WO2023032762A1 - Centrifugal fan - Google Patents
Centrifugal fan Download PDFInfo
- Publication number
- WO2023032762A1 WO2023032762A1 PCT/JP2022/031753 JP2022031753W WO2023032762A1 WO 2023032762 A1 WO2023032762 A1 WO 2023032762A1 JP 2022031753 W JP2022031753 W JP 2022031753W WO 2023032762 A1 WO2023032762 A1 WO 2023032762A1
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- WIPO (PCT)
- Prior art keywords
- fan
- side plate
- blade
- radial direction
- trailing edge
- Prior art date
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- 230000000694 effects Effects 0.000 description 18
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Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/30—Vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
Definitions
- the present disclosure relates to a centrifugal fan that causes air to flow by rotating.
- the centrifugal fan described in Patent Document 1 includes a plurality of three-dimensional blades (that is, blades), a main plate, and side plates. One spanwise end face of each blade is fixed to the main plate, and the other spanwise end face of each blade is fixed to the side plate. In addition, in the three-dimensional blade, the main stream of the intake air flow does not follow the side plate and is blown off to the main plate side, and the intake air flow has a biased velocity distribution and noise is generated. Document 1 shows this as a problem.
- each blade is formed so that the diameter of the trailing edge portion of the blade is larger on the main plate side than on the side plate side. Patent Document 1 describes that this improves the distribution of the mainstream velocity between the blades and reduces the noise.
- the ratio of fan inner and outer diameters is the ratio obtained by dividing the suction diameter, which is the inner diameter of the side plate (i.e., the diameter of the intake hole of the centrifugal fan), by the outlet diameter (i.e., the outer diameter of the side plate). are assumed to vary.
- Patent Document 1 does not mention the fan inner/outer diameter ratio.
- the air flow in the inter-blade passage separates from the back surface of the side plate (i.e., the blade-side surface of the side plate) near the intake holes and is once biased toward the main plate. Flow to reattach. Therefore, at the outlet of the inter-blade passage, the air flow is biased toward the side plate, and the air flow velocity distribution is biased to one side in the axial direction of the fan. Then, noise is generated due to the biased airflow velocity distribution near the exit of the inter-blade passage. The inventors have newly discovered this fact.
- an object of the present disclosure is to provide a centrifugal fan capable of suppressing noise caused by uneven velocity distribution of airflow near the outlet of the inter-blade passage.
- a centrifugal fan that rotates around the fan axis to suck air from one side in the axial direction of the fan axis and blow the sucked air outward in the radial direction of the fan axis, a plurality of blades arranged side by side around the fan axis and having blade trailing edges radially outward; a side plate provided on one side in the axial direction with respect to the plurality of blades and connected to each of the plurality of blades; A main plate connected to each of the plurality of blades on the side opposite to the side plate side and extending in the radial direction, When the inner diameter of the side plate is Dsi and the outer diameter of the side plate is Dso, Dsi/Dso is 0.5 ⁇ Dsi/Dso ⁇ 0.7, The trailing edge portion of the blade is formed so as to be located radially inward toward one side in the axial direction.
- the air flows along one side in the axial direction so as to once separate from the side plates and then reattach to the side plates. biased.
- the centrifugal fan described above since the trailing edge of the blades is positioned radially inward toward one side in the axial direction, the amount of work performed by each blade on the main plate side is compared to that on the side plate side. , and the air flow can be drawn toward the main plate again in the vicinity of the exit of the interblade passage.
- the air flow velocity distribution near the outlet of the inter-blade passage can be brought closer to a distribution free from axial bias, It is possible to reduce the noise of the centrifugal fan.
- Dsi/Dso satisfies 0.5 ⁇ Dsi/Dso ⁇ 0.7, where Dsi is the inner diameter of the side plate and Dso is the outer diameter of the side plate. Therefore, if the blade trailing edge is parallel to the fan axis, the air flow in the inter-blade passage is biased toward the side plate near the exit of the inter-blade passage. It is possible to use the above-described configuration in which the side is located radially inward. Therefore, it is possible to use the configuration of the blade trailing edge so as to appropriately reduce the noise of the centrifugal fan.
- FIG. 2 is a vertical cross-sectional view showing the blower cut along a plane including the fan axis in the first embodiment, that is, a cross-sectional view schematically showing the II-II cross section of FIG. 1;
- FIG. 3 is a plan view showing a centrifugal fan and a rotating shaft of the blower in the first embodiment, viewed from one side to the other side in the axial direction of the fan. 3 is a cross-sectional view showing the same cross section as FIG. 2;
- FIG. FIG. 2 is a perspective view showing a trailing edge of the blade of the centrifugal fan and its surroundings in the first embodiment.
- FIG. 2 is a cross-sectional view showing a cross section obtained by cutting a trailing edge portion of the blade of the centrifugal fan and its periphery along a plane perpendicular to the fan axis in the first embodiment
- FIG. 4A is a cross-sectional view of a portion connected to a side plate
- FIG. 4B is a cross-sectional view of a portion of a blade trailing edge portion connected to a main plate.
- FIG. 3 is a diagram in which the SPL of noise generated by the fan of the first embodiment is indicated by a solid line S1, and the SPL of noise generated by the fan of a comparative example is indicated by a dashed line S2.
- FIG. 5 is a diagram comparing the noise generated by the blower of the first embodiment and the noise generated by the blower of the comparative example in terms of overall values;
- FIG. 4 is a graph showing the relationship between Dmo/Db2, which is the ratio of the outer diameter Dmo of the main plate to the other diameter Db2 of the trailing edge portion of the blade, and the noise reduction effect in the first embodiment.
- Dmo/Db2 is the ratio of the outer diameter Dmo of the main plate to the other diameter Db2 of the trailing edge portion of the blade, and the noise reduction effect in the first embodiment.
- FIG. 3 is a longitudinal cross-sectional view schematically showing the blower cut along a plane including the fan axis in the second embodiment, and corresponding to FIG. 2 ;
- FIG. 10 is a vertical cross-sectional view schematically showing the blower cut along a plane including the fan axis in the third embodiment, and corresponding to FIG. 2 ;
- FIG. 10 is a longitudinal sectional view schematically showing the blower cut along a plane including the fan axis in the fourth embodiment, corresponding to FIG. 2 ;
- FIG. 11 is a longitudinal sectional view schematically showing the blower cut along a plane including the fan axis in the fifth embodiment, corresponding to FIG. 2 ;
- FIG. 10 is a vertical cross-sectional view schematically showing the blower cut along a plane including the fan axis in the third embodiment, and corresponding to FIG. 2 ;
- FIG. 10 is a longitudinal sectional view schematically showing the blower cut along a plane including the fan axis in the fourth embodiment, corresponding to
- FIG. 12 is a longitudinal sectional view schematically showing the blower cut along a plane including the fan axis in the sixth embodiment, corresponding to FIG. 2 ;
- FIG. 12 is a longitudinal sectional view schematically showing the blower cut along a plane including the fan axis in the seventh embodiment, corresponding to FIG. 2 ;
- it is a vertical cross-sectional view schematically showing the blower cut along a plane including the fan axis, and corresponding to FIG. 2 .
- it is a vertical cross-sectional view schematically showing the blower cut along a plane including the fan axis, and corresponding to FIG. 2 .
- the tenth embodiment it is a vertical cross-sectional view schematically showing the blower cut along a plane including the fan axis, and corresponding to FIG. 2 .
- the blower 10 of this embodiment is a centrifugal blower, more specifically a turbo blower.
- the blower 10 includes a casing 12 which is a housing of the blower 10, a rotary shaft 14, an electric motor 16, an electronic substrate 17, a centrifugal fan 18, a bearing 28, a bearing housing 29, and the like.
- the fan axis CL shown in FIG. 2 is the center of rotation of the centrifugal fan 18 .
- An arrow Da in FIG. 2 indicates the axial direction Da of the fan axis CL, that is, the fan axis direction Da.
- An arrow Dr in FIG. 2 indicates the radial direction Dr of the fan axis CL, that is, the fan radial direction Dr.
- the illustration of the right side of the fan 10 with respect to the fan axis CL is omitted.
- the casing 12 protects the electric motor 16, the electronic board 17, and the centrifugal fan 18 from dust and dirt outside the blower 10.
- casing 12 houses electric motor 16 , electronic board 17 , and centrifugal fan 18 .
- the casing 12 is composed of a first case member 22 and a second case member 24 .
- the casing 12 is a non-rotating member of the blower 10 .
- the first case member 22 of the casing 12 is made of, for example, resin, has a larger diameter than the centrifugal fan 18, and has a substantially disk shape.
- the first case member 22 is composed of a first cover portion 221 , a first case outer peripheral portion 222 , a first peripheral edge portion 223 and a plurality of struts 224 .
- the first case member 22 is a cover that covers the centrifugal fan 18 on one side of the centrifugal fan 18 in the fan axial direction Da. Therefore, the first case member 22 is provided on the side opposite to the blade 32 side with respect to the side plate 34 of the centrifugal fan 18 . Further, since the centrifugal fan 18 rotates with respect to the casing 12, the first case member 22 is arranged away from the side plate 34 of the centrifugal fan 18 in order to prevent mutual interference.
- the first case member 22 corresponds to the side plate adjacent case of the present disclosure.
- the first cover portion 221 of the first case member 22 has a shape expanding in the fan radial direction Dr.
- the first cover portion 221 is arranged on one side of the centrifugal fan 18 in the fan axial direction Da and covers the one side of the centrifugal fan 18 in the fan axial direction Da.
- An air intake port 221a is formed on the inner peripheral side of the first cover portion 221 and extends through the first cover portion 221 in the fan axial direction Da. sucked into. Further, the first cover portion 221 has an intake port forming portion 221b provided as a bell mouth forming the periphery of the air intake port 221a.
- the suction port forming portion 221b forms an air suction port 221a inside the suction port forming portion 221b, and smoothly guides the air flowing into the air suction port 221a from the outside of the blower 10 into the air suction port 221a.
- the first case outer peripheral portion 222 of the first case member 22 is arranged outside the first cover portion 221 in the fan radial direction Dr and is connected to the first cover portion 221 .
- the first case outer peripheral portion 222 is arranged outside the side plate 34 of the centrifugal fan 18 in the fan radial direction Dr.
- the first case perimeter 222 corresponds to the case perimeter of the present disclosure.
- the first peripheral edge portion 223 of the first case member 22 is provided outside the first case outer peripheral portion 222 in the fan radial direction Dr, and extends around the fan axial center CL. It constitutes the periphery of the member 22 .
- a plurality of struts 224 of the first case member 22 each protrude from the first case outer peripheral portion 222 toward the inside of the casing 12 in parallel with the fan axis CL. Also, the strut 224 has a thick cylindrical shape with a central axis parallel to the fan axis CL. A screw hole through which a screw 26 that joins the first case member 22 and the second case member 24 is inserted is formed inside the support 224 .
- Each strut 224 of the first case member 22 is arranged outside the centrifugal fan 18 in the fan radial direction Dr.
- the first case member 22 and the second case member 24 are connected by screws 26 inserted through the support 224 with the tip of the support 224 abutting against the second case member 24 .
- the second case member 24 has a substantially disk shape with substantially the same diameter as the first case member 22 .
- the second case member 24 is made of metal such as iron or stainless steel or resin, and functions also as a motor housing that covers the electric motor 16 and the electronic substrate 17 .
- the second case member 24 is composed of a second cover portion 241 , a second case outer peripheral portion 242 and a second peripheral edge portion 243 .
- the second cover portion 241 is arranged on the other side in the fan axial direction Da with respect to the centrifugal fan 18 and the electric motor 16, and covers the other side of the centrifugal fan 18 and the electric motor 16 in the fan axial direction Da.
- the second case outer peripheral portion 242 of the second case member 24 is arranged outside the second cover portion 241 in the fan radial direction Dr and is connected to the second cover portion 241 .
- the second case outer peripheral portion 242 is arranged outside the main plate 36 of the centrifugal fan 18 in the fan radial direction Dr.
- the second case outer peripheral portion 242 and the first case outer peripheral portion 222 are formed so as to face each other in the fan axial direction Da. Between the second case outer peripheral portion 242 and the first case outer peripheral portion 222, a fan outer peripheral flow path 12b is formed to flow the air blown out from the outlet 18a of the centrifugal fan 18 to the outside in the fan radial direction Dr. .
- the fan outer peripheral flow path 12b is formed over the entire circumference of the centrifugal fan 18. As shown in FIG.
- the second peripheral edge portion 243 of the second case member 24 is provided outside the second case outer peripheral portion 242 in the fan radial direction Dr, and constitutes the peripheral edge of the second case member 24 around the fan axis CL.
- the first peripheral edge portion 223 and the second peripheral edge portion 243 constitute an air blowing portion for blowing air in the casing 12 .
- the first peripheral edge portion 223 and the second peripheral edge portion 243 are provided between the first peripheral edge portion 223 and the second peripheral edge portion 243 in the fan axial direction Da, and the air outlet 12a through which the air blown out from the centrifugal fan 18 is blown out.
- the air outlet 12a is also the downstream end of the fan outer peripheral channel 12b.
- the air outlet 12a is formed on the side surface of the fan of the blower 10 and opens outward in the fan radial direction Dr.
- the air outlet 12a is open over the entire circumference of the casing 12 around the fan axis CL, and blows out the air from the centrifugal fan 18.
- the blower 10 is an all-around blower in which the air outlet 12a is provided over the entire circumference of the casing 12 . It should be noted that, at a location where the strut 224 is provided, the blowing of air from the casing 12 is blocked by the strut 224. It is a meaning including opening.
- the rotating shaft 14 is made of metal such as iron, stainless steel, or brass.
- the rotating shaft 14 is a columnar bar as shown in FIG. 2, and is press-fitted into the inner ring of the bearing 28, for example. Therefore, the rotating shaft 14 is fixed with respect to the inner ring of the bearing 28 .
- the outer ring of the bearing 28 is fixed to the bearing housing 29 by, for example, being press-fitted.
- the bearing housing 29 is made of metal such as aluminum alloy, brass, iron, or stainless steel, and is fixed to the second cover portion 241 .
- the rotating shaft 14 is supported by the second cover portion 241 via the bearings 28 . That is, the rotary shaft 14 is rotatable about the fan axis CL with respect to the second cover portion 241 .
- one end of the rotating shaft 14 in the fan axial direction Da is fitted into the inner peripheral hole 36 a of the main plate 36 of the centrifugal fan 18 . fixed against. That is, the centrifugal fan 18 rotates integrally with the rotary shaft 14 around the fan axis CL.
- the electric motor 16 is an outer rotor type brushless DC motor.
- the electric motor 16 is arranged together with the electronic board 17 between the main plate 36 of the centrifugal fan 18 and the second cover portion 241 in the fan axial direction Da.
- the electric motor 16 has a motor rotor 161 , a rotor magnet 162 and a motor stator 163 .
- the motor rotor 161 is made of metal such as a steel plate, and is formed, for example, by press forming the steel plate.
- the rotor magnet 162 is a permanent magnet, and is composed of, for example, a rubber magnet containing ferrite, neodymium, or the like.
- the rotor magnet 162 is integrally fixed to the motor rotor 161 .
- the motor rotor 161 is fixed to the rotor connecting portion 38 of the centrifugal fan 18 . That is, the motor rotor 161 and the rotor magnet 162 rotate integrally with the centrifugal fan 18 about the fan axis CL.
- the motor stator 163 includes a stator coil 163a and a stator core 163b electrically connected to the electronic board 17.
- the motor stator 163 is arranged radially inside the rotor magnet 162 with a small gap therebetween.
- the motor stator 163 is fixed to the second cover portion 241 of the second case member 24 via the bearing housing 29 .
- a plurality of electric components (not shown) are mounted on the electronic board 17 .
- an electric circuit for rotating the electric motor 16 is configured on the electronic board 17 .
- the stator coil 163a of the motor stator 163 when the stator coil 163a of the motor stator 163 is energized from an external power supply, the stator coil 163a causes a magnetic flux change in the stator core 163b. A magnetic flux change in the stator core 163 b generates a force that attracts the rotor magnet 162 . Since the motor rotor 161 is fixed to the rotating shaft 14 rotatably supported by the bearing 28, it rotates around the fan axis CL under the force of attracting the rotor magnet 162. As shown in FIG. In short, when the electric motor 16 is energized, it rotates the centrifugal fan 18 to which the motor rotor 161 is fixed around the fan axis CL.
- the centrifugal fan 18 is an impeller applied to the blower 10, as shown in FIGS.
- the centrifugal fan 18 blows air by rotating around the fan axis CL in a predetermined fan rotation direction DRf. That is, the centrifugal fan 18 rotates around the fan axis CL to draw air from one side in the fan axis direction Da through the air intake port 221a as indicated by the arrow FLa. Then, the centrifugal fan 18 blows out the sucked air radially outward of the centrifugal fan 18 as indicated by an arrow FLb.
- the centrifugal fan 18 of this embodiment is a turbo fan.
- the centrifugal fan 18 has a plurality of blades 32 , side plates 34 , main plates 36 and rotor connecting portions 38 .
- the centrifugal fan 18 is made of resin, for example, and its plurality of blades 32, side plates 34, main plate 36, and rotor connecting portion 38 are integrally constructed.
- a plurality of blades 32 are arranged around the fan axis CL. Specifically, the plurality of blades 32 are arranged side by side in the circumferential direction Dc of the fan axial center CL while leaving an interval for air flow between them. Airfoils 32 are also referred to as fan blades.
- the blades 32 are provided on one side of the blades 32 in the fan axial direction Da, and on the other side of the blades 32 opposite to the one side in the fan axial direction Da. and a wing other end portion 322 which is closed.
- the plurality of blades 32 form inter-blade passages 32a through which air flows between adjacent blades 32 among the plurality of blades 32 .
- the side plate 34 has a disk shape that expands in the fan radial direction Dr.
- An air intake hole 34a through which air from the air intake port 221a of the casing 12 is sucked as indicated by an arrow FLa is formed inside the side plate 34 in the radial direction. Therefore, the side plate 34 has an annular shape around the fan axis CL.
- the side plate 34 has a side plate inner peripheral end portion 341 and a side plate outer peripheral end portion 342 .
- the side plate inner peripheral end portion 341 is an end portion provided inside the side plate 34 in the fan radial direction Dr, and forms the intake hole 34a.
- the side plate outer peripheral end portion 342 is an end portion of the side plate 34 provided on the outside in the fan radial direction Dr.
- the side plate outer peripheral edge 342 corresponds to the outer peripheral edge of the present disclosure that the side plate 34 has.
- the side plate 34 is provided on one side of the plurality of blades 32 in the fan axial direction Da, that is, on the side of the air intake port 221a. Along with that, the side plate 34 is connected to each of the plurality of wings 32 . In other words, the side plate 34 is connected to each of its blades 32 at one blade end 321 .
- the side plate 34 also has a side plate other surface 343 facing the other side in the fan axial direction Da.
- This side plate other surface 343 faces the inter-blade flow path 32 a and guides the airflow inside the centrifugal fan 18 .
- the side plate other surface 343 is a curved surface that expands in the fan radial direction Dr, and is located on the other side in the fan axial direction Da toward the outside in the fan radial direction Dr. 2, which is a longitudinal section including the fan axis CL, the radius of curvature of the side plate other surface 343 increases toward the outer side in the fan radial direction Dr.
- the side plate other surface 343 has an inner arc shape 343a, an outer arc shape 343b, and an outer linear shape 343c.
- the inner arc shape 343a, the outer arc shape 343b, and the outer linear shape 343c are smoothly connected in the order of the inner arc shape 343a, the outer arc shape 343b, and the outer linear shape 343c from the inside in the fan radial direction Dr.
- the curvature radius R2 of the outer arcuate shape 343b is larger than the curvature radius R1 of the inner arcuate shape 343a, and the outer linear shape 343c is linear perpendicular to the fan axis CL.
- the main plate 36 Since the main plate 36 is fixed to the rotating shaft 14 rotatable around the fan axis CL, it is supported rotatably around the fan axis CL with respect to the casing 12 .
- the main plate 36 has a disk-like shape extending in the fan radial direction Dr around the fan axis CL.
- the main plate 36 is connected to each of the plurality of blades 32 on the side opposite to the side plate 34 side. That is, the main plate 36 is connected to each of the plurality of blades 32 at the blade other end portion 322 .
- the main plate 36 also has a main plate guide surface 36b that guides the airflow inside the centrifugal fan 18.
- the main plate guide surface 36b faces the inter-blade passage 32a and faces the other side plate surface 343 across the inter-blade passage 32a.
- the main plate guide surface 36b is a curved surface that faces one side in the fan axial direction Da and expands in the fan radial direction Dr, and is located on the other side in the fan axial direction Da toward the outside in the fan radial direction Dr. formed. With such a shape, the main plate guide surface 36b guides the airflow sucked into the air inlet 221a and directed in the fan axial direction Da so as to be directed outward in the fan radial direction Dr.
- an inner peripheral hole 36a is formed radially inside the main plate 36 so as to penetrate the main plate 36 in the fan axial direction Da.
- the rotor connecting portion 38 is a cylindrical rib centered on the fan axis CL, and protrudes from the main plate 36 to the other side in the fan axis direction Da.
- a motor rotor 161 is fitted and stored inside the rotor connecting portion 38 in the radial direction. Thereby, the rotor connecting portion 38 is fixed to the motor rotor 161 .
- the centrifugal fan 18 is fixed to the motor rotor 161 .
- the main plate 36 has a main plate outer peripheral end portion 362 .
- the main plate outer peripheral end portion 362 is an end portion of the main plate 36 provided outside in the fan radial direction Dr.
- the main plate outer peripheral end portion 362 and the side plate outer peripheral end portion 342 are arranged apart from each other in the fan axial direction Da.
- the main plate outer peripheral end portion 362 and the side plate outer peripheral end portion 342 form the outlet 18a from which the air that has passed through the inter-blade passage 32a is blown out between the main plate outer peripheral end portion 362 and the side plate outer peripheral end portion 342.
- the main plate outer peripheral end portion 362 and the side plate outer peripheral end portion 342 constitute an air blowing portion of the centrifugal fan 18 in which the blowing port 18a is formed.
- the blowout port 18a of the centrifugal fan 18 faces outward in the fan radial direction Dr and is formed along the entire circumference of the centrifugal fan 18 around the fan axis CL.
- the position of the main plate outer peripheral end portion 362 in the fan radial direction Dr is aligned with the position of the side plate outer peripheral end portion 342 . That is, as shown in FIGS. 2 and 4, the outer diameter Dmo of the main plate 36 and the outer diameter Dso of the side plate 34 are the same size, which is the outer diameter Dout of the centrifugal fan 18 .
- each of the plurality of blades 32 has a blade leading edge portion 323 provided on the inner side in the fan radial direction Dr and a blade trailing edge portion 324 provided on the outer side in the fan radial direction Dr. and
- the leading edge portion 323 of the blade is an edge portion formed on the upstream side in the airflow direction of the air passing through the intake hole 34a and flowing into the inter-blade passage 32a.
- the blade trailing edge portion 324 is an edge portion formed on the downstream side of the blade 32 in the airflow direction of the air flowing through the inter-blade passage 32a.
- the blade leading edge portion 323 is connected to the side plate 34 and the main plate 36 and extends from the side plate 34 side to the main plate 36 side.
- a blade trailing edge 324 is also connected to the side plate 34 and the main plate 36 and extends from the side plate 34 side to the main plate 36 side.
- the blade leading edge portion 323 is formed so as to be located inside in the fan radial direction Dr toward the main plate 36 side. Specifically, the blade leading edge portion 323 includes a first leading edge portion 323a and a second leading edge portion 323b. The first front edge portion 323a and the second front edge portion 323b are formed to extend linearly, and the first front edge portion 323a and the second front edge portion 323b are connected in series. The first front edge portion 323 a is connected to the side plate 34 . The second front edge portion 323 b is connected to the main plate 36 and provided between the first front edge portion 323 a and the main plate 36 .
- the angle formed by the second front edge portion 323b with respect to the fan axis CL is smaller than the angle formed with the first front edge portion 323a with respect to the fan axis CL.
- the first front edge portion 323a extends linearly in a direction perpendicular to the fan axis CL.
- the second front edge portion 323b extends linearly while being inclined with respect to the fan axis CL so as to be located outside in the fan radial direction Dr toward one side in the fan axis direction Da.
- the one-side diameter Df1 of the second front edge portion 323b is larger than the other-side diameter Df2 of the second front edge portion 323b.
- the one-side diameter Df1 of the second front edge portion 323b is a diameter around the fan axis CL that the second front edge portion 323b has at one end in the fan axis direction Da.
- the other side diameter Df2 of the second front edge portion 323b is a diameter centered on the fan axis CL that the second front edge portion 323b has at the other side end in the fan axis direction Da.
- the trailing edge portion 324 of the blade extends toward the inside in the fan radial direction Dr toward one side in the fan axial direction Da. Specifically, in the vertical cross sections of FIGS. 2 and 4, the blade trailing edge portion 324 is inclined with respect to the fan axis CL such that the side plate 34 side is located inside the main plate 36 side in the fan radial direction Dr. It is formed linearly.
- the one side diameter Db1 of the blade trailing edge portion 324 is smaller than the other side diameter Db2 of the blade trailing edge portion 324.
- the one-side diameter Db1 of the blade trailing edge portion 324 is the diameter of the blade trailing edge portion 324 at one end in the fan axial direction Da centered on the fan axial center CL.
- the other side diameter Db2 of the blade trailing edge portion 324 is a diameter around the fan axis CL that the blade trailing edge portion 324 has at the other side end in the fan axis direction Da.
- the other side diameter Db2 of the blade trailing edge portion 324 is also the maximum outer diameter of the blade 32 around the fan axis CL.
- a relationship of "Db2 ⁇ Dmo ⁇ 1.13 ⁇ Db2" is established.
- part of the blade leading edge 323 falls within an axial range Hb1 included in the full width Hb of the blade trailing edge 324 in the fan axial direction Da.
- the portion of the blade leading edge portion 323 within the axial range Hb1 is, in detail, a portion of the second leading edge portion 323b including the end on the main plate 36 side.
- a portion Psi of the side plate other surface 343 that starts expanding outward in the fan radial direction Dr from the side plate inner peripheral end portion 341 has an axial height H2 along the fan axial direction Da with respect to the main plate guide surface 36b,
- the outer diameter Dso has a relationship of "0.06 ⁇ H2/Dso ⁇ 0.20".
- the blade trailing edge portion 324 is connected to the side plate 34 inside the side plate outer peripheral end portion 342 in the fan radial direction Dr.
- the blade trailing edge portion 324 is connected to the main plate 36 inside the main plate outer peripheral end portion 362 in the fan radial direction Dr. That is, the side plate 34 and the main plate 36 each extend outside the blade trailing edge portion 324 in the fan radial direction Dr.
- the size relationship between the outer diameter Dso of the side plate 34 and the one-side diameter Db1 of the blade trailing edge portion 324 is "Dso>Db1".
- the size relationship with the other side diameter Db2 is "Dmo>Db2".
- the side plate 34 forms a case side plate clearance 34b between itself and the first case member 22.
- the case side plate gap 34b is formed to be as narrow a gap as possible within a range where interference between the first case member 22 and the centrifugal fan 18 can be prevented.
- first case outer peripheral portion 222 extends from the first cover portion 221 and is provided so as to overlap the side plate outer peripheral end portion 342 on the outside in the fan radial direction Dr.
- the inner diameter Dc1 of the first case outer peripheral portion 222 is larger than the outer diameter Dso of the side plate 34 . Therefore, the side plate outer peripheral end portion 342 faces the first case outer peripheral portion 222 in the fan radial direction Dr, and forms an opening end 34c of the case side plate gap 34b between the first case outer peripheral portion 222 and the first case outer peripheral portion 222 .
- An open end 34c of the case side plate gap 34b is located inside the fan radial direction Dr from the air outlet 12a of the casing 12, and the case side plate gap 34b is connected to the fan outer peripheral flow path 12b at the open end 34c.
- the thickness tb of the blade 32 is not constant at the blade trailing edge portion 324 .
- the thickness tb of the blade 32 increases toward the side plate 34 at the blade trailing edge portion 324 .
- the side plate side trailing edge thickness tb1 which is the thickness tb of the blade 32 at the portion of the blade trailing edge portion 324 connected to the side plate 34, is the thickness of the blade 32 at the portion of the blade trailing edge portion 324 connected to the main plate 36. It is larger than the main plate side trailing edge thickness tb2, which is the thickness tb.
- the surface shape of the blade trailing edge portion 324 also changes according to the axial position. ing.
- the air flow around the blade 32 is represented by a dashed line.
- the blade trailing edge 324 has a trailing edge outer surface 324 a that is the surface of the blade trailing edge 324 .
- a trailing edge outer surface 324a connects the pressure surface and the suction surface of the blade 32 at the blade trailing edge 324, and is convexly curved in a cross section perpendicular to the fan axis CL. Furthermore, in its cross section, the radius of curvature Rb of the rear edge portion outer surface 324a increases toward the side plate 34 side.
- the side plate side curvature radius Rb1 which is the curvature radius Rb of the trailing edge outer surface 324a at the portion of the blade trailing edge portion 324 connected to the side plate 34, is the radius of curvature Rb1 at the portion of the blade trailing edge portion 324 connected to the main plate 36. It is larger than the main plate side curvature radius Rb2, which is the curvature radius Rb.
- the blade trailing edge portion 91 of the centrifugal fan of the comparative example compared with the present embodiment is indicated by broken lines.
- the trailing edge portion 91 of the blade is parallel to the fan axis CL, and the thickness tb of the blade 32 at the trailing edge portion 91 of the blade is constant. Except for these points, the centrifugal fan of the comparative example is the same as the centrifugal fan 18 of this embodiment.
- the centrifugal fan 18 configured as described above rotates integrally with the motor rotor 161 in the fan rotation direction DRf as shown in FIGS.
- the blades 32 of the centrifugal fan 18 give momentum to the air, so the centrifugal fan 18 sucks air from the intake holes 34a as indicated by the arrow FLa, and the sucked air flows as indicated by the arrows FL1, FL2, and FL3. flows radially outward through the inter-blade passage 32a.
- the centrifugal fan 18 blows out the air that has passed through the inter-blade passage 32a radially outward from the outlet 18a as indicated by an arrow FLb.
- the air blown out from the blowout port 18a passes through the fan outer peripheral flow path 12b of the casing 12 and is discharged to the outside of the blower 10 from the air blowout port 12a.
- the blade trailing edge portion 324 extends in the fan radial direction toward one side in the fan axial direction Da. It is formed so as to be located inside Dr.
- the air flow in the inter-blade passages 32a formed between the blades 32 will be described. Then, the vortex WH is generated on the side plate other surface 343 once separated from the side plate 34 . Then, the air flow in the inter-blade passage 32a once separates from the side plate 34 and then advances as indicated by the arrow FL2. That is, the air flow deviates to one side in the fan axial direction Da so as to once separate from the side plate 34 and then reattach to the side plate 34 .
- the blade trailing edge portion 324 is formed so as to be located inside the fan radial direction Dr toward one side in the fan axial direction Da. , the amount of work performed by each blade 32 on the side of the main plate 36 is greater than that on the side of the side plate 34 . As a result, the air flow can be drawn again toward the main plate 36 near the outlet of the inter-blade passage 32a as indicated by the arrow FL3.
- the velocity distribution of the airflow near the outlet of the inter-blade passage 32a is a distribution with no deviation in the fan axis direction Da. , and the noise of the centrifugal fan 18 can be reduced.
- Dsi/Dso which is the ratio of the inner diameter Dsi of the side plate 34 to the outer diameter Dso of the side plate 34, is "0.5 ⁇ Dsi/Dso ⁇ 0.7". Therefore, if the blade trailing edge 324 is parallel to the fan axis CL, the air flow in the inter-blade passage 32a is biased toward the side plate 34 near the exit of the inter-blade passage 32a.
- the above configuration in which 324 is located inside in the fan radial direction Dr toward one side in the fan axial direction Da can be used. Therefore, the above configuration of the blade trailing edge portion 324 of the present embodiment can be used so as to appropriately reduce the noise of the centrifugal fan 18 .
- the length of the inter-blade passage 32a after the air flow is biased to one side in the fan axial direction Da as indicated by arrow FL2 is sufficiently long. Secured. Therefore, even if the trailing edge 324 of the blade is parallel to the fan axis CL, the air flow will not reach the trailing edge 324 until it reaches the trailing edge 324 after being biased to one side in the direction Da of the fan axis. The deviation of the airflow toward one side in the fan axial direction Da is alleviated.
- centrifugal fan of this simulation example the configuration of the blades 32 is the same as that of the comparative example. That is, in the centrifugal fan of the simulation example, the blade trailing edge 91 (see FIG. 5) is parallel to the fan axis CL, and the thickness tb of the blade 32 at the blade trailing edge 91 is constant. Except for these points, the centrifugal fan of this simulation example is the same as the centrifugal fan 18 of this embodiment.
- FIGS. 7A to 7D The analysis results obtained from this CFD simulation are shown in FIGS. 7A to 7D.
- the rotation speed of the centrifugal fan is assumed to be constant.
- arrows A1 and A2 in FIGS. 7A to 7D indicate the direction of the air flow in the inter-blade passage 32a.
- a position P1 indicates a position where the side plate 34 faces the inter-blade passage 32a
- a position P2 indicates a position where the main plate 36 faces the inter-blade passage 32a.
- the difference in hatching indicates the speed of the airflow (in other words, the flow speed) in the inter-blade passage 32a.
- the velocity distribution of the airflow near the outlet of the inter-blade passage 32a that is, near the blade trailing edge 91 in FIG. 5 is The high-speed portion is biased toward the other side of the fan axial direction Da (that is, the main plate 36 side).
- 3 shows the velocity distribution of the airflow in the inter-blade passage 32a obtained in FIG.
- the air flow velocity near the exit of the inter-blade passage 32a The distribution is such that the high-speed portion is biased toward one side in the fan axial direction Da (that is, the side plate 34 side).
- FIGS. 7A to 7D The following can be said from the airflow velocity distribution shown in FIGS. 7A to 7D. That is, when "0.5 ⁇ Dsi/Dso ⁇ 0.7" as shown in FIGS. 7B and 7C, the blade trailing edge 324 is tilted with respect to the fan axial direction Da as in the present embodiment.
- the velocity distribution of the airflow near the outlet of the inter-blade passage 32a approaches one with no bias in the fan axial direction Da. This is because the blade trailing edge 324 (see FIG. 2) inclined with respect to the fan axis direction Da as in the present embodiment is compared with the blade trailing edge 91 parallel to the fan axis CL.
- the velocity distribution of the airflow near the exit of the inter-blade passage 32a is not one in which the high-speed portion is biased toward the side plate 34 side. Therefore, in the case of "0.7 ⁇ Dsi/Dso" and in the case of "Dsi/Dso ⁇ 0.5", even if the air flow is drawn toward the main plate 36 near the outlet of the inter-blade passage 32a, , the velocity distribution of the airflow near the outlet does not come close to the one with no deviation in the fan axial direction Da. That is, in this case, even if the blade trailing edge portion 324 is inclined with respect to the fan axial direction Da as in the present embodiment, this does not lead to noise reduction of the centrifugal fan 18 .
- the configuration in which the blade trailing edge 324 is inclined with respect to the fan axial direction Da as in the present embodiment is effective in reducing the noise of the centrifugal fan 18. It can be said that the relationship "0.5 ⁇ Dsi/Dso ⁇ 0.7" is required to be useful.
- the centrifugal fan 18 of the present embodiment when comparing the centrifugal fan 18 of the present embodiment with the centrifugal fan of the comparative example in which the blade trailing edge 91 (see FIG. 5) is parallel to the fan axis CL, as shown in FIG. Low noise of the centrifugal fan 18 is realized in the region.
- the solid line S1 indicates the SPL of this embodiment
- the dashed line S2 indicates the SPL of the comparative example.
- SPL is an abbreviation for "Sound Pressure Level".
- the noise of the centrifugal fan 18 was reduced by 2 dB in overall value as compared with the comparative example.
- "OA" on the vertical axis of Fig. 9 is an abbreviation for the overall value.
- the side plate other surface 343 is located on the other side in the fan axial direction Da toward the outside in the fan radial direction Dr. 2 and 4, the curvature radius of the side plate other surface 343 increases toward the outer side in the fan radial direction Dr. Therefore, while the blade trailing edge portion 324 is located inside the fan radial direction Dr toward one side in the fan axial direction Da, the air is sucked into the centrifugal fan 18 from one side in the fan axial direction Da while obtaining the noise reduction effect. It is possible to guide the trapped air so as to face outward in the fan radial direction Dr.
- the blade leading edge portion 323 extends from the side plate 34 side to the main plate 36 side.
- the main plate 36 side is located inside the fan radial direction Dr. Therefore, since the blades 32 are longer on the side of the main plate 36 than on the side of the side plate 34, the work done by each blade 32 on the side of the main plate 36 can be made larger than that on the side of the side plate 34. This also makes it possible to correct the bias of the airflow in the inter-blade passage 32a to one side in the fan axial direction Da.
- the side plate 34 and the main plate 36 each extend outside the blade trailing edge portion 324 in the fan radial direction Dr. Therefore, the trailing edge portion 324 of the blade where the flow velocity of the air flow is maximized can be kept away from the opening end 34c of the case side plate gap 34b. This is advantageous in reducing the noise of the centrifugal fan 18 .
- the side plate 34 and the main plate 36 each extend to the outer side of the fan radial direction Dr from the blade trailing edge portion 324, the air flow suddenly moves in the fan axial direction Da immediately after coming out of the inter-blade passage 32a. Expansion is suppressed. As a result, the loss caused by the rapid expansion of the airflow can be suppressed, and the centrifugal fan 18 can contribute to noise reduction.
- FIG. 10 shows the relationship between Dmo/Db2, which is the ratio of the outer diameter Dmo of the main plate 36 to the other diameter Db2 of the blade trailing edge 324, and the noise reduction effect. That is, the greater the Dmo/Db2, the higher the noise reduction effect.
- the extension of the side plate 34 and the main plate 36 to the outer side in the fan radial direction Dr from the blade trailing edge portion 324 acts to enhance the noise reduction effect.
- the outer diameter Dso of the side plate 34 is the same as the outer diameter Dmo of the main plate 36.
- the relationship "Db2 ⁇ Dmo ⁇ 1.13 ⁇ Db2" is established between the diameter Db2 on the other side of the blade trailing edge portion 324 and the outer diameter Dmo of the main plate 36. .
- Dmo/Db2 exceeds 1.13
- the noise reduction effect gradually increases as Dmo/Db2 increases, but does not change much with respect to Dmo/Db2. Therefore, it is possible to obtain a noise reduction effect while avoiding the size of the centrifugal fan 18 from becoming unnecessarily large.
- the first case outer peripheral portion 222 of the first case member 22 is provided so as to overlap the side plate outer peripheral end portion 342 of the centrifugal fan 18 on the outside in the fan radial direction Dr. there is
- the side plate outer peripheral end portion 342 faces the first case outer peripheral portion 222 in the fan radial direction Dr, and forms an opening end 34c of the case side plate gap 34b between the first case outer peripheral portion 222 and the first case outer peripheral portion 222 .
- the opening end 34c of the case-side plate gap 34b is located inside the air outlet 12a of the casing 12 in the fan radial direction Dr, the air pressure at the opening end 34c is lower than the air pressure at the air outlet 12a. .
- the opening end 34c is open outside the air outlet 12a, for example, it is possible to suppress the backflow of the blown air flowing into the case side plate gap 34b from the opening end 34c.
- the blade trailing edge portion 324 extends from the side plate 34 side to the main plate 36 side, and the thickness tb of the blade 32 is At the edge portion 324, the side plate 34 side is larger. Therefore, the airflow stall area ST adjacent to the blade trailing edge 324 is larger on the side plate 34 side than on the main plate 36 side. This also acts to prevent the airflow around the trailing edge portion 324 of the blade from deviating to one side in the fan axial direction Da.
- the trailing edge portion of the blade trailing edge portion 324 is The outer surface 324a is curved in a convex shape, and the radius of curvature Rb of the rear edge portion outer surface 324a increases toward the side plate 34 side. Therefore, the pressure surface and the suction surface of the blade 32 can be smoothly connected at the blade trailing edge portion 324 . Therefore, the pressure surface and the suction surface are smoothed at the blade trailing edge 324 while maintaining the tendency that the air flow resistance around the blade trailing edge 324 is larger on the side plate 34 side than on the main plate 36 side. Compared to the case where they are not connected, the overall flow resistance can be lowered.
- the blade trailing edge portion 324 is formed so as to be positioned more inward in the fan radial direction Dr toward one side in the fan axial direction Da.
- the shape of the blade trailing edge portion 324 is different from that in the first embodiment.
- the blade trailing edge portion 324 of the present embodiment is formed to have a single stepped shape, and is located stepwise toward the inside in the fan radial direction Dr toward one side in the fan axial direction Da.
- this embodiment is the same as the first embodiment.
- the trailing edge portion 324 of the blade is formed so as to be positioned more inward in the fan radial direction Dr toward one side in the fan axial direction Da.
- the shape of the blade trailing edge portion 324 is different from that in the first embodiment.
- the blade trailing edge portion 324 of this embodiment is formed to have a plurality of stepped shapes, and is located stepwise toward the inside in the fan radial direction Dr toward one side in the fan axial direction Da.
- this embodiment is the same as the first embodiment.
- the blade trailing edge portion 324 is formed so as to be positioned more inward in the fan radial direction Dr toward one side in the fan axial direction Da.
- the shape of the blade trailing edge portion 324 is different from that in the first embodiment.
- a portion on one side in the fan axial direction Da including the portion connected to the side plate 34 of the blade trailing edge portion 324 is parallel to the fan axial center CL. extended.
- the blade trailing edge portion 324 includes a portion connected to the main plate 36, and the blade trailing edge portion 324 is more inclined toward the fan radial direction Dr. is inclined with respect to the fan axis CL so as to be located outside the .
- this embodiment is the same as the first embodiment.
- the blade trailing edge portion 324 is formed so as to be positioned more inward in the fan radial direction Dr toward one side in the fan axial direction Da.
- the shape of the blade trailing edge portion 324 is different from that in the first embodiment.
- the blade trailing edge 324 of this embodiment extends while bending.
- this embodiment is the same as the first embodiment.
- the side plate other surface 343 of the centrifugal fan 18 faces the other side of the fan axial direction Da and extends in the fan radial direction Dr.
- the outer side in the radial direction Dr is positioned on the other side in the fan axial direction Da.
- the shape of the side plate other surface 343 is different from that in the first embodiment.
- the side plate other surface 343 has an inner arc shape 343a and an outer linear shape 343d.
- This outer linear shape 343d replaces the outer circular arc shape 343b and the outer linear shape 343c (see FIG. 2) in the first embodiment.
- the inner arcuate shape 343a and the outer linear shape 343d of the present embodiment smoothly connect in the order of the inner arcuate shape 343a and the outer linear shape 343d from the inside in the fan radial direction Dr.
- the outer linear shape 343d is a linear shape that is inclined with respect to the fan axis CL so that the outer side in the fan radial direction Dr is positioned on the other side in the fan axis direction Da.
- the side plate other surface 343 of this embodiment is formed by one circular arc and one straight line.
- this embodiment is the same as the first embodiment.
- this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to fifth embodiments.
- the side plate other surface 343 of the centrifugal fan 18 faces the other side of the fan axial direction Da and extends in the fan radial direction Dr.
- the outer side in the radial direction Dr is positioned on the other side in the fan axial direction Da.
- the shape of the side plate other surface 343 is different from that in the first embodiment.
- the side plate other surface 343 is inclined with respect to the fan axis CL so that the outer side in the fan radial direction Dr is located on the other side in the fan axis direction Da. It is formed in the shape of a straight line.
- the side plate other surface 343 of this embodiment is formed by one straight line.
- the centrifugal fan 18 can be rotated from one side in the fan axial direction Da while obtaining the noise reduction effect due to the configuration in which the blade trailing edge portion 324 is located on the inner side in the fan radial direction Dr toward one side in the fan axial direction Da.
- the air sucked inside can be guided outward in the fan radial direction Dr.
- this embodiment is the same as the first embodiment.
- this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to fifth embodiments.
- the side plate other surface 343 of the centrifugal fan 18 faces the other side of the fan axial direction Da and extends in the fan radial direction Dr.
- the outer side in the radial direction Dr is positioned on the other side in the fan axial direction Da.
- the shape of the side plate other surface 343 is different from that in the first embodiment.
- the side plate other side surface 343 is formed in a single arc shape extending so as to be located on the other side in the fan axial direction Da toward the outside in the fan radial direction Dr. It is thus, in the longitudinal section of FIG. 17, the side plate other surface 343 of this embodiment is formed by one circular arc.
- this embodiment is the same as the first embodiment.
- this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to fifth embodiments.
- the blade leading edge portion 323 extends from the side plate 34 side to the main plate 36 side, and extends inward in the fan radial direction Dr toward the main plate 36 side. formed to be located.
- the shape of the blade leading edge portion 323 is different from that in the first embodiment.
- the blade leading edge portion 323 of the present embodiment has a third leading edge portion 323c in addition to the first leading edge portion 323a and the second leading edge portion 323b.
- These first front edge portion 323a, second front edge portion 323b and third front edge portion 323c are divided into first front edge portion 323a, second front edge portion 323b and third front edge portion 323c from the side plate 34 side. connected in series in order.
- the third front edge portion 323 c is connected to the main plate 36 and provided between the second front edge portion 323 b and the main plate 36 . Also, the third front edge portion 323c is formed parallel to the fan axis CL in the longitudinal section of FIG.
- this embodiment is the same as the first embodiment.
- this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to eighth embodiments.
- the electric motor 16 of this embodiment has a motor rotor 40 instead of the motor rotor 161 (see FIG. 2) of the first embodiment.
- the centrifugal fan 18 of this embodiment has a main plate outer peripheral portion 43 instead of the main plate 36 of the first embodiment, and a rotor connection portion 44 instead of the rotor connection portion 38 of the first embodiment.
- the plurality of blades 32, the side plates 34, the main plate outer peripheral portion 43, and the rotor connecting portion 44 are integrally constructed.
- an inner peripheral hole 40a corresponding to the inner peripheral hole 36a of the first embodiment is formed in the motor rotor 40 of the present embodiment, and the rotary shaft 14 is fitted into the inner peripheral hole 40a.
- the motor rotor 40 is directly fixed to the rotating shaft 14 and rotates integrally with the rotating shaft 14 around the fan axis CL.
- the motor rotor 40 has a main plate inner peripheral portion 401 and a tubular portion 402 .
- the main plate inner peripheral portion 401 has a disk-like shape that spreads in the fan radial direction Dr around the fan axis CL.
- the main plate inner peripheral portion 401 has an inner peripheral main plate surface 401a.
- the inner peripheral main plate surface 401a is a curved surface that faces one side in the fan axial direction Da and expands in the fan radial direction Dr. formed.
- the inner peripheral portion 401 of the main plate is a part of the motor rotor 40 , but also a part of the centrifugal fan 18 because it has a function of guiding the air sucked by the centrifugal fan 18 .
- FIG. 19 shows a gap between the blade 32 and the main plate inner peripheral portion 401 of the motor rotor 40, but this is for the sake of easy understanding.
- Each blade 32 may be in contact with the main plate inner peripheral portion 401 or may be spaced apart from the main plate inner peripheral portion 401 as shown.
- the cylindrical portion 402 of the motor rotor 40 has a cylindrical shape centered on the fan axis CL, and extends from the radially outer end of the main plate inner peripheral portion 401 toward the other side in the fan axis direction Da.
- a rotor magnet 162 is fixed inside the tubular portion 402 .
- the main plate outer peripheral portion 43 is arranged outside the main plate inner peripheral portion 401 in the fan radial direction Dr, and has a disk-like shape expanding in the fan radial direction Dr around the fan axial center CL. More specifically, the main plate outer peripheral portion 43 continues from the main plate inner peripheral portion 401 and expands outward in the fan radial direction Dr. Therefore, the main plate outer peripheral portion 43 and the main plate inner peripheral portion 401 as a whole correspond to the main plate 36 (see FIG. 2) of the first embodiment.
- the main plate outer peripheral portion 43 has an outer peripheral main plate surface 43a facing one side in the fan axial direction Da.
- the outer peripheral main plate surface 43a continues from the inner peripheral main plate surface 401a and spreads outward in the fan radial direction Dr.
- the blade other end portions 322 of the plurality of blades 32 are respectively connected to the outer peripheral main plate surface 43a.
- the outer peripheral main plate surface 43 a and the inner peripheral main plate surface 401 a as a whole constitute a main plate guide surface 36 b that guides the airflow inside the centrifugal fan 18 .
- the main plate outer peripheral portion 43 has an outer peripheral end portion 431 that is an end portion provided outside in the fan radial direction Dr.
- This outer peripheral end portion 431 corresponds to the main plate outer peripheral end portion 362 (see FIG. 2) of the first embodiment.
- the rotor connecting portion 44 has a cylindrical shape centered on the fan axis CL, and extends from the radially inner end of the main plate outer peripheral portion 43 to the other side in the fan axis direction Da.
- the cylindrical portion 402 of the motor rotor 40 is fitted inside the rotor connecting portion 44 in the radial direction. Thereby, the rotor connecting portion 44 is fixed to the motor rotor 40 .
- the centrifugal fan 18 is fixed to the motor rotor 40 and rotates together with the motor rotor 40 .
- this embodiment is the same as the first embodiment.
- the same effects as in the first embodiment can be obtained from the configuration common to that of the first embodiment.
- this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to ninth embodiments.
- the centrifugal fan 18 is a turbo fan, but it may be another type of centrifugal fan such as a radial fan.
- the electric motor 16 is an outer rotor type brushless DC motor, but the motor type is not limited.
- the electric motor 16 may be an inner rotor type motor or a motor with brushes.
- the second front edge portion 323b extends linearly in the vertical cross sections of FIGS. 2 and 4, but it may be curved.
- the outer diameter Dmo of the main plate 36 and the outer diameter Dso of the side plate 34 are the same size, but this is an example.
- the outer diameter Dmo of the main plate 36 may be larger than the outer diameter Dso of the side plate 34 or may be smaller than the outer diameter Dso of the side plate 34 .
- a fan a plurality of blades (32) arranged side by side around the fan axis and having a blade trailing edge (324) on the radially outer side; a side plate (34) formed with an intake hole (34a) through which air is sucked, provided on the one side of the plurality of blades in the axial direction and connected to each of the plurality of blades; a main plate (36, 43, 401) connected to each of the plurality of blades on the side opposite to the side plate side and extending in the radial direction;
- Dsi/Dso is 0.5 ⁇ Dsi/Dso ⁇ 0.7
- the centrifugal fan wherein the trailing edge portion of the blade is formed so as to be located radially inward toward the one side in the axial direction.
- the side plate has a side plate other surface (343) that faces the other side opposite to the one side in the axial direction and spreads in the radial direction, the other surface of the side plate is located on the other side in the axial direction toward the outer side in the radial direction;
- the centrifugal fan according to the first aspect wherein in a longitudinal section including the fan axis, the radius of curvature of the other surface of the side plate increases toward the outer side in the radial direction.
- the side plate has a side plate other surface (343) that faces the other side opposite to the one side in the axial direction and spreads in the radial direction, the other surface of the side plate is located on the other side in the axial direction toward the outer side in the radial direction;
- the centrifugal fan according to the first aspect wherein the other side surface of the side plate is formed by a single arc or straight line in a longitudinal section including the fan axis.
- each of the plurality of blades has a blade leading edge (323) on the inner side in the radial direction; Any one of the first to third aspects, wherein the leading edge portion of the blade extends from the side plate side to the main plate side and is positioned radially inward toward the main plate side. centrifugal fan described in .
- each of the side plate and the main plate extends outward in the radial direction from the trailing edge of the blade.
- each of the side plate and the main plate extends outward in the radial direction from the trailing edge of the blade; Any one of the first to fifth aspects, wherein a relationship of Db2 ⁇ Dmo ⁇ 1.13 ⁇ Db2 holds, where Db2 is the maximum outer diameter of the plurality of blades and Dmo is the outer diameter of the main plate. 1.
- a centrifugal fan forming part of a blower (10) The blower has a side plate adjacent case (22) provided on the side opposite to the blade side with respect to the side plate and arranged away from the side plate,
- the side plate has an outer peripheral end portion (342) provided on the outer side in the radial direction, and forms a case side plate gap (34b) between the side plate adjacent case and the side plate
- the side plate adjacent case has a case outer peripheral portion (222) provided so as to overlap the outer peripheral end portion of the side plate in the radial direction,
- the first to seventh aspects wherein the outer peripheral edge of the side plate faces the outer peripheral portion of the case in the radial direction, and an opening end (34c) of the gap between the case side plates is formed between the outer peripheral portion of the case and the outer peripheral portion of the case.
- a centrifugal fan according to any one of .
- the blade trailing edge extends from the side plate side to the main plate side, The centrifugal fan according to any one of the first to eighth aspects, wherein the thickness (tb) of each of the plurality of blades increases toward the side plate at the trailing edge of the blade.
- the blade trailing edge In a cross section perpendicular to the fan axis, the blade trailing edge has a convexly curved trailing edge outer surface (324a), and the radius of curvature (Rb) of the trailing edge outer surface increases toward the side plate.
- a centrifugal fan according to the ninth aspect which is enlarged.
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Abstract
This centrifugal fan rotates around the fan axial center (CL) thereof and thereby suctions air from one side in the axial direction (Da) of the fan axial center and blows the suctioned air toward the outside in the radial direction (Dr) of the fan axial center. The centrifugal fan comprises a plurality of blades (32), a side plate (34), and a main plate (36, 43, 401). The plurality of blades are disposed side-by-side around the fan axial center and have a blade rear edge (324) at the outside thereof in the radial direction. The side plate has formed therein an air suction hole (34a) into which air is suctioned, and the side plate is provided at one side in the axial direction relative to the plurality of blades and is linked to each of the plurality of blades. The main plate is linked to each of the plurality of blades at the side opposite of the side plate and widens in the radial direction. In addition: where the inner diameter of the side plate is Dsi and the outer diameter of the side plate is Dso, the relationship Dsi/Dso is 0.5 < Dsi/Dso < 0.7; and the blade rear edges are formed so as to be located further inward in the radial direction the further toward the one side in the axial direction.
Description
本出願は、2021年9月2日に出願された日本特許出願番号2021-143526号と、2022年5月26日に出願された日本特許出願番号2022-86280号とに基づくもので、ここにその記載内容が参照により組み入れられる。
This application is based on Japanese Patent Application No. 2021-143526 filed on September 2, 2021 and Japanese Patent Application No. 2022-86280 filed on May 26, 2022, hereby The contents of which are incorporated by reference.
本開示は、回転することで空気を流す遠心ファンに関するものである。
The present disclosure relates to a centrifugal fan that causes air to flow by rotating.
特許文献1に記載された遠心ファンは、三次元形状の複数のブレード(すなわち、翼)と、主板と、側板とを備えている。その主板には、各翼のスパン方向の一端面が固定され、側板には、各翼のスパン方向の他端面が固定される。
そして、三次元形状の翼において吸込空気流れの主流が側板に沿わずに主板側に偏って吹き出すことに起因して、その吸込空気流れが偏った速度分布を生じ騒音が発生することが、特許文献1に課題として示されている。 The centrifugal fan described inPatent Document 1 includes a plurality of three-dimensional blades (that is, blades), a main plate, and side plates. One spanwise end face of each blade is fixed to the main plate, and the other spanwise end face of each blade is fixed to the side plate.
In addition, in the three-dimensional blade, the main stream of the intake air flow does not follow the side plate and is blown off to the main plate side, and the intake air flow has a biased velocity distribution and noise is generated.Document 1 shows this as a problem.
そして、三次元形状の翼において吸込空気流れの主流が側板に沿わずに主板側に偏って吹き出すことに起因して、その吸込空気流れが偏った速度分布を生じ騒音が発生することが、特許文献1に課題として示されている。 The centrifugal fan described in
In addition, in the three-dimensional blade, the main stream of the intake air flow does not follow the side plate and is blown off to the main plate side, and the intake air flow has a biased velocity distribution and noise is generated.
これに対し、特許文献1の遠心ファンにおいて各翼は、その翼が有する翼後縁部の直径が側板側に比して主板側の方で大きくなるように形成されている。これにより、翼の相互間における主流速度の分布が良化し、騒音が改善するということが、特許文献1に記載されている。
On the other hand, in the centrifugal fan of Patent Document 1, each blade is formed so that the diameter of the trailing edge portion of the blade is larger on the main plate side than on the side plate side. Patent Document 1 describes that this improves the distribution of the mainstream velocity between the blades and reduces the noise.
一般的に、遠心ファンとして、側板の内径(すなわち、遠心ファンの吸気孔の直径)である吸込径を出口径(すなわち、側板の外径)で除して得られる比率であるファン内外径比が種々異なるものが想定される。しかしながら、特許文献1には、そのファン内外径比についての言及がない。
In general, for a centrifugal fan, the ratio of fan inner and outer diameters is the ratio obtained by dividing the suction diameter, which is the inner diameter of the side plate (i.e., the diameter of the intake hole of the centrifugal fan), by the outlet diameter (i.e., the outer diameter of the side plate). are assumed to vary. However, Patent Document 1 does not mention the fan inner/outer diameter ratio.
また、ファン内外径比が小さくなるほど、翼の相互間に形成される空気流路(別言すると、翼間流路)は長くなるので、ファン内外径比が或る程度以上に小さい遠心ファンにおいては、特許文献1に記載されていない空気流れが翼間流路に生じる。
In addition, the smaller the fan inner/outer diameter ratio, the longer the air flow path formed between the blades (in other words, the inter-blade flow path). , an air flow that is not described in Patent Document 1 is generated in the inter-blade flow path.
具体的に、翼間流路の空気流れは、吸気孔付近で側板裏面(すなわち、側板の翼側の面)から剥離して一旦主板側に偏るが、その後、翼間流路の途中で側板に再付着するように流れる。そのため、翼間流路の出口では、空気流れが側板側に偏って流れ、ファンの軸方向で片側に偏った空気流れの速度分布が生じる。そして、その翼間流路の出口付近における偏った空気流れの速度分布に起因した騒音が発生してしまう。このようなことを、発明者らは新たに見出した。
Specifically, the air flow in the inter-blade passage separates from the back surface of the side plate (i.e., the blade-side surface of the side plate) near the intake holes and is once biased toward the main plate. Flow to reattach. Therefore, at the outlet of the inter-blade passage, the air flow is biased toward the side plate, and the air flow velocity distribution is biased to one side in the axial direction of the fan. Then, noise is generated due to the biased airflow velocity distribution near the exit of the inter-blade passage. The inventors have newly discovered this fact.
本開示は上記点に鑑みて、翼間流路の出口付近における偏った空気流れの速度分布に起因した騒音の発生を抑制することが可能な遠心ファンを提供することを目的とする。
In view of the above points, an object of the present disclosure is to provide a centrifugal fan capable of suppressing noise caused by uneven velocity distribution of airflow near the outlet of the inter-blade passage.
上記目的を達成するため、本開示の1つの観点によれば、遠心ファンは、
ファン軸心まわりに回転することでそのファン軸心の軸方向の一方側から空気を吸い込むと共にその吸い込んだ空気をファン軸心の径方向の外側へ吹き出す遠心ファンであって、
ファン軸心まわりに並んで配置され、径方向の外側に翼後縁部を有する複数枚の翼と、
空気が吸い込まれる吸気孔が形成され、複数枚の翼に対して軸方向の一方側に設けられその複数枚の翼のそれぞれに連結された側板と、
複数枚の翼のそれぞれに対し側板側とは反対側で連結され、径方向に拡がる主板とを備え、
側板の内径をDsiとし且つ側板の外径をDsoとした場合に、Dsi/Dsoは、0.5<Dsi/Dso<0.7であり、
翼後縁部は、軸方向の一方側ほど径方向の内側に位置するように形成されている。 In order to achieve the above object, according to one aspect of the present disclosure, a centrifugal fan
A centrifugal fan that rotates around the fan axis to suck air from one side in the axial direction of the fan axis and blow the sucked air outward in the radial direction of the fan axis,
a plurality of blades arranged side by side around the fan axis and having blade trailing edges radially outward;
a side plate provided on one side in the axial direction with respect to the plurality of blades and connected to each of the plurality of blades;
A main plate connected to each of the plurality of blades on the side opposite to the side plate side and extending in the radial direction,
When the inner diameter of the side plate is Dsi and the outer diameter of the side plate is Dso, Dsi/Dso is 0.5<Dsi/Dso<0.7,
The trailing edge portion of the blade is formed so as to be located radially inward toward one side in the axial direction.
ファン軸心まわりに回転することでそのファン軸心の軸方向の一方側から空気を吸い込むと共にその吸い込んだ空気をファン軸心の径方向の外側へ吹き出す遠心ファンであって、
ファン軸心まわりに並んで配置され、径方向の外側に翼後縁部を有する複数枚の翼と、
空気が吸い込まれる吸気孔が形成され、複数枚の翼に対して軸方向の一方側に設けられその複数枚の翼のそれぞれに連結された側板と、
複数枚の翼のそれぞれに対し側板側とは反対側で連結され、径方向に拡がる主板とを備え、
側板の内径をDsiとし且つ側板の外径をDsoとした場合に、Dsi/Dsoは、0.5<Dsi/Dso<0.7であり、
翼後縁部は、軸方向の一方側ほど径方向の内側に位置するように形成されている。 In order to achieve the above object, according to one aspect of the present disclosure, a centrifugal fan
A centrifugal fan that rotates around the fan axis to suck air from one side in the axial direction of the fan axis and blow the sucked air outward in the radial direction of the fan axis,
a plurality of blades arranged side by side around the fan axis and having blade trailing edges radially outward;
a side plate provided on one side in the axial direction with respect to the plurality of blades and connected to each of the plurality of blades;
A main plate connected to each of the plurality of blades on the side opposite to the side plate side and extending in the radial direction,
When the inner diameter of the side plate is Dsi and the outer diameter of the side plate is Dso, Dsi/Dso is 0.5<Dsi/Dso<0.7,
The trailing edge portion of the blade is formed so as to be located radially inward toward one side in the axial direction.
ここで、翼の相互間に形成される空気流路である翼間流路において空気流れは、上記したように、側板から一旦剥離してから側板に再付着するように軸方向の一方側に偏る。これに対し、上記の遠心ファンでは、翼後縁部が軸方向の一方側ほど径方向の内側に位置するように形成されているので、各翼が行う主板側の仕事量を側板側に比して増やし、翼間流路の出口付近で空気流れを主板側に再度引き寄せることができる。その結果、例えば翼後縁部がファン軸心と平行である場合と比較して、翼間流路の出口付近で空気流れの速度分布を、軸方向の偏りが無い分布に近づけることができ、遠心ファンの低騒音化を図ることが可能である。
Here, as described above, in the inter-blade passages, which are the air passages formed between the blades, the air flows along one side in the axial direction so as to once separate from the side plates and then reattach to the side plates. biased. On the other hand, in the centrifugal fan described above, since the trailing edge of the blades is positioned radially inward toward one side in the axial direction, the amount of work performed by each blade on the main plate side is compared to that on the side plate side. , and the air flow can be drawn toward the main plate again in the vicinity of the exit of the interblade passage. As a result, compared to the case where the trailing edge of the blade is parallel to the fan axis, for example, the air flow velocity distribution near the outlet of the inter-blade passage can be brought closer to a distribution free from axial bias, It is possible to reduce the noise of the centrifugal fan.
また、上記の遠心ファンでは、側板の内径をDsiとし且つ側板の外径をDsoとした場合に、Dsi/Dsoは、0.5<Dsi/Dso<0.7である。そのため、翼後縁部がファン軸心に仮に平行であれば翼間流路の空気流れが翼間流路の出口付近で側板側に偏る遠心ファンに対し、翼後縁部が軸方向の一方側ほど径方向の内側に位置する上記構成を用いることができる。従って、その翼後縁部の構成を、遠心ファンの低騒音化を適切に図ることができるように用いることが可能である。
In the above centrifugal fan, Dsi/Dso satisfies 0.5<Dsi/Dso<0.7, where Dsi is the inner diameter of the side plate and Dso is the outer diameter of the side plate. Therefore, if the blade trailing edge is parallel to the fan axis, the air flow in the inter-blade passage is biased toward the side plate near the exit of the inter-blade passage. It is possible to use the above-described configuration in which the side is located radially inward. Therefore, it is possible to use the configuration of the blade trailing edge so as to appropriately reduce the noise of the centrifugal fan.
なお、各構成要素等に付された括弧付きの参照符号は、その構成要素等と後述する実施形態に記載の具体的な構成要素等との対応関係の一例を示すものである。
It should be noted that the reference numerals in parentheses attached to each component etc. indicate an example of the correspondence relationship between the component etc. and the specific component etc. described in the embodiment described later.
以下、図面を参照しながら、各実施形態を説明する。なお、以下の各実施形態相互において、互いに同一もしくは均等である部分には、図中、同一符号を付してある。
Each embodiment will be described below with reference to the drawings. In addition, in each of the following embodiments, the same or equivalent portions are denoted by the same reference numerals in the drawings.
(第1実施形態)
図1および図2に示すように、本実施形態の送風機10は遠心式送風機であり、詳細に言えばターボ型送風機である。送風機10は、その送風機10の筐体であるケーシング12、回転軸14、電動モータ16、電子基板17、遠心ファン18、ベアリング28、およびベアリングハウジング29等を備えている。 (First embodiment)
As shown in FIGS. 1 and 2, theblower 10 of this embodiment is a centrifugal blower, more specifically a turbo blower. The blower 10 includes a casing 12 which is a housing of the blower 10, a rotary shaft 14, an electric motor 16, an electronic substrate 17, a centrifugal fan 18, a bearing 28, a bearing housing 29, and the like.
図1および図2に示すように、本実施形態の送風機10は遠心式送風機であり、詳細に言えばターボ型送風機である。送風機10は、その送風機10の筐体であるケーシング12、回転軸14、電動モータ16、電子基板17、遠心ファン18、ベアリング28、およびベアリングハウジング29等を備えている。 (First embodiment)
As shown in FIGS. 1 and 2, the
なお、図2に示すファン軸心CLは遠心ファン18の回転中心である。また、図2の矢印Daは、ファン軸心CLの軸方向Daすなわちファン軸心方向Daを示している。また、図2の矢印Drは、ファン軸心CLの径方向Drすなわちファン径方向Drを示している。また、図2および後述の図2相当の図では、送風機10のうちファン軸心CLに対する紙面右側の図示が省略されている。
Note that the fan axis CL shown in FIG. 2 is the center of rotation of the centrifugal fan 18 . An arrow Da in FIG. 2 indicates the axial direction Da of the fan axis CL, that is, the fan axis direction Da. An arrow Dr in FIG. 2 indicates the radial direction Dr of the fan axis CL, that is, the fan radial direction Dr. In addition, in FIG. 2 and the figures corresponding to FIG. 2 to be described later, the illustration of the right side of the fan 10 with respect to the fan axis CL is omitted.
ケーシング12は、電動モータ16、電子基板17、および遠心ファン18を、送風機10外部の塵および汚れから保護する。そのために、ケーシング12は、電動モータ16、電子基板17、および遠心ファン18を収容している。また、ケーシング12は、第1ケース部材22と第2ケース部材24とから構成されている。ケーシング12は、送風機10のうち回転しない非回転部材である。
The casing 12 protects the electric motor 16, the electronic board 17, and the centrifugal fan 18 from dust and dirt outside the blower 10. For this purpose, casing 12 houses electric motor 16 , electronic board 17 , and centrifugal fan 18 . Also, the casing 12 is composed of a first case member 22 and a second case member 24 . The casing 12 is a non-rotating member of the blower 10 .
ケーシング12の第1ケース部材22は例えば樹脂で構成されており、遠心ファン18よりも大径であって略円盤形状を成している。第1ケース部材22は、第1カバー部221と第1ケース外周部222と第1周縁部223と複数本の支柱224とから構成されている。
The first case member 22 of the casing 12 is made of, for example, resin, has a larger diameter than the centrifugal fan 18, and has a substantially disk shape. The first case member 22 is composed of a first cover portion 221 , a first case outer peripheral portion 222 , a first peripheral edge portion 223 and a plurality of struts 224 .
第1ケース部材22は、遠心ファン18に対するファン軸心方向Daの一方側で遠心ファン18を覆うカバーである。従って、第1ケース部材22は、遠心ファン18の側板34に対し翼32側とは反対側に設けられている。また、遠心ファン18はケーシング12に対して回転するので、相互の干渉防止のため、第1ケース部材22は、遠心ファン18の側板34から離れて配置されている。第1ケース部材22は、本開示の側板隣接ケースに対応する。
The first case member 22 is a cover that covers the centrifugal fan 18 on one side of the centrifugal fan 18 in the fan axial direction Da. Therefore, the first case member 22 is provided on the side opposite to the blade 32 side with respect to the side plate 34 of the centrifugal fan 18 . Further, since the centrifugal fan 18 rotates with respect to the casing 12, the first case member 22 is arranged away from the side plate 34 of the centrifugal fan 18 in order to prevent mutual interference. The first case member 22 corresponds to the side plate adjacent case of the present disclosure.
第1ケース部材22の第1カバー部221は、ファン径方向Drに拡がった形状を成している。第1カバー部221は、遠心ファン18に対しファン軸心方向Daの一方側に配置され、ファン軸心方向Daにおける遠心ファン18の一方側を覆っている。
The first cover portion 221 of the first case member 22 has a shape expanding in the fan radial direction Dr. The first cover portion 221 is arranged on one side of the centrifugal fan 18 in the fan axial direction Da and covers the one side of the centrifugal fan 18 in the fan axial direction Da.
第1カバー部221の内周側には、第1カバー部221をファン軸心方向Daに貫通した空気吸入口221aが形成されており、空気は、この空気吸入口221aを介して遠心ファン18へ吸い込まれる。また、第1カバー部221は、その空気吸入口221aの周縁を構成するベルマウスとして設けられた吸入口形成部221bを有している。吸入口形成部221bは、その吸入口形成部221bの内側に空気吸入口221aを形成し、送風機10の外部から空気吸入口221aへ流入する空気を円滑に空気吸入口221a内へと導く。
An air intake port 221a is formed on the inner peripheral side of the first cover portion 221 and extends through the first cover portion 221 in the fan axial direction Da. sucked into. Further, the first cover portion 221 has an intake port forming portion 221b provided as a bell mouth forming the periphery of the air intake port 221a. The suction port forming portion 221b forms an air suction port 221a inside the suction port forming portion 221b, and smoothly guides the air flowing into the air suction port 221a from the outside of the blower 10 into the air suction port 221a.
第1ケース部材22の第1ケース外周部222は、第1カバー部221に対するファン径方向Drの外側に配置され、その第1カバー部221に連結している。第1ケース外周部222は、遠心ファン18の側板34よりもファン径方向Drの外側に配置されている。第1ケース外周部222は、本開示のケース外周部に対応する。
The first case outer peripheral portion 222 of the first case member 22 is arranged outside the first cover portion 221 in the fan radial direction Dr and is connected to the first cover portion 221 . The first case outer peripheral portion 222 is arranged outside the side plate 34 of the centrifugal fan 18 in the fan radial direction Dr. The first case perimeter 222 corresponds to the case perimeter of the present disclosure.
図1および図2に示すように、第1ケース部材22の第1周縁部223は、第1ケース外周部222に対しファン径方向Drの外側に設けられ、ファン軸心CLまわりにおいて第1ケース部材22の周縁を構成している。
As shown in FIGS. 1 and 2 , the first peripheral edge portion 223 of the first case member 22 is provided outside the first case outer peripheral portion 222 in the fan radial direction Dr, and extends around the fan axial center CL. It constitutes the periphery of the member 22 .
第1ケース部材22が有する複数本の支柱224はそれぞれ、第1ケース外周部222からケーシング12の内側へファン軸心CLと平行に突き出ている。また、支柱224は、ファン軸心CLと平行な中心軸を有する厚肉の円筒形状を成している。支柱224の内側には、第1ケース部材22と第2ケース部材24とを結合するビス26が挿通されるビス孔が形成されている。
A plurality of struts 224 of the first case member 22 each protrude from the first case outer peripheral portion 222 toward the inside of the casing 12 in parallel with the fan axis CL. Also, the strut 224 has a thick cylindrical shape with a central axis parallel to the fan axis CL. A screw hole through which a screw 26 that joins the first case member 22 and the second case member 24 is inserted is formed inside the support 224 .
第1ケース部材22の各支柱224は、遠心ファン18よりもファン径方向Drの外側に配置されている。そして、第1ケース部材22および第2ケース部材24は、支柱224の先端が第2ケース部材24に突き当てられた状態で、支柱224内に挿通されたビス26によって結合されている。
Each strut 224 of the first case member 22 is arranged outside the centrifugal fan 18 in the fan radial direction Dr. The first case member 22 and the second case member 24 are connected by screws 26 inserted through the support 224 with the tip of the support 224 abutting against the second case member 24 .
第2ケース部材24は、第1ケース部材22と略同じ直径の略円盤形状を成している。第2ケース部材24は、例えば鉄やステンレス等の金属または樹脂で構成されており、電動モータ16および電子基板17を覆うモータハウジングとしても機能する。第2ケース部材24は、第2カバー部241と第2ケース外周部242と第2周縁部243とから構成されている。
The second case member 24 has a substantially disk shape with substantially the same diameter as the first case member 22 . The second case member 24 is made of metal such as iron or stainless steel or resin, and functions also as a motor housing that covers the electric motor 16 and the electronic substrate 17 . The second case member 24 is composed of a second cover portion 241 , a second case outer peripheral portion 242 and a second peripheral edge portion 243 .
第2カバー部241は、遠心ファン18および電動モータ16に対しファン軸心方向Daの他方側に配置され、ファン軸心方向Daにおける遠心ファン18および電動モータ16の他方側を覆っている。
The second cover portion 241 is arranged on the other side in the fan axial direction Da with respect to the centrifugal fan 18 and the electric motor 16, and covers the other side of the centrifugal fan 18 and the electric motor 16 in the fan axial direction Da.
第2ケース部材24の第2ケース外周部242は、第2カバー部241に対するファン径方向Drの外側に配置され、その第2カバー部241に連結している。第2ケース外周部242は、遠心ファン18の主板36よりもファン径方向Drの外側に配置されている。
The second case outer peripheral portion 242 of the second case member 24 is arranged outside the second cover portion 241 in the fan radial direction Dr and is connected to the second cover portion 241 . The second case outer peripheral portion 242 is arranged outside the main plate 36 of the centrifugal fan 18 in the fan radial direction Dr.
第2ケース外周部242と第1ケース外周部222はファン軸心方向Daに相対向するように形成されている。その第2ケース外周部242と第1ケース外周部222との間には、遠心ファン18の吹出口18aから吹き出た空気をファン径方向Drの外側へ流すファン外周流路12bが形成されている。このファン外周流路12bは、遠心ファン18まわりの全周にわたって形成されている。
The second case outer peripheral portion 242 and the first case outer peripheral portion 222 are formed so as to face each other in the fan axial direction Da. Between the second case outer peripheral portion 242 and the first case outer peripheral portion 222, a fan outer peripheral flow path 12b is formed to flow the air blown out from the outlet 18a of the centrifugal fan 18 to the outside in the fan radial direction Dr. . The fan outer peripheral flow path 12b is formed over the entire circumference of the centrifugal fan 18. As shown in FIG.
第2ケース部材24の第2周縁部243は、第2ケース外周部242に対しファン径方向Drの外側に設けられ、ファン軸心CLまわりにおいて第2ケース部材24の周縁を構成している。
The second peripheral edge portion 243 of the second case member 24 is provided outside the second case outer peripheral portion 242 in the fan radial direction Dr, and constitutes the peripheral edge of the second case member 24 around the fan axis CL.
第1周縁部223および第2周縁部243は、ケーシング12において空気を吹き出す空気吹出部を構成している。また、第1周縁部223および第2周縁部243は、ファン軸心方向Daにおける第1周縁部223と第2周縁部243との間に、遠心ファン18から吹き出た空気を吹き出す空気吹出口12aを形成している。この空気吹出口12aは、ファン外周流路12bの空気流れ下流端でもある。
The first peripheral edge portion 223 and the second peripheral edge portion 243 constitute an air blowing portion for blowing air in the casing 12 . In addition, the first peripheral edge portion 223 and the second peripheral edge portion 243 are provided between the first peripheral edge portion 223 and the second peripheral edge portion 243 in the fan axial direction Da, and the air outlet 12a through which the air blown out from the centrifugal fan 18 is blown out. forming The air outlet 12a is also the downstream end of the fan outer peripheral channel 12b.
詳細に言うと、その空気吹出口12aは、送風機10のファン側面に形成され、ファン径方向Drの外側を向いて開口している。そして、空気吹出口12aは、ファン軸心CLを中心としたケーシング12の全周にわたって開口し遠心ファン18からの空気を吹き出す。すなわち、送風機10は、空気吹出口12aがケーシング12の全周にわたって設けられた全周吹出送風機である。なお、支柱224が設けられている箇所では、ケーシング12からの空気の吹出しは支柱224に妨げられるので、空気吹出口12aがケーシング12の全周にわたって開口していることとは、おおよそ全周にわたって開口していることを含む意味である。
Specifically, the air outlet 12a is formed on the side surface of the fan of the blower 10 and opens outward in the fan radial direction Dr. The air outlet 12a is open over the entire circumference of the casing 12 around the fan axis CL, and blows out the air from the centrifugal fan 18. As shown in FIG. That is, the blower 10 is an all-around blower in which the air outlet 12a is provided over the entire circumference of the casing 12 . It should be noted that, at a location where the strut 224 is provided, the blowing of air from the casing 12 is blocked by the strut 224. It is a meaning including opening.
回転軸14は、例えば鉄、ステンレス、または黄銅等の金属で構成されている。回転軸14は、図2に示すように円柱形状の棒材であり、ベアリング28の内輪へ例えば圧入されている。そのため、回転軸14はベアリング28の内輪に対して固定されている。また、ベアリング28の外輪はベアリングハウジング29に対し例えば圧入されることで固定されている。そのベアリングハウジング29は、例えばアルミニウム合金、黄銅、鉄、またはステンレス等の金属で構成され、第2カバー部241に固定されている。
The rotating shaft 14 is made of metal such as iron, stainless steel, or brass. The rotating shaft 14 is a columnar bar as shown in FIG. 2, and is press-fitted into the inner ring of the bearing 28, for example. Therefore, the rotating shaft 14 is fixed with respect to the inner ring of the bearing 28 . Also, the outer ring of the bearing 28 is fixed to the bearing housing 29 by, for example, being press-fitted. The bearing housing 29 is made of metal such as aluminum alloy, brass, iron, or stainless steel, and is fixed to the second cover portion 241 .
従って、回転軸14は、第2カバー部241に対してベアリング28を介して支持されている。すなわち、回転軸14は、第2カバー部241に対し、ファン軸心CLを中心として回転自在になっている。
Therefore, the rotating shaft 14 is supported by the second cover portion 241 via the bearings 28 . That is, the rotary shaft 14 is rotatable about the fan axis CL with respect to the second cover portion 241 .
それと共に、回転軸14が有するファン軸心方向Daの一方側の端部が、遠心ファン18が有する主板36の内周孔36aに嵌め入れられ、これにより、遠心ファン18は、回転軸14に対して固定されている。すなわち、遠心ファン18は、ファン軸心CLを中心として回転軸14と一体的に回転する。
At the same time, one end of the rotating shaft 14 in the fan axial direction Da is fitted into the inner peripheral hole 36 a of the main plate 36 of the centrifugal fan 18 . fixed against. That is, the centrifugal fan 18 rotates integrally with the rotary shaft 14 around the fan axis CL.
電動モータ16はアウターロータ型ブラシレスDCモータである。電動モータ16は電子基板17と共に、ファン軸心方向Daにおいて遠心ファン18の主板36と第2カバー部241との間に配置されている。そして、電動モータ16は、モータロータ161とロータマグネット162とモータステータ163とを備えている。モータロータ161は鋼板等の金属で構成され、例えばその鋼板がプレス成形されることによって形成されている。
The electric motor 16 is an outer rotor type brushless DC motor. The electric motor 16 is arranged together with the electronic board 17 between the main plate 36 of the centrifugal fan 18 and the second cover portion 241 in the fan axial direction Da. The electric motor 16 has a motor rotor 161 , a rotor magnet 162 and a motor stator 163 . The motor rotor 161 is made of metal such as a steel plate, and is formed, for example, by press forming the steel plate.
ロータマグネット162は永久磁石であって、例えばフェライトやネオジム等を含むゴムマグネットで構成されている。そのロータマグネット162はモータロータ161に一体固定されている。また、モータロータ161は、遠心ファン18のロータ連結部38に固定されている。すなわち、モータロータ161およびロータマグネット162は、ファン軸心CLを中心として遠心ファン18と一体的に回転する。
The rotor magnet 162 is a permanent magnet, and is composed of, for example, a rubber magnet containing ferrite, neodymium, or the like. The rotor magnet 162 is integrally fixed to the motor rotor 161 . Also, the motor rotor 161 is fixed to the rotor connecting portion 38 of the centrifugal fan 18 . That is, the motor rotor 161 and the rotor magnet 162 rotate integrally with the centrifugal fan 18 about the fan axis CL.
モータステータ163は、電子基板17に電気的に接続されたステータコイル163aおよびステータコア163bを含んで構成されている。モータステータ163は、ロータマグネット162に対し微小な隙間を空けて径方向内側に配置されている。そして、モータステータ163は、ベアリングハウジング29を介して第2ケース部材24の第2カバー部241に固定されている。電子基板17には不図示の複数の電気部品が実装されており、例えば、電動モータ16を回転駆動するための電気回路などが電子基板17に構成されている。
The motor stator 163 includes a stator coil 163a and a stator core 163b electrically connected to the electronic board 17. The motor stator 163 is arranged radially inside the rotor magnet 162 with a small gap therebetween. The motor stator 163 is fixed to the second cover portion 241 of the second case member 24 via the bearing housing 29 . A plurality of electric components (not shown) are mounted on the electronic board 17 . For example, an electric circuit for rotating the electric motor 16 is configured on the electronic board 17 .
このように構成された電動モータ16では、モータステータ163のステータコイル163aへ外部電源から通電されると、そのステータコイル163aによってステータコア163bに磁束変化が生じる。そして、そのステータコア163bでの磁束変化は、ロータマグネット162を引き寄せる力を発生する。モータロータ161は、ベアリング28により回転可能に支持されている回転軸14に対して固定されているので、上記ロータマグネット162を引き寄せる力を受けてファン軸心CLまわりに回転運動をする。要するに、電動モータ16は、通電されることにより、モータロータ161が固定された遠心ファン18をファン軸心CLまわりに回転させる。
In the electric motor 16 configured in this way, when the stator coil 163a of the motor stator 163 is energized from an external power supply, the stator coil 163a causes a magnetic flux change in the stator core 163b. A magnetic flux change in the stator core 163 b generates a force that attracts the rotor magnet 162 . Since the motor rotor 161 is fixed to the rotating shaft 14 rotatably supported by the bearing 28, it rotates around the fan axis CL under the force of attracting the rotor magnet 162. As shown in FIG. In short, when the electric motor 16 is energized, it rotates the centrifugal fan 18 to which the motor rotor 161 is fixed around the fan axis CL.
遠心ファン18は、図2、図3に示すように、送風機10に適用されるインペラである。遠心ファン18は、所定のファン回転方向DRfへファン軸心CLまわりに回転することで送風する。すなわち、遠心ファン18は、ファン軸心CLまわりに回転することにより、矢印FLaのようにファン軸心方向Daの一方側から空気吸入口221aを介して空気を吸い込む。そして、遠心ファン18は、遠心ファン18の径方向外側へ矢印FLbのように、その吸い込んだ空気を吹き出す。
The centrifugal fan 18 is an impeller applied to the blower 10, as shown in FIGS. The centrifugal fan 18 blows air by rotating around the fan axis CL in a predetermined fan rotation direction DRf. That is, the centrifugal fan 18 rotates around the fan axis CL to draw air from one side in the fan axis direction Da through the air intake port 221a as indicated by the arrow FLa. Then, the centrifugal fan 18 blows out the sucked air radially outward of the centrifugal fan 18 as indicated by an arrow FLb.
具体的に、本実施形態の遠心ファン18はターボファンである。そして、遠心ファン18は、複数枚の翼32と側板34と主板36とロータ連結部38とを有している。遠心ファン18は例えば樹脂製であり、その複数枚の翼32と側板34と主板36とロータ連結部38は一体構成になっている。
Specifically, the centrifugal fan 18 of this embodiment is a turbo fan. The centrifugal fan 18 has a plurality of blades 32 , side plates 34 , main plates 36 and rotor connecting portions 38 . The centrifugal fan 18 is made of resin, for example, and its plurality of blades 32, side plates 34, main plate 36, and rotor connecting portion 38 are integrally constructed.
複数枚の翼32は、ファン軸心CLまわりに配置されている。詳細には、複数枚の翼32は、互いの間に空気が流れる間隔を空けつつ、ファン軸心CLの周方向Dcへ並んで配置されている。翼32はファンブレードとも称される。
A plurality of blades 32 are arranged around the fan axis CL. Specifically, the plurality of blades 32 are arranged side by side in the circumferential direction Dc of the fan axial center CL while leaving an interval for air flow between them. Airfoils 32 are also referred to as fan blades.
また、翼32はそれぞれ、翼32のうちファン軸心方向Daの一方側に設けられた翼一端部321と、翼32のうちファン軸心方向Daの一方側とは反対側の他方側に設けられた翼他端部322とを有している。複数枚の翼32は、その複数枚の翼32のうち互いに隣り合う翼32同士の間にそれぞれ、空気が流れる翼間流路32aを形成している。
The blades 32 are provided on one side of the blades 32 in the fan axial direction Da, and on the other side of the blades 32 opposite to the one side in the fan axial direction Da. and a wing other end portion 322 which is closed. The plurality of blades 32 form inter-blade passages 32a through which air flows between adjacent blades 32 among the plurality of blades 32 .
側板34は、図2、図3に示すように、ファン径方向Drへ円盤状に拡がる形状を成している。そして、その側板34の径方向内側には、ケーシング12の空気吸入口221aからの空気が矢印FLaのように吸い込まれる吸気孔34aが形成されている。従って、側板34は、ファン軸心CLを中心とした環形状を成している。
As shown in FIGS. 2 and 3, the side plate 34 has a disk shape that expands in the fan radial direction Dr. An air intake hole 34a through which air from the air intake port 221a of the casing 12 is sucked as indicated by an arrow FLa is formed inside the side plate 34 in the radial direction. Therefore, the side plate 34 has an annular shape around the fan axis CL.
また、側板34は、側板内周端部341と側板外周端部342とを有している。その側板内周端部341は、側板34のうちファン径方向Drの内側に設けられた端部であり、吸気孔34aを形成している。また、側板外周端部342は、側板34のうちファン径方向Drの外側に設けられた端部である。側板外周端部342は、側板34が有する本開示の外周端部に対応する。
In addition, the side plate 34 has a side plate inner peripheral end portion 341 and a side plate outer peripheral end portion 342 . The side plate inner peripheral end portion 341 is an end portion provided inside the side plate 34 in the fan radial direction Dr, and forms the intake hole 34a. The side plate outer peripheral end portion 342 is an end portion of the side plate 34 provided on the outside in the fan radial direction Dr. The side plate outer peripheral edge 342 corresponds to the outer peripheral edge of the present disclosure that the side plate 34 has.
また、側板34は、複数枚の翼32に対しファン軸心方向Daの一方側すなわち空気吸入口221a側に設けられている。それと共に、側板34は、その複数枚の翼32のそれぞれに連結されている。言い換えれば、側板34は、その翼32のそれぞれに対し翼一端部321にて連結されている。
Also, the side plate 34 is provided on one side of the plurality of blades 32 in the fan axial direction Da, that is, on the side of the air intake port 221a. Along with that, the side plate 34 is connected to each of the plurality of wings 32 . In other words, the side plate 34 is connected to each of its blades 32 at one blade end 321 .
また、側板34は、ファン軸心方向Daの他方側を向いた側板他方面343を有している。この側板他方面343は翼間流路32aに面しており、遠心ファン18内の気流を案内する。側板他方面343は、ファン径方向Drに拡がる湾曲面であり、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置する。そして、ファン軸心CLを含む縦断面である図2の断面において、側板他方面343の曲率半径はファン径方向Drの外側ほど大きくなる。
The side plate 34 also has a side plate other surface 343 facing the other side in the fan axial direction Da. This side plate other surface 343 faces the inter-blade flow path 32 a and guides the airflow inside the centrifugal fan 18 . The side plate other surface 343 is a curved surface that expands in the fan radial direction Dr, and is located on the other side in the fan axial direction Da toward the outside in the fan radial direction Dr. 2, which is a longitudinal section including the fan axis CL, the radius of curvature of the side plate other surface 343 increases toward the outer side in the fan radial direction Dr.
例えば本実施形態では、図2に示す送風機10の縦断面において、側板他方面343は、内側円弧形状343aと外側円弧形状343bと外側直線形状343cとを有している。これらの内側円弧形状343aと外側円弧形状343bと外側直線形状343cは、ファン径方向Drの内側から、内側円弧形状343a、外側円弧形状343b、外側直線形状343cの順に滑らかに連なっている。そして、外側円弧形状343bの曲率半径R2は内側円弧形状343aの曲率半径R1よりも大きく、外側直線形状343cは、ファン軸心CLに垂直な直線状になっている。
For example, in this embodiment, in the vertical cross section of the fan 10 shown in FIG. 2, the side plate other surface 343 has an inner arc shape 343a, an outer arc shape 343b, and an outer linear shape 343c. The inner arc shape 343a, the outer arc shape 343b, and the outer linear shape 343c are smoothly connected in the order of the inner arc shape 343a, the outer arc shape 343b, and the outer linear shape 343c from the inside in the fan radial direction Dr. The curvature radius R2 of the outer arcuate shape 343b is larger than the curvature radius R1 of the inner arcuate shape 343a, and the outer linear shape 343c is linear perpendicular to the fan axis CL.
主板36は、ファン軸心CLまわりに回転可能な回転軸14に固定されているので、ケーシング12に対してファン軸心CLまわりに回転可能に支持されている。主板36は、ファン軸心CLを中心としてファン径方向Drへ円盤状に拡がった形状を成している。
Since the main plate 36 is fixed to the rotating shaft 14 rotatable around the fan axis CL, it is supported rotatably around the fan axis CL with respect to the casing 12 . The main plate 36 has a disk-like shape extending in the fan radial direction Dr around the fan axis CL.
また、主板36は、複数枚の翼32のそれぞれに対し側板34側とは反対側に連結されている。すなわち、主板36は、複数枚の翼32のそれぞれに対し翼他端部322にて連結されている。
Also, the main plate 36 is connected to each of the plurality of blades 32 on the side opposite to the side plate 34 side. That is, the main plate 36 is connected to each of the plurality of blades 32 at the blade other end portion 322 .
また、主板36は、遠心ファン18内の気流を案内する主板案内面36bを有している。主板案内面36bは翼間流路32aに面し、側板他方面343に対しその翼間流路32aを挟んで対向している。そして、主板案内面36bは、ファン軸心方向Daの一方側を向いてファン径方向Drへ拡がる湾曲面であり、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置するように形成されている。このような形状により、主板案内面36bは、空気吸入口221aへ吸い込まれファン軸心方向Daを向いた空気流れをファン径方向Drの外側へ向くように案内する。
The main plate 36 also has a main plate guide surface 36b that guides the airflow inside the centrifugal fan 18. The main plate guide surface 36b faces the inter-blade passage 32a and faces the other side plate surface 343 across the inter-blade passage 32a. The main plate guide surface 36b is a curved surface that faces one side in the fan axial direction Da and expands in the fan radial direction Dr, and is located on the other side in the fan axial direction Da toward the outside in the fan radial direction Dr. formed. With such a shape, the main plate guide surface 36b guides the airflow sucked into the air inlet 221a and directed in the fan axial direction Da so as to be directed outward in the fan radial direction Dr.
また、主板36を回転軸14に固定するために、主板36の径方向内側には、主板36をファン軸心方向Daへ貫通した内周孔36aが形成されている。
Further, in order to fix the main plate 36 to the rotating shaft 14, an inner peripheral hole 36a is formed radially inside the main plate 36 so as to penetrate the main plate 36 in the fan axial direction Da.
ロータ連結部38は、ファン軸心CLを中心とした円筒状のリブであり、主板36からファン軸心方向Daの他方側へ突き出ている。このロータ連結部38の径方向内側には、モータロータ161が嵌め込まれて格納されている。これにより、ロータ連結部38は、モータロータ161に固定される。そして、ロータ連結部38がモータロータ161に固定されることにより、遠心ファン18は、そのモータロータ161に固定されている。
The rotor connecting portion 38 is a cylindrical rib centered on the fan axis CL, and protrudes from the main plate 36 to the other side in the fan axis direction Da. A motor rotor 161 is fitted and stored inside the rotor connecting portion 38 in the radial direction. Thereby, the rotor connecting portion 38 is fixed to the motor rotor 161 . By fixing the rotor connecting portion 38 to the motor rotor 161 , the centrifugal fan 18 is fixed to the motor rotor 161 .
また、主板36は、主板外周端部362を有している。その主板外周端部362は、主板36のうちファン径方向Drの外側に設けられた端部である。主板外周端部362と側板外周端部342は、ファン軸心方向Daにおいて互いに離れて配置されている。そして、主板外周端部362と側板外周端部342は、翼間流路32aを通過した空気が吹き出る吹出口18aを、その主板外周端部362と側板外周端部342との間に形成している。すなわち、主板外周端部362と側板外周端部342は、遠心ファン18のうち、吹出口18aが形成された空気吹出部を構成している。遠心ファン18の吹出口18aは、ファン径方向Drの外側を向いて開口しており、ファン軸心CLを中心とした遠心ファン18の全周にわたって形成されている。
In addition, the main plate 36 has a main plate outer peripheral end portion 362 . The main plate outer peripheral end portion 362 is an end portion of the main plate 36 provided outside in the fan radial direction Dr. The main plate outer peripheral end portion 362 and the side plate outer peripheral end portion 342 are arranged apart from each other in the fan axial direction Da. The main plate outer peripheral end portion 362 and the side plate outer peripheral end portion 342 form the outlet 18a from which the air that has passed through the inter-blade passage 32a is blown out between the main plate outer peripheral end portion 362 and the side plate outer peripheral end portion 342. there is That is, the main plate outer peripheral end portion 362 and the side plate outer peripheral end portion 342 constitute an air blowing portion of the centrifugal fan 18 in which the blowing port 18a is formed. The blowout port 18a of the centrifugal fan 18 faces outward in the fan radial direction Dr and is formed along the entire circumference of the centrifugal fan 18 around the fan axis CL.
本実施形態では、ファン径方向Drにおける主板外周端部362の位置は側板外周端部342の位置に揃えられている。すなわち、図2、図4に示すように、主板36の外径Dmoと側板34の外径Dsoは同じ大きさであり、遠心ファン18の外径Doutとなっている。
In this embodiment, the position of the main plate outer peripheral end portion 362 in the fan radial direction Dr is aligned with the position of the side plate outer peripheral end portion 342 . That is, as shown in FIGS. 2 and 4, the outer diameter Dmo of the main plate 36 and the outer diameter Dso of the side plate 34 are the same size, which is the outer diameter Dout of the centrifugal fan 18 .
また、側板34の外径Dsoに対する側板34の内径Dsiの比率である側板内外径比はDsi/Dsoで算出され、本実施形態において、そのDsi/Dsoは、「0.5<Dsi/Dso<0.7」となっている。詳細にいうと、本実施形態では、そのDsi/Dsoは、「Dsi/Dso=0.55」である。なお、側板34の内径Dsiは、別言すれば、側板34に形成された吸気孔34aの直径でもある。
The side plate inner/outer diameter ratio, which is the ratio of the inner diameter Dsi of the side plate 34 to the outer diameter Dso of the side plate 34, is calculated by Dsi/Dso. 0.7". Specifically, in this embodiment, the Dsi/Dso is "Dsi/Dso=0.55". In other words, the inner diameter Dsi of the side plate 34 is also the diameter of the intake hole 34 a formed in the side plate 34 .
図2、図4に示すように、複数枚の翼32はそれぞれ、ファン径方向Drの内側に設けられた翼前縁部323と、ファン径方向Drの外側に設けられた翼後縁部324とを有している。その翼前縁部323とは、翼32のうち、吸気孔34aを通過して翼間流路32aに流れる空気の気流方向における上流側に構成された端縁部である。また、翼後縁部324とは、翼32のうち、その翼間流路32aに流れる空気の気流方向における下流側に構成された端縁部である。
As shown in FIGS. 2 and 4, each of the plurality of blades 32 has a blade leading edge portion 323 provided on the inner side in the fan radial direction Dr and a blade trailing edge portion 324 provided on the outer side in the fan radial direction Dr. and The leading edge portion 323 of the blade is an edge portion formed on the upstream side in the airflow direction of the air passing through the intake hole 34a and flowing into the inter-blade passage 32a. The blade trailing edge portion 324 is an edge portion formed on the downstream side of the blade 32 in the airflow direction of the air flowing through the inter-blade passage 32a.
翼前縁部323は、側板34と主板36とに連結し、側板34側から主板36側へと延びている。そして、翼後縁部324も、側板34と主板36とに連結し、側板34側から主板36側へと延びている。
The blade leading edge portion 323 is connected to the side plate 34 and the main plate 36 and extends from the side plate 34 side to the main plate 36 side. A blade trailing edge 324 is also connected to the side plate 34 and the main plate 36 and extends from the side plate 34 side to the main plate 36 side.
翼前縁部323は、主板36側ほどファン径方向Drの内側に位置するように形成されている。具体的に、翼前縁部323は、第1前縁部323aと第2前縁部323bとを含んで構成されている。その第1前縁部323aと第2前縁部323bはそれぞれ直線的に延びるように形成され、第1前縁部323aと第2前縁部323bは直列に連結されている。そして、第1前縁部323aは側板34に連結されている。第2前縁部323bは主板36に連結され、第1前縁部323aと主板36との間に設けられている。
The blade leading edge portion 323 is formed so as to be located inside in the fan radial direction Dr toward the main plate 36 side. Specifically, the blade leading edge portion 323 includes a first leading edge portion 323a and a second leading edge portion 323b. The first front edge portion 323a and the second front edge portion 323b are formed to extend linearly, and the first front edge portion 323a and the second front edge portion 323b are connected in series. The first front edge portion 323 a is connected to the side plate 34 . The second front edge portion 323 b is connected to the main plate 36 and provided between the first front edge portion 323 a and the main plate 36 .
また、第2前縁部323bがファン軸心CLに対して成す角度は、第1前縁部323aがファン軸心CLに対して成す角度よりも小さい。詳細には、図2、図4の縦断面において、第1前縁部323aは、ファン軸心CLに対して垂直な向きで直線的に延伸している。そして、第2前縁部323bは、ファン軸心方向Daの一方側ほどファン径方向Drの外側に位置するようにファン軸心CLに対して傾いて直線的に延伸している。
Also, the angle formed by the second front edge portion 323b with respect to the fan axis CL is smaller than the angle formed with the first front edge portion 323a with respect to the fan axis CL. Specifically, in the vertical cross sections of FIGS. 2 and 4, the first front edge portion 323a extends linearly in a direction perpendicular to the fan axis CL. Further, the second front edge portion 323b extends linearly while being inclined with respect to the fan axis CL so as to be located outside in the fan radial direction Dr toward one side in the fan axis direction Da.
従って、第2前縁部323bの一方側直径Df1の方が第2前縁部323bの他方側直径Df2よりも大きい。その第2前縁部323bの一方側直径Df1とは、第2前縁部323bがファン軸心方向Daの一方側の端にて有するファン軸心CLを中心とした直径である。また、第2前縁部323bの他方側直径Df2とは、第2前縁部323bがファン軸心方向Daの他方側の端にて有するファン軸心CLを中心とした直径である。
Therefore, the one-side diameter Df1 of the second front edge portion 323b is larger than the other-side diameter Df2 of the second front edge portion 323b. The one-side diameter Df1 of the second front edge portion 323b is a diameter around the fan axis CL that the second front edge portion 323b has at one end in the fan axis direction Da. The other side diameter Df2 of the second front edge portion 323b is a diameter centered on the fan axis CL that the second front edge portion 323b has at the other side end in the fan axis direction Da.
翼後縁部324は、ファン軸心方向Daの一方側ほどファン径方向Drの内側に位置するように延びている。具体的には、図2、図4の縦断面において、翼後縁部324は、側板34側が主板36側に対しファン径方向Drの内側に位置するようにファン軸心CLに対して傾いた直線状に形成されている。
The trailing edge portion 324 of the blade extends toward the inside in the fan radial direction Dr toward one side in the fan axial direction Da. Specifically, in the vertical cross sections of FIGS. 2 and 4, the blade trailing edge portion 324 is inclined with respect to the fan axis CL such that the side plate 34 side is located inside the main plate 36 side in the fan radial direction Dr. It is formed linearly.
従って、翼後縁部324の一方側直径Db1の方が翼後縁部324の他方側直径Db2よりも小さい。その翼後縁部324の一方側直径Db1とは、翼後縁部324がファン軸心方向Daの一方側の端にて有するファン軸心CLを中心とした直径である。また、翼後縁部324の他方側直径Db2とは、翼後縁部324がファン軸心方向Daの他方側の端にて有するファン軸心CLを中心とした直径である。
Therefore, the one side diameter Db1 of the blade trailing edge portion 324 is smaller than the other side diameter Db2 of the blade trailing edge portion 324. The one-side diameter Db1 of the blade trailing edge portion 324 is the diameter of the blade trailing edge portion 324 at one end in the fan axial direction Da centered on the fan axial center CL. Further, the other side diameter Db2 of the blade trailing edge portion 324 is a diameter around the fan axis CL that the blade trailing edge portion 324 has at the other side end in the fan axis direction Da.
図2、図4に示すように、翼後縁部324の他方側直径Db2は、ファン軸心CLを中心とした翼32の最大外径でもある。その翼後縁部324の他方側直径Db2と主板36の外径Dmoとの間では、「Db2<Dmo≦1.13×Db2」の関係が成立する。詳細にいうと、本実施形態では、翼後縁部324の他方側直径Db2と主板36の外径Dmoとの関係は、「Dmo=1.06×Db2」となっている。
As shown in FIGS. 2 and 4, the other side diameter Db2 of the blade trailing edge portion 324 is also the maximum outer diameter of the blade 32 around the fan axis CL. Between the other side diameter Db2 of the blade trailing edge portion 324 and the outer diameter Dmo of the main plate 36, a relationship of "Db2<Dmo≦1.13×Db2" is established. Specifically, in this embodiment, the relationship between the other side diameter Db2 of the blade trailing edge portion 324 and the outer diameter Dmo of the main plate 36 is "Dmo=1.06×Db2".
また、図2、図4に示すように、翼前縁部323の一部は、翼後縁部324がファン軸心方向Daに占める全幅Hbに含まれる軸方向範囲Hb1内に入っている。その軸方向範囲Hb1内に入っている翼前縁部323の一部は、詳細には、第2前縁部323bのうち主板36側の端を含む一部である。
Also, as shown in FIGS. 2 and 4, part of the blade leading edge 323 falls within an axial range Hb1 included in the full width Hb of the blade trailing edge 324 in the fan axial direction Da. The portion of the blade leading edge portion 323 within the axial range Hb1 is, in detail, a portion of the second leading edge portion 323b including the end on the main plate 36 side.
側板他方面343のうち側板内周端部341からファン径方向Drの外側へ拡がり始める部位Psiが主板案内面36bに対しファン軸心方向Daに沿って有する軸方向高さH2と、側板34の外径Dsoは、「0.06<H2/Dso<0.20」の関係にある。詳細にいうと、本実施形態では、そのH2/Dsoは、「H2/Dso=0.082」である。
A portion Psi of the side plate other surface 343 that starts expanding outward in the fan radial direction Dr from the side plate inner peripheral end portion 341 has an axial height H2 along the fan axial direction Da with respect to the main plate guide surface 36b, The outer diameter Dso has a relationship of "0.06<H2/Dso<0.20". Specifically, in this embodiment, the H2/Dso is "H2/Dso=0.082".
また、本実施形態の遠心ファン18では、翼後縁部324は、側板外周端部342よりもファン径方向Drの内側で側板34に連結している。それと共に、翼後縁部324は、主板外周端部362よりもファン径方向Drの内側で主板36に連結している。つまり、側板34と主板36はそれぞれ、翼後縁部324よりもファン径方向Drの外側にまで延びている。具体的に言うと、側板34の外径Dsoと翼後縁部324の一方側直径Db1との大小関係は、「Dso>Db1」であり、主板36の外径Dmoと翼後縁部324の他方側直径Db2との大小関係は、「Dmo>Db2」である。
Further, in the centrifugal fan 18 of the present embodiment, the blade trailing edge portion 324 is connected to the side plate 34 inside the side plate outer peripheral end portion 342 in the fan radial direction Dr. At the same time, the blade trailing edge portion 324 is connected to the main plate 36 inside the main plate outer peripheral end portion 362 in the fan radial direction Dr. That is, the side plate 34 and the main plate 36 each extend outside the blade trailing edge portion 324 in the fan radial direction Dr. Specifically, the size relationship between the outer diameter Dso of the side plate 34 and the one-side diameter Db1 of the blade trailing edge portion 324 is "Dso>Db1". The size relationship with the other side diameter Db2 is "Dmo>Db2".
上記したように第1ケース部材22は遠心ファン18の側板34から離れて配置されているので、その側板34は、第1ケース部材22との間にケース側板隙間34bを形成している。例えば、このケース側板隙間34bは、第1ケース部材22と遠心ファン18との干渉を防止できる範囲で出来るだけ狭い隙間となるように形成されている。
As described above, since the first case member 22 is arranged away from the side plate 34 of the centrifugal fan 18, the side plate 34 forms a case side plate clearance 34b between itself and the first case member 22. For example, the case side plate gap 34b is formed to be as narrow a gap as possible within a range where interference between the first case member 22 and the centrifugal fan 18 can be prevented.
また、第1ケース外周部222は、第1カバー部221から延設されて、側板外周端部342に対しファン径方向Drの外側に重なるように設けられている。そして、第1ケース外周部222の内径Dc1は側板34の外径Dsoよりも大きい。そのため、側板外周端部342は、第1ケース外周部222に対しファン径方向Drに対向し、ケース側板隙間34bの開口端34cを第1ケース外周部222との間に形成している。ケース側板隙間34bの開口端34cはケーシング12の空気吹出口12aよりもファン径方向Drの内側に位置し、ケース側板隙間34bは、この開口端34cでファン外周流路12bに連結している。
Further, the first case outer peripheral portion 222 extends from the first cover portion 221 and is provided so as to overlap the side plate outer peripheral end portion 342 on the outside in the fan radial direction Dr. The inner diameter Dc1 of the first case outer peripheral portion 222 is larger than the outer diameter Dso of the side plate 34 . Therefore, the side plate outer peripheral end portion 342 faces the first case outer peripheral portion 222 in the fan radial direction Dr, and forms an opening end 34c of the case side plate gap 34b between the first case outer peripheral portion 222 and the first case outer peripheral portion 222 . An open end 34c of the case side plate gap 34b is located inside the fan radial direction Dr from the air outlet 12a of the casing 12, and the case side plate gap 34b is connected to the fan outer peripheral flow path 12b at the open end 34c.
本実施形態では図5、図6に示すように、翼後縁部324において翼32の厚みtbは一定ではない。具体的に、翼32の厚みtbは、翼後縁部324では側板34側ほど大きくなっている。例えば、翼後縁部324のうち側板34に連結する部位での翼32の厚みtbである側板側後縁厚みtb1は、翼後縁部324のうち主板36に連結する部位での翼32の厚みtbである主板側後縁厚みtb2よりも大きくなっている。
In this embodiment, as shown in FIGS. 5 and 6, the thickness tb of the blade 32 is not constant at the blade trailing edge portion 324 . Specifically, the thickness tb of the blade 32 increases toward the side plate 34 at the blade trailing edge portion 324 . For example, the side plate side trailing edge thickness tb1, which is the thickness tb of the blade 32 at the portion of the blade trailing edge portion 324 connected to the side plate 34, is the thickness of the blade 32 at the portion of the blade trailing edge portion 324 connected to the main plate 36. It is larger than the main plate side trailing edge thickness tb2, which is the thickness tb.
このように、翼後縁部324において翼32の厚みtbが軸方向位置に応じて変化しているので、これに合わせて、翼後縁部324の表面形状も軸方向位置に応じて変化している。なお、図6において翼32周りの空気流れは破線で表されている。
Since the thickness tb of the blade 32 at the blade trailing edge portion 324 changes according to the axial position, the surface shape of the blade trailing edge portion 324 also changes according to the axial position. ing. In addition, in FIG. 6, the air flow around the blade 32 is represented by a dashed line.
詳細には、図6に示すように、翼後縁部324は、その翼後縁部324の表面である後縁部外面324aを有している。そして、その後縁部外面324aは、翼32の正圧面と負圧面とを翼後縁部324にて連結し、ファン軸心CLに垂直な横断面において凸状に湾曲している。更に、その横断面において、後縁部外面324aの曲率半径Rbは側板34側ほど大きくなっている。例えば、翼後縁部324のうち側板34に連結する部位での後縁部外面324aの曲率半径Rbである側板側曲率半径Rb1は、翼後縁部324のうち主板36に連結する部位での上記曲率半径Rbである主板側曲率半径Rb2よりも大きくなっている。
Specifically, as shown in FIG. 6 , the blade trailing edge 324 has a trailing edge outer surface 324 a that is the surface of the blade trailing edge 324 . A trailing edge outer surface 324a connects the pressure surface and the suction surface of the blade 32 at the blade trailing edge 324, and is convexly curved in a cross section perpendicular to the fan axis CL. Furthermore, in its cross section, the radius of curvature Rb of the rear edge portion outer surface 324a increases toward the side plate 34 side. For example, the side plate side curvature radius Rb1, which is the curvature radius Rb of the trailing edge outer surface 324a at the portion of the blade trailing edge portion 324 connected to the side plate 34, is the radius of curvature Rb1 at the portion of the blade trailing edge portion 324 connected to the main plate 36. It is larger than the main plate side curvature radius Rb2, which is the curvature radius Rb.
なお、図5には、本実施形態と比較される比較例の遠心ファンが有する翼後縁部91が破線で示されている。その比較例の遠心ファンでは、翼後縁部91がファン軸心CLに平行とされ、その翼後縁部91における翼32の厚みtbが一定とされている。これらの点を除き、比較例の遠心ファンは本実施形態の遠心ファン18と同じである。
In FIG. 5, the blade trailing edge portion 91 of the centrifugal fan of the comparative example compared with the present embodiment is indicated by broken lines. In the centrifugal fan of the comparative example, the trailing edge portion 91 of the blade is parallel to the fan axis CL, and the thickness tb of the blade 32 at the trailing edge portion 91 of the blade is constant. Except for these points, the centrifugal fan of the comparative example is the same as the centrifugal fan 18 of this embodiment.
以上のように構成された遠心ファン18は、図2、図3に示すようにモータロータ161と一体にファン回転方向DRfへ回転運動する。それに伴い、遠心ファン18の翼32が空気に運動量を与えるので、遠心ファン18は、吸気孔34aから矢印FLaのように空気を吸い込み、その吸い込まれた空気は、矢印FL1、FL2、FL3のように翼間流路32aを径方向外側へと流れる。そして、遠心ファン18は、その翼間流路32aを通過した空気を吹出口18aから径方向外側へ矢印FLbのように吹き出す。その吹出口18aから吹き出された空気は、ケーシング12のファン外周流路12bを通って空気吹出口12aから送風機10の外部へ放出される。
The centrifugal fan 18 configured as described above rotates integrally with the motor rotor 161 in the fan rotation direction DRf as shown in FIGS. Along with this, the blades 32 of the centrifugal fan 18 give momentum to the air, so the centrifugal fan 18 sucks air from the intake holes 34a as indicated by the arrow FLa, and the sucked air flows as indicated by the arrows FL1, FL2, and FL3. flows radially outward through the inter-blade passage 32a. Then, the centrifugal fan 18 blows out the air that has passed through the inter-blade passage 32a radially outward from the outlet 18a as indicated by an arrow FLb. The air blown out from the blowout port 18a passes through the fan outer peripheral flow path 12b of the casing 12 and is discharged to the outside of the blower 10 from the air blowout port 12a.
上述したように、本実施形態によれば、図2、図4に示すように、複数枚の翼32のそれぞれにおいて、翼後縁部324は、ファン軸心方向Daの一方側ほどファン径方向Drの内側に位置するように形成されている。
As described above, according to the present embodiment, as shown in FIGS. 2 and 4, in each of the plurality of blades 32, the blade trailing edge portion 324 extends in the fan radial direction toward one side in the fan axial direction Da. It is formed so as to be located inside Dr.
ここで、翼32の相互間に形成される翼間流路32aの空気流れについて説明すると、その翼間流路32aの空気流れは、翼間流路32aのうちの上流側で矢印FL1のように側板34から一旦剥離して側板他方面343上に渦WHを生じる。そして、その翼間流路32aの空気流れは、そのように側板34から一旦剥離してから矢印FL2のように進む。すなわち、その空気流れは、側板34から一旦剥離してから側板34に再付着するようにファン軸心方向Daの一方側に偏る。
Here, the air flow in the inter-blade passages 32a formed between the blades 32 will be described. Then, the vortex WH is generated on the side plate other surface 343 once separated from the side plate 34 . Then, the air flow in the inter-blade passage 32a once separates from the side plate 34 and then advances as indicated by the arrow FL2. That is, the air flow deviates to one side in the fan axial direction Da so as to once separate from the side plate 34 and then reattach to the side plate 34 .
これに対し、本実施形態の遠心ファン18では、上記したように、翼後縁部324が、ファン軸心方向Daの一方側ほどファン径方向Drの内側に位置するように形成されているので、各翼32が行う主板36側の仕事量が側板34側に比して大きくなる。これにより、翼間流路32aの出口付近で空気流れを矢印FL3のように主板36側に再度引き寄せることができる。その結果、例えば翼後縁部324がファン軸心CLと平行である場合と比較して、翼間流路32aの出口付近で空気流れの速度分布を、ファン軸心方向Daの偏りが無い分布に近づけることができ、遠心ファン18の低騒音化を図ることが可能である。
On the other hand, in the centrifugal fan 18 of the present embodiment, as described above, the blade trailing edge portion 324 is formed so as to be located inside the fan radial direction Dr toward one side in the fan axial direction Da. , the amount of work performed by each blade 32 on the side of the main plate 36 is greater than that on the side of the side plate 34 . As a result, the air flow can be drawn again toward the main plate 36 near the outlet of the inter-blade passage 32a as indicated by the arrow FL3. As a result, compared to the case where the trailing edge 324 of the blade is parallel to the fan axis CL, for example, the velocity distribution of the airflow near the outlet of the inter-blade passage 32a is a distribution with no deviation in the fan axis direction Da. , and the noise of the centrifugal fan 18 can be reduced.
また、遠心ファン18では、側板34の外径Dsoに対する側板34の内径Dsiの比率であるDsi/Dsoは、「0.5<Dsi/Dso<0.7」となっている。そのため、翼後縁部324がファン軸心CLに仮に平行であれば翼間流路32aの空気流れが翼間流路32aの出口付近で側板34側に偏る遠心ファンに対し、翼後縁部324がファン軸心方向Daの一方側ほどファン径方向Drの内側に位置する上記構成を用いることができる。従って、本実施形態の翼後縁部324の上記構成を、遠心ファン18の低騒音化を適切に図ることができるように用いることが可能である。
In addition, in the centrifugal fan 18, Dsi/Dso, which is the ratio of the inner diameter Dsi of the side plate 34 to the outer diameter Dso of the side plate 34, is "0.5<Dsi/Dso<0.7". Therefore, if the blade trailing edge 324 is parallel to the fan axis CL, the air flow in the inter-blade passage 32a is biased toward the side plate 34 near the exit of the inter-blade passage 32a. The above configuration in which 324 is located inside in the fan radial direction Dr toward one side in the fan axial direction Da can be used. Therefore, the above configuration of the blade trailing edge portion 324 of the present embodiment can be used so as to appropriately reduce the noise of the centrifugal fan 18 .
なお、Dsi/Dsoが例えば0.5以下である場合には、空気流れが矢印FL2のようにファン軸心方向Daの一方側に偏った後の翼間流路32aの長さが十分に長く確保される。そのため、翼後縁部324が仮にファン軸心CLに平行であったとしても、空気流れがファン軸心方向Daの一方側に偏った後、翼後縁部324に到達するまでには、そのファン軸心方向Daの一方側への空気流れの偏りが緩和される。一方、Dsi/Dsoが例えば0.7以上である場合には、翼間流路32aの空気流れは、側板34に再付着するようにファン軸心方向Daの一方側に偏る前に、翼後縁部324に到達する。要するに、矢印FL1、FL2で示される空気流れが途中で切れる。従って、翼後縁部324がファン軸心方向Daの一方側ほどファン径方向Drの内側に位置するという上記構成を遠心ファン18の低騒音化に有効に役立てるためには、「0.5<Dsi/Dso<0.7」という関係が必要である。
When Dsi/Dso is, for example, 0.5 or less, the length of the inter-blade passage 32a after the air flow is biased to one side in the fan axial direction Da as indicated by arrow FL2 is sufficiently long. Secured. Therefore, even if the trailing edge 324 of the blade is parallel to the fan axis CL, the air flow will not reach the trailing edge 324 until it reaches the trailing edge 324 after being biased to one side in the direction Da of the fan axis. The deviation of the airflow toward one side in the fan axial direction Da is alleviated. On the other hand, when Dsi/Dso is, for example, 0.7 or more, the airflow in the inter-blade flow passage 32a is shifted to one side in the fan axial direction Da so as to adhere to the side plate 34 again. Edge 324 is reached. In short, the air flows indicated by arrows FL1 and FL2 are interrupted. Therefore, in order to effectively reduce the noise of the centrifugal fan 18 with the configuration in which the blade trailing edge portion 324 is positioned closer to the one side in the fan axial direction Da toward the inner side in the fan radial direction Dr, it is necessary that "0.5< Dsi/Dso<0.7" is required.
その「0.5<Dsi/Dso<0.7」という関係が必要であることは、例えばCFDによるシミュレーションでDsi/Dsoの大きさを変化させて解析結果を得ることによって確認されている。CFDとは、「Computational Fluid Dynamics」の略である。このシミュレーション例の遠心ファンでは、翼32の構成は上記比較例と同様とされている。すなわち、シミュレーション例の遠心ファンでは、翼後縁部91(図5参照)がファン軸心CLに平行とされ、その翼後縁部91における翼32の厚みtbが一定とされている。これらの点を除き、このシミュレーション例の遠心ファンは本実施形態の遠心ファン18と同じである。
The necessity of the relationship "0.5<Dsi/Dso<0.7" has been confirmed, for example, by obtaining analysis results by changing the magnitude of Dsi/Dso in CFD simulations. CFD is an abbreviation for "Computational Fluid Dynamics". In the centrifugal fan of this simulation example, the configuration of the blades 32 is the same as that of the comparative example. That is, in the centrifugal fan of the simulation example, the blade trailing edge 91 (see FIG. 5) is parallel to the fan axis CL, and the thickness tb of the blade 32 at the blade trailing edge 91 is constant. Except for these points, the centrifugal fan of this simulation example is the same as the centrifugal fan 18 of this embodiment.
そして、このCFDによるシミュレーションから得られた解析結果が図7A~図7Dに示されている。このシミュレーションでは、遠心ファンの回転数は一定とされている。なお、図7A~図7Dにおいて矢印A1、A2は、翼間流路32aの空気流れの向きを示している。また、位置P1は、側板34が翼間流路32aに面する位置を示し、位置P2は、主板36が翼間流路32aに面する位置を示している。また、図7A~図7Dにおいて、翼間流路32aにおける空気流れの速度(言い換えれば、流速)の高低は、ハッチングの差異によって表されている。
The analysis results obtained from this CFD simulation are shown in FIGS. 7A to 7D. In this simulation, the rotation speed of the centrifugal fan is assumed to be constant. Note that arrows A1 and A2 in FIGS. 7A to 7D indicate the direction of the air flow in the inter-blade passage 32a. A position P1 indicates a position where the side plate 34 faces the inter-blade passage 32a, and a position P2 indicates a position where the main plate 36 faces the inter-blade passage 32a. In addition, in FIGS. 7A to 7D, the difference in hatching indicates the speed of the airflow (in other words, the flow speed) in the inter-blade passage 32a.
具体的に、図7Aは、「Dsi/Dso=0.72」の場合において得られた翼間流路32aの空気流れの速度分布を示している。この図7Aによれば、「Dsi/Dso=0.72」の場合には、翼間流路32aの出口付近(すなわち、図5の翼後縁部91付近)における空気流れの速度分布は、高速部分がファン軸心方向Daの他方側(すなわち、主板36側)へ偏ったものになる。
Specifically, FIG. 7A shows the airflow velocity distribution in the inter-blade passage 32a obtained when "Dsi/Dso=0.72". According to FIG. 7A, when "Dsi/Dso=0.72", the velocity distribution of the airflow near the outlet of the inter-blade passage 32a (that is, near the blade trailing edge 91 in FIG. 5) is The high-speed portion is biased toward the other side of the fan axial direction Da (that is, the main plate 36 side).
また、図7Bは、「Dsi/Dso=0.68」の場合において得られた翼間流路32aの空気流れの速度分布を示し、図7Cは、「Dsi/Dso=0.55」の場合において得られた翼間流路32aの空気流れの速度分布を示している。この図7B、図7Cによれば、「Dsi/Dso=0.68」の場合、および「Dsi/Dso=0.55」の場合には、翼間流路32aの出口付近における空気流れの速度分布は、高速部分がファン軸心方向Daの一方側(すなわち、側板34側)へ偏ったものになる。
Further, FIG. 7B shows the velocity distribution of the airflow in the inter-blade passage 32a obtained when "Dsi/Dso=0.68", and FIG. 7C shows the velocity distribution when "Dsi/Dso=0.55". 3 shows the velocity distribution of the airflow in the inter-blade passage 32a obtained in FIG. According to FIGS. 7B and 7C, in the case of "Dsi/Dso=0.68" and in the case of "Dsi/Dso=0.55", the air flow velocity near the exit of the inter-blade passage 32a The distribution is such that the high-speed portion is biased toward one side in the fan axial direction Da (that is, the side plate 34 side).
また、図7Dは、「Dsi/Dso=0.48」の場合において得られた翼間流路32aの空気流れの速度分布を示している。この図7Dによれば、「Dsi/Dso=0.48」の場合には、翼間流路32aの出口付近における空気流れの速度分布は、ファン軸心方向Daの偏りが無いものになる。
FIG. 7D shows the air flow velocity distribution in the inter-blade passage 32a obtained when "Dsi/Dso=0.48". According to FIG. 7D, when "Dsi/Dso=0.48", the velocity distribution of the airflow in the vicinity of the outlet of the inter-blade passage 32a has no deviation in the fan axial direction Da.
これらの図7A~図7Dに示された空気流れの速度分布から次のようなことが言える。すなわち、図7B、図7Cのように「0.5<Dsi/Dso<0.7」の場合には、翼後縁部324が本実施形態のようにファン軸心方向Daに対して傾けられれば、翼間流路32aの出口付近での空気流れの速度分布は、ファン軸心方向Daの偏りが無いものに近付く。なぜなら、本実施形態のようにファン軸心方向Daに対して傾けられた翼後縁部324(図2参照)は、ファン軸心CLに平行とされた翼後縁部91との比較で、上記したように、翼間流路32aの出口付近で空気流れを主板36側に引き寄せるように作用するからである。従って、この場合、翼後縁部324が本実施形態のようにファン軸心方向Daに対して傾けられることは、遠心ファン18の低騒音化につながる。
The following can be said from the airflow velocity distribution shown in FIGS. 7A to 7D. That is, when "0.5<Dsi/Dso<0.7" as shown in FIGS. 7B and 7C, the blade trailing edge 324 is tilted with respect to the fan axial direction Da as in the present embodiment. For example, the velocity distribution of the airflow near the outlet of the inter-blade passage 32a approaches one with no bias in the fan axial direction Da. This is because the blade trailing edge 324 (see FIG. 2) inclined with respect to the fan axis direction Da as in the present embodiment is compared with the blade trailing edge 91 parallel to the fan axis CL. This is because, as described above, the air flow is pulled toward the main plate 36 in the vicinity of the outlet of the inter-blade passage 32a. Therefore, in this case, the inclination of the blade trailing edge 324 with respect to the fan axial direction Da as in the present embodiment leads to noise reduction of the centrifugal fan 18 .
その一方で、図7A、図7Dでは、翼間流路32aの出口付近における空気流れの速度分布は、高速部分が側板34側へ偏ったものではない。従って、「0.7≦Dsi/Dso」の場合、および「Dsi/Dso≦0.5」の場合には、翼間流路32aの出口付近で空気流れが主板36側に引き寄せられたとしても、その出口付近の空気流れの速度分布は、ファン軸心方向Daの偏りが無いものには近付かない。すなわち、この場合、翼後縁部324が本実施形態のようにファン軸心方向Daに対して傾けられても、そのことは遠心ファン18の低騒音化につながらない。
On the other hand, in FIGS. 7A and 7D, the velocity distribution of the airflow near the exit of the inter-blade passage 32a is not one in which the high-speed portion is biased toward the side plate 34 side. Therefore, in the case of "0.7≤Dsi/Dso" and in the case of "Dsi/Dso≤0.5", even if the air flow is drawn toward the main plate 36 near the outlet of the inter-blade passage 32a, , the velocity distribution of the airflow near the outlet does not come close to the one with no deviation in the fan axial direction Da. That is, in this case, even if the blade trailing edge portion 324 is inclined with respect to the fan axial direction Da as in the present embodiment, this does not lead to noise reduction of the centrifugal fan 18 .
以上のように、図7A~図7Dの解析結果から、翼後縁部324が本実施形態のようにファン軸心方向Daに対して傾けられた構成を遠心ファン18の低騒音化に有効に役立てるためには、「0.5<Dsi/Dso<0.7」という関係が必要であると言える。
As described above, from the analysis results of FIGS. 7A to 7D, the configuration in which the blade trailing edge 324 is inclined with respect to the fan axial direction Da as in the present embodiment is effective in reducing the noise of the centrifugal fan 18. It can be said that the relationship "0.5<Dsi/Dso<0.7" is required to be useful.
また、本実施形態の遠心ファン18と、翼後縁部91(図5参照)がファン軸心CLに平行な上記比較例の遠心ファンとを対比すると、図8に示すように、殆どの周波数域で遠心ファン18の低騒音化が実現されている。図8では、実線S1が本実施形態のSPLを示し、破線S2が比較例のSPLを示している。SPLとは、「Sound Pressure Level」の略である。
Further, when comparing the centrifugal fan 18 of the present embodiment with the centrifugal fan of the comparative example in which the blade trailing edge 91 (see FIG. 5) is parallel to the fan axis CL, as shown in FIG. Low noise of the centrifugal fan 18 is realized in the region. In FIG. 8, the solid line S1 indicates the SPL of this embodiment, and the dashed line S2 indicates the SPL of the comparative example. SPL is an abbreviation for "Sound Pressure Level".
また、図9に示すように、本実施形態では比較例に対し、遠心ファン18の騒音がオーバーオール値で2dB低減された。図9の縦軸の「O.A.」はオーバーオール値の略である。
Also, as shown in FIG. 9, in this embodiment, the noise of the centrifugal fan 18 was reduced by 2 dB in overall value as compared with the comparative example. "OA" on the vertical axis of Fig. 9 is an abbreviation for the overall value.
(1)また、本実施形態によれば、側板他方面343は、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置する。そして、図2、図4の縦断面において、側板他方面343の曲率半径はファン径方向Drの外側ほど大きくなる。従って、翼後縁部324がファン軸心方向Daの一方側ほどファン径方向Drの内側に位置する構成による騒音低減効果を得つつ、ファン軸心方向Daの一方側から遠心ファン18内に吸い込まれた空気をファン径方向Drの外側へ向くように案内することができる。
(1) Further, according to the present embodiment, the side plate other surface 343 is located on the other side in the fan axial direction Da toward the outside in the fan radial direction Dr. 2 and 4, the curvature radius of the side plate other surface 343 increases toward the outer side in the fan radial direction Dr. Therefore, while the blade trailing edge portion 324 is located inside the fan radial direction Dr toward one side in the fan axial direction Da, the air is sucked into the centrifugal fan 18 from one side in the fan axial direction Da while obtaining the noise reduction effect. It is possible to guide the trapped air so as to face outward in the fan radial direction Dr.
(2)また、本実施形態によれば、図2、図4に示すように、複数枚の翼32のそれぞれにおいて、翼前縁部323は、側板34側から主板36側へと延びており、主板36側ほどファン径方向Drの内側に位置するように形成されている。従って、翼32の長さが側板34側よりも主板36側の方で長くなるので、各翼32が行う主板36側の仕事量を側板34側に比して大きくすることができる。これによっても、翼間流路32aの空気流れがファン軸心方向Daの一方側に偏ることを是正することができる。
(2) Further, according to the present embodiment, as shown in FIGS. 2 and 4, in each of the plurality of blades 32, the blade leading edge portion 323 extends from the side plate 34 side to the main plate 36 side. , the main plate 36 side is located inside the fan radial direction Dr. Therefore, since the blades 32 are longer on the side of the main plate 36 than on the side of the side plate 34, the work done by each blade 32 on the side of the main plate 36 can be made larger than that on the side of the side plate 34. This also makes it possible to correct the bias of the airflow in the inter-blade passage 32a to one side in the fan axial direction Da.
(3)また、本実施形態によれば、側板34と主板36はそれぞれ、翼後縁部324よりもファン径方向Drの外側にまで延びている。従って、空気流れの流速が最大になる翼後縁部324をケース側板隙間34bの開口端34cから遠ざけることができる。このことは、遠心ファン18の低騒音化を図る上で有利に作用する。
(3) Further, according to the present embodiment, the side plate 34 and the main plate 36 each extend outside the blade trailing edge portion 324 in the fan radial direction Dr. Therefore, the trailing edge portion 324 of the blade where the flow velocity of the air flow is maximized can be kept away from the opening end 34c of the case side plate gap 34b. This is advantageous in reducing the noise of the centrifugal fan 18 .
また、側板34と主板36とがそれぞれ翼後縁部324よりもファン径方向Drの外側にまで延びているので、空気流れが翼間流路32aから出た直後にファン軸心方向Daに急拡大することが抑制される。これにより、その空気流れの急拡大に起因した損失を抑制し、遠心ファン18の低騒音化に寄与することができる。
In addition, since the side plate 34 and the main plate 36 each extend to the outer side of the fan radial direction Dr from the blade trailing edge portion 324, the air flow suddenly moves in the fan axial direction Da immediately after coming out of the inter-blade passage 32a. Expansion is suppressed. As a result, the loss caused by the rapid expansion of the airflow can be suppressed, and the centrifugal fan 18 can contribute to noise reduction.
例えば、翼後縁部324の他方側直径Db2に対する主板36の外径Dmoの比率であるDmo/Db2と、騒音低減効果との関係は、図10に示すようになる。すなわち、Dmo/Db2が大きいほど騒音低減効果は高くなる。この図10から判るように、側板34と主板36が翼後縁部324よりもファン径方向Drの外側にまで延びていることは、騒音低減効果を高めるように作用する。なお、図10の実験では、側板34の外径Dsoは主板36の外径Dmoと同じである。
For example, FIG. 10 shows the relationship between Dmo/Db2, which is the ratio of the outer diameter Dmo of the main plate 36 to the other diameter Db2 of the blade trailing edge 324, and the noise reduction effect. That is, the greater the Dmo/Db2, the higher the noise reduction effect. As can be seen from FIG. 10, the extension of the side plate 34 and the main plate 36 to the outer side in the fan radial direction Dr from the blade trailing edge portion 324 acts to enhance the noise reduction effect. 10, the outer diameter Dso of the side plate 34 is the same as the outer diameter Dmo of the main plate 36. As shown in FIG.
(4)また、本実施形態によれば、翼後縁部324の他方側直径Db2と主板36の外径Dmoとの間では、「Db2<Dmo≦1.13×Db2」の関係が成立する。そして、図10によれば、Dmo/Db2が1.13を超えた場合、Dmo/Db2が大きいほど騒音低減効果は緩やかに高まるが、Dmo/Db2に対しあまり変化しない。従って、遠心ファン18の体格が必要以上に大きくなることを回避しつつ騒音低減効果を得ることが可能である。
(4) Further, according to the present embodiment, the relationship "Db2<Dmo≦1.13×Db2" is established between the diameter Db2 on the other side of the blade trailing edge portion 324 and the outer diameter Dmo of the main plate 36. . Then, according to FIG. 10, when Dmo/Db2 exceeds 1.13, the noise reduction effect gradually increases as Dmo/Db2 increases, but does not change much with respect to Dmo/Db2. Therefore, it is possible to obtain a noise reduction effect while avoiding the size of the centrifugal fan 18 from becoming unnecessarily large.
(5)また、本実施形態によれば、第1ケース部材22の第1ケース外周部222は、遠心ファン18の側板外周端部342に対しファン径方向Drの外側に重なるように設けられている。そして、側板外周端部342は、第1ケース外周部222に対しファン径方向Drに対向し、ケース側板隙間34bの開口端34cを第1ケース外周部222との間に形成している。
(5) Further, according to the present embodiment, the first case outer peripheral portion 222 of the first case member 22 is provided so as to overlap the side plate outer peripheral end portion 342 of the centrifugal fan 18 on the outside in the fan radial direction Dr. there is The side plate outer peripheral end portion 342 faces the first case outer peripheral portion 222 in the fan radial direction Dr, and forms an opening end 34c of the case side plate gap 34b between the first case outer peripheral portion 222 and the first case outer peripheral portion 222 .
従って、ケース側板隙間34bの開口端34cはケーシング12の空気吹出口12aよりもファン径方向Drの内側に位置するので、その開口端34cでの気圧が空気吹出口12aでの気圧よりも低くなる。これにより、例えば開口端34cが空気吹出口12aの外側で開放されている場合と比較して、開口端34cからケース側板隙間34bへ流入する吹出空気の逆流を抑制することが可能である。
Therefore, since the opening end 34c of the case-side plate gap 34b is located inside the air outlet 12a of the casing 12 in the fan radial direction Dr, the air pressure at the opening end 34c is lower than the air pressure at the air outlet 12a. . As a result, compared to the case where the opening end 34c is open outside the air outlet 12a, for example, it is possible to suppress the backflow of the blown air flowing into the case side plate gap 34b from the opening end 34c.
(6)また、本実施形態によれば、図4~図6に示すように、翼後縁部324は側板34側から主板36側へと延びており、翼32の厚みtbは、翼後縁部324では側板34側ほど大きくなっている。従って、翼後縁部324に隣接する空気流れの失速域STが主板36側よりも側板34側の方で大きくなるので、この失速域STによる空気流れ損失が側板34側ほど大きくなる。このことも、翼後縁部324周りの空気流れがファン軸心方向Daの一方側に偏ることを抑制するように作用する。
(6) According to the present embodiment, as shown in FIGS. 4 to 6, the blade trailing edge portion 324 extends from the side plate 34 side to the main plate 36 side, and the thickness tb of the blade 32 is At the edge portion 324, the side plate 34 side is larger. Therefore, the airflow stall area ST adjacent to the blade trailing edge 324 is larger on the side plate 34 side than on the main plate 36 side. This also acts to prevent the airflow around the trailing edge portion 324 of the blade from deviating to one side in the fan axial direction Da.
(7)また、本実施形態によれば、図5、図6に示すように、ファン軸心CLに垂直な横断面(例えば、図6の断面)において、翼後縁部324の後縁部外面324aは凸状に湾曲しており、後縁部外面324aの曲率半径Rbは側板34側ほど大きくなっている。従って、翼32の正圧面と負圧面とを翼後縁部324で滑らかにつなぐことができる。そのため、翼後縁部324周りでの空気の流通抵抗が主板36側よりも側板34側の方で大きくなるという傾向を確保しつつ、正圧面と負圧面とが翼後縁部324で滑らかにつながっていない場合と比較して、その流通抵抗の全体を引き下げることができる。
(7) Further, according to the present embodiment, as shown in FIGS. 5 and 6, the trailing edge portion of the blade trailing edge portion 324 is The outer surface 324a is curved in a convex shape, and the radius of curvature Rb of the rear edge portion outer surface 324a increases toward the side plate 34 side. Therefore, the pressure surface and the suction surface of the blade 32 can be smoothly connected at the blade trailing edge portion 324 . Therefore, the pressure surface and the suction surface are smoothed at the blade trailing edge 324 while maintaining the tendency that the air flow resistance around the blade trailing edge 324 is larger on the side plate 34 side than on the main plate 36 side. Compared to the case where they are not connected, the overall flow resistance can be lowered.
(第2実施形態)
次に、第2実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。また、前述の実施形態と同一または均等な部分については省略または簡略化して説明する。このことは後述の実施形態の説明においても同様である。 (Second embodiment)
Next, a second embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described. Also, the same or equivalent parts as those of the above-described embodiment will be omitted or simplified. This also applies to the description of the embodiments that will be described later.
次に、第2実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。また、前述の実施形態と同一または均等な部分については省略または簡略化して説明する。このことは後述の実施形態の説明においても同様である。 (Second embodiment)
Next, a second embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described. Also, the same or equivalent parts as those of the above-described embodiment will be omitted or simplified. This also applies to the description of the embodiments that will be described later.
図11に示すように、本実施形態でも第1実施形態と同様に、翼後縁部324は、ファン軸心方向Daの一方側ほどファン径方向Drの内側に位置するように形成されている。但し、本実施形態では、その翼後縁部324の形状が第1実施形態に対して異なる。
As shown in FIG. 11, in the present embodiment, similarly to the first embodiment, the blade trailing edge portion 324 is formed so as to be positioned more inward in the fan radial direction Dr toward one side in the fan axial direction Da. . However, in this embodiment, the shape of the blade trailing edge portion 324 is different from that in the first embodiment.
具体的に、本実施形態の翼後縁部324は、1つの段差形状を有するように形成され、ファン軸心方向Daの一方側ほどファン径方向Drの内側に段階的に位置する。
Specifically, the blade trailing edge portion 324 of the present embodiment is formed to have a single stepped shape, and is located stepwise toward the inside in the fan radial direction Dr toward one side in the fan axial direction Da.
以上説明したことを除き、本実施形態は第1実施形態と同様である。そして、本実施形態では、前述の第1実施形態と共通の構成から奏される効果を第1実施形態と同様に得ることができる。
Except for what has been described above, this embodiment is the same as the first embodiment. In addition, in the present embodiment, it is possible to obtain the same effects as in the first embodiment, which are provided by the configuration common to that of the first embodiment.
(第3実施形態)
次に、第3実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Third Embodiment)
Next, a third embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
次に、第3実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Third Embodiment)
Next, a third embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
図12に示すように、本実施形態でも第1実施形態と同様に、翼後縁部324は、ファン軸心方向Daの一方側ほどファン径方向Drの内側に位置するように形成されている。但し、本実施形態では、その翼後縁部324の形状が第1実施形態に対して異なる。
As shown in FIG. 12, in this embodiment, similarly to the first embodiment, the trailing edge portion 324 of the blade is formed so as to be positioned more inward in the fan radial direction Dr toward one side in the fan axial direction Da. . However, in this embodiment, the shape of the blade trailing edge portion 324 is different from that in the first embodiment.
具体的に、本実施形態の翼後縁部324は、複数の段差形状を有するように形成され、ファン軸心方向Daの一方側ほどファン径方向Drの内側に段階的に位置する。
Specifically, the blade trailing edge portion 324 of this embodiment is formed to have a plurality of stepped shapes, and is located stepwise toward the inside in the fan radial direction Dr toward one side in the fan axial direction Da.
以上説明したことを除き、本実施形態は第1実施形態と同様である。そして、本実施形態では、前述の第1実施形態と共通の構成から奏される効果を第1実施形態と同様に得ることができる。
Except for what has been described above, this embodiment is the same as the first embodiment. In addition, in the present embodiment, it is possible to obtain the same effects as in the first embodiment, which are provided by the configuration common to that of the first embodiment.
(第4実施形態)
次に、第4実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Fourth embodiment)
Next, a fourth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
次に、第4実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Fourth embodiment)
Next, a fourth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
図13に示すように、本実施形態でも第1実施形態と同様に、翼後縁部324は、ファン軸心方向Daの一方側ほどファン径方向Drの内側に位置するように形成されている。但し、本実施形態では、その翼後縁部324の形状が第1実施形態に対して異なる。
As shown in FIG. 13, in the present embodiment, similarly to the first embodiment, the blade trailing edge portion 324 is formed so as to be positioned more inward in the fan radial direction Dr toward one side in the fan axial direction Da. . However, in this embodiment, the shape of the blade trailing edge portion 324 is different from that in the first embodiment.
具体的に、本実施形態の翼後縁部324は、その翼後縁部324のうち側板34に連結する部位を含むファン軸心方向Daの一方側の部位では、ファン軸心CLと平行に延びている。そして、翼後縁部324は、その翼後縁部324のうち主板36に連結する部位を含むファン軸心方向Daの他方側の部位では、ファン軸心方向Daの他方側ほどファン径方向Drの外側に位置するようにファン軸心CLに対し傾斜している。
Specifically, in the blade trailing edge portion 324 of the present embodiment, a portion on one side in the fan axial direction Da including the portion connected to the side plate 34 of the blade trailing edge portion 324 is parallel to the fan axial center CL. extended. At the other side of the fan axial direction Da, the blade trailing edge portion 324 includes a portion connected to the main plate 36, and the blade trailing edge portion 324 is more inclined toward the fan radial direction Dr. is inclined with respect to the fan axis CL so as to be located outside the .
以上説明したことを除き、本実施形態は第1実施形態と同様である。そして、本実施形態では、前述の第1実施形態と共通の構成から奏される効果を第1実施形態と同様に得ることができる。
Except for what has been described above, this embodiment is the same as the first embodiment. In addition, in the present embodiment, it is possible to obtain the same effects as in the first embodiment, which are provided by the configuration common to that of the first embodiment.
(第5実施形態)
次に、第5実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Fifth embodiment)
Next, a fifth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
次に、第5実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Fifth embodiment)
Next, a fifth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
図14に示すように、本実施形態でも第1実施形態と同様に、翼後縁部324は、ファン軸心方向Daの一方側ほどファン径方向Drの内側に位置するように形成されている。但し、本実施形態では、その翼後縁部324の形状が第1実施形態に対して異なる。
As shown in FIG. 14, in the present embodiment, similarly to the first embodiment, the blade trailing edge portion 324 is formed so as to be positioned more inward in the fan radial direction Dr toward one side in the fan axial direction Da. . However, in this embodiment, the shape of the blade trailing edge portion 324 is different from that in the first embodiment.
具体的に、本実施形態の翼後縁部324は、曲がりながら延伸している。
Specifically, the blade trailing edge 324 of this embodiment extends while bending.
以上説明したことを除き、本実施形態は第1実施形態と同様である。そして、本実施形態では、前述の第1実施形態と共通の構成から奏される効果を第1実施形態と同様に得ることができる。
Except for what has been described above, this embodiment is the same as the first embodiment. In addition, in the present embodiment, it is possible to obtain the same effects as in the first embodiment, which are provided by the configuration common to that of the first embodiment.
(第6実施形態)
次に、第6実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Sixth embodiment)
Next, a sixth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
次に、第6実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Sixth embodiment)
Next, a sixth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
図15に示すように、本実施形態でも第1実施形態と同様に、遠心ファン18の側板他方面343は、ファン軸心方向Daの他方側を向いてファン径方向Drに拡がっており、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置する。但し、本実施形態では、側板他方面343の形状が第1実施形態に対して異なる。
As shown in FIG. 15, in this embodiment, as in the first embodiment, the side plate other surface 343 of the centrifugal fan 18 faces the other side of the fan axial direction Da and extends in the fan radial direction Dr. The outer side in the radial direction Dr is positioned on the other side in the fan axial direction Da. However, in this embodiment, the shape of the side plate other surface 343 is different from that in the first embodiment.
具体的に、図15に示す送風機10の縦断面において、側板他方面343は、内側円弧形状343aと外側直線形状343dとを有している。この外側直線形状343dは、第1実施形態における外側円弧形状343bと外側直線形状343c(図2参照)とに置き換わるものである。
Specifically, in the longitudinal section of the blower 10 shown in FIG. 15, the side plate other surface 343 has an inner arc shape 343a and an outer linear shape 343d. This outer linear shape 343d replaces the outer circular arc shape 343b and the outer linear shape 343c (see FIG. 2) in the first embodiment.
図15の縦断面において、本実施形態の内側円弧形状343aと外側直線形状343dは、ファン径方向Drの内側から、内側円弧形状343a、外側直線形状343dの順に滑らかに連なっている。また、外側直線形状343dは、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置するようにファン軸心CLに対し傾斜した直線状になっている。このように、図15の縦断面において、本実施形態の側板他方面343は、1つの円弧と1つの直線とで形成されている。
In the longitudinal section of FIG. 15, the inner arcuate shape 343a and the outer linear shape 343d of the present embodiment smoothly connect in the order of the inner arcuate shape 343a and the outer linear shape 343d from the inside in the fan radial direction Dr. In addition, the outer linear shape 343d is a linear shape that is inclined with respect to the fan axis CL so that the outer side in the fan radial direction Dr is positioned on the other side in the fan axis direction Da. Thus, in the longitudinal section of FIG. 15, the side plate other surface 343 of this embodiment is formed by one circular arc and one straight line.
以上説明したことを除き、本実施形態は第1実施形態と同様である。そして、本実施形態では、前述の第1実施形態と共通の構成から奏される効果を第1実施形態と同様に得ることができる。
Except for what has been described above, this embodiment is the same as the first embodiment. In addition, in the present embodiment, it is possible to obtain the same effects as in the first embodiment, which are provided by the configuration common to that of the first embodiment.
なお、本実施形態は第1実施形態に基づいた変形例であるが、本実施形態を前述の第2~第5実施形態の何れかと組み合わせることも可能である。
Although this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to fifth embodiments.
(第7実施形態)
次に、第7実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Seventh embodiment)
Next, a seventh embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
次に、第7実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Seventh embodiment)
Next, a seventh embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
図16に示すように、本実施形態でも第1実施形態と同様に、遠心ファン18の側板他方面343は、ファン軸心方向Daの他方側を向いてファン径方向Drに拡がっており、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置する。但し、本実施形態では、側板他方面343の形状が第1実施形態に対して異なる。
As shown in FIG. 16, in this embodiment, as in the first embodiment, the side plate other surface 343 of the centrifugal fan 18 faces the other side of the fan axial direction Da and extends in the fan radial direction Dr. The outer side in the radial direction Dr is positioned on the other side in the fan axial direction Da. However, in this embodiment, the shape of the side plate other surface 343 is different from that in the first embodiment.
具体的に、図16に示す送風機10の縦断面において、側板他方面343は、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置するようにファン軸心CLに対し傾斜した1本の直線状に形成されている。このように、図16の縦断面において、本実施形態の側板他方面343は、1つの直線で形成されている。
Specifically, in the vertical cross section of the fan 10 shown in FIG. 16, the side plate other surface 343 is inclined with respect to the fan axis CL so that the outer side in the fan radial direction Dr is located on the other side in the fan axis direction Da. It is formed in the shape of a straight line. Thus, in the longitudinal section of FIG. 16, the side plate other surface 343 of this embodiment is formed by one straight line.
(1)従って、翼後縁部324がファン軸心方向Daの一方側ほどファン径方向Drの内側に位置する構成による騒音低減効果を得つつ、ファン軸心方向Daの一方側から遠心ファン18内に吸い込まれた空気をファン径方向Drの外側へ向くように案内することができる。
(1) Therefore, the centrifugal fan 18 can be rotated from one side in the fan axial direction Da while obtaining the noise reduction effect due to the configuration in which the blade trailing edge portion 324 is located on the inner side in the fan radial direction Dr toward one side in the fan axial direction Da. The air sucked inside can be guided outward in the fan radial direction Dr.
以上説明したことを除き、本実施形態は第1実施形態と同様である。そして、本実施形態では、前述の第1実施形態と共通の構成から奏される効果を第1実施形態と同様に得ることができる。
Except for what has been described above, this embodiment is the same as the first embodiment. In addition, in the present embodiment, it is possible to obtain the same effects as in the first embodiment, which are provided by the configuration common to that of the first embodiment.
なお、本実施形態は第1実施形態に基づいた変形例であるが、本実施形態を前述の第2~第5実施形態の何れかと組み合わせることも可能である。
Although this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to fifth embodiments.
(第8実施形態)
次に、第8実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Eighth embodiment)
Next, an eighth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
次に、第8実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Eighth embodiment)
Next, an eighth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
図17に示すように、本実施形態でも第1実施形態と同様に、遠心ファン18の側板他方面343は、ファン軸心方向Daの他方側を向いてファン径方向Drに拡がっており、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置する。但し、本実施形態では、側板他方面343の形状が第1実施形態に対して異なる。
As shown in FIG. 17, in this embodiment, as in the first embodiment, the side plate other surface 343 of the centrifugal fan 18 faces the other side of the fan axial direction Da and extends in the fan radial direction Dr. The outer side in the radial direction Dr is positioned on the other side in the fan axial direction Da. However, in this embodiment, the shape of the side plate other surface 343 is different from that in the first embodiment.
具体的に、図17に示す送風機10の縦断面において、側板他方面343は、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置するように延伸する1本の円弧状に形成されている。このように、図17の縦断面において、本実施形態の側板他方面343は、1つの円弧で形成されている。
Specifically, in the longitudinal section of the fan 10 shown in FIG. 17, the side plate other side surface 343 is formed in a single arc shape extending so as to be located on the other side in the fan axial direction Da toward the outside in the fan radial direction Dr. It is Thus, in the longitudinal section of FIG. 17, the side plate other surface 343 of this embodiment is formed by one circular arc.
以上説明したことを除き、本実施形態は第1実施形態と同様である。そして、本実施形態では、前述の第1実施形態と共通の構成から奏される効果を第1実施形態と同様に得ることができる。
Except for what has been described above, this embodiment is the same as the first embodiment. In addition, in the present embodiment, it is possible to obtain the same effects as in the first embodiment, which are provided by the configuration common to that of the first embodiment.
なお、本実施形態は第1実施形態に基づいた変形例であるが、本実施形態を前述の第2~第5実施形態の何れかと組み合わせることも可能である。
Although this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to fifth embodiments.
(第9実施形態)
次に、第9実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Ninth embodiment)
Next, a ninth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
次に、第9実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Ninth embodiment)
Next, a ninth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
図18に示すように、本実施形態でも第1実施形態と同様に、翼前縁部323は、側板34側から主板36側へと延びており、主板36側ほどファン径方向Drの内側に位置するように形成されている。但し、本実施形態では、その翼前縁部323の形状が第1実施形態に対して異なる。
As shown in FIG. 18, in this embodiment, as in the first embodiment, the blade leading edge portion 323 extends from the side plate 34 side to the main plate 36 side, and extends inward in the fan radial direction Dr toward the main plate 36 side. formed to be located. However, in this embodiment, the shape of the blade leading edge portion 323 is different from that in the first embodiment.
具体的に、本実施形態の翼前縁部323は、第1前縁部323aと第2前縁部323bとに加え、第3前縁部323cを有している。これらの第1前縁部323aと第2前縁部323bと第3前縁部323cは、側板34側から、第1前縁部323a、第2前縁部323b、第3前縁部323cの順番で直列に連結されている。
Specifically, the blade leading edge portion 323 of the present embodiment has a third leading edge portion 323c in addition to the first leading edge portion 323a and the second leading edge portion 323b. These first front edge portion 323a, second front edge portion 323b and third front edge portion 323c are divided into first front edge portion 323a, second front edge portion 323b and third front edge portion 323c from the side plate 34 side. connected in series in order.
第3前縁部323cは主板36に連結され、第2前縁部323bと主板36との間に設けられている。また、第3前縁部323cは、図18の縦断面においてファン軸心CLと平行に形成されている。
The third front edge portion 323 c is connected to the main plate 36 and provided between the second front edge portion 323 b and the main plate 36 . Also, the third front edge portion 323c is formed parallel to the fan axis CL in the longitudinal section of FIG.
以上説明したことを除き、本実施形態は第1実施形態と同様である。そして、本実施形態では、前述の第1実施形態と共通の構成から奏される効果を第1実施形態と同様に得ることができる。
Except for what has been described above, this embodiment is the same as the first embodiment. In addition, in the present embodiment, it is possible to obtain the same effects as in the first embodiment, which are provided by the configuration common to that of the first embodiment.
なお、本実施形態は第1実施形態に基づいた変形例であるが、本実施形態を前述の第2~第8実施形態の何れかと組み合わせることも可能である。
Although this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to eighth embodiments.
(第10実施形態)
次に、第10実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Tenth embodiment)
Next, a tenth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
次に、第10実施形態について説明する。本実施形態では、前述の第1実施形態と異なる点を主として説明する。 (Tenth embodiment)
Next, a tenth embodiment will be described. In this embodiment, differences from the above-described first embodiment will be mainly described.
図19に示すように、本実施形態の電動モータ16は、第1実施形態のモータロータ161(図2参照)に替えてモータロータ40を有している。また、本実施形態の遠心ファン18は、第1実施形態の主板36に替えて主板外周部43を有し、第1実施形態のロータ連結部38に替えてロータ連結部44を有している。本実施形態では、複数枚の翼32と側板34と主板外周部43とロータ連結部44は一体構成になっている。
As shown in FIG. 19, the electric motor 16 of this embodiment has a motor rotor 40 instead of the motor rotor 161 (see FIG. 2) of the first embodiment. Further, the centrifugal fan 18 of this embodiment has a main plate outer peripheral portion 43 instead of the main plate 36 of the first embodiment, and a rotor connection portion 44 instead of the rotor connection portion 38 of the first embodiment. . In this embodiment, the plurality of blades 32, the side plates 34, the main plate outer peripheral portion 43, and the rotor connecting portion 44 are integrally constructed.
具体的に、本実施形態のモータロータ40には、第1実施形態の内周孔36aに相当する内周孔40aが形成されており、その内周孔40aには回転軸14が嵌め入れられている。これにより、モータロータ40は回転軸14に対して直接固定され、ファン軸心CLを中心として回転軸14と一体的に回転する。
Specifically, an inner peripheral hole 40a corresponding to the inner peripheral hole 36a of the first embodiment is formed in the motor rotor 40 of the present embodiment, and the rotary shaft 14 is fitted into the inner peripheral hole 40a. there is As a result, the motor rotor 40 is directly fixed to the rotating shaft 14 and rotates integrally with the rotating shaft 14 around the fan axis CL.
モータロータ40は、主板内周部401と筒状部402とを有している。主板内周部401は、ファン軸心CLを中心としてファン径方向Drへ円盤状に拡がった形状を成している。そして主板内周部401は、内周主板面401aを有している。この内周主板面401aは、ファン軸心方向Daの一方側を向いてファン径方向Drへ拡がる湾曲面であり、ファン径方向Drの外側ほどファン軸心方向Daの他方側に位置するように形成されている。主板内周部401はモータロータ40の一部分であるが、遠心ファン18が吸い込んだ空気を案内する機能も有するので、遠心ファン18の一部分でもある。
The motor rotor 40 has a main plate inner peripheral portion 401 and a tubular portion 402 . The main plate inner peripheral portion 401 has a disk-like shape that spreads in the fan radial direction Dr around the fan axis CL. The main plate inner peripheral portion 401 has an inner peripheral main plate surface 401a. The inner peripheral main plate surface 401a is a curved surface that faces one side in the fan axial direction Da and expands in the fan radial direction Dr. formed. The inner peripheral portion 401 of the main plate is a part of the motor rotor 40 , but also a part of the centrifugal fan 18 because it has a function of guiding the air sucked by the centrifugal fan 18 .
なお、図19では、翼32とモータロータ40の主板内周部401との間に隙間が示されているが、これは、判りやすい図示とするためである。各翼32は、主板内周部401に接触していてもよいし、図示のとおり主板内周部401に対し隙間をあけて離れていてもよい。
Note that FIG. 19 shows a gap between the blade 32 and the main plate inner peripheral portion 401 of the motor rotor 40, but this is for the sake of easy understanding. Each blade 32 may be in contact with the main plate inner peripheral portion 401 or may be spaced apart from the main plate inner peripheral portion 401 as shown.
モータロータ40の筒状部402は、ファン軸心CLを中心とした円筒形状を成しており、主板内周部401の径方向外側端からファン軸心方向Daの他方側へ延伸している。この筒状部402の内側にはロータマグネット162が固定されている。
The cylindrical portion 402 of the motor rotor 40 has a cylindrical shape centered on the fan axis CL, and extends from the radially outer end of the main plate inner peripheral portion 401 toward the other side in the fan axis direction Da. A rotor magnet 162 is fixed inside the tubular portion 402 .
主板外周部43は、主板内周部401に対しファン径方向Drの外側に配置され、ファン軸心CLを中心としてファン径方向Drへ円盤状に拡がった形状を成している。詳細には、主板外周部43は、主板内周部401から続いてファン径方向Drの外側へ拡がった形状を成している。従って、主板外周部43と主板内周部401は全体として、第1実施形態の主板36(図2参照)に対応する。
The main plate outer peripheral portion 43 is arranged outside the main plate inner peripheral portion 401 in the fan radial direction Dr, and has a disk-like shape expanding in the fan radial direction Dr around the fan axial center CL. More specifically, the main plate outer peripheral portion 43 continues from the main plate inner peripheral portion 401 and expands outward in the fan radial direction Dr. Therefore, the main plate outer peripheral portion 43 and the main plate inner peripheral portion 401 as a whole correspond to the main plate 36 (see FIG. 2) of the first embodiment.
また、主板外周部43は、ファン軸心方向Daの一方側を向いた外周主板面43aを有している。この外周主板面43aは、内周主板面401aから続いてファン径方向Drの外側へ拡がっている。外周主板面43aには、複数枚の翼32の翼他端部322がそれぞれ連結されている。外周主板面43aと内周主板面401aは全体として、遠心ファン18内の気流を案内する主板案内面36bを構成している。
In addition, the main plate outer peripheral portion 43 has an outer peripheral main plate surface 43a facing one side in the fan axial direction Da. The outer peripheral main plate surface 43a continues from the inner peripheral main plate surface 401a and spreads outward in the fan radial direction Dr. The blade other end portions 322 of the plurality of blades 32 are respectively connected to the outer peripheral main plate surface 43a. The outer peripheral main plate surface 43 a and the inner peripheral main plate surface 401 a as a whole constitute a main plate guide surface 36 b that guides the airflow inside the centrifugal fan 18 .
また、主板外周部43は、ファン径方向Drの外側に設けられた端部である外周端部431を有している。この外周端部431は、第1実施形態の主板外周端部362(図2参照)に対応する。
In addition, the main plate outer peripheral portion 43 has an outer peripheral end portion 431 that is an end portion provided outside in the fan radial direction Dr. This outer peripheral end portion 431 corresponds to the main plate outer peripheral end portion 362 (see FIG. 2) of the first embodiment.
ロータ連結部44は、ファン軸心CLを中心とした円筒形状を成しており、主板外周部43の径方向内側端からファン軸心方向Daの他方側へ延伸している。ロータ連結部44の径方向内側には、モータロータ40の筒状部402が嵌め込まれている。これにより、ロータ連結部44はモータロータ40に固定される。そして、ロータ連結部44がモータロータ40に固定されることにより、遠心ファン18は、そのモータロータ40に固定され、モータロータ40と一体に回転する。
The rotor connecting portion 44 has a cylindrical shape centered on the fan axis CL, and extends from the radially inner end of the main plate outer peripheral portion 43 to the other side in the fan axis direction Da. The cylindrical portion 402 of the motor rotor 40 is fitted inside the rotor connecting portion 44 in the radial direction. Thereby, the rotor connecting portion 44 is fixed to the motor rotor 40 . By fixing the rotor connecting portion 44 to the motor rotor 40 , the centrifugal fan 18 is fixed to the motor rotor 40 and rotates together with the motor rotor 40 .
以上説明したことを除き、本実施形態は第1実施形態と同様である。そして、本実施形態では、前述の第1実施形態と共通の構成から奏される効果を第1実施形態と同様に得ることができる。
Except for what has been described above, this embodiment is the same as the first embodiment. In addition, in the present embodiment, the same effects as in the first embodiment can be obtained from the configuration common to that of the first embodiment.
なお、本実施形態は第1実施形態に基づいた変形例であるが、本実施形態を前述の第2~第9実施形態の何れかと組み合わせることも可能である。
Although this embodiment is a modification based on the first embodiment, it is also possible to combine this embodiment with any of the above-described second to ninth embodiments.
(他の実施形態)
(1)上述の各実施形態では、図2に示すように、遠心ファン18はターボファンであるが、例えばラジアルファンなど、他の形式の遠心ファンであっても差し支えない。 (Other embodiments)
(1) In each of the above-described embodiments, as shown in FIG. 2, thecentrifugal fan 18 is a turbo fan, but it may be another type of centrifugal fan such as a radial fan.
(1)上述の各実施形態では、図2に示すように、遠心ファン18はターボファンであるが、例えばラジアルファンなど、他の形式の遠心ファンであっても差し支えない。 (Other embodiments)
(1) In each of the above-described embodiments, as shown in FIG. 2, the
(2)上述の各実施形態では、図2に示すように、電動モータ16はアウターロータ型ブラシレスDCモータであるが、そのモータ形式に限定はない。例えば、電動モータ16はインナーロータ型モータであってもよいし、ブラシ付きモータであってもよい。
(2) In each of the above-described embodiments, as shown in FIG. 2, the electric motor 16 is an outer rotor type brushless DC motor, but the motor type is not limited. For example, the electric motor 16 may be an inner rotor type motor or a motor with brushes.
(3)上述の各実施形態では、図2、図4の縦断面において、第2前縁部323bは直線的に延伸しているが、湾曲していても差し支えない。
(3) In each of the embodiments described above, the second front edge portion 323b extends linearly in the vertical cross sections of FIGS. 2 and 4, but it may be curved.
(4)上述の第1実施形態では、図2に示すように、主板36の外径Dmoと側板34の外径Dsoは同じ大きさであるが、これは一例である。例えば、主板36の外径Dmoは、側板34の外径Dsoに対し大きくてもよいし、或いは、側板34の外径Dsoに対し小さくてもよい。
(4) In the first embodiment described above, as shown in FIG. 2, the outer diameter Dmo of the main plate 36 and the outer diameter Dso of the side plate 34 are the same size, but this is an example. For example, the outer diameter Dmo of the main plate 36 may be larger than the outer diameter Dso of the side plate 34 or may be smaller than the outer diameter Dso of the side plate 34 .
(5)なお、本開示は、上述の実施形態に限定されることなく、種々変形して実施することができる。また、上記各実施形態は、互いに無関係なものではなく、組み合わせが明らかに不可な場合を除き、適宜組み合わせが可能である。
(5) It should be noted that the present disclosure is not limited to the above-described embodiments, and can be implemented in various modifications. Moreover, the above-described embodiments are not unrelated to each other, and can be appropriately combined unless the combination is clearly impossible.
また、上記各実施形態において、実施形態を構成する要素は、特に必須であると明示した場合および原理的に明らかに必須であると考えられる場合等を除き、必ずしも必須のものではないことは言うまでもない。また、上記各実施形態において、実施形態の構成要素の個数、数値、量、範囲等の数値が言及されている場合、特に必須であると明示した場合および原理的に明らかに特定の数に限定される場合等を除き、その特定の数に限定されるものではない。また、上記各実施形態において、構成要素等の材質、形状、位置関係等に言及するときは、特に明示した場合および原理的に特定の材質、形状、位置関係等に限定される場合等を除き、その材質、形状、位置関係等に限定されるものではない。
Further, in each of the above-described embodiments, it goes without saying that the elements constituting the embodiment are not necessarily essential, unless it is explicitly stated that they are essential, or they are clearly considered essential in principle. stomach. In addition, in each of the above-described embodiments, when numerical values such as the number, numerical value, amount, range, etc. of the constituent elements of the embodiment are mentioned, when it is explicitly stated that they are particularly essential, and when they are clearly limited to a specific number in principle It is not limited to that specific number, except when In addition, in each of the above-described embodiments, when referring to the material, shape, positional relationship, etc. of the constituent elements, unless otherwise specified or in principle limited to a specific material, shape, positional relationship, etc. , its material, shape, positional relationship, and the like.
(本開示の特徴)
[第1の観点]
ファン軸心(CL)まわりに回転することで該ファン軸心の軸方向(Da)の一方側から空気を吸い込むと共に該吸い込んだ空気を前記ファン軸心の径方向(Dr)の外側へ吹き出す遠心ファンであって、
前記ファン軸心まわりに並んで配置され、前記径方向の外側に翼後縁部(324)を有する複数枚の翼(32)と、
空気が吸い込まれる吸気孔(34a)が形成され、前記複数枚の翼に対して前記軸方向の前記一方側に設けられ該複数枚の翼のそれぞれに連結された側板(34)と、
前記複数枚の翼のそれぞれに対し前記側板側とは反対側で連結され、前記径方向に拡がる主板(36、43、401)とを備え、
前記側板の内径をDsiとし且つ前記側板の外径をDsoとした場合に、Dsi/Dsoは、0.5<Dsi/Dso<0.7であり、
前記翼後縁部は、前記軸方向の前記一方側ほど前記径方向の内側に位置するように形成されている、遠心ファン。
[第2の観点]
前記側板は、前記軸方向の前記一方側とは反対側の他方側を向いて前記径方向に拡がる側板他方面(343)を有し、
前記側板他方面は前記径方向の外側ほど前記軸方向の前記他方側に位置し、
前記ファン軸心を含む縦断面において、前記側板他方面の曲率半径は前記径方向の外側ほど大きくなる、第1の観点に記載の遠心ファン。
[第3の観点]
前記側板は、前記軸方向の前記一方側とは反対側の他方側を向いて前記径方向に拡がる側板他方面(343)を有し、
前記側板他方面は前記径方向の外側ほど前記軸方向の前記他方側に位置し、
前記ファン軸心を含む縦断面において、前記側板他方面は1つの円弧または直線で形成される、第1の観点に記載の遠心ファン。
[第4の観点]
前記複数枚の翼はそれぞれ、前記径方向の内側に翼前縁部(323)を有し、
前記翼前縁部は、前記側板側から前記主板側へと延びると共に、前記主板側ほど前記径方向の内側に位置するように形成されている、第1ないし第3の観点のいずれか1つに記載の遠心ファン。
[第5の観点]
前記翼前縁部の一部は、前記翼後縁部が前記軸方向に占める全幅(Hb)に含まれる軸方向範囲(Hb1)内に入っている、第4の観点に記載の遠心ファン。
[第6の観点]
前記側板と前記主板はそれぞれ、前記翼後縁部よりも前記径方向の外側にまで延びている、第1ないし第5の観点のいずれか1つに記載の遠心ファン。
[第7の観点]
前記側板と前記主板はそれぞれ、前記翼後縁部よりも前記径方向の外側にまで延びており、
前記複数枚の翼の最大外径をDb2とし且つ前記主板の外径をDmoとした場合に、Db2<Dmo≦1.13×Db2の関係が成立する、第1ないし第5の観点のいずれか1つに記載の遠心ファン。
[第8の観点]
送風機(10)の一部を構成する遠心ファンであって、
前記送風機は、前記側板に対し前記翼側とは反対側に設けられ前記側板から離れて配置される側板隣接ケース(22)を有し、
前記側板は、前記径方向の外側に設けられた外周端部(342)を有し、前記側板隣接ケースとの間にケース側板隙間(34b)を形成し、
前記側板隣接ケースは、前記側板の外周端部に対し前記径方向の外側に重なるように設けられるケース外周部(222)を有し、
前記側板の外周端部は、前記ケース外周部に対し前記径方向に対向し、前記ケース側板隙間の開口端(34c)を前記ケース外周部との間に形成する、第1ないし第7の観点のいずれか1つに記載の遠心ファン。
[第9の観点]
前記翼後縁部は、前記側板側から前記主板側へと延びており、
前記複数枚の翼の厚み(tb)はそれぞれ、前記翼後縁部では前記側板側ほど大きくなっている、第1ないし第8の観点のいずれか1つに記載の遠心ファン。
[第10の観点]
前記ファン軸心に垂直な横断面において、前記翼後縁部は、凸状に湾曲した後縁部外面(324a)を有し、該後縁部外面の曲率半径(Rb)は前記側板側ほど大きくなっている、第9の観点に記載の遠心ファン。 (Features of the present disclosure)
[First viewpoint]
A centrifugal force that rotates around the fan axis (CL) to suck air from one side in the axial direction (Da) of the fan axis and blow the sucked air outward in the radial direction (Dr) of the fan axis. being a fan
a plurality of blades (32) arranged side by side around the fan axis and having a blade trailing edge (324) on the radially outer side;
a side plate (34) formed with an intake hole (34a) through which air is sucked, provided on the one side of the plurality of blades in the axial direction and connected to each of the plurality of blades;
a main plate (36, 43, 401) connected to each of the plurality of blades on the side opposite to the side plate side and extending in the radial direction;
When the inner diameter of the side plate is Dsi and the outer diameter of the side plate is Dso, Dsi/Dso is 0.5<Dsi/Dso<0.7,
The centrifugal fan, wherein the trailing edge portion of the blade is formed so as to be located radially inward toward the one side in the axial direction.
[Second Viewpoint]
The side plate has a side plate other surface (343) that faces the other side opposite to the one side in the axial direction and spreads in the radial direction,
the other surface of the side plate is located on the other side in the axial direction toward the outer side in the radial direction;
The centrifugal fan according to the first aspect, wherein in a longitudinal section including the fan axis, the radius of curvature of the other surface of the side plate increases toward the outer side in the radial direction.
[Third Viewpoint]
The side plate has a side plate other surface (343) that faces the other side opposite to the one side in the axial direction and spreads in the radial direction,
the other surface of the side plate is located on the other side in the axial direction toward the outer side in the radial direction;
The centrifugal fan according to the first aspect, wherein the other side surface of the side plate is formed by a single arc or straight line in a longitudinal section including the fan axis.
[Fourth point of view]
each of the plurality of blades has a blade leading edge (323) on the inner side in the radial direction;
Any one of the first to third aspects, wherein the leading edge portion of the blade extends from the side plate side to the main plate side and is positioned radially inward toward the main plate side. centrifugal fan described in .
[Fifth Viewpoint]
A centrifugal fan according to a fourth aspect, wherein a portion of the blade leading edge falls within an axial range (Hb1) included in the overall width (Hb) occupied by the blade trailing edge in the axial direction.
[Sixth viewpoint]
The centrifugal fan according to any one of the first to fifth aspects, wherein each of the side plate and the main plate extends outward in the radial direction from the trailing edge of the blade.
[Seventh viewpoint]
each of the side plate and the main plate extends outward in the radial direction from the trailing edge of the blade;
Any one of the first to fifth aspects, wherein a relationship of Db2<Dmo≦1.13×Db2 holds, where Db2 is the maximum outer diameter of the plurality of blades and Dmo is the outer diameter of the main plate. 1. A centrifugal fan according to one.
[Eighth point of view]
A centrifugal fan forming part of a blower (10),
The blower has a side plate adjacent case (22) provided on the side opposite to the blade side with respect to the side plate and arranged away from the side plate,
The side plate has an outer peripheral end portion (342) provided on the outer side in the radial direction, and forms a case side plate gap (34b) between the side plate adjacent case and the side plate,
The side plate adjacent case has a case outer peripheral portion (222) provided so as to overlap the outer peripheral end portion of the side plate in the radial direction,
The first to seventh aspects, wherein the outer peripheral edge of the side plate faces the outer peripheral portion of the case in the radial direction, and an opening end (34c) of the gap between the case side plates is formed between the outer peripheral portion of the case and the outer peripheral portion of the case. A centrifugal fan according to any one of .
[Ninth Aspect]
The blade trailing edge extends from the side plate side to the main plate side,
The centrifugal fan according to any one of the first to eighth aspects, wherein the thickness (tb) of each of the plurality of blades increases toward the side plate at the trailing edge of the blade.
[Tenth Aspect]
In a cross section perpendicular to the fan axis, the blade trailing edge has a convexly curved trailing edge outer surface (324a), and the radius of curvature (Rb) of the trailing edge outer surface increases toward the side plate. A centrifugal fan according to the ninth aspect, which is enlarged.
[第1の観点]
ファン軸心(CL)まわりに回転することで該ファン軸心の軸方向(Da)の一方側から空気を吸い込むと共に該吸い込んだ空気を前記ファン軸心の径方向(Dr)の外側へ吹き出す遠心ファンであって、
前記ファン軸心まわりに並んで配置され、前記径方向の外側に翼後縁部(324)を有する複数枚の翼(32)と、
空気が吸い込まれる吸気孔(34a)が形成され、前記複数枚の翼に対して前記軸方向の前記一方側に設けられ該複数枚の翼のそれぞれに連結された側板(34)と、
前記複数枚の翼のそれぞれに対し前記側板側とは反対側で連結され、前記径方向に拡がる主板(36、43、401)とを備え、
前記側板の内径をDsiとし且つ前記側板の外径をDsoとした場合に、Dsi/Dsoは、0.5<Dsi/Dso<0.7であり、
前記翼後縁部は、前記軸方向の前記一方側ほど前記径方向の内側に位置するように形成されている、遠心ファン。
[第2の観点]
前記側板は、前記軸方向の前記一方側とは反対側の他方側を向いて前記径方向に拡がる側板他方面(343)を有し、
前記側板他方面は前記径方向の外側ほど前記軸方向の前記他方側に位置し、
前記ファン軸心を含む縦断面において、前記側板他方面の曲率半径は前記径方向の外側ほど大きくなる、第1の観点に記載の遠心ファン。
[第3の観点]
前記側板は、前記軸方向の前記一方側とは反対側の他方側を向いて前記径方向に拡がる側板他方面(343)を有し、
前記側板他方面は前記径方向の外側ほど前記軸方向の前記他方側に位置し、
前記ファン軸心を含む縦断面において、前記側板他方面は1つの円弧または直線で形成される、第1の観点に記載の遠心ファン。
[第4の観点]
前記複数枚の翼はそれぞれ、前記径方向の内側に翼前縁部(323)を有し、
前記翼前縁部は、前記側板側から前記主板側へと延びると共に、前記主板側ほど前記径方向の内側に位置するように形成されている、第1ないし第3の観点のいずれか1つに記載の遠心ファン。
[第5の観点]
前記翼前縁部の一部は、前記翼後縁部が前記軸方向に占める全幅(Hb)に含まれる軸方向範囲(Hb1)内に入っている、第4の観点に記載の遠心ファン。
[第6の観点]
前記側板と前記主板はそれぞれ、前記翼後縁部よりも前記径方向の外側にまで延びている、第1ないし第5の観点のいずれか1つに記載の遠心ファン。
[第7の観点]
前記側板と前記主板はそれぞれ、前記翼後縁部よりも前記径方向の外側にまで延びており、
前記複数枚の翼の最大外径をDb2とし且つ前記主板の外径をDmoとした場合に、Db2<Dmo≦1.13×Db2の関係が成立する、第1ないし第5の観点のいずれか1つに記載の遠心ファン。
[第8の観点]
送風機(10)の一部を構成する遠心ファンであって、
前記送風機は、前記側板に対し前記翼側とは反対側に設けられ前記側板から離れて配置される側板隣接ケース(22)を有し、
前記側板は、前記径方向の外側に設けられた外周端部(342)を有し、前記側板隣接ケースとの間にケース側板隙間(34b)を形成し、
前記側板隣接ケースは、前記側板の外周端部に対し前記径方向の外側に重なるように設けられるケース外周部(222)を有し、
前記側板の外周端部は、前記ケース外周部に対し前記径方向に対向し、前記ケース側板隙間の開口端(34c)を前記ケース外周部との間に形成する、第1ないし第7の観点のいずれか1つに記載の遠心ファン。
[第9の観点]
前記翼後縁部は、前記側板側から前記主板側へと延びており、
前記複数枚の翼の厚み(tb)はそれぞれ、前記翼後縁部では前記側板側ほど大きくなっている、第1ないし第8の観点のいずれか1つに記載の遠心ファン。
[第10の観点]
前記ファン軸心に垂直な横断面において、前記翼後縁部は、凸状に湾曲した後縁部外面(324a)を有し、該後縁部外面の曲率半径(Rb)は前記側板側ほど大きくなっている、第9の観点に記載の遠心ファン。 (Features of the present disclosure)
[First viewpoint]
A centrifugal force that rotates around the fan axis (CL) to suck air from one side in the axial direction (Da) of the fan axis and blow the sucked air outward in the radial direction (Dr) of the fan axis. being a fan
a plurality of blades (32) arranged side by side around the fan axis and having a blade trailing edge (324) on the radially outer side;
a side plate (34) formed with an intake hole (34a) through which air is sucked, provided on the one side of the plurality of blades in the axial direction and connected to each of the plurality of blades;
a main plate (36, 43, 401) connected to each of the plurality of blades on the side opposite to the side plate side and extending in the radial direction;
When the inner diameter of the side plate is Dsi and the outer diameter of the side plate is Dso, Dsi/Dso is 0.5<Dsi/Dso<0.7,
The centrifugal fan, wherein the trailing edge portion of the blade is formed so as to be located radially inward toward the one side in the axial direction.
[Second Viewpoint]
The side plate has a side plate other surface (343) that faces the other side opposite to the one side in the axial direction and spreads in the radial direction,
the other surface of the side plate is located on the other side in the axial direction toward the outer side in the radial direction;
The centrifugal fan according to the first aspect, wherein in a longitudinal section including the fan axis, the radius of curvature of the other surface of the side plate increases toward the outer side in the radial direction.
[Third Viewpoint]
The side plate has a side plate other surface (343) that faces the other side opposite to the one side in the axial direction and spreads in the radial direction,
the other surface of the side plate is located on the other side in the axial direction toward the outer side in the radial direction;
The centrifugal fan according to the first aspect, wherein the other side surface of the side plate is formed by a single arc or straight line in a longitudinal section including the fan axis.
[Fourth point of view]
each of the plurality of blades has a blade leading edge (323) on the inner side in the radial direction;
Any one of the first to third aspects, wherein the leading edge portion of the blade extends from the side plate side to the main plate side and is positioned radially inward toward the main plate side. centrifugal fan described in .
[Fifth Viewpoint]
A centrifugal fan according to a fourth aspect, wherein a portion of the blade leading edge falls within an axial range (Hb1) included in the overall width (Hb) occupied by the blade trailing edge in the axial direction.
[Sixth viewpoint]
The centrifugal fan according to any one of the first to fifth aspects, wherein each of the side plate and the main plate extends outward in the radial direction from the trailing edge of the blade.
[Seventh viewpoint]
each of the side plate and the main plate extends outward in the radial direction from the trailing edge of the blade;
Any one of the first to fifth aspects, wherein a relationship of Db2<Dmo≦1.13×Db2 holds, where Db2 is the maximum outer diameter of the plurality of blades and Dmo is the outer diameter of the main plate. 1. A centrifugal fan according to one.
[Eighth point of view]
A centrifugal fan forming part of a blower (10),
The blower has a side plate adjacent case (22) provided on the side opposite to the blade side with respect to the side plate and arranged away from the side plate,
The side plate has an outer peripheral end portion (342) provided on the outer side in the radial direction, and forms a case side plate gap (34b) between the side plate adjacent case and the side plate,
The side plate adjacent case has a case outer peripheral portion (222) provided so as to overlap the outer peripheral end portion of the side plate in the radial direction,
The first to seventh aspects, wherein the outer peripheral edge of the side plate faces the outer peripheral portion of the case in the radial direction, and an opening end (34c) of the gap between the case side plates is formed between the outer peripheral portion of the case and the outer peripheral portion of the case. A centrifugal fan according to any one of .
[Ninth Aspect]
The blade trailing edge extends from the side plate side to the main plate side,
The centrifugal fan according to any one of the first to eighth aspects, wherein the thickness (tb) of each of the plurality of blades increases toward the side plate at the trailing edge of the blade.
[Tenth Aspect]
In a cross section perpendicular to the fan axis, the blade trailing edge has a convexly curved trailing edge outer surface (324a), and the radius of curvature (Rb) of the trailing edge outer surface increases toward the side plate. A centrifugal fan according to the ninth aspect, which is enlarged.
Claims (10)
- ファン軸心(CL)まわりに回転することで該ファン軸心の軸方向(Da)の一方側から空気を吸い込むと共に該吸い込んだ空気を前記ファン軸心の径方向(Dr)の外側へ吹き出す遠心ファンであって、
前記ファン軸心まわりに並んで配置され、前記径方向の外側に翼後縁部(324)を有する複数枚の翼(32)と、
空気が吸い込まれる吸気孔(34a)が形成され、前記複数枚の翼に対して前記軸方向の前記一方側に設けられ該複数枚の翼のそれぞれに連結された側板(34)と、
前記複数枚の翼のそれぞれに対し前記側板側とは反対側で連結され、前記径方向に拡がる主板(36、43、401)とを備え、
前記側板の内径をDsiとし且つ前記側板の外径をDsoとした場合に、Dsi/Dsoは、0.5<Dsi/Dso<0.7であり、
前記翼後縁部は、前記軸方向の前記一方側ほど前記径方向の内側に位置するように形成されている、遠心ファン。 A centrifugal force that rotates around the fan axis (CL) to suck air from one side in the axial direction (Da) of the fan axis and blow the sucked air outward in the radial direction (Dr) of the fan axis. being a fan
a plurality of blades (32) arranged side by side around the fan axis and having a blade trailing edge (324) on the radially outer side;
a side plate (34) formed with an intake hole (34a) through which air is sucked, provided on the one side of the plurality of blades in the axial direction and connected to each of the plurality of blades;
a main plate (36, 43, 401) connected to each of the plurality of blades on the side opposite to the side plate side and extending in the radial direction;
When the inner diameter of the side plate is Dsi and the outer diameter of the side plate is Dso, Dsi/Dso is 0.5<Dsi/Dso<0.7,
The centrifugal fan, wherein the trailing edge portion of the blade is formed so as to be located radially inward toward the one side in the axial direction. - 前記側板は、前記軸方向の前記一方側とは反対側の他方側を向いて前記径方向に拡がる側板他方面(343)を有し、
前記側板他方面は前記径方向の外側ほど前記軸方向の前記他方側に位置し、
前記ファン軸心を含む縦断面において、前記側板他方面の曲率半径は前記径方向の外側ほど大きくなる、請求項1に記載の遠心ファン。 The side plate has a side plate other surface (343) that faces the other side opposite to the one side in the axial direction and spreads in the radial direction,
the other surface of the side plate is located on the other side in the axial direction toward the outer side in the radial direction;
2. The centrifugal fan according to claim 1, wherein, in a longitudinal section including the fan axis, the radius of curvature of the other surface of the side plate increases toward the outer side in the radial direction. - 前記側板は、前記軸方向の前記一方側とは反対側の他方側を向いて前記径方向に拡がる側板他方面(343)を有し、
前記側板他方面は前記径方向の外側ほど前記軸方向の前記他方側に位置し、
前記ファン軸心を含む縦断面において、前記側板他方面は1つの円弧または直線で形成される、請求項1に記載の遠心ファン。 The side plate has a side plate other surface (343) that faces the other side opposite to the one side in the axial direction and spreads in the radial direction,
the other surface of the side plate is located on the other side in the axial direction toward the outer side in the radial direction;
2. The centrifugal fan according to claim 1, wherein the other side surface of the side plate is formed by a single arc or straight line in a longitudinal section including the fan axis. - 前記複数枚の翼はそれぞれ、前記径方向の内側に翼前縁部(323)を有し、
前記翼前縁部は、前記側板側から前記主板側へと延びると共に、前記主板側ほど前記径方向の内側に位置するように形成されている、請求項1ないし3のいずれか1つに記載の遠心ファン。 each of the plurality of blades has a blade leading edge (323) on the inner side in the radial direction;
4. The blade leading edge portion according to any one of claims 1 to 3, wherein said blade leading edge portion extends from said side plate side toward said main plate side and is formed so as to be positioned radially inward toward said main plate side. centrifugal fan. - 前記翼前縁部の一部は、前記翼後縁部が前記軸方向に占める全幅(Hb)に含まれる軸方向範囲(Hb1)内に入っている、請求項4に記載の遠心ファン。 The centrifugal fan according to claim 4, wherein a part of said blade leading edge is within an axial range (Hb1) included in the total width (Hb) occupied by said blade trailing edge in said axial direction.
- 前記側板と前記主板はそれぞれ、前記翼後縁部よりも前記径方向の外側にまで延びている、請求項1ないし3のいずれか1つに記載の遠心ファン。 The centrifugal fan according to any one of claims 1 to 3, wherein each of said side plate and said main plate extends outward in said radial direction from said blade trailing edge portion.
- 前記側板と前記主板はそれぞれ、前記翼後縁部よりも前記径方向の外側にまで延びており、
前記複数枚の翼の最大外径をDb2とし且つ前記主板の外径をDmoとした場合に、Db2<Dmo≦1.13×Db2の関係が成立する、請求項1ないし3のいずれか1つに記載の遠心ファン。 each of the side plate and the main plate extends outward in the radial direction from the trailing edge of the blade;
4. Any one of claims 1 to 3, wherein a relationship of Db2<Dmo≦1.13×Db2 holds when Db2 is the maximum outer diameter of the plurality of blades and Dmo is the outer diameter of the main plate. centrifugal fan described in . - 送風機(10)の一部を構成する遠心ファンであって、
前記送風機は、前記側板に対し前記翼側とは反対側に設けられ前記側板から離れて配置される側板隣接ケース(22)を有し、
前記側板は、前記径方向の外側に設けられた外周端部(342)を有し、前記側板隣接ケースとの間にケース側板隙間(34b)を形成し、
前記側板隣接ケースは、前記側板の外周端部に対し前記径方向の外側に重なるように設けられるケース外周部(222)を有し、
前記側板の外周端部は、前記ケース外周部に対し前記径方向に対向し、前記ケース側板隙間の開口端(34c)を前記ケース外周部との間に形成する、請求項1ないし3のいずれか1つに記載の遠心ファン。 A centrifugal fan forming part of a blower (10),
The blower has a side plate adjacent case (22) provided on the side opposite to the blade side with respect to the side plate and arranged away from the side plate,
The side plate has an outer peripheral end portion (342) provided on the outer side in the radial direction, and forms a case side plate gap (34b) between the side plate adjacent case and the side plate,
The side plate adjacent case has a case outer peripheral portion (222) provided so as to overlap the outer peripheral end portion of the side plate in the radial direction,
4. The outer peripheral end portion of the side plate is opposed to the outer peripheral portion of the case in the radial direction, and forms an opening end (34c) of the gap between the case side plates and the outer peripheral portion of the case. or a centrifugal fan according to one of the preceding claims. - 前記翼後縁部は、前記側板側から前記主板側へと延びており、
前記複数枚の翼の厚み(tb)はそれぞれ、前記翼後縁部では前記側板側ほど大きくなっている、請求項1ないし3のいずれか1つに記載の遠心ファン。 The blade trailing edge extends from the side plate side to the main plate side,
4. The centrifugal fan according to any one of claims 1 to 3, wherein the thickness (tb) of each of said plurality of blades increases toward said side plate side at said blade trailing edge portion. - 前記ファン軸心に垂直な横断面において、前記翼後縁部は、凸状に湾曲した後縁部外面(324a)を有し、該後縁部外面の曲率半径(Rb)は前記側板側ほど大きくなっている、請求項9に記載の遠心ファン。 In a cross section perpendicular to the fan axis, the blade trailing edge has a convexly curved trailing edge outer surface (324a), and the radius of curvature (Rb) of the trailing edge outer surface increases toward the side plate. 10. The centrifugal fan of claim 9, being enlarged.
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JPH0270997A (en) * | 1988-09-06 | 1990-03-09 | Matsushita Refrig Co Ltd | Centrifugal blower |
JPH02166323A (en) * | 1988-12-20 | 1990-06-27 | Daikin Ind Ltd | Airconditioning device |
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WO2015170401A1 (en) * | 2014-05-09 | 2015-11-12 | 三菱電機株式会社 | Centrifugal blower and electric vacuum cleaner |
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JPH0270997A (en) * | 1988-09-06 | 1990-03-09 | Matsushita Refrig Co Ltd | Centrifugal blower |
JPH02166323A (en) * | 1988-12-20 | 1990-06-27 | Daikin Ind Ltd | Airconditioning device |
JP2001132687A (en) * | 1999-11-10 | 2001-05-18 | Mitsubishi Electric Corp | Impeller of centrifugal air blower and air conditioner |
WO2009139422A1 (en) * | 2008-05-14 | 2009-11-19 | ダイキン工業株式会社 | Centrifugal fan |
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