the inner circumferential end. The plurality of blades include a first blade portion provided on one plate side of the main plate, and a second blade portion provided on an other plate side of the main plate. The impeller includes a region in which a first inter-blade distance is greater than a second inter-blade distance, where an inter-blade distance is a distance between any adjacent two of the plurality of blades in the circumferential direction, the first inter-blade distance is the inter-blade distance of the first blade portion, and the second inter-blade distance is the inter-blade distance of the second blade portion.
A multi-blade fan according to another embodiment of the present disclosure includes the impeller; and a scroll casing housing the impeller, and having a peripheral wall formed into a volute shape and a side wall including a bellmouth that forms an air inlet communicating with a space defined by the main plate and the plurality of blades.
An air-conditioning apparatus according to still another embodiment of the present disclosure includes the multi-blade fan having the above configuration.
According to the embodiments of the present disclosure, the plurality of blades include a first blade portion formed on one plate side of the main plate and a second blade portion formed on the other plate side of the main plate, and the impeller includes a region in which a first inter-blade distance of the first blade portion is greater than a second inter-blade distance of the second blade portion. Therefore, even in the case where the impeller is of a double-suction type and the flow of sucked air varies between one suction side and the other suction side, depending on the type of usage, the environment of usage, or other conditions, by providing the first blade portion whose inter-blade distance is greater than that of the second blade portion, on a side through which a smaller amount of sucked air flows, it is possible to increase the flow rate of air that is sucked on the side where the first blade portion is located. As a result, the impeller can reduce a loss of suction.
In the following, an impeller, a multi-blade fan, and an air-conditioning apparatus according to embodiments are described, for example, with reference to the drawings. It should be noted that in figures including
[Multi-Blade Fan 100]
(Scroll Casing 40)
The scroll casing 40 houses the impeller 10 for use in the multi-blade fan 100, and rectifies air that is blown from the impeller 10. The scroll casing 40 has a scroll portion 41 and a discharge portion 42.
(Scroll Portion 41)
The scroll portion 41 forms an air passage through which a dynamic pressure of an air current produced by the impeller 10 is converted into a static pressure. The scroll portion 41 has a side wall 44a and a peripheral wall 44c. The side wall 44a covers the impeller 10 in an axial direction of a rotation axis RS of a shaft portion 11b of the impeller 10 and has a suction port 45 through which air is taken in. The peripheral wall 44c surrounds the impeller 10 in such a manner as to cover the impeller 10 in a radial direction of the rotation axis RS of the shaft portion 11b of the impeller 10. Furthermore, the scroll portion 41 has a tongue portion 43 that is located between the discharge portion 42 and a scroll start portion 41a of the peripheral wall 44c to form a curved surface and that guides the air current produced by the impeller 10 to a discharge port 42a via the scroll portion 41. It should be noted that the radial direction of the rotation axis RS is a direction perpendicular to the axial direction of the rotation axis RS. An internal space of the scroll portion 41 that is defined by the peripheral wall 44c and the side wall 44a serves as a space in which air blown from the impeller 10 flows along the peripheral wall 44c.
(Side Wall 44a)
Side walls 44a are provided on the both sides of the impeller 10 in the axial direction of the rotation axis RS of the impeller 10. In each of the side walls 44a of the scroll casing 40, the suction port 45 is formed such that air can flow between the impeller 10 and the outside of the scroll casing 40. The suction port 45 is formed in a circular shape, and is provided such that the center of the suction port 45 and the center of the shaft portion 11b of the impeller 10 substantially coincide with each other. It should be noted that the shape of the suction port 45 is not limited to the circular shape, and may be another shape such as an elliptical shape. The scroll casing 40 of the multi-blade fan 100 is a double-suction casing in which the side walls 44a are provided on both sides of the main plate 11 in the axial direction of the rotation axis RS of the shaft portion 11b, the side walls 44a having respective air inlets 45.
The multi-blade fan 100 has two side walls 44a in the scroll casing 40. The two side walls 44a are provided opposite to each other, with the peripheral wall 44c interposed between the side walls 44a. More specifically, as illustrated in
The suction port 45 provided in the side wall 44a is defined by a bellmouth 46. That is, the bellmouth 46 forms an suction port 45 that communicates with a space defined by the main plate 11 and a plurality of blades 12. The bellmouth 46 rectifies an air current to be sucked into the impeller 10 and causes the air current to flow into an air inlet 10e of the impeller 10. The bellmouth 46 is formed to have an opening whose diameter gradually decreases from the outside of the scroll casing 40 toward the inside of the scroll casing 40. Because of such a configuration of the side wall 44a, air in the vicinity the suction port 45 smoothly flows along the bellmouth 46 and efficiently flow into the impeller 10 through the suction port 45.
(Peripheral Wall 44c)
The peripheral wall 44c guides the air current produced by the impeller 10 toward the discharge port 42a along a curved wall surface. The peripheral wall 44c is a wall provided between side walls 44a that face each other, and has a curved surface along a rotation direction R of the impeller 10. The peripheral wall 44c is, for example, provided parallel to the axial direction of the rotation axis RS of the impeller 10 to cover the impeller 10; however, the location of the peripheral wall 44c is not limited to this. The peripheral wall 44c may be inclined relative to the axial direction of the rotation axis RS of the impeller 10. The peripheral wall 44c has an inner circumferential surface that covers the impeller 10 in the radial direction of the shaft portion 11b and faces the plurality of blades 12, which will be described later. The peripheral wall 44c faces a side of each of the blades 12 through which air is blown from the impeller 10. As illustrated in
The peripheral wall 44c is formed in a volute shape. An example of the volute shape is a shape based on a logarithmic spiral, a spiral of Archimedes, or an involute curve. An inner peripheral surface of the peripheral wall 44c constitutes a curved surface that is smoothly curved along a circumferential direction of the impeller 10 from the scroll start portion 41a, which is the start of the scroll of the volute shape, to the scroll end portion 41b, air sent out from the impeller 10 smoothly flows through the space between the impeller 10 and the peripheral wall 44c in a direction toward the discharge portion 42. Thus, in the scroll casing 40, the static pressure of air from the tongue portion 43 toward the discharge portion 42 in the scroll casing 40 efficiently rises.
(Discharge Portion 42)
The discharge portion 42 forms a discharge port 42a through which an air current produced by the impeller 10 is discharged after passing through the scroll portion 41. The discharge portion 42 is a hollow pipe having a rectangular cross section orthogonal to the flow direction of air that flows along the peripheral wall 44c. It should be noted that the cross-sectional shape of the discharge portion 42 is not limited to a rectangle. The discharge portion 42 forms a flow passage through which air sent out from the impeller 10 and flowing through a gap between the peripheral wall 44c and the impeller 10 is guided to be let out of the scroll casing 40.
As illustrated in
(Tongue Portion 43)
In the scroll casing 40, the tongue portion 43 is formed between the diffuser plate 42c of the discharge portion 42 and the scroll start portion 41a of the peripheral wall 44c. The tongue portion 43 is formed to have a predetermined radius of curvature, and the peripheral wall 44c is smoothly connected to the diffuser plate 42c, with the tongue portion 43 interposed between the peripheral wall 44c and the diffuser plate 42c. The tongue portion 43 reduces inflow of air from the start to the end of the scroll of a volute flow passage. The tongue portion 43 is provided at upstream part of a ventilation flue, and has a role to divert the flow of air in the rotation direction R of the impeller 10 and the flow of air in a discharge direction from downstream part of the ventilation flue toward the discharge port 42a from each other. Furthermore, the static pressure of air that is to flow into the discharge portion 42 rises while the air is passing through the scroll casing 40 and becomes higher than in the scroll casing 40. Therefore, the tongue portion 43 has a function of isolating different pressures from each other.
(Impeller 10)
The impeller 10 is a centrifugal fan. The impeller 10 is driven to rotate, for example, by a motor (not illustrated), and forcibly sends out air outwards in the radial direction of the impeller 10 with a centrifugal force generated by the rotation of the impeller 10. The impeller 10 is rotated, for example, by the motor in the rotation direction R, which is indicated by an arrow. As illustrated in
Regarding the shape of the main plate 11, it suffices that the main plate 11 is formed in the shape of a plate. The main plate may, for example, have a shape other than a discoid shape, for example, a polygonal shape. Furthermore, the main plate 11 may be formed such that as illustrated in
The plurality of blades 12 are arranged in the circumferential direction around the imaginary rotation axis RS of the main plate 11. One end of each of the plurality of blades 12 is connected to the main plate 11, and the other end of each of the plurality of blades 12 is connected to the side plate 13. Each of the plurality of blades 12 is provided between the main plate 11 and the side plate 13. The plurality of blades 12 are provided on both sides of the main plate 11 in the axial direction of the rotation axis RS of the shaft portion 11b. The blades 12 are arranged at regular intervals on the peripheral edge of the main plate 11. A configuration of each of the blades 12 will be described in detail later.
The annular side plate 13 of the impeller 10 is attached to ends of the plurality of blades 12 that are opposite to the main plate 11 in the axial direction of the rotation axis RS of the shaft portion 11b. In the impeller 10, the side plate 13 is provided opposite to the main plate 11. The side plate 13 couples the plurality of blades 12 with each other, thereby maintaining a positional relationship between a distal end of each blade 12 and the distal end of the other blade 12 and reinforcing the plurality of blades 12.
As illustrated in
The first blade portion 112a is provided on one plate side of the main plate 11, and the second blade portion 112b is provided on the other plate side of the main plate 11. That is, the plurality of blades 12 are provided on both sides of the main plate 11 in the axial direction of the rotation axis RS, and the first blade portion 112a and the second blade portion 112b are provided opposite to each other, with the main plate 11 interposed between the first blade portion 112a and the second blade portion 112b. It should be noted that referring to
The plurality of blades 12 of the impeller 10 are arranged on the main plate 11 such that the impeller 10 is formed in a tubular shape. Moreover, the impeller 10 has an air inlet 10e formed on a side of the side plate 13 that is opposite to the main plate 11 in the axial direction of the rotation axis RS of the shaft portion 11b and configured to cause gas to flow into a space surrounded by the main plate 11 and the plurality of blades 12. In the impeller 10, the blades 12 and side plates 13 are provided on plate sides of the main plate 11, and air inlets 10e are formed on the plate sides of the main plate 11.
The impeller 10 is driven to rotate around the rotation axis RS by driving of the motor (not illustrated). When the impeller 10 is rotated, air that flows at the outside of the multi-blade fan 100 is sucked into the space surrounded by the main plate 11 and the plurality of blades 12 through the suction port 45 formed in the scroll casing 40 and the air inlet 10e of the impeller 10. Further, when the impeller 10 is rotated, the air sucked into the space surrounded by the main plate 11 and the plurality of blades 12 is sent out outward in the radial direction of the impeller 10 through spaces between adjacent ones of the blades 12.
(Detailed Configuration of Blade 12)
As illustrated in
As illustrated in
A basic configuration of the blades 12 in the second blade portion 112b is similar to a basic configuration of the blades 12 in the first blade portion 112a. That is, the middle position MP of the impeller 10 as indicated in
As illustrated in
In the first section of the impeller 10 that is taken along the first plane 71 perpendicular to the rotation axis RS, each of the first blades 12A has an inner circumferential end 14A located closer to the rotation axis RS in a radial direction around the rotation axis RS and an outer circumferential end 15A located closer to an outer circumferential side than the inner circumferential end 14A in the radial direction. In each of the first blades 12A, the inner circumferential end 14A is provided more forward than the outer circumferential end 15A in the rotation direction R of the impeller 10. As illustrated in
In the first section of the impeller 10 that is taken along the first plane 71 perpendicular to the rotation axis RS, each of the second blades 12B has an inner circumferential end 14B located closer to the rotation axis RS in the radial direction around the rotation axis RS and an outer circumferential end 15B located closer to an outer circumferential side than the inner circumferential end 14B in the radial direction. In each of the plurality of second blades 12B, the inner circumferential end 14B is provided more forward than the outer circumferential end 15B in the rotation direction R of the impeller 10. As illustrated in
Next, a relationship between the first blades 12A and the second blades 12B will be described. As illustrated in
It is assumed that as illustrated in
Furthermore, it is also assumed that in the first section, the diameter of a circle C2 drawn through the inner circumferential ends 14B of the second blades 12B around the rotation axis RS, that is, the inside diameter of the second blades 12B, is an inside diameter ID2 that is larger than the inside diameter ID1 (inside diameter ID2>inside diameter ID1); and the diameter of the circle C3 drawn through the outer circumferential ends 15B of the second blades 12B around the rotation axis RS, that is, the outside diameter of the second blades 12B, is an outside diameter OD2 that is equal to the outside diameter OD1 (outside diameter OD2=outside diameter OD1). Half of the difference between the outside diameter OD2 and the inside diameter ID2 is equal to the blade length L2a of each of the second blades 12B in the first section (blade length L2a=[outside diameter OD2−inside diameter ID2]/2). In the first section, the blade length L2a of each of the second blades 12B is smaller than the blade length L1a of each of the first blades 12A (blade length L2a<blade length L1a). It should be noted that the ratio of the inside diameter of the second blades 12B to the outside diameter of the second blades 12B is lower than or equal to 0.7. That is, in the second blades 12B, the ratio of the inside diameter ID2 of the circle drawn through the inner circumferential ends 14B of the second blades 12B to the outside diameter OD2 of the circle drawn through the outer circumferential ends 15B of the second blades 12B is lower than or equal to 0.7.
Furthermore, it is assumed that as illustrated in
Also, it is assumed that in the second section, the diameter of the circle C7 drawn through the inner circumferential ends 14B of the second blades 12B around the rotation axis RS is an inside diameter ID4. In the second section, the inside diameter ID4 is equal to the inside diameter ID3 (inside diameter ID4=inside diameter ID3). It is assumed that the diameter of the circle C8 drawn through the outer circumferential ends 15B of the second blades 12B around the rotation axis RS is an outside diameter OD4. In the second section, the outside diameter OD4 is equal to the outside diameter OD3 (outside diameter OD4=outside diameter OD3). Half of the difference between the outside diameter OD4 and the inside diameter ID4 is equal to the blade length L2b of each of the second blades 12B in the second section (blade length L2b=(outside diameter OD4−inside diameter ID4)/2). In the second section, the blade length L2b of each of the second blades 12B is equal to the blade length LIb of each of the first blades 12A (blade length L2b=blade length L1b).
As viewed from a direction parallel to the rotation axis RS, the first blades 12A in the second section as illustrated in
Similarly, as viewed in the direction parallel to the rotation axis RS, the second blades 12B in the second section as illustrated in
It should be noted that as described above, the ratio of the inside diameter ID1 to the outside diameter OD1 of the first blades 12A is lower than or equal to 0.7. Since the blades 12 are configured such that the inside diameter ID3≥the inside diameter ID1, the inside diameter ID4≥an inside diameter ID2, and the inside diameter ID2>the inside diameter ID1, the inside diameter of the first blades 12A can be the blade inside diameter of the blades 12. Furthermore, since the blades 12 are configured such that the outside diameter OD3=the outside diameter OD1, the outside diameter OD4=the outside diameter OD2, and the outside diameter OD2=the outside diameter OD1, the outside diameter of the first blades 12A can be the blade outside diameter of the blades 12. Moreover, in the case where the blades 12 included in the impeller 10 are seen as a whole, the blades 12 are configured such that the ratio of the blade inside diameter to the blade outside diameter of the blades 12 is lower than or equal to 0.7. It should be noted that the blade inside diameter of the blades 12 is the diameter of the circle drawn through the inner circumferential ends of the plurality of blades 12. That is, the blade inside diameter of the blades 12 is the diameter of a circle drawn through the leading edges 14A1 of the plurality of blades 12. Furthermore, the blade outside diameter of the blades 12 is the diameter of the circle drawn through the outer circumferential ends of the plurality of blades 12. That is, the blade outside diameter of the blades 12 is the diameter of a circle drawn through the trailing edges 15A1 and 15B1 of the blades 12.
(Configuration of First Blades 12A and Second Blades 12B)
In a comparison between the first section as illustrated in
As illustrated in
(Sirocco Blade Portion and Turbo Blade Portion)
As illustrated in
In the radial direction of the impeller 10, a region where the first sirocco blade portion 12A1 of the first blade 12A is formed will be referred to as a first sirocco region 12A11, and an area where the first turbo blade portion 12A2 of the first blade 12A is formed will be referred to as a first turbo region 12A21. The first blade 12A is configured such that the first turbo region 12A21 is larger than the first sirocco region 12A11 in the radial direction of the impeller 10. Moreover, in both the main-plate-side blade region 122a serving as the first region and the side-plate-side blade region 122b serving as the second region, the impeller 10 has the relationship “first sirocco region 12A11<first turbo region 12A21” in the radial direction of the impeller 10. In the impeller 10 and the first blade 12A, in both the main-plate-side blade region 122a serving as the first region and the side-plate-side blade region 122b serving as the second region, the ratio of the first turbo blade portion 12A2 to the first sirocco blade portion 12A1 in the radial direction of the impeller 10 is high.
Similarly, as illustrated in
In the radial direction of the impeller 10, a region where the second sirocco blade portion 12B1 of the second blade 12B is formed will be referred to as a second sirocco region 12B11, and a region where the second turbo blade portion 12B2 of the second blade 12B is formed will be referred to as a second turbo region 12B21. The second blade 12B is configured such that the second turbo region 12B21 is larger than the second sirocco region 12B11 in the radial direction of the impeller 10. Moreover, in both the main-plate-side blade region 122a serving as the first region and the side-plate-side blade region 122b serving as the second region, the impeller 10 has the relationship “second sirocco region 12B11<second turbo region 12B21” in the radial direction of the impeller 10. In the impeller 10 and the second blade 12B, in both the main-plate-side blade region 122a serving as the first region and the side-plate-side blade region 122b serving as the second region, the ratio of the second turbo blade portion 12B2 to the second sirocco blade portion 12B1 in the radial direction of the impeller 10 is high.
In the above configuration, each of the plurality of blades 12 is configured such that in both the main-plate-side blade region 122a and the side-plate-side blade region 122b, a region where the turbo blade portion is formed is larger than a region where the sirocco blade portion is formed, in the radial direction of the impeller 10. That is, each of the plurality of blades 12 is configured such that in both the main-plate-side blade region 122a and the side-plate-side blade region 122b, the ratio of the turbo blade portion to the sirocco blade portion in the radial direction of the impeller 10 is high, and have the relationship “sirocco region <turbo region”. In other words, each of the plurality of blades 12 is configured such that in the first region and the second region, a ratio of the turbo blade portion in the radial direction is larger than a ratio of the sirocco blade portion in the radial direction. It should be noted that the configuration of the plurality of blades 12 is not limited to a configuration in which both the main-plate-side blade region 122a and the side-plate-side blade region 122b, the ratio of the turbo blade portion to the sirocco blade portion in the radial direction of the impeller 10 is high, and the relationship “sirocco region <turbo region” is satisfied. Each of the plurality of blades 12 may be configured such that in the first region and the second region, the ratio of the turbo blade portion to the sirocco blade portion in the radial direction is low, or the ratio of the turbo blade portion to the sirocco blade portion in the radial direction is equal to the ratio of the sirocco blade portion to the turbo blade portion in the radial direction.
(Outlet Angle)
It is assumed that as illustrated in
As illustrated in
Furthermore, it is assumed that as illustrated in
Although it is not illustrated in
(Radial Blade Portion)
As illustrated in
(Inter-Blade Distance)
It should be noted that the between any adjacent two of the blades 12 arranged in the circumferential direction will be referred to as an inter-blade distance. In the blades 12, the inter-blade distance increases from the leading edges 14A1 toward the trailing edges 15A1 as illustrated in
As illustrated in
The first blade portion 112a and the second blade portion 112b each have a blade inclined region 142 that is inclined such that in the direction from the main plate 11 toward the side plate 13, the distances between the leading edges 14A1 and the leading edges 14B1 and the rotation axis RS increase, and the blade inside diameters increase. In the case where the plurality of blades 12 are made up of first blades 12A only as illustrated in
The blade inclined region 142 is formed at least in a region between the circle C1 drawn through portions of the inner circumferential ends 14A of the first blades 12A that are closer to the main plate 11 and the circle C7 drawn through portions of the inner circumferential ends 14A of the first blades 12A that are closer to the side plate 13. That is, the blade inclined region 142 is formed at least in a region between portions of the first blades 12A in the first section that have the inside diameter ID1 and are closer to the main plate 11 than the middle position MP and portions of the first blades 12A in the second section that have the inside diameter ID3 and are closer to the side plate 13 than the middle position MP. It should be noted that the blade inclined region 142 is a region in which the above inclined portions 141A and 141B are formed.
As illustrated in
More specifically, as illustrated in
As illustrated in
The first inter-blade distance a1 and the second inter-blade distance b1 are distances measured at points that are separated by the same distance from the rotation axis RS in the radial direction of the impeller 10 from the rotation axis RS. Similarly, the first inter-blade distance a1-1 and the second inter-blade distance b1-1 are distances measured at points that are separated by the same distance from the rotation axis RS in the radial direction of the impeller 10 from the rotation axis RS. Similarly, the first inter-blade distance a1-2 and the second inter-blade distance b1-2 are distances measured at points that are separated by the same distance from the rotation axis RS in the radial direction of the impeller 10 from the rotation axis RS. Similarly, the first inter-blade distance a1-3 and the second inter-blade distance b1-3 are distances measured at points that are separated by the same distance from the rotation axis RS in the radial direction of the impeller 10 from the rotation axis RS. Similarly, the first inter-blade distance a1-4 and the second inter-blade distance b1-4 are distances measured at points that are separated by the same distance from the rotation axis RS in the radial direction of the impeller 10 from the rotation axis RS.
The impeller 10 of the multi-blade fan 100 is formed such that the first inter-blade distance a1-1 in the first blade portion 112a, which the motor 50 is provided to face, is greater than the second inter-blade distance b1-1 in the second blade portion 112b, which the motor 50 is not provided to face (first inter-blade distance a1-1>second inter-blade distance b1-1). Similarly, the impeller 10 is formed such that the first inter-blade distance a1-2 in the first blade portion 112a, which the motor 50 is provided to face, is greater than the second inter-blade distance b1-2 in the second blade portion 112b, which the motor 50 is not provided to face (first inter-blade distance a1-2>second inter-blade distance b1-2). Similarly, the impeller 10 is formed such that the first inter-blade distance a1-3 in the first blade portion 112a, which the motor 50 is provided to face, is greater than the second inter-blade distance b1-3 in the second blade portion 112b, which the motor 50 is not provided to face (first inter-blade distance a1-3>second inter-blade distance b1-3). Similarly, the impeller 10 is formed such that the first inter-blade distance a1-4 in the first blade portion 112a, which the motor 50 is provided to face, is greater than the second inter-blade distance b1-4 in the second blade portion 112b, which the motor 50 is not provided to face (first inter-blade distance a1-4>second inter-blade distance b1-4).
The impeller 10 is formed such that the first inter-blade distance a1 between any adjacent two of blades 12 included in the first blade portion 112a, which the motor 50 is provided to face, is greater than the second inter-blade distance b1 between any adjacent two of blades 12 included in the second blade portion 112b, which the motor 50 is not provided to face (first inter-blade distance a1>second inter-blade distance b1). Moreover, the multi-blade fan 100 includes a region in which the first inter-blade distance a1 between any adjacent two of a plurality of blades 12 included in the first blade portion 112a, which the motor 50 is provided to face, is greater than the second inter-blade distance b1 between any adjacent two of a plurality of blades 12 included in the second blade portion 112b, which the motor 50 is not provided to face. In the case where the multi-blade fan 100 includes the impeller 10A as illustrated in
The impeller 10 of the multi-blade fan 100 is formed such that the first inter-blade distance a1 of the first blade portion 112a beside the main plate 11 as illustrated in
The impeller 10 of the multi-blade fan 100 is formed such that the first inter-blade distance a2 of the first blade portion 112a beside the side plate 13 as illustrated in
The impeller 10 of the multi-blade fan 100 is formed such that the first inter-blade distance a2 of the first blade portion 112a beside the side plate 13 as illustrated in
As described above, the main-plate-side blade region 122a of the impeller 10 that is closer to the main plate 11 is a first region, and the side-plate-side blade region 122b of the impeller 10 that is closer to the side plate 13 is a second region. Therefore, the impeller 10 and the multi-blade fan 100 are formed such that the first inter-blade distance a1 in the first region is greater than the second inter-blade distance b1 in the first region (first inter-blade distance a1>second inter-blade distance b1) and the first inter-blade distance a2 in the second region is greater than or equal to the second inter-blade distance b2 in the second region (first inter-blade distance a2≥second inter-blade distance b2). Furthermore, the impeller 10 and the multi-blade fan 100 may be further formed such that the first inter-blade distance a2 in the second region is greater than the first inter-blade distance a1 in the first region (first inter-blade distance a1<first inter-blade distance a2) and the second inter-blade distance b2 in the second region is greater than the second inter-blade distance b1 in the first region (second inter-blade distance b1<second inter-blade distance b2). That is, the impeller 10 and the multi-blade fan 100 may be formed such that the inter-blade distance in a region closer to the side plate 13 is greater than the inter-blade distance in a region closer to the main plate 11. Furthermore, the impeller 10 and the multi-blade fan 100 may be formed such that the first inter-blade distance a2 in the second region is greater than the second inter-blade distance b1 in the first region (first inter-blade distance a2>second inter-blade distance b1). Therefore, the impeller 10 of the multi-blade fan 100 is formed such that the inter-blade distance between any adjacent ones of the blades 12 included in the first blade portion 112a, which the motor 50 is provided to face, is greater than or equal to the inter-blade distance between the blades 12 included in the second blade portion 112b, which the motor 50 is not provided to face. In addition, the impeller 10 of the multi-blade fan 100 is formed such that the inter-blade distance between any adjacent ones of the blades 12 included in the region closer to the side plate 13 is greater than the inter-blade distance between any adjacent ones of the blades 12 included in the region closer to the main plate 11.
[Relationship Between Impeller 10 and Scroll Casing 40]
The impeller 10 is configured such that the first turbo region 12A21 is larger than the first sirocco region 12A11 in the radial direction with respect to the rotation axis RS. That is, the impeller 10 and each of the first blades 12A are configured such that in the radial direction with respect to the rotation axis RS, the ratio of the first turbo blade portion 12A2 to the first sirocco blade portion 12A1 is higher than the ratio of the first sirocco blade portion 12A1 to the first turbo blade portion 12A2, and the relationship “first sirocco blade portion 12A1<first turbo blade portion 12A2” is satisfied. The relationship regarding the ratio between the first sirocco blade portion 12A1 and the ratio of the first turbo blade portion 12A2 in the radial direction of the rotation axis RS is established in both the main-plate-side blade region 122a corresponding to the first region and the side-plate-side blade region 122b corresponding to the second region. It should be noted that the configuration of the impeller 10 and each of the first blades 12A is not limited to a configuration in which in the radial direction with respect to the rotation axis RS, the ratio of the first turbo blade portion 12A2 to the first sirocco blade portion 12A1 is higher than the ratio of the first sirocco blade portion 12A1 to the first turbo blade portion 12A2, and the relationship “first sirocco blade portion 12A1<first turbo blade portion 12A2” is satisfied. The impeller 10 and each of the first blades 12A may be configured such that in the radial direction with respect to the rotation axis RS, the ratio of the first turbo blade portion 12A2 to the first sirocco blade portion 12A1 is lower than or equal to the ratio of the first sirocco blade portion 12A1 to the first turbo blade portion 12A2.
Furthermore, as viewed in the direction parallel to the rotation axis RS, a region including portions of the blades 12 that are closer to the outer circumferential side than the inner circumferential side of the bellmouth 46 that has inside diameter BI in the radial direction with respect to the rotation axis RS will be referred to as an outer circumferential region 12R. It is preferable that the impeller 10 be configured such that in the outer circumferential region 12R also, the ratio of the first turbo blade portion 12A2 to the first sirocco blade portion 12A1 is higher than the ratio of the first sirocco blade portion 12A1 to the first turbo blade portion 12A2. That is, as viewed in the direction parallel to the rotation axis RS, in the outer circumferential region 12R of the impeller 10 that is closer to the outer circumferential side than the inner circumferential side of the bellmouth 46 that has the inside diameter BI, a first turbo region 12A21a is larger than the first sirocco region 12A11 in the radial direction with respect to the rotation axis RS. The first turbo region 12A21a is a region of the first turbo region 12A21 that is closer to the outer circumferential side than the inner circumferential side of the bellmouth that has the inside diameter BI, as viewed in the direction parallel to the rotation axis RS. Moreover, where a first turbo blade portion 12A2a is a first turbo blade portion 12A2 that forms the first turbo region 12A21a, it is preferable that the outer circumferential region 12R of the impeller 10 be configured such that the ratio of the first turbo blade portion 12A2a to the first sirocco blade portion 12A1 is higher than the ratio of the first sirocco blade portion 12A1 to the first turbo portion 12A2a. The relationship regarding the ratio between the first sirocco blade portion 12A1 and the ratio of the first turbo blade portion 12A2a in the outer circumferential region 12R is established in both the main-plate-side blade region 122a corresponding to the first region and the side-plate-side blade region 122b corresponding to the second region.
Similarly, the impeller 10 is configured such that the second turbo region 12B21 is larger than the second sirocco region 12B11 in the radial direction with respect to the rotation axis RS. That is, the impeller 10 and each of the second blades 12B are configured such that the ratio of the second turbo blade portion 12B2 to the second sirocco blade portion 12B1 is higher than the ratio of the second sirocco blade portion 12B1 to the second turbo blade portion 12B2 in the radial direction with respect to the rotation axis RS, and the relationship “second sirocco blade portion 12B1<second turbo blade portion 12B2” is satisfied. The relationship regarding the ratio between the second sirocco blade portion 12B1 and the second turbo blade portion 12B2 in the radial direction of the rotation axis RS is also satisfied in both the main-plate-side blade region 122a corresponding to the first region and the side-plate-side blade region 122b corresponding to the second region. It should be noted that the configuration of the impeller 10 and each of the second blades 12B is not limited to a configuration in which the ratio of the second turbo blade portion 12B2 to the second sirocco blade portion 12B1 is higher than the ratio of the second sirocco blade portion 12B1 to the second turbo blade portion 12B2 in the radial direction with respect to the rotation axis RS, and the relationship “second sirocco blade portion 12B1<second turbo blade portion 12B2” is satisfied. The impeller 10 and each of the second blades 12B may be configured such that the ratio of the second turbo blade portion 12B2 to the second sirocco blade portion 12B1 is lower than or equal to the ratio of the second sirocco blade portion 12B1 to the second sirocco blade portion 12B1 in the radial direction with respect to the rotation axis RS.
Furthermore, it is preferable for the impeller 10 that in the outer circumferential region 12R also, the ratio of the second turbo blade portion 12B2 to the second sirocco blade portion 12B1 is higher than the ratio of the second sirocco blade portion 12B1 to the second turbo blade portion 12B2. That is, as viewed in the direction parallel to the rotation axis RS, in the outer circumferential region 12R of the impeller 10 that is closer to the outer circumferential side than the inner circumferential side of the bellmouth 46 that has the inside diameter B, a second turbo region 12B21a is larger than the second sirocco region 12B11 in the radial direction with respect to the rotation axis RS. The second turbo region 12B21a is a region included in the second turbo region 12B21 that is closer to the outer circumferential side than the inner circumferential side of the bellmouth 46 that has inside diameter BI, as viewed in the direction parallel to the rotation axis RS. Moreover, in the case where a second turbo blade portion 12B2 that forms the second turbo region 12B21a is a second turbo blade portion 12B2a, it is desirable that the outer circumferential region 12R of the impeller 10 be configured such that the ratio of the second turbo blade portion 12B2a to the second sirocco blade portion 12B1 is higher than the ratio of the second sirocco blade portion 12B1 to the second turbo blade portion 12B2a. The relationship regarding the ratio between the second sirocco blade portion 12B1 and the second turbo blade portion 12B2a in the outer circumferential region 12R is established in both the main-plate-side blade region 122a corresponding to the first region and the side-plate-side blade region 122b corresponding to the second region.
As illustrated in
Furthermore, as illustrated in
As illustrated in
The motor 50 is provided adjacent to the side wall 44a of the scroll casing 40. The motor 50 includes a motor shaft 51 that extends along the rotation axis RS of the impeller 10 and is inserted in the scroll casing 40 through a side surface of the scroll casing 40.
The main plate 11 is provided perpendicular to the rotation axis RS along the side wall 44a of the scroll casing 40 that is closer to the motor 50. The main plate 11 has, at central part thereof, a shaft portion 11b to which the motor shaft 51 is connected, and the motor shaft 51 is fixed to the shaft portion 11b of the main plate 11 while being inserted in the scroll casing 40. The motor shaft 51 of the motor 50 is connected to and fixed to the main plate 11 of the impeller 10.
When the motor 50 is driven, the blades 12 is rotated around the rotation axis RS via the motor shaft 51 and the main plate 11. As a result, outside air is sucked into the impeller 10 through the suction port 45 and blown into the scroll casing 40 by a pressure-rising action of the impeller 10. The air blown into the scroll casing 40 is decelerated in an expanded air passage formed by the peripheral wall 44c of the scroll casing 40 to recover its static pressure, and is blown to the outside through the discharge port 42a illustrated in
An outer peripheral wall 52 that forms an end portion 50a of the motor 50 that has the outside diameter MO1 is located between an imaginary extended surface VF1 that is formed by increasing the blade inside diameter of the portions of the blades 12 that are closer to the main plate 11, in the axial direction of the rotation axis RS, and an imaginary extended surface VF3 that is formed by increasing the blade inside diameter of the portions of the blades 12 that are closer to the side plate 13, in the axial direction of the rotation axis RS. Furthermore, the outer peripheral wall 52 that forms the end portion 50a of the motor 50 which has the outside diameter MO1 is provided in such a location as to face the first turbo blade portions 12A2 and the second turbo blade portions 12B2 in the axial direction of the rotation axis RS. More specifically, the outside diameter MO1 of the end portion 50a of the motor 50 is larger than the inside diameter ID1 of the portions of the first blades 12A that are closer to the main plate 11, and smaller than the inside diameter ID3 of the portions of the first blades 12A that are closer to the side plate 13. That is, the outside diameter MO1 of the end portion 50a of the motor 50 is larger than the blade inside diameter of the portions of the blades 12 that are closer to the main plate 11 and smaller than the blade inside diameter of the portions of the blades 12 that are closer to the side plate 13. Further, the outer peripheral wall 52 at the end portion 50a of the motor 50 is located between portions of the first turbo blade portions 12A2 and the second turbo blade portions 12B2 that are located between the above circles C1a and C7a, as viewed in the direction parallel to the rotation axis RS. It should be noted that regarding the multi-blade fan 100, the value of the outside diameter MO2 of part of the motor 50 that is other than the end portion 50a is not limited.
Furthermore, an outer peripheral wall 52b of the motor 50B that has the outermost diameter MO2a is located between the imaginary extended surface VF1 that is formed by increasing the blade inside diameter of the portions of the blades 12 that are closer to the main plate 11 in the axial direction of the rotation axis RS and an imaginary extended surface VF3 that is formed by increasing the blade inside diameter of the portions of the blades 12 that are closer to the side plate 13 in the axial direction of the rotation axis RS. Furthermore, the outer peripheral wall 52b of the motor 50B, which has the outermost diameter MO2a, is provided in such a location as to face the first turbo blade portions 12A2 and the second turbo blade portions 12B2 in the axial direction of the rotation axis RS. More specifically, the outermost diameter MO2a of the motor 50B is larger than the inside diameter ID1 of the portions of the first blades 12A that are closer to the main plate 11 and smaller than the inside diameter ID3 of the first blades 12A beside the side plate 13. That is, the outermost diameter MO2a of the motor 50B is larger than the blade inside diameter of the portions of the blades 12 that are closer to the main plate 11 and smaller than the blade inside diameter of the portions of the blades 12 that are closer to the side plate 13. Furthermore, the outer peripheral wall 52b of the motor 50B, which has the outermost diameter MO2a, is located in a region of the first turbo blade portions 12A2 and the second turbo blade portions 12B2 between the above circles C1a and C7a as viewed in the direction parallel to the rotation axis RS.
[Advantages of Impeller 10 and Multi-Blade Fan 100]
In the impeller 10 and the multi-blade fan 100, the blades 12 include a first blade portion 112a formed on one plate side of the main plate 11 and a second blade portion 112b formed on the other plate side of the main plate 11. Moreover, the impeller 10 and the multi-blade fan 100 include a region in which a first inter-blade distance of the first blade portion 112a is greater than a second inter-blade distance of the second blade portion 112b. Therefore, even if the area of suction of air in the impeller 10 is reduced because of provision of the motor 50, it is possible to reduce a loss of suction on a side of the impeller 10 where the motor 50 is provided, by providing the motor 50 on the side where the first blade portion 112a, whose inter-blade distance is great, is formed. That is, even in the case where the impeller 10 is of a double-suction type and the flow of sucked air varies between one suction side and the other suction side, depending on the type of usage, the environment of usage, or other conditions, by providing the first blade portion 112a, whose inter-blade distance is greater than that of the second blade portion 112b, on a side through which a smaller amount of sucked air flows, it is possible to increase the flow rate of air that is sucked on the side where the first blade portion 112a is located. As a result, the impeller 10 can reduce a loss of suction.
Furthermore, in the first and second regions of the impeller 10, the ratio of the turbo blade portion to the sirocco blade portion in the radial direction is higher than the ratio of the sirocco blade portion to the turbo blade portion in the radial direction. Since the impeller 10 is configured such that the ratio of the turbo blade portion to the sirocco blade portion is higher in any region between the main plate 11 and the side plate 13, sufficient pressure recovery can be achieved by the blades. Therefore, the impeller 10 can further improve pressure recovery than an impeller or a multi-blade fan that does not have the above configuration.
Furthermore, each of the blades 12 has a blade inclined region 142 that is inclined such that in the direction from the main plate 11 toward the side plate 13, the distances between the inner circumferential end 14A and the inner circumferential end 14B and the rotation axis RS increase. Moreover, the first inter-blade distance a1 is an inter-blade distance of the blade inclined region 142 of the first blade portion 112a, and the second inter-blade distance b1 is an inter-blade distance of the blade inclined region 142 of the second blade portion 112b. In the case where the motor 50 is provided, the blade inclined region 142 is located to face the first blade portion 112a in the axial direction of the rotation axis RS. Moreover, the impeller 10 and the multi-blade fan 100 include a region which the first inter-blade distance a1 of the first blade portion 112a is greater than the second inter-blade distance b1 of the second blade portion 112b. Therefore, even if the area of suction of air in the impeller 10 is reduced because of provision of the motor 50, it possible to reduce a loss of suction on a side of the impeller 10 where the motor 50 is provided, by providing the motor 50 on the side where the first blade portion 112a, whose inter-blade distance is great, is formed. That is, even in the case where the impeller 10 is of a double-suction type and the flow of sucked air varies between one suction side and the other suction side, depending on the type of usage, the environment of usage, or other conditions, by providing the first blade portion 112a, whose inter-blade distance is greater than that of the second blade portion 112b, on a side through which sucked air flows at a low rate, it is possible to increase the flow rate of air that is sucked on the side where the first blade portion 112a is located. As a result, the impeller 10 can reduce a loss of suction.
In the impeller 10 and the multi-blade fan 100, the first inter-blade distance of the first region is greater than the second inter-blade distance of the first region (first inter-blade distance a1>second inter-blade distance b1) and the first inter-blade distance of the second region is greater than or equal to the second inter-blade distance of the second region (first inter-blade distance a2≥second inter-blade distance b2). Therefore, even if the area of suction of air in the impeller 10 is reduced because of provision of the motor 50, it possible to reduce a loss of suction on a side of the impeller 10 where the motor 50 is provided, providing the motor 50 on the side on which the first blade portion 112a, whose inter-blade distance is great, is formed. Furthermore, since the impeller 10 is configured such that the ratio of the turbo blade portion is high in any region between the main plate 11 and the side plate 13, sufficient pressure recovery can be achieved by the blades. Therefore, the impeller 10 can further improve pressure recovery than an impeller or a multi-blade fan that does not include the configuration.
Furthermore, in the impeller 10 and the multi-blade fan 100, the first inter-blade distance of the second region is greater than the first inter-blade distance of the first region (first inter-blade distance a1<first inter-blade distance a2) and the second inter-blade distance of the second region is greater than the second inter-blade distance of the first region (second inter-blade distance b1<second inter-blade distance b2). That is, in the impeller 10 and the multi-blade fan 100, the inter-blade distance of the portions closer to the side plate 13 is greater than the inter-blade distance of the portions closer to the main plate 11. Therefore, the impeller 10 and the multi-blade fan 100 can further improve pressure recovery than an impeller or a multi-blade fan that does not include the configuration. As a result, the impeller 10 can improve the efficiency of the multi-blade fan 100. Furthermore, by virtue of the above configuration, the impeller 10 can reduce separation of air current at the leading edges of the portions closer to the side plate 13.
Furthermore, in the impeller 10 and the multi-blade fan 100, in the first and second regions of the impeller 10, the ratio of the turbo blade portion in the radial direction to the sirocco blade portion is higher than the ratio of the sirocco blade portion to the turbo blade portion in the radial direction. Since the impeller 10 and the multi-blade fan 100 are configured such that the ratio of the turbo blade portion is high in any region between the main plate 11 and the side plate 13, sufficient pressure recovery can be achieved by the blades 12. Therefore, the impeller 10 and the multi-blade fan 100 can further improve pressure recovery than an impeller or a multi-blade fan that does not include the a configuration. As a result, the impeller 10 can improve the efficiency of the multi-blade fan 100. Furthermore, by virtue of the above configuration, the impeller 10 can reduce I separation of an air current at the leading edges of the portions closer to the side plate 13.
Moreover, each of the blades 12 has a radial blade portion that connects the turbo blade portion and the sirocco blade portion and has a blade angle of 90 degrees. In the impeller 10, since the radial blade portion is provided between the turbo blade portion and the sirocco blade portion, the angle of a region between the sirocco blade portion and the turbo blade portion does not vary steeply. Therefore, the impeller 10 can reduce pressure fluctuations in the scroll casing 40, increase the fan efficiency of the multi-blade fan 100, and further reduce noise.
Furthermore, the blades 12 are configured such that at least one second blade 12B is provided between any adjacent two of the first blades 12A arranged in the circumferential direction. Also, in the impeller 10 and the multi-blade fan 100, in each of the second blades 12B, the ratio of the turbo blade portion is high in any region between the main plate 11 and the side plate 13, sufficient pressure recovery can be achieved by the second blades 12B. Therefore, the impeller 10 and the multi-blade fan 100 can further improve pressure recovery than an impeller or a multi-blade fan that does not include the configuration. As a result, the impeller 10 can improve the efficiency of the multi-blade fan 100. Furthermore, by virtue of the above configuration, the impeller 10 can reduce separation of an air current at the leading edge of the portions closer to the side plate 13.
Furthermore, the second blades 12B are formed such that the ratio of the inside diameter of the second blades 12B, which is the diameter of a circle drawn through the inner circumferential ends 14B of the second blades 12B, to the outside diameter of the second blades 12B, which is the diameter of a circle drawn through the outer circumferential ends 15B of the second blades 12B, is lower than or equal to 0.7. Also, in the impeller 10 and the multi-blade fan 100, since in each of the second blades 12B, the ratio of the turbo blade portion is high in any region between the main plate 11 and the side plate 13, sufficient pressure recovery can be achieved by the second blades 12B. Therefore, the impeller 10 and the multi-blade fan 100 can further improve pressure recovery than an impeller or a multi-blade fan that does not include the above configuration. As a result, the impeller 10 can improve the efficiency of the multi-blade fan 100. In addition, by virtue of the above configuration, the impeller 10 can reduce separation of an air current at the leading edges of the portions closer to the side plate 13.
Furthermore, the blades 12 are configured such that in part of the blades 12 that is located further outward than part of the bellmouth 46 that has the inside diameter BI, in the radial direction with respect to the rotation axis RS, the ratio of the turbo blade portion to the sirocco blade portion in the radial direction of the main plate 11 is higher than the ratio of the sirocco blade portion to the turbo blade portion in the radial direction of the main plate 11 throughout the blades 12. In the blades 12, the above configuration is provided in any region between the main plate 11 and the side plate 13. Accordingly, the blades 12 can increase the amount of air that is sucked at part of the blades 12 that is located inward of the part of the bellmouth 46 that has the inside diameter BI. Furthermore, by increasing the ratio of the turbo blade portion in the part of the blades 12 that is located further outward than the part of the bellmouth 46 that has inside diameter BI, the blades 12 can increase the volume of air that is drawn out from the impeller 10. In addition, by virtue of the above configuration, the blades 12 can increase the pressure recovery in the scroll casing 40 of the multi-blade fan 100 and improve the fan efficiency.
Furthermore, the inside diameter BI of the bellmouth 46 is larger than the blade inside diameter of the portions of the blades 12 that are closer to the main plate 11 and smaller than the blade inside diameter of the portions of the blades 12 that are closer to the side plate 13. Therefore, the multi-blade fan 100 can reduce interference between the flow of sucked air that flows into the scroll casing from the suction port 45 of the bellmouth 46 and the portions of the blades 12 that are closer to the side plate 13, and can further reduce noise.
Moreover, the inside diameter BI of the bellmouth 46 is larger than the blade inside diameter of the portions of the second blades 12B that are closer to the main plate 11 and smaller than the blade inside diameter of the portions of the second blades 12B that are closer to the side plate 13. Therefore, the multi-blade fan 100 can reduce interference between the flow of sucked gas that flows in the bellmouth 46 from the suction port 45 of the bellmouth 46 and the portions of the second blades 12B that are closer to the side plate 13, and can further reduce noise.
Furthermore, the distance MS, which is the shortest possible distance between the blades 12 and the peripheral wall 44c, is greater than twice the length of the sirocco blade portion in the radial direction. Therefore, the multi-blade fan 100 can achieve pressure recovery with the turbo blade portion, increase the distance between the scroll casing 40 and the impeller 10 in a region where the scroll casing 40 and the impeller 10 are closest to each other, and can therefore reduce noise.
Furthermore, the multi-blade fan 100 is formed such that the outside diameter MO1 of an end portion 50a of the motor 50 is larger than the blade inside diameter of the portions of the blades 12 that are closer to the main plate 11 and smaller than the blade inside diameter of the portions of the blades 12 that are closer to the side plate 13. By virtue of the above configuration, in the multi-blade fan 100, the flow direction of an air current from a region closer to the motor 50 is changed such that the air current flows in the axial direction of the rotation axis RS of the impeller 10 and the air smoothly flows into the scroll casing 40, whereby the volume of air that is drawn out from the impeller 10 can be increased. In addition, by virtue of the above configuration, the multi-blade fan 100 can increase the pressure recovery in the scroll casing 40 and improve the fan efficiency.
Furthermore, the multi-blade fan 100A is formed such that the outside diameter MO of the motor 50A is larger than the blade inside diameter of the portions of the blades 12 that are closer to the main plate 11 and smaller than the blade inside diameter of the portions of the blades 12 that are closer to the side plate 13. By virtue of the above configuration, the multi-blade fan 100A can change the flow direction of an air current from a region close to the motor 50A to the axial direction of the rotation axis RS of the impeller 10 to cause air to smoothly flow into the scroll casing 40, thereby increasing the volume of air that is drawn out from the impeller 10. In addition, by virtue of the above configuration, the multi-blade fan 100A can improve the pressure recovery in the scroll casing 40 and also improve the fan efficiency.
Furthermore, the multi-blade fan 100B is formed such that the outermost diameter MO2a of the motor 50B is larger than the blade inside diameter of the portions of the blades 12 that are closer to the main plate 11 and smaller than the blade inside diameter of the portions of the blades 12 that are closer to the side plate 13. In addition, the multi-blade fan 100B is formed such that the outside diameter MO1a of an end portion 50a of the motor 50B is smaller than the blade inside diameter of the portions of the blades 12 that are closer to the main plate 11. By virtue of the above configuration, the multi-blade fan 100B can better cause air to be smoothly flow into the scroll casing 40 and increase the volume of air that is emitted from the impeller 10 than the multi-blade fan 100A or other devices. Furthermore, by virtue of the above configuration, the multi-blade fan 100B can further improve the pressure recovery in the scroll casing 40 and also improve fan efficiency, as compared with the multi-blade fan 100A or other devices.
[Multi-Blade Fan 100C]
As described above, each of the blades 12 has an inclined portion 141A that is inclined such that the leading edge 14A1 is inclined such that in the direction from the main plate 11 toward the side plate 13, the distance between the leading edge 14A1 and the rotation axis RS gradually increases and the blade inside diameter increases. That is, in the blade 12, the inclined portion 141A is inclined such that in the direction from the main plate 11 toward the side plate 13, the inner circumferential end 14A is inclined such that the distance between the inner circumferential end 14A and the rotation axis RS gradually increases and the blade inside diameter increases. Similarly, each of the blades 12 has an inclined portion 141B that is inclined such that in the direction from the main plate 11 toward the side plate 13, the leading edge 14B1 is inclined such that the distance between the leading edge 14B1 and the rotation axis RS gradually increases and the blade inside diameter increases. That is, in the blade 12, the inclined portion 141B is inclined such that in the direction from the main plate 11 toward the side plate 13, the inner circumferential end 14B is inclined such that the distance between the inner circumferential end 24B and the rotation axis RS gradually increases and the blade inside diameter increases.
The inclined portion 141A is inclined relative to the rotation axis RS. Preferably, the angle of inclination of the inclined portion 141A should be greater than 0 degree and smaller than or equal to 60 degrees, and more preferably, should be greater than 0 degree and smaller than or equal to 45 degrees. That is, preferably, an angle θ1 of inclination between the inclined portion 141A and the rotation axis RS should satisfy the relationship “0 degree <θ1≤60 degrees”, and more preferably, the angle θ1 of inclination between the inclined portion 141A and the rotation axis RS should satisfy the relationship “0 degree <θ1≤45 degrees”. The imaginary line VL1 as indicated in
Similarly, the inclined portion 141B is inclined relative to the rotation axis RS. Preferably, the angle of inclination of the inclined portion 141B should be greater than 0 degree and smaller than or equal to 60 degrees, and more preferably, should be greater than 0 degree and smaller than or equal to 45 degrees. That is, preferably, the angle of inclination θ2 between the inclined portion 141B and the rotation axis RS should satisfy the relationship “0 degree <θ2≤60 degrees”, and more preferably, should satisfy the relationship “0 degree <θ2≤45 degrees”. The imaginary line VL2 as indicated in
The blade height WH as indicated in
[Advantages of Impeller 10C and Multi-Blade Fan 100C]
As illustrated in
By contrast, as illustrated in
The angle of inclination of the inclined portions 141A and 141B of the multi-blade fan 100C can be set as appropriate. By further increasing the angles of inclination of the inclined portions 141A and 141B, in the multi-blade fan 100C, it is possible to ensure a larger area of the leading edges of the blades 12 for the air current. However, it is necessary to increase the sizes of the impeller 10C and the multi-blade fan 100C in the radial direction to increase the angles of inclination while ensuring the predetermined blade height WH. To ensure a large area of the leading edges of the blades 12 while preventing upsizing of the impeller 10C and the multi-blade fan 100C, it is preferable that the angles of inclination of the inclined portions 141A and 141B be set smaller than or equal to 60 degrees. Furthermore, in order that the impeller 10C and the multi-blade fan 100C be made smaller, it is preferable that the angles of inclination of the inclined portions 141A and 141B be set smaller than or equal to 45 degrees.
[Multi-Blade Fan 100D]
As described above, each of the blades 12 has an inclined portion 141A that is inclined such that in the direction from the main plate 11 toward the side plate 13, the leading edge 14A1 is inclined such that the distance between the leading edge 14A1 and the rotation axis RS gradually increases and the blade inside diameter increases. Similarly, each of the blades 12 has an inclined portion 141B that is inclined such that in the direction from the main plate 11 toward the side plate 13, the leading edge 14B1 is inclined such that the distance between the leading edge 14B1 and the rotation axis RS gradually increases and the blade inside diameter increases. The blades 12 each have a gradient that is formed on the inner circumferential side by the inclined portion 141A and the inclined portion 141B.
The inclined portion 141A is inclined relative to the rotation axis RS. Preferably, the angle of inclination of the inclined portion 141A should be greater than 0 degree and smaller than or equal to 60 degrees, and more preferably, should greater than 0 degree and smaller than or equal to 45 degrees. That is, preferably, the angle of inclination θ1 of the inclined portion 141A to the rotation axis RS should be set to satisfy the relationship “0 degree <θ1≤60 degrees”, and more preferably should be set to satisfy the relationship “0 degree <θ1≤45 degrees”. Similarly, the inclined portion 141B is inclined relative to the rotation axis RS. Preferably, the angle of inclination of the inclined portion 141B should be greater than 0 degree and smaller than or equal to 60 degrees, and more preferably, should be greater than 0 degree and smaller than or equal to 45 degrees. That is, preferably, the angle θ2 of inclination of the inclined portion 141B to the rotation axis RS should be set to satisfy the relationship “0 degree <θ2≤60 degrees”, and more preferably should be set to satisfy the relationship “0 degree <θ2≤45 degrees”.
The blade height WH as indicated in
The blades 12 have linear portions 141C1 that are provided at the leading edges 14A1 between the main plate 11 and the side plate 13 and that are parallel to the rotation axis RS in
Similarly, the blades 12 have linear portions 141C2 that are provided at the leading edges 14B1 between the main plate 11 and the side plate 13 and that are parallel to the rotation axis RS as indicated in
[Advantages of Impeller 10D and Multi-Blade Fan 100D]
As illustrated in
[Multi-Blade Fan 100E]
As described above, each of the blades 12 has an inclined portion 141A that is inclined such that in the direction from the main plate 11 toward the side plate 13, the leading edge 14A1 is inclined such that the distance between the leading edge 14A1 and the rotation axis RS gradually increases and a blade inside diameter IDe increases. Furthermore, the blade 12 has an inclined portion 141A2 that is inclined such that in the direction from the main plate 11 toward the side plate 13, the leading edge 14A1 is inclined such that the distance between the leading edge 14A1 and the rotation axis RS gradually increases and the blade inside diameter IDe increases. The inclined portion 141A2 is provided between the main plate 11 and the side plate 13 and closer to the main plate 11 than the side plate 13. Therefore, the leading edge 14A1 of the first blade 12A has the inclined portion 141A2 provided closer to the main plate 11 and the inclined portion 141A provided closer to the side plate 13. That is, between the main plate 11 and the side plate 13, the first blade 12A of the blade 12 has two inclined portions, namely the inclined portion 141A and the inclined portion 141A2. The configuration of the first blade 12A of the blade 12 is not limited to a configuration in which the first blade 12A has two inclined portions, namely an inclined portion 141A and an inclined portion 141A2. That is, the first blade 12A has only to have two or more inclined portions.
Similarly, each of the blades 12 has an inclined portion 141B that is inclined such that in the direction from the main plate 11 toward the side plate 13, the leading edge 14B1 is inclined such that the distance between the leading edge 14B1 and the rotation axis RS gradually increases and the blade inside diameter IDe increases. Furthermore, the blade 12 has an inclined portion 141B2 that is inclined such that in the direction from the main plate 11 toward the side plate 13, the leading edge 14B1 is inclined such that the leading edge 14B1 and the rotation axis RS increases and the blade inside diameter IDe increases. The inclined portion 141B2 is provided between the main plate 11 and the side plate 13 and closer to the main plate 11 than the side plate 13. Therefore, the leading edge 14B1 of each second blade 12B has an inclined portion 141B2 provided closer to the main plate 11 and an inclined portion 141B provided closer to the side plate 13. That is, between the main plate 11 and the side plate 13, the second blade 12B of the blade 12 has two inclined portions, namely an inclined portion 141B and an inclined portion 141B2. The configuration of the second blade 12B of the blade 12 is not limited to a configuration in which the second blade 12B has two inclined portions, namely an inclined portion 141B and an inclined portion 141B2; that is, the second blade 12B has only to have two or more inclined portions. The blades 12 have gradients formed on the inner circumferential side by the inclined portion 141A, the inclined portion 141A2, the inclined portion 141B, and the inclined portion 141B2.
At least one of the inclined portion 141A and the inclined portion 141A2 is inclined relative to the rotation axis RS. Preferably, the angles of inclination of the inclined portion 141A and/or the inclined portion 141A2 should be greater than 0 degree and smaller than or equal to 60 degrees, and more preferably, should be greater than 0 degree and smaller than or equal to 45 degrees. That is, preferably, the angle θ1 of inclination between the inclined portion 141A and the rotation axis RS should be set to satisfy the relationship “0 degree <θ1≤60 degrees” or more preferably, should be set to satisfy the relationship “0 degree <θ1≤45 degrees”. Alternatively, preferably, the angle θ11 of inclination between the inclined portion 141A2 and the rotation axis RS should be set to satisfy the relationship “0 degree <θ11≤60 degrees”, and more preferably, should be set to satisfy the relationship “0 degree <θ11≤45 degrees”. It should be noted that the imaginary line VL3 as indicated in
The angle θ1 of inclination of the inclined portion 141A and the angle θ11 of inclination of the inclined portion 141A2 are different from each other. In the case where the first blade 12A has two or more inclined portions, the angles of inclination of the inclined portions are different from each other. The relationship between the angle 01 of inclination of the inclined portion 141A and the angle θ11 of inclination of the inclined portion 141A2 is not limited. For example, as illustrated in
Similarly, at least one of the inclined portion 141B and the inclined portion 141B2 is inclined relative to the rotation axis RS. Preferably, the angles of inclination of the inclined portion 141B and/or the inclined portion 141B2 should be greater than 0 degree and smaller than or equal to 60 degrees, and more preferably should be greater than 0 degree and smaller than or equal to 45 degrees. That is, preferably, the angle θ2 of inclination between the inclined portion 141B and the rotation axis RS should be set to satisfy the relationship “0 degree <θ2≤60 degrees”, and more preferably, should be set to satisfy the relationship “0 degree <θ2≤45 degrees”. Alternatively, preferably, the angle θ22 of inclination between the inclined portion 141B2 and the rotation axis RS should be set to satisfy the relationship “0 degree <θ22≤60 degrees”, and more preferably, should be set to satisfy the relationship “0 degree <θ22≤45 degrees”. The imaginary line VL4 as indicated in
The angle θ2 of inclination of the inclined portion 141B and the angle θ22 of inclination of the inclined portion 141B2 are different from each other. In the case where the second blade 12B has two or more inclined portions, the angles of inclination of the inclined portions are different from each other. The relationship between the angle θ2 of inclination of the inclined portion 141B and the angle θ22 of inclination of inclination θ22 of the inclined portion 141B2 is not limited. For example, as illustrated in
The blade height WH as indicated in
[Advantages of Impeller 10E and Multi-Blade Fan 100E]
As illustrated in
[Multi-Blade Fan 100F]
The impeller 10F of the multi-blade fan 100F according to Embodiment 3 have step portions 12D formed at end portions 12t of respective turbo blade portions, which is closer to the side plate 13. Each of the step portions 12D will be described referring to the first blade 12A as illustrated in
The second blade 12B has also a step portion 12D, although this illustration will be omitted since the configuration of the step portion 12D of the second blade 12B is similar to that of the step portion 12D of the first blade 12A. The step portion 12D is formed at an end portion 12t of the second turbo blade portion 12B2, which is closer to the side plate 13. That is, the step portion 12D is formed at the end portion 12t of the inclined portion 141B, which is closer to the side plate 13. The step portion 12D is formed by notching a wall that forms the second blade 12B. The step portion 12D is formed by notching a continuous portion between the leading edge 14B1 of the second blade 12B and the end portion 12t of the second turbo blade portion 12B2, which is closer to the side plate 13.
The blades 12 of the multi-blade fan 100F according to Embodiment 3 are formed such that a blade outside diameter of the blades 12 that is the diameter of a circle drawn through the outer circumferential ends of the blades 12 is larger than the inside diameter BI of the bellmouth 46. Moreover, as illustrated in
[Advantages of Impeller 10F and Multi-Blade Fan 100F]
The impeller 10F and the multi-blade fan 100F have the step portions 12D formed at the end portions 12t of the turbo blade portions that are closer to the side plate 13. In the impeller 10F and the multi-blade fan 100F, because of provision of the step portions 12D, it is possible to widen the gap between the bellmouth 46 and each of the blades 12. Therefore, in the impeller 10F and the multi-blade fan 100F, it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, whereby it is possible to reduce noise that is generated by the air current that passes through the gap between the bellmouth 46 and the blade 12.
Furthermore, in the impeller 10F and the multi-blade fan 100F, it is possible to provide the bellmouth 46 closer to the impeller 10F than in the case where the blade 12 has no step portion 12D. Moreover, in the impeller 10F and the multi-blade fan 100F, since the bellmouth 46 is provided close to the impeller 10F, it is possible to reduce the gap between the bellmouth 46 and the blade 12. As a result, the impeller 10F and the multi-blade fan 100F can reduce leakage of sucked air, that is, they can reduce the amount of air that does not pass through the space between adjacent blades 12 of the impeller 10F. Since the bellmouth 46 and the side edge portions 12D1 are provided to face each other as illustrated in
[Multi-Blade Fans 100J, 100K, and 100L]
In each of
As illustrated in
In the case where the impeller 10J includes second blades 12B, each of the end portions 12u of the impeller 10J that are closer to the side plate 13 has the first sirocco blade portion 12A1 and the second sirocco blade portion 12B1. Moreover, the second sirocco blade portion 12B1 is formed such that the ratio of the inside diameter of the second blades 12B to the outside diameter of the second blades 12B is higher than or equal to 0.7. That is, the multi-blade fan 100J is configured such that a region of each of the blades 12 that is closer to the side plate 13 is formed as a sirocco blade portion in which the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 is higher than or equal to 0.7. Since the multi-blade fan 100 has the first sirocco blade portion 12A1 and the second sirocco blade portion 12B1 that are formed such that the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 in the region beside the side plate 13 is higher than or equal to 0.7, it is possible to widen in the radial direction, part of each of the second blades 12B that is close to the air inlet 10e.
Similarly, as illustrated in
In the case where the impeller 10K includes second blades 12B, each of the end portions 12u of the impeller 10K that are closer to the side plate 13 has the first sirocco blade portion 12A1 and the second sirocco blade portion 12B1. Moreover, the second sirocco blade portion 12B1 is formed such that the ratio of the inside diameter of the second blades 12B to the outside diameter of the second blades 12B is higher than or equal to 0.7. That is, in the multi-blade fan 100K, the region of each of the blades 12 that is closer to the side plate 13 is formed as a sirocco blade portion in which the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 is higher than or equal to 0.7. Since the multi-blade fan 100K has the first sirocco blade portion 12A1 and the second sirocco blade portion 12B1 that that are formed such that the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 in the region beside the side plate 13 is higher than or equal to 0.7, it is possible to widen in the radial direction, part of each of the second blades 12B that is close to the air inlet 10e.
The impeller 10K of the multi-blade fan 100K has step portions 12D that are formed at the end portions 12u of the respective turbo blade portions that are closer to the side plate 13.
Similarly, as illustrated in
In the case where the impeller 10L includes second blades 12B, each of the end portions 12u of the impeller 10L that are closer to the side plate 13 has the first sirocco blade portion 12A1 and the second sirocco blade portion 12B1. Moreover, the second sirocco blade portion 12B1 is formed such that the ratio of the inside diameter of the second blades 12B to the outside diameter of the second blades 12B is higher than or equal to 0.7. That is, in the multi-blade fan 100L, the region of each of the blades 12, which is closer to the side plate 13, is formed as a sirocco blade portion in which the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 is higher than or equal to 0.7. Since the multi-blade fan 100L has the first sirocco blade portion 12A1 and the second sirocco blade portion 12B1 that are formed such that the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 in the region closer to the side plate 13 is higher than or equal to 0.7, it is possible to widen in the radio direction, part of each of the second blades 12B near the air inlet 10e.
In the impeller 10L of the multi-blade fan 100L, between the end portion 12u and the inclined portion 141A, a linear portion 143 is formed. The linear portion 143 extends in a direction along the axial direction of the rotation axis RS, as compared with the inclined portion 141A. That is, the linear portion 143 is inclined at a smaller angle than the inclined portion 141A in the axial direction of the rotation axis RS. The linear portion 143 may be formed to extend in a direction parallel to the axial direction of the rotation axis RS. It should be noted that the direction in which the linear portion 143 extends may not be parallel to the axial direction of the rotation axis RS. In the impeller 10L of the multi-blade fan 100L, the linear portion 143, which extends in the axial direction of the rotation axis RS, and the inclined portion 141A, which is inclined with respect to the axial direction of the rotation axis RS, form a step portion 12D.
[Advantages of Impeller 10J, Multi-Blade Fan 100J, and Other Devices]
Each of the blades 12 has a sirocco blade portion formed such that at an end portion closer to the side plate 13 in the axial direction of the rotation axis RS, the ratio of the blade inside diameter of the blades 12 that is the diameter of a circle drawn through the inner circumferential ends of the blades 12 to the blade outside diameter of the blades that is the diameter of a circle drawn through the outer circumferential ends of the blades 12 is higher than or equal to 0.7. Since the impeller 10J, the multi-blade fan 100J, etc., each have sirocco blade portions in which the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 at the end portions 12u closer to the side plate 13 is higher than or equal to 0.7, it is possible to widen the gap between the bellmouth 46 and each of the blades 12. Therefore, in the impeller 10J, the multi-blade fan 100J, etc., it is possible reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, thus reducing noise that is generated by an air current that passes through the gap between the bellmouth 46 and the blade 12. Furthermore, by virtue of the above configuration, in the case where the motor 50 and the blade 12 are close to each other, in the impeller 10J, the multi-blade fan 100J, etc., it is possible to reduce a resistance during suction and reduce generated noise.
Furthermore, in the impeller 10K, the multi-blade fan 100K, etc., step portions 12D are formed at end portions 12u of a turbo blade portion that are closer to the side plate 13. Because of provision of the step portions 12D, in the impeller 10K, the multi-blade fan 100K, etc., it is possible to widen the gap between the bellmouth 46 and each of the blades 12. Therefore, in the impeller 10K, the multi-blade fan 100K, etc., it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, and thus reduce noise that is generated by the air current passing through the gap between the bellmouth 46 and the blade 12.
In addition, in the impeller 10L of the multi-blade fan 100L, h the linear portion 143 and the inclined portion 141A form the step portion 12D. Since each of the first blades 12A has the inclined portion 141A and the linear portion 143, in the impeller 10L and the multi-blade fan 100L, it is possible to reduce the areas of the first blades 12A and reduce a resistance against sucked air.
[Modifications of Multi-Blade Fans 100J, 100K, and 100L, Etc.]
The modifications of the multi-blade fan 100J, etc. each include a plurality of blades 12. Moreover, the blades 12 have respective turbo blade portions and sirocco blade portion that are formed such that at the end portions 12u closer to the side plate 13, the ratio of the blade inside diameter of the blades 12 that is the diameter of a circle drawn through the inner circumferential ends of the blades 12 to the blade outside diameter of the blades that is the diameter of a circle drawn through the outer circumferential ends of the blades 12 is higher than or equal to 0.7.
The first turbo blade portion 12A2 of the modification of the multi-blade fan 100J, etc. is formed outward of the inner circumferential end portion 46b of the bellmouth 46 in the radial direction with respect to the rotation axis RS as viewed in the direction parallel to the axial direction of the rotation axis RS. The multi-blade fans 100J, 100K, and 100L are each configured such that each of the end portions 12u close to the side plate 13 in the axial direction of the rotation axis RS has the first sirocco blade portion 12A1 and the first turbo blade portion 12A2. The modification of the multi-blade fan 100J or other devices is configured such that at the end portions 12u closer to the side plate 13 in the axial direction of the rotation axis RS, the diameter of a circle drawn through the first turbo blade portions 12A2 corresponds to the inside diameter of the modification of the impeller 10J, etc.
As viewed in the direction parallel to the axial direction of the rotation axis RS, at each of the end portions 12u of each of the impellers 10J, 10K, and 10L, an outer circumferential end portion 12A22 of the first turbo blade portion 12A2 is provided outward of the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. Moreover, as viewed in the direction parallel to the axial direction of the rotation axis RS, the boundary between the first sirocco blade portion 12A1 and the first turbo blade portion 12A2 as indicated by the dotted line BD is provided outward of the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. That is, each of the multi-blade fans 100J, 100K, and 100L is formed such that an outside diameter of the first turbo blade portions 12A2 that is the diameter of a circle drawn through the outer circumferential end portions 12A22 of the first turbo blade portions 12A2 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
In the case where the modification of the multi-blade fan 100J or other devices includes second blades 12B, each of the second turbo blade portions 12B2 of the modification of the multi-blade fan 100J or other devices is provided outward of the inner circumferential end portion 46b of the bellmouth 46 in the radial direction with respect to the rotation axis RS as viewed in the direction parallel to the axial direction of the rotation axis RS (not illustrated). In this case, the modification of the multi-blade fan 100J or other devices is configured such that the end portions 12u closer to the side plate 13 in the axial direction of the rotation axis RS are formed by the first sirocco blade portions 12A1 and the first turbo blade portions 12A2 as well as the second sirocco blade portions 12B1 and the second turbo blade portions 12B2. In the case where the modification of the multi-blade fan 100J or other devices includes second blades 12B, the modification of the multi-blade fan 100J or other devices is configured such that at the end portions 12u closer to the side plate 13 in the axial direction of the rotation axis RS, the diameter of a circle drawn through the first turbo blade portions 12A2 and the second turbo blade portions 12B2 is the inside diameter of the modification of the impeller 10J or other impellers.
As viewed in the direction parallel to the axial direction of the rotation axis RS, at each of the end portions 12u of each of the impellers 10J, 10K, and 10L, an outer circumferential end portion 12A22 of the second turbo blade portion 12B2 is provided closer to the outer circumferential side than the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. Moreover, as viewed in the direction parallel to the axial direction of the rotation axis RS, the boundary between the second sirocco blade portion 12B1 and the second turbo blade portion 12B2 as indicated by the dotted line BD is provided closer to the outer circumferential side than the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. That is, each of the multi-blade fans 100J, 100K, and 100L is formed such that an outside diameter of the second turbo blade portions 12B2 that is the diameter of a circle drawn through the outer circumferential end portions 12A22 of the second turbo blade portions 12B2 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
[Advantages of Modifications of Impeller 10J, Multi-Blade Fan 100J, Etc.]
In the multi-blade fans 100J, 100K, and 100L, an outside diameter of turbo blade portions that is the diameter of a circle drawn through outer circumferential end portions of the turbo blade portions is larger than the inside diameter BI of the bellmouth 46 as illustrated in
In addition, in the modifications of the impeller 10J, the multi-blade fan 100J, etc., it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and each of the blades 12, and thus reduce noise that is generated by the air current that passes through the gap between the bellmouth 46 and the blade 12. In addition, in the impeller 10J and the multi-blade fan 100J, it is possible to reduce the resistance during suction and also reduce the generation of noise in the case where the motor 50 and the blade 12 are close to each other.
Furthermore, the blades 12 have turbo blade portions and sirocco blade portions that are formed such that at the end portions closer to the side plate 13, the ratio of a blade inside diameter of the blades 12 that is the diameter of a circle drawn through the inner circumferential ends of the blades 12 to a blade outside diameter of the blades 12 that is the diameter of a circle drawn through the outer circumferential ends of the blades 12 is higher than or equal to 0.7. By virtue of the sirocco blade portions and the turbo blade portions formed such that the ratio of the above inside diameter of the blades 12 to the above outside diameter of the blades 12 at the end portion 12u beside the side plate 13 is higher than or equal to 0.7, the modifications of the impeller 10J, the multi-blade fan 100J, etc. can widen the gap between the bellmouth 46 and each of the blades 12. Therefore, in the modifications of the impeller 10J, the multi-blade fan 100J, etc., it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, and thus reduce noise that is generated by the air current that passes through the gap between the bellmouth 46 and the blade 12. Furthermore, by virtue of the above configuration, in the modifications of the impeller 10J, the multi-blade fan 100J, etc., it is possible to reduce the resistance during suction and reduce the generation of noise in the case where the motor 50 and the blade 12 are close to each other.
[Multi-Blade Fans 100M, 100N, and 100P]
The multi-blade fans 100M, 100N, and 100P according to Embodiment 5 will be described with reference to
Each of end portions 12u of each of the impeller 10M, 10N, and 10P that are closer to the side plate 13 has the first sirocco blade portion 12A1. The first sirocco blade portion 12A1 is formed such that the ratio of the above inside diameter of the first blades 12A to the outside diameter of the first blades 12A is higher than or equal to 0.7. That is, the multi-blade fan 100M, etc., are each configured such that portions of the blades 12 that are closer to the side plate 13 are formed as sirocco blade portions in which the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 is higher than or equal to 0.7. By virtue of the first sirocco blade portions 12A1 formed such that the ratio of the inside diameter of the first blades 12A to the outside diameter of the first blades 12A in the regions closer to the side plate 13 is higher than or equal to 0.7, it is possible for the multi-blade fan 100M, etc., to widen in the radial direction, part of each of the first blades 12A that is close to the air inlet 10e.
In the case where the impellers 10M, 10N, and 10P include second blades 12B, end portions 12u of each of the impellers 10M, 10N, and 10P that are closer to the side plate 13 has the first sirocco blade portion 12A1 and the second sirocco blade portion 12B1. Moreover, the second sirocco blade portion 12B1 is formed such that the ratio of the inside diameter of the second blades 12B to the outside diameter of the second blades 12B is higher than or equal to 0.7. That is, the multi-blade fan 100M, etc., are each configured such that a region of each of the blades 12 that is closer to the side plate 13 is formed as a sirocco blade portion in which the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 is higher than or equal to 0.7. By virtue of the first sirocco blade portion 12A1 and the second sirocco blade portion 12B1 that are formed such that the ratio of the inside diameter of the blades 12 to the outside diameter of the blades 12 in the regions closer to the side plate 13 is higher than or equal to 0.7, it is possible for the multi-blade fan 100M, etc., to widen in the radial direction, part of each of the second blades 12B that is close to the air inlet 10e.
At the end portions 12u of each of the impellers 10M, 10N, and 10P that are closer to the side plate 13, the first sirocco blade portions 12A1 are formed such that the inside diameter of the blades 12 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
Moreover, as viewed in the direction parallel to the axial direction of the rotation axis RS, the boundary between the first sirocco blade portion 12A1 and the first turbo blade portion 12A2 as indicated by the dotted line BD is provided closer to the outer circumferential side than the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. That is, each of the multi-blade fans 100M, 100N, and 100P is formed such that an outside diameter of the first turbo blade portions 12A2 that is the diameter of a circle drawn through the outer circumferential end portions 12A22 of the first turbo blade portions 12A2 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
In the case where the impellers 10M, 10N, and 10P include second blades 12B, the second sirocco blade portions 12B1 at the end portions 12u of each of the impellers 10M, 10N, and 10P that are closer to the side plate 13 are formed such that the above inside diameter of the blades 12 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
As viewed in the direction parallel to the axial direction of the rotation axis RS, the boundary between the second sirocco blade portion 12B1 and the second turbo blade portion 12B2 as indicated by the dotted line BD is provided closer to the outer circumferential side than the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. That is, in each of the multi-blade fans 100M, 100N and 100P, an outside diameter of the second turbo blade portions 12B2 that is the diameter of a circle drawn through the outer circumferential end portions 12A22 of the second turbo blade portions 12B2 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
[Advantages of Impeller 10M, Multi-Blade Fan 100M, Etc.]
Each of the multi-blade fans 100M, 100N and 100P is formed such that at the end portions 12u closer to the side plate 13, the inside diameters of the blades 12 at the sirocco blade portions is larger than the inside diameter BI of the bellmouth 46. Thus, in the multi-blade fans 100M, etc., it is possible to widen the gap between the bellmouth 46 and each of the blades 12. As a result, in the impeller 10M, the multi-blade fan 100M, etc., it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, and thus reduce noise that is generated by the air current passing through the gap between the bellmouth 46 and the blade 12. Furthermore, in the impeller 10M, the multi-blade fan 100M, etc., it is possible to reduce the resistance during suction and reduce the generation of noise in the case where the motor 50 and the blade 12 are close to each other.
Furthermore, in the impeller 10N, the multi-blade fan 100N, etc., step portions 12D are formed at end portions 12u of the turbo blade portions that are closer to the side plate 13. Because of provision of the step portions 12D, in the impeller 10N, the multi-blade fan 100N, etc., it is possible to widen the gap between the bellmouth 46 and a blade 12. Therefore, in the impeller 10N, the multi-blade fan 100N, etc., it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, and thus reduce noise that is generated by the air current that passes through the gap between the bellmouth 46 and the blade 12.
In the impeller 10P of the multi-blade fan 100P, step portions 12D are each formed by a linear portion 143 and an inclined portion 141A. In the impeller 10P and the multi-blade fan 100P, since each of the first blades 12A has an inclined portion 141A and a linear portion 143, it is possible to reduce the areas of the first blades 12A and reduce the resistance against sucked air.
[Modifications of Multi-Blade Fans 100M, 100N, and 100P, Etc.]
The modification of the multi-blade fan 100M, etc., includes a plurality of blades 12. The blades 12 have turbo blade portions and sirocco blade portions formed such that at end portions close to the side plate 13, the ratio of a blade inside diameter of the blades 12 that is the diameter of a circle drawn through the inner circumferential ends of the blades 12 to a blade outside diameter of the blades 12 that is the diameter of a circle drawn through the outer circumferential ends of the blades 12 is higher than or equal to 0.7.
The first turbo blade portions 12A2 of each of the multi-blade fans 100M, 100N, and 100P are provided outward of the inner circumferential end portion 46b of the bellmouth 46 in the radial direction with respect to the rotation axis RS as viewed in the direction parallel to the axial direction of the rotation axis RS. In the multi-blade fans 100M, 100N, and 100P, each of end portions 12u close to the side plate 13 in the axial direction of the rotation axis RS is formed by a first sirocco blade portion 12A1 and a first turbo blade portion 12A2. In each of the multi-blade fan 100M, 100N, and 100P, at the end portions 12u closer to the side plate 13 in the axial direction of the rotation axis RS, the diameter of a circle drawn through the first turbo blade portions 12A2 is the inside diameter of an associated one of the impellers 10M, 10N, and 10P.
As viewed in the direction parallel to the axial direction of the rotation axis RS, at each of the end portions 12u of each of the impellers 10M, 10N, and 10P, an outer circumferential end portion 12A22 of the first turbo blade portion 12A2 is provided closer to the outer circumferential side than the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. Moreover, as viewed in the direction parallel to the axial direction of the rotation axis RS, the boundary between the first sirocco blade portion 12A1 and the first turbo blade portion 12A2 as indicated by the dotted line BD is located closer to the outer circumferential side than the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. That is, in the multi-blade fans 100M, 100N, and 100P, an outside diameter of the first turbo blade portions 12A2 that is the diameter of a circle drawn through the outer circumferential end portions 12A22 of the first turbo blade portions 12A2 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
In the case where the multi-blade fan 100M, etc., include second blades 12B, the second turbo blade portions 12B2 are each located outward of the inner circumferential end portion 46b of the bellmouth 46 in the radial direction as viewed in the direction parallel to the axial direction of the rotation axis RS. In the multi-blade fan 100M, etc., each of end portions 12u closer to the side plate 13 in the axial direction of the rotation axis RS is formed by a first sirocco blade portion 12A1 and a first turbo blade portion 12A2 as well as a second sirocco blade portion 12B1 and a second turbo blade portion 12B2. In the case where the multi-blade fan s100M, etc., include second blades 12B, in the multi-blade fan 100M, etc., at the end portions 12u closer to the side plate 13 in the axial direction of the rotation axis RS, the diameter at the first turbo blade portions 12A2 and the second turbo blade portions 12B2 is the inside diameter of an associated one of the impellers 10M, 10N, and 10P.
As viewed in the direction parallel to the axial direction of the rotation axis RS, at each of the end portions 12u of each of the impellers 10M, 10N, and 10P, an outer circumferential end portion 12A22 of the second turbo blade portion 12B2 is located closer to the outer circumferential side than the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. Moreover, as viewed in the direction parallel to the axial direction of the rotation axis RS, the boundary between the second sirocco blade portion 12B1 and the second turbo blade portion 12B2 as indicated by the dotted line BD is located closer to the outer circumferential side than the inner circumferential end portion 46b of the bellmouth 46 in the radial direction. That is, in each of the multi-blade fans 100M, 100N, and 100P, an outside diameter of the second turbo blade portions 1B2 that is the diameter of a circle drawn through the outer circumferential end portions 12A22 of the second turbo blade portions 12B2 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
The first turbo blade portion 12A2 at each of the end portions 12u of each of the impellers 10M, 10N, and 10P that are closer to the side plate 13 is formed such that the inside diameter of the blades 12 is larger than the inside diameter BI of the bellmouth 46 illustrated in
In each of the impellers 10M, 10N, and 10P, in the case where second blades 12B are provided, the second turbo blade portions 12B2 at the end portions 12u closer to the side plate 13 are formed such that the inside diameter of the blades 12 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
[Advantages of Modifications of Impeller 10M, Multi-Blade Fan 100M, Etc.]
Each of the multi-blade fan 100M, 100N, and 100P is formed such that an outside diameter of the first turbo blade portions 12A2 that is the diameter of a circle drawn through the outer circumferential end portions 12A22 of the first turbo blade portions 12A2 is larger than the inside diameter BI of the bellmouth 46 as illustrated in
Furthermore, in the modifications of the impeller 10M, the multi-blade fan 100M, etc., it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, and thus reduce noise that is generated by the air current passing through the gap between the bellmouth 46 and the blade 12. Also, in the impeller 10M and the multi-blade fan 100M, it is possible to reduce the resistance during suction and also reduce the generation of noise in the case where the motor 50 and the blade 12 are close to each other.
Furthermore, in each of the multi-blade fans 100M, 100N and 100P of the modifications, at the end portions 12u closer to the side plate 13, the inside diameter of the blades 12 at the turbo blade portions is larger than the inside diameter BI of the bellmouth 46. Thus, in the multi-blade fans 100M, etc., It is possible to widen the gap between the bellmouth 46 and each of the blades 12. As a result, in the modifications of the impeller 10M, the multi-blade fan 100M, etc., it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, and thus reduce noise that is generated by the air current passing through the gap between the bellmouth 46 and the blade 12. In addition, in the impeller 10M, the multi-blade fan 100M, etc., it is possible to reduce the resistance during suction and reduce the generation of noise in the case where the motor 50 and the blade 12 are close to each other.
Moreover, the blades 12 have turbo blade portions and sirocco blade portions formed such that at end portions closer to the side plate 13, the ratio of a blade inside diameter of the blades 12 that is the diameter of a circle drawn through the inner circumferential ends of the blades 12 to a blade outside diameter of the blades 12 that is the diameter of a circle drawn through the outer circumferential ends of the blades 12 is higher than or equal to 0.7. By virtue of the sirocco blade portions and the turbo blade portions formed such that at the end portions 12u closer to the side plate 13, the ratio of the above inside diameter of the blades 12 to the above outside diameter of the blades 12 is higher than or equal to 0.7, in the modifications of the impeller 10M, the multi-blade fan 100M, etc., it is possible to widen the gap between the bellmouth 46 and each of the blades 12. Furthermore, in the modifications of the impeller 10M, the multi-blade fan 100M, etc., it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, and thus reduce noise that is generated by the air current passing through the gap between the bellmouth 46 and the blade 12. Furthermore, by virtue of the above configuration, in the modifications of the impeller 10M, the multi-blade fan 100M, etc., it is possible to reduce the resistance during suction and reduce the generation of noise in the case where the motor 50 and the blade 12 are close to each other.
Furthermore, in the modifications of the impeller 10N, the multi-blade fan 100N, etc., step portions 12D are formed at end portions 12u of turbo blade portion beside the side plate 13. Because of formation of the step portions 12D, in the impeller 10N, the multi-blade fan 100N, etc., it is possible to widen the gap between the bellmouth 46 and each of the blades 12. Therefore, in the impeller 10N, the multi-blade fan 100N, etc., it is possible to reduce an increase in velocity of an air current in the gap between the bellmouth 46 and the blade 12, and thus reduce noise that is generated by the air current passing through the gap between the bellmouth 46 and the blade 12.
[Multi-Blade Fan 100G]
As illustrated in
Each of the first blades 12A satisfies the relationship “blade length L1a>blade length Lib”. To be more specific, in each of the first blades 12A, the blade length decreases from the main plate 11 toward the side plate 13 in the axial direction of the rotation axis RS. In addition, as illustrated in
Each of the first blades 12A has a first sirocco blade portion 12A1 that is formed as a forward-swept blade portion and a first turbo blade portion 12A2 that is formed as a swept-back blade portion. Each of the first blades 12A is configured such that the first turbo region 12A21 is larger than the first sirocco region 12A11 in the radial direction of the impeller 10. The impeller 10 and each of the first blades 12A are configured such that in both the main-plate-side blade region 122a serving as the first region and the side-plate-side blade region 122b serving as the second region, in the radial direction of the impeller 10, the ratio of the first turbo blade portion 12A2 to the first sirocco blade portion 12A1 is higher than the ratio of the first sirocco blade portion 12A1 to the first turbo blade portion 12A2.
Where an inter-blade distance is the distance between any adjacent two of the blades 12 in the circumferential direction, the inter-blade distance increases from the leading edges 14A1 toward the trailing edges 15A1 as illustrated in
As illustrated in
[Advantages of Impeller 10G and Multi-Blade Fan 100G]
The impeller 10G and the multi-blade fan 100G can obtain advantages similar to those of the multi-blade fan 100 and the impeller 10 according to Embodiment 1. For example, the impeller 10G and the multi-blade fan 100G are configured such that in any region between the main plate 11 and the side plate 13, in the radial direction of the main plate 11, the ratio of the first turbo blade portion 12A2 to the first sirocco blade portion 12A1 is higher than the ratio of the first sirocco blade portion 12A1 to the first turbo blade portion 12A2. In the impeller 10G and the multi-blade fan 100G, since the ratio of the turbo blade portion is high in any region between the main plate 11 and the side plate 13, sufficient pressure recovery can be achieved by the blades 12. Therefore, the impeller 10G and the multi-blade fan 100G can further improve the pressure recovery than an impeller or a multi-blade fan that does not have the above configuration. As a result, the impeller 10G can improve the efficiency of the multi-blade fan 100G. Furthermore, by virtue of the above configuration, the impeller 10G can reduce separation of an air current at the leading edge in a region closer to the side plate 13.
Embodiments 1 to 6 are described above by referring to by way of example a multi-blade fan 100 including a double-suction impeller 10 provided with a plurality of blades 12 formed on both sides of a main plate 11. However, Embodiments 1 to 6 are also applicable to a multi-blade fan 100 including a single-suction impeller 10 having a plurality of blades 12 formed only on one side of a main plate 11.
[Air-Conditioning Apparatus 140]
The air-conditioning apparatus 140 according to Embodiment 7 includes any one or more of the multi-blade fans 100, etc., according to Embodiments 1 to 6 and a heat exchanger 15 provided to face a discharge port 42a of the multi-blade fan 100. Furthermore, the air-conditioning apparatus 140 according to Embodiment 7 includes a case 16 installed above a ceiling of a room to be air-conditioned. In the following description, the term “multi-blade fan 100” means any one of the multi-blade fans 100, etc., according to Embodiments 1 to 6. Furthermore, although
(Case 16)
As illustrated in
In the case 16, the multi-blade fan 100 and the heat exchanger 15 are housed. The multi-blade fan 100 includes an impeller 10, a scroll casing 40 having a bellmouth 46 formed therein, and a motor 50. The motor 50 is supported by a motor support 9a fixed to the upper surface portion 16a of the case 16. The motor 50 has a motor shaft 51. The motor shaft 51 is provided to extend parallel to the side surface portion 16c having the case air inlet 18 and the side surface portion 16c having the case discharge port 17. As illustrated in
As illustrated in
The heat exchanger 15 is provided in such a manner as to face the discharge port 42a of the multi-blade fan 100, and is provided in the case 16 and on an air passage for air to be discharged by the multi-blade fan 100. The heat exchanger 15 adjusts the temperature of air that is sucked into the case 16 through the case air inlet 18 and blown into the air-conditioned space through the case discharge port 17. As the heat exchanger 15, a heat exchanger having a well-known configuration can be applied. Regarding the location of the case air inlet 18, it suffices that the case air inlet 18 is provided at a location perpendicular to the axial direction of the rotation axis RS of the multi-blade fan 100. For example, the case air inlet 18 may be formed in the lower surface portion 16b.
When the impeller 10 of the multi-blade fan 100 is rotated, air in the air-conditioned space is sucked into the case 16 through the case air inlet 18. The air sucked into the case 16 is guided toward the bellmouth 46 and sucked into the impeller 10. The air sucked into the impeller 10 is blown outward in the radial direction of the impeller 10. After passing through the inside of the scroll casing 40, the air blown from the impeller 10b is blown from the scroll casing 40 through the discharge port 42a, and then supplied to the heat exchanger 15. When passing through the heat exchanger 15, the air supplied to the heat exchanger 15 exchanges heat with refrigerant that flows in the heat exchanger 15, and is thus controlled in temperature and humidity. The air that has passed through the heat exchanger 15 is blown to the air-conditioned space through the case discharge port 17.
The air-conditioning apparatus 140 according to Embodiment 7 includes any one of the multi-blade fans 100, etc., according to Embodiments 1 to 6. Therefore, the air-conditioning apparatus 140 can obtain advantages similar to those of any of Embodiments 1 to 6.
Each of Embodiment 1 to 7 can be put to practical use in combination with any of the others. Furthermore, the configurations described above regarding the embodiments are examples and may be each combined with another well-known technique, and part of the configurations can be omitted or changed without departing from the gist of the present disclosure. For example, regarding embodiments, the impeller 10, etc., that includes the main-plate-side blade region 122a serving as the first region and the side-plate-side blade region 122b serving as the second region is described above. The impeller 10 is not limited to the impeller including the first region and the second region solely. The impeller 10 may further have another region as well as the first region and the second region. For example, regarding in Embodiment 1, although each of the blades are shaped such that the blade length continuously changes from the main plate 11 toward the side plate 13, each of the blades may have, in some part between the main plate 11 and the side plate 13, a portion in which the blade length is constant, that is, a portion in which the inside diameter ID is constant and which is not inclined with respect to the rotation axis RS.
9
a: motor support, 10: impeller, 10A: impeller, 10C: impeller, 10D: impeller, 10E: impeller, 10F: impeller, 10G: impeller, 10H: impeller, 10J: impeller, 10K: impeller, 10L: impeller, 10M: impeller, 10N: impeller, 10P: impeller, 10e: air inlet, 11: main plate, 11b: shaft portion, 12: blade, 12A: first blade, 12A1: first sirocco blade portion, 12A11: first sirocco region, 12A2: first turbo blade portion, 12A21: first turbo region, 12A21a: first turbo region, 12A22: outer circumferential end portion, 12A2a: first turbo blade portion, 12A3: first radial blade portion, 12B: second blade, 12B1: second sirocco blade portion, 12B11: second sirocco region, 12B2: second turbo blade portion, 12B21: second turbo region, 12B21a: second turbo region, 12B2a: second turbo blade portion, 12B3: second radial blade portion, 12D: step portion, 12D1: side edge portion, 12D2: upper edge portion, 12R: outer circumferential region, 12t: end portion, 12u: end portion, 13: side plate, 13a: first side plate, 13b: second side plate, 14A: inner circumferential end, 14A1: leading edge, 14B: inner circumferential end, 14B1: leading edge, 14H: leading edge, 15: heat exchanger, 15A: outer circumferential end, 15A1: trailing edge, 15B: outer circumferential end, 15B1: trailing edge, 16: case, 16a: upper surface portion, 16b: lower surface portion, 16c: side surface portion, 17: case discharge port, 18: case air inlet, 19: partition plate, 40: scroll casing, 41: scroll portion, 41a: scroll start portion, 41b: scroll end portion, 42: discharge portion, 42a: discharge port, 42b: extension plate, 42c: diffuser plate, 42d: first side plate portion, 42e: second side plate portion, 43: tongue portion, 44a: side wall, 44a1: first side wall, 44a2: second side wall, 44c: peripheral wall, 45: suction port, 45a: first suction port 45b: second air inlet, 46: bellmouth, 46a: opening, 46b: inner circumferential end portion, 50: motor, 50A: motor, 50B: motor, 50a: end portion, 51: motor shaft, 52: outer peripheral wall, 52a: outer peripheral wall, 52b: outer peripheral wall, 71: first plane, 72: second plane, 100: multi-blade fan, 100A: multi-blade fan, 100B: multi-blade fan, 100C: multi-blade fan, 100D: multi-blade fan, 100E: multi-blade fan, 100F: multi-blade fan, 100G: multi-blade fan, 100H: multi-blade fan, 100J: multi-blade fan, 100K: multi-blade fan, 100L: multi-blade fan, 100M: multi-blade fan, 100N: multi-blade fan, 100P: multi-blade fan, 112a: first blade portion, 112b: second blade portion, 122a: main-plate-side blade region, 122b: side-plate-side blade region, 140: air-conditioning apparatus, 141A: inclined portion, 141A2: inclined portion, 141B: inclined portion, 141B2: inclined portion, 141C1: linear portion, 141C2: linear portion, 142: blade inclined region, 143: linear portion
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/JP2019/050392 | 12/23/2019 | WO |
| Publishing Document | Publishing Date | Country | Kind |
|---|---|---|---|
| WO2021/130821 | 7/1/2021 | WO | A |
| Number | Name | Date | Kind |
|---|---|---|---|
| 20170234323 | Pirouzpanah et al. | Aug 2017 | A1 |
| 20210033104 | Teramoto et al. | Feb 2021 | A1 |
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| 2019082378 | May 2019 | WO |
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| Entry |
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| Machine Translation of JP2011226410A PDF File Name: “JP2011226410A_Machine_Translation.pdf”. |
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| Number | Date | Country | |
|---|---|---|---|
| 20220372990 A1 | Nov 2022 | US |
