WO2024038622A1 - Multiblade centrifugal blower - Google Patents
Multiblade centrifugal blower Download PDFInfo
- Publication number
- WO2024038622A1 WO2024038622A1 PCT/JP2022/039681 JP2022039681W WO2024038622A1 WO 2024038622 A1 WO2024038622 A1 WO 2024038622A1 JP 2022039681 W JP2022039681 W JP 2022039681W WO 2024038622 A1 WO2024038622 A1 WO 2024038622A1
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- WIPO (PCT)
- Prior art keywords
- blade
- fan
- centrifugal blower
- blades
- axial direction
- Prior art date
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- 230000002093 peripheral effect Effects 0.000 claims abstract description 137
- 238000004804 winding Methods 0.000 description 12
- 230000007423 decrease Effects 0.000 description 7
- 238000000926 separation method Methods 0.000 description 7
- 230000001965 increasing effect Effects 0.000 description 6
- 230000003068 static effect Effects 0.000 description 5
- 230000000694 effects Effects 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 2
- 238000000638 solvent extraction Methods 0.000 description 2
- 238000011144 upstream manufacturing Methods 0.000 description 2
- 238000009423 ventilation Methods 0.000 description 2
- 238000007664 blowing Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000009751 slip forming Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
-
- 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
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
Definitions
- the present disclosure relates to a multi-blade centrifugal blower with a scroll casing.
- a conventional multi-blade centrifugal blower includes a fan having a disc-shaped main plate, a plurality of blades installed on the peripheral edge of the main plate, and side plates that fix the ends of the blades.
- conventional multi-blade centrifugal blowers are equipped with a scroll casing that has a spiral peripheral wall that covers the fan, and a bell mouth is provided at the suction port of the scroll casing to smoothly draw airflow to the fan. .
- the airflow that flows out between the blades as the fan rotates is boosted by the expanded air passage inside the scroll casing, so the blades are forward-facing blades that are inclined in the direction of fan rotation.
- the inner circumferential side of the blade is the backward-facing blade
- the outer circumferential side of the blade is the forward-facing blade
- the angle of the blade surface between the inner circumferential side and the outer circumferential side of the blade is Because the change is large, there is a risk that new separation of airflow will occur on the suction surface of the blade, resulting in a decrease in air volume.
- the present disclosure is intended to solve the above-mentioned problems, and provides a multi-blade centrifugal blower that can suppress separation of airflow on the negative pressure surface of the blade and suppress a decrease in air volume.
- a multi-blade centrifugal blower includes a main plate that is circular when viewed in the axial direction of the rotating shaft, a plurality of blades installed on the peripheral edge of the main plate, and a plurality of blades in the axial direction of the rotating shaft.
- an annular side plate fixing an end opposite to the main plate of the fan, a peripheral wall formed in a spiral shape, and at least one side wall having a bell mouth forming a suction port; a scroll casing that forms a discharge port through which airflow generated by the fan is discharged and houses a fan, the fan having a rearward direction at the inner peripheral side of each of the plurality of blades in the radial direction of the fan.
- the rearward blade part that constitutes the blade When viewed in the axial direction of the rotating shaft, the rearward blade part that constitutes the blade, the forward blade part that constitutes the forward blade at the outer peripheral side of each of the plurality of blades in the radial direction of the fan, , an inflection point part forming an inflection point between the rearward blade part and the forward blade part, and the inflection point part is located on the main plate side of each of the plurality of blades in the axial direction of the rotation shaft. It is formed over the entire length of the blade, which is the part between the base end of the fan and the tip of the side plate, and the entire axial part of the inflection point extends along the inner edge of the bell mouth in the radial direction of the fan. It is formed so as to be located on the inner peripheral side of the inner peripheral end portion to be formed.
- the fan of the multi-blade centrifugal blower includes a backward blade portion, a forward blade portion, and an inflection point portion that forms an inflection point between the rearward blade portion and the forward blade portion.
- the inflection point portion is formed over the entire length of the blade, which is a portion between the base end portion on the main plate side and the tip portion on the side plate side of each of the plurality of blades in the axial direction of the rotating shaft. Further, all portions of the inflection point portion in the axial direction of the rotation shaft are formed so as to be located on the inner circumferential side of the inner circumferential end forming the inner edge of the bell mouth in the radial direction of the fan. .
- the multi-blade centrifugal blower can gradually change the blade angle from the leading edge side toward the trailing edge side, suppressing separation of airflow on the negative pressure surface and suppressing a decrease in air volume.
- FIG. 1 is an external view schematically showing a configuration of a multi-blade centrifugal blower 1 according to a first embodiment when viewed parallel to a rotation axis RA.
- FIG. 1 is a perspective view of a multi-blade centrifugal blower according to Embodiment 1.
- FIG. 1 is a perspective view of a fan of a multi-blade centrifugal blower according to Embodiment 1.
- FIG. 1 is a plan view of a fan of a multi-blade centrifugal blower according to Embodiment 1.
- FIG. FIG. 3 is a partially enlarged view of a fan in the multi-blade centrifugal blower according to the first embodiment.
- FIG. 1 is a partial cross-sectional view of a multi-blade centrifugal blower according to Embodiment 1.
- FIG. FIG. 2 is a partial cross-sectional view of a multi-blade centrifugal blower according to a second embodiment.
- FIG. 7 is a partial cross-sectional view of a multi-blade centrifugal blower according to Embodiment 3.
- FIG. 7 is a partially enlarged view of a fan in a multi-blade centrifugal blower according to Embodiment 4;
- FIG. 1 is an external view schematically showing the configuration of a multi-blade centrifugal blower 1 according to Embodiment 1, viewed parallel to the rotation axis RA.
- FIG. 2 is a perspective view of the multi-blade centrifugal blower 1 according to the first embodiment.
- the arrow R in FIG. 1 indicates the rotation direction of the fan 2
- the broken line arrow CD indicates the circumferential direction of the fan 2.
- FIG. 2 explains the external appearance of the multi-blade centrifugal blower 1, and the internal configuration of the multi-blade centrifugal blower 1 is shown in a simplified manner.
- the basic structure of the multi-blade centrifugal blower 1 will be explained using FIGS. 1 and 2.
- the multi-blade centrifugal blower 1 is a device that sends air using centrifugal force generated by the rotation of the fan 2, and is, for example, a sirocco fan.
- the multi-blade centrifugal blower 1 is a single-suction type centrifugal blower in which air is sucked in from one side of the scroll casing 4 in the axial direction of the imaginary rotational axis RA of the fan 2 .
- the multi-blade centrifugal blower 1 is not limited to a single suction type centrifugal blower, but may be a double suction type centrifugal blower in which air is sucked in from both sides of the scroll casing 4 in the axial direction of the rotation axis RA.
- the multi-blade centrifugal blower 1 includes a fan 2 that generates airflow and a scroll casing 4 that houses the fan 2 therein.
- FIG. 3 is a perspective view of the fan 2 of the multi-blade centrifugal blower 1 according to the first embodiment.
- FIG. 4 is a plan view of the fan 2 of the multi-blade centrifugal blower 1 according to the first embodiment. Note that FIG. 4 is a diagram of the fan 2 viewed in the axial direction of the rotation axis RA. The fan 2 will be explained using FIGS. 1 to 4.
- the fan 2 is a centrifugal fan.
- the fan 2 is connected to a motor (not shown) having a drive shaft.
- the fan 2 is rotationally driven by a motor, and uses centrifugal force generated by the rotation to forcibly send air outward in the radial direction.
- the fan 2 is rotated in the direction of rotation indicated by an arrow R by a motor or the like.
- the fan 2 when viewed in the direction of the rotation axis RA, has a circular main plate 2a, an annular side plate 2c, and a peripheral edge 2a1 of the main plate 2a. It has a plurality of wings 2d arranged at.
- the fan 2 is formed into a bottomed cylindrical shape by a main plate 2a and a plurality of blades 2d arranged on the main plate 2a.
- the fan 2 has a fan suction port 2e formed in a portion on the side plate 2c side opposite to the main plate 2a in the axial direction of the rotation axis RA.
- the fan suction port 2e is an opening of the fan 2 through which air flows into the fan 2, and allows gas to flow into a space surrounded by the main plate 2a and the plurality of blades 2d.
- the main plate 2a is formed into a circular shape when viewed in the axial direction of the rotation axis RA. In the radial direction centered on the rotation axis RA, it has a peripheral portion two a1 formed on the outer circumferential side and a central portion two a2 formed on the inner circumferential side.
- the peripheral portion two a1 is formed on the outer peripheral side of the central portion two a2, and is formed in an annular shape when viewed in the axial direction of the rotation axis RA.
- the peripheral portion two a1 is formed into a plate shape.
- the central portion two a2 is formed on the inner peripheral side of the peripheral edge two a1, and is formed to protrude from the inner peripheral edge portion of the peripheral edge two a1.
- the central portion 2a2 is formed of a plate-like member formed in a mountain shape.
- the central portion 2a2 is formed inside the plurality of wings 2d.
- the main plate 2a may have a peripheral portion two a1 and a central portion two a2 integrally formed.
- the main plate 2a may be formed into a flat plate shape as a whole.
- the main plate 2a may be formed into a disk shape, a polygonal shape, or the like.
- the thickness of the main plate 2a may be formed such that the thickness of the wall becomes thicker toward the center in the radial direction centered on the rotation axis RA, or a constant thickness in the radial direction centered on the rotation axis RA. It may be formed in the same way.
- the main plate 2a is not limited to being composed of a single plate-like member, but may be composed of a plurality of plate-like members fixed integrally. Note that the radial direction centered on the rotation axis RA is a direction perpendicular to the axial direction of the rotation axis RA.
- a boss portion 2b to which the drive shaft of the motor is connected is provided at the center of the main plate 2a.
- a shaft hole into which the drive shaft of the motor is inserted is formed in the boss portion 2b.
- the boss portion 2b is formed, for example, in a cylindrical shape, but the shape of the boss portion 2b is not limited to the cylindrical shape.
- the boss portion 2b may be formed into a columnar shape, for example, a polygonal columnar shape.
- the main plate 2a is rotationally driven by a motor via the boss portion 2b.
- the fan 2 has an annular side plate 2c attached to an end of a plurality of blades 2d opposite to the main plate 2a in the axial direction of the rotation axis RA.
- the side plate 2c fixes the ends of the plurality of blades 2d on the side opposite to the main plate 2a in the axial direction of the rotation axis RA.
- the side plate 2c is provided on the outer peripheral surface 2f of the fan 2.
- the side plate 2c is provided on the outer side of the blade 2d in the radial direction centered on the rotation axis RA.
- the side plate 2c may be provided at the tip portion 2g of a plurality of blades 2d that protrude from the main plate 2a in the direction of the rotation axis RA.
- the side plate 2c maintains the positional relationship of the tips of each wing 2d by connecting the plurality of wings 2d.
- the side plate 2c reinforces the strength of the plurality of wings 2d by connecting the plurality of wings 2d.
- the plurality of wings 2d are installed on the peripheral edge portion two a1 of the main plate 2a.
- the plurality of blades 2d have one end connected to the main plate 2a, the other end connected to the side plate 2c, and are arranged in a circumferential direction centered on the rotation axis RA.
- Each of the plurality of wings 2d is arranged at least between the main plate 2a and the side plate 2c.
- the plurality of wings 2d are arranged circumferentially around the boss portion 2b, and their base ends are fixed on the surface of the main plate 2a.
- the surface on the rotation direction side is a pressure surface 2d1
- the surface on the opposite side to the rotation direction is a suction surface 2d2.
- the blades 2d are arranged circumferentially at a constant interval from each other on the peripheral edge 2a1 of the main plate 2a.
- Each wing 2d is provided so as to rise from the main plate 2a, and is formed in a plate shape.
- Each wing 2d is provided so as to stand up almost perpendicularly to the main plate 2a, but the invention is not limited to this, and each wing 2d may be provided at an angle with respect to the vertical direction of the main plate 2a. .
- the blade 2d is inclined such that the leading edge 25a moves away from the rotation axis RA as it goes from the main plate 2a side to the side plate 2c side.
- the leading edge 25a is formed by the inner peripheral end 25 of the blade 2d.
- the inner peripheral end 25 is an end on the inner peripheral side of the blade 2d in a cross section perpendicular to the rotation axis RA, and the leading edge 25a is a part where the inner peripheral end 25 is continuous in the axial direction of the rotation axis.
- the leading edge 25a of the blade 2d is inclined such that the inner diameter of the blade increases from the main plate 2a side toward the side plate 2c side.
- FIG. 5 is a partially enlarged view of the fan 2 in the multi-blade centrifugal blower 1 according to the first embodiment.
- FIG. 5 is an enlarged view of the fan 2 viewed in the axial direction of the rotation axis RA.
- the wing 2d is shown with the bell mouth 3 transparent in order to show the shape of the wing 2d.
- a part of the inner circumferential side of the wing 2d is formed to be located inside the inner circumferential end portion 35 of the bell mouth 3.
- the blade 2d of the fan 2 has a forward blade portion 21 and a backward blade portion 22 integrally formed.
- the blade 2d has a forward blade portion 21 that includes an outer peripheral end 24 and is configured as a forward blade, and a backward blade portion 22 that includes an inner peripheral end 25 and is configured as a backward blade. Further, the blade 2 d has an inflection point portion 26 that forms an inflection point between the backward blade portion 22 and the forward blade portion 21 when viewed in the axial direction of the rotation axis RA of the fan 2 . In the radial direction of the fan 2, the blades 2d are integrally formed in the order of the backward blade portion 22, the inflection point portion 26, and the forward blade portion 21 from the rotation axis RA toward the outer circumferential side.
- the backward blade portion 22 is a portion that constitutes a backward blade in the inner peripheral side of each of the plurality of blades 2d in the radial direction of the fan 2.
- the forward blade portion 21 is a portion that constitutes a forward blade on the outer peripheral side of each of the plurality of blades 2d in the radial direction of the fan 2.
- the inflection point portion 26 changes from the backward blade portion 22 to the forward blade portion 21 in the blade 2d, in which the inner peripheral side portion is formed by the backward blade and the outer peripheral side portion is formed by the forward blade. form part. That is, when viewed in the axial direction of the rotation axis RA of the fan 2, the inflection point portion 26 is a blade in which the inner circumferential side portion is formed by backward-facing blades, and the outer circumferential side portion is formed by forward-facing blades. At 2d, an inflection point between the backward blade portion 22 and the forward blade portion 21 is formed.
- the inflection point portion 26 forms a connection point between the backward blade portion 22 and the forward blade portion 21 when viewed in the axial direction of the rotation axis RA of the fan 2 .
- the inflection point portion 26 is a portion where inflection points at the boundary between the backward blade portion 22 and the forward blade portion 21 are connected in the axial direction of the rotation axis RA, and the backward blade portion 22 and the forward blade portion This is a part where connection points with 21 are connected.
- the fan 2 is driven to rotate around the rotation axis RA by being driven by a motor (not shown). As the fan 2 rotates, gas outside the multi-blade centrifugal blower 1 passes through the suction port 5 formed in the scroll casing 4 shown in FIG. It is sucked into the space surrounded by the two wings 2d. As the fan 2 rotates, the air sucked into the space surrounded by the main plate 2a and the plurality of blades 2d passes through the space between the blade 2d and the adjacent blade 2d, and passes in the radial direction of the fan 2. sent outward.
- the scroll casing 4 will be explained using FIGS. 1 and 2.
- the scroll casing 4 houses the fan 2 therein and rectifies the air blown out from the fan 2.
- the scroll casing 4 is a single suction type casing that has a side wall 4a in which a suction port 5 (described later) is formed on one side of the main plate 2a in the axial direction of the rotation axis RA.
- the scroll casing 4 is not limited to a single suction type casing, but may be a double suction type casing having side walls 4a in which suction ports 5, which will be described later, are formed on both sides of the main plate 2a in the axial direction of the rotation axis RA. But that's fine.
- the scroll casing 4 has a scroll part 41 and a discharge part 42.
- the scroll casing 4 has a peripheral wall 4c formed in a spiral shape and side walls 4a provided on both sides of the fan 2 in the axial direction of the rotation axis RA.
- the scroll portion 41 forms an air path that converts the dynamic pressure of the airflow generated by the fan 2 into static pressure.
- the scroll portion 41 has a side wall 4a that covers the fan 2 from the axial direction of the rotation axis RA, and a peripheral wall 4c that surrounds the fan 2 from the radial direction of the rotation axis RA of the boss portion 2b.
- the scroll portion 41 has a tongue portion 43 that is located between the scroll portion 41 and the discharge portion 42 and forms a curved surface, and that guides the airflow generated by the fan 2 to the discharge port 42a via the scroll portion 41.
- the internal space of the scroll portion 41 constituted by the peripheral wall 4c and the side wall 4a is a space through which air blown out from the fan 2 flows along the peripheral wall 4c.
- the scroll casing 4 includes two side walls 4a.
- the side wall 4a having the bell mouth 3 forming the suction port 5 is referred to as a first side wall 4a1
- the side wall 4a without the suction port 5 and the bell mouth 3 is referred to as a second side wall 4a2.
- Two side walls 4a arranged on both sides of the fan 2 are formed to face each other with a peripheral wall 4c interposed therebetween.
- the scroll casing 4 of the first embodiment includes a first side wall 4a1 and a second side wall 4a2 as the side walls 4a. That is, the scroll casing 4 has at least one side wall 4a provided with a bell mouth 3 that forms a suction port 5 that communicates with the space formed by the main plate 2a and the plurality of blades 2d.
- the first side wall 4a1 is a side wall 4a located on the side where the side plate 2c is arranged with respect to the main plate 2a.
- the second side wall 4a2 is a side wall 4a located on the side where the main plate 2a is disposed with respect to the side plate 2c.
- the side wall 4a is a general term for the first side wall four a1 and the second side wall four a2.
- a suction port 5 is formed in the first side wall 4a1 of the scroll casing 4 so that air can flow between the fan 2 and the outside of the scroll casing 4.
- the suction port 5 communicates with the fan suction port 2e, and is an air intake port that allows gas to flow into the space surrounded by the main plate 2a and the plurality of blades 2d.
- the suction port 5 is formed at a position facing the plate surface of the main plate 2a.
- the suction port 5 provided in the first side wall 4a1 is formed by the bell mouth 3. That is, the bell mouth 3 forms a suction port 5 that communicates the space outside the scroll casing 4 with the space formed by the main plate 2a and the plurality of blades 2d.
- the bell mouth 3 rectifies the gas sucked into the fan 2 and causes it to flow into the fan suction port 2e of the fan 2.
- the bell mouth 3 is formed so that the opening diameter gradually decreases from the outside to the inside of the scroll casing 4.
- the bell mouth 3 is formed to extend in the axial direction of the rotation axis RA.
- An inner circumferential end portion 35 forming an inner edge of the bell mouth 3 is located inside the scroll casing 4. Air near the suction port 5 flows smoothly along the bell mouth 3 and efficiently flows into the fan 2 from the suction port 5.
- the peripheral wall 4c is a wall that guides the airflow generated by the fan 2 to the discharge port 42a along the curved wall surface.
- the peripheral wall 4c is formed in a spiral shape.
- the circumferential wall 4c is formed such that the distance from the rotation axis RA gradually increases in the rotational direction of the fan 2, starting from the tongue portion 43. In the rotation direction of the fan 2, the gap between the peripheral wall 4c and the outer periphery of the fan 2 increases at a predetermined rate from the tongue portion 43 to the discharge portion 42, and the air flow path area gradually increases. It is formed to be.
- the spiral shape of the peripheral wall 4c includes, for example, a logarithmic spiral, an Archimedean spiral, or a shape based on an involute curve.
- the inner circumferential surface of the peripheral wall 4c constitutes a curved surface that curves smoothly along the circumferential direction of the fan 2 from the tongue portion 43 where the spiral winding begins to the winding end portion 41b where the spiral winding ends.
- the peripheral wall 4c is a wall provided between the side walls 4a facing each other, and forms a curved surface along the rotation direction of the fan 2.
- the peripheral wall 4c is arranged parallel to the axial direction of the rotation axis RA and covers the fan 2. Note that the peripheral wall 4c may have a form that is inclined with respect to the axial direction of the rotation axis RA of the fan 2, and is not limited to a form that is arranged parallel to the axial direction of the rotation axis RA.
- the peripheral wall 4c constitutes an inner wall surface facing the outer peripheral surface 2f of the fan 2.
- the peripheral wall 4c faces the outer peripheral side ends of the plurality of blades 2d that constitute the outer peripheral surface 2f of the fan 2.
- the peripheral wall 4c faces the air blowing side of the blades 2d of the fan 2.
- the peripheral wall 4c extends from a tongue portion 43 that is a spiral-shaped winding start portion to a winding end portion 41b that is located at the boundary between the discharge portion 42 and the scroll portion 41 on the side away from the tongue portion 43. , are provided along the rotation direction of the fan 2.
- the tongue portion 43 is an upstream end of the peripheral wall 4c that forms a curved surface in the direction in which gas flows through the internal space of the scroll casing 4 along the peripheral wall 4c due to the rotation of the fan 2.
- the winding end portion 41b is a downstream end of the peripheral wall 4c that forms a curved surface in the direction in which gas flows through the internal space of the scroll casing 4 along the peripheral wall 4c due to the rotation of the fan 2.
- the scroll casing 4 forms a curved surface at a winding start portion of the peripheral wall 4c near the rotation axis RA of the fan 2, and has a tongue portion 43 that guides the airflow generated by the fan 2 to the discharge port 42a.
- the peripheral wall 4c includes a tongue portion 43 at the end on the discharge portion 42 side.
- the tongue portion 43 is formed at the beginning of the spiral-shaped peripheral wall 4c.
- the tongue portion 43 is provided at the boundary between the discharge portion 42 and the diffuser plate 42c, which will be described later.
- the tongue portion 43 is formed to have a curved surface, and is formed in an arc shape when viewed from the axial direction of the rotation axis RA.
- the tongue portion 43 is formed with a predetermined radius of curvature, and the peripheral wall 4c is smoothly connected to the diffuser plate 42c via the tongue portion 43.
- the tongue portion 43 has substantially the same shape in the axial direction of the rotation axis RA when viewed from the discharge port 42a, and has a shape along the axial direction of the rotation axis RA.
- the tongue portion 43 suppresses the inflow of air from the end of the spiral flow path to the beginning of the winding inside the scroll casing 4.
- the tongue portion 43 is provided at the upstream portion of the ventilation path, and has the role of separating the air flow in the rotation direction of the fan 2 and the air flow in the discharge direction from the downstream portion of the ventilation path toward the discharge port 42a.
- the static pressure of the air flowing into the discharge portion 42 increases while passing through the scroll casing 4, and becomes high pressure. Therefore, the tongue portion 43 has a function of partitioning off such a pressure difference.
- the tongue portion 43 has a function of partitioning a pressure difference, and also has a function of guiding air flowing into the discharge portion 42 to each flow path due to its curved surface.
- the discharge part 42 forms a discharge port 42a through which the airflow generated by the fan 2 and passed through the scroll part 41 is discharged.
- the discharge portion 42 is constituted by a hollow tube having a rectangular cross section perpendicular to the direction in which air flows along the peripheral wall 4c. Note that the cross-sectional shape of the discharge portion 42 is not limited to a rectangle.
- the discharge part 42 forms a flow path that guides the air sent out from the fan 2 and flowing through the gap between the peripheral wall 4c and the fan 2 so as to be discharged to the outside of the scroll casing 4.
- One end of the discharge section 42 forms an inlet (not shown) through which air flows into the discharge section 42 from the scroll casing 4. Further, the other end of the discharge section 42 forms a discharge port 42a through which the air that has flowed through the flow path within the discharge section 42 is discharged to the outside air.
- the discharge part 42 has an extension plate 42b, a diffuser plate 42c, a first side plate part 42d, and a second side plate part 42e.
- the extension plate 42b is formed integrally with the peripheral wall 4c so as to smoothly continue to the winding end portion 41b on the downstream side of the peripheral wall 4c.
- the diffuser plate 42c is formed integrally with the tongue portion 43 of the scroll casing 4, and faces the extension plate 42b.
- the diffuser plate 42c is formed at a predetermined angle with respect to the extension plate 42b so that the cross-sectional area of the flow path gradually expands along the direction in which air flows in the discharge portion 42. It is not limited to this configuration.
- the first side plate portion 42d is formed integrally with the first side wall 4a1 of the scroll casing 4
- the second side plate portion 42e is formed integrally with the second side wall 4a2 of the scroll casing 4 on the opposite side.
- the first side plate portion 42d and the second side plate portion 42e are formed between the extension plate 42b and the diffuser plate 42c.
- a flow path having a rectangular cross section is formed by the extension plate 42b, the diffuser plate 42c, the first side plate part 42d, and the second side plate part 42e.
- FIG. 6 is a partial cross-sectional view of the multi-blade centrifugal blower 1 according to the first embodiment.
- FIG. 6 is a cross-sectional view taken along line AA of the multi-blade centrifugal blower 1 in FIG. 1, viewed in the direction of the arrows.
- FIG. 6 is a sectional view of the multi-blade centrifugal blower 1 viewed in the radial direction of the rotation axis RA.
- the inflection point portion 26 is formed over the entire length of the blade 2d.
- the total length of the blade 2d is the length of the blade 2d along the axial direction of the rotation axis RA, and is the length between the base end 2h of the blade 2d on the main plate 2a side and the tip 2g of the blade 2d on the side plate 2c side. is the length of the part.
- the base end portion 2h is one end portion of the blade 2d in the axial direction of the rotation axis RA, and is an end portion on the main plate 2a side.
- the tip portion 2g is the other end of the blade 2d in the axial direction of the rotation axis RA, and is the end on the opposite side from the main plate 2a.
- all parts of the inflection point portion 26 form an inner circumferential end portion 35 that forms the inner edge of the bell mouth 3. It is formed so as to be located on the inner circumferential side. That is, in the multi-blade centrifugal blower 1, as shown in FIG. It is formed so as to be located on the rotation axis RA side. In the multi-blade centrifugal blower 1, all portions of the inflection point portion 26 in the axial direction of the rotation axis RA are inner than the inner peripheral end portion 35 forming the inner edge of the bell mouth 3 in the radial direction of the fan 2. It is formed to be located on the side.
- an imaginary line B formed by an inflection point 26 from a base end 2h on the main plate 2a side of the blade 2d to a tip end 2g on the side plate 2c side is parallel to the rotation axis RA of the fan 2. It is formed to be.
- the imaginary line B is formed to be parallel to the rotation axis RA of the fan 2, for example, when viewed in the radial direction of the rotation axis RA, the imaginary line B is formed to be parallel to the rotation axis RA by ⁇ 1 degree. It is in a state where it is formed so that the angle is within the range.
- FIG. 2 The operation of the multi-blade centrifugal blower 1 will be explained using FIG. 2.
- a motor not shown
- a main plate 2a to which a motor shaft is connected rotates, and a plurality of blades 2d rotate around a rotation axis RA via the main plate 2a.
- the fan 2 rotates, air outside the scroll casing 4 is sucked into the scroll casing 4 through the suction port 5.
- Air sucked into the scroll casing 4 is guided by the bell mouth 3 and sucked into the fan 2.
- the air sucked into the fan 2 becomes an airflow to which dynamic pressure and static pressure are added during the process of passing between the plurality of blades 2d, and is blown out toward the outside in the radial direction of the fan 2.
- the airflow blown out from the fan 2 is blown out into the scroll casing 4 from the fan 2 due to the pressure increasing action of the fan 2 .
- the airflow flowing inside the scroll casing 4 is pressurized by flowing through an air path that gradually expands from the winding start side to the winding end side by the spiral-shaped peripheral wall 4c.
- the air blown into the scroll casing 4 from the fan 2 is decelerated in the enlarged air path formed by the peripheral wall 4c of the scroll casing 4, recovers static pressure, and is blown out from the discharge port 42a shown in FIG. Ru.
- the fan 2 of the multi-blade centrifugal blower 1 includes a backward blade portion 22, a forward blade portion 21, an inflection point portion 26 forming an inflection point between the backward blade portion 22 and the forward blade portion 21, has.
- the inflection point portion 26 is the entire length of the blade 2d, which is a portion between the base end 2h on the main plate 2a side and the tip end 2g on the side plate 2c side of each of the plurality of blades 2d in the axial direction of the rotation axis RA. It is formed over a period of time.
- all portions of the inflection point portion 26 in the axial direction of the rotation axis RA are located on the inner circumferential side of the inner circumferential end portion 35 forming the inner edge of the bell mouth 3 in the radial direction of the fan 2. is formed.
- configuration A the case where all parts of the inflection point part 26 are formed so as to be located on the inner peripheral side than the inner peripheral end part 35 of the bell mouth 3 is referred to as configuration A
- configuration B the case in which a part or all of the inner circumferential end portion 35 is located on the outer circumferential side is referred to as configuration B.
- the multi-blade centrifugal blower 1 compared to a configuration in which at least a part or all of the inflection point portion 26 is located on the outer peripheral side than the inner peripheral end portion 35, the multi-blade centrifugal blower 1 is closer to the leading edge 25a. It is possible to make the change in the blade angle gentle from the part toward the part on the trailing edge 24a side, and it is possible to suppress the separation of the airflow on the negative pressure surface 2d2 and suppress the decrease in the air volume.
- a virtual line B formed by an inflection point 26 from a base end 2h on the main plate 2a side to a tip 2g on the side plate 2c side of each of the plurality of blades 2d is aligned with the rotation axis RA. They are formed to be parallel.
- the fan 2 is made of metal during manufacturing. Easy to pull out from the mold and easy to manufacture.
- FIG. 7 is a partial cross-sectional view of the multi-blade centrifugal blower 1 according to the second embodiment.
- FIG. 7 is a cross-sectional view taken along line AA of the multi-blade centrifugal blower 1 in FIG. 1, viewed in the direction of the arrows.
- Components having the same configuration as the multi-blade centrifugal blower 1 shown in FIGS. 1 to 6 are designated by the same reference numerals, and the description thereof will be omitted.
- the multi-blade centrifugal blower 1 according to the second embodiment further specifies the relationship between the shapes of the blades 2d. Furthermore, in the multi-blade centrifugal blower 1 according to the second embodiment, the positional relationship between the blades 2d and the bell mouth 3 is further specified.
- the configuration of other parts other than the shape of the blade 2d and the positional relationship between the blade 2d and the bell mouth 3 is the same as that of the multi-blade centrifugal blower 1 according to the first embodiment. Therefore, in the following description, the configurations of the blades 2d and the bell mouth 3 of the multi-blade centrifugal blower 1 according to the second embodiment will be mainly described using FIG.
- the blade 2d of the multi-blade centrifugal blower 1 has a notch-shaped stepped portion 27 formed on the leading edge 25a on the side plate 2c side. More specifically, in the leading edge 25a of the blade 2d, a notch-shaped step portion 27 is formed at the tip 2g on the side plate 2c side.
- the stepped portion 27 is a portion formed by cutting out the wall that constitutes the front edge 25a and the tip portion 2g.
- the step portion 27 is formed in a portion of the front edge 25a, and is also formed in a portion of the tip portion 2g.
- the end portion of the front edge 25a on the side plate 2c side is cut out, and the end portion of the tip portion 2g on the rotation axis RA side is cut out.
- the stepped portion 27 is a portion formed by cutting out a continuous corner portion between the front edge 25a and the tip portion 2g. As shown in FIG. 7, the stepped portion 27 is formed at the tip portion 2g of the rearward blade portion 22 and the forward blade portion 21 on the side plate 2c side.
- the stepped portion 27 is formed by a side edge 27A extending in the axial direction of the rotation axis RA of the fan 2 and an upper edge 27B extending in the radial direction of the fan 2.
- the upper edge 27B is an edge located closer to the main plate 2a than the tip 2g.
- the fan 2 has a step formed between the upper edge 27B and the tip 2g in the axial direction of the rotation axis RA.
- the fan 2 is formed such that the side edge 27A is located on the outer peripheral side of the fan 2 with respect to an imaginary extension line C of the front edge 25a of the stepped portion 27.
- the fan 2 has a step formed between the front edge 25a and the side edge 27A in the radial direction of the rotation axis RA.
- the stepped portion 27 is not limited to a configuration formed by a side edge 27A extending in the axial direction of the rotation axis RA of the fan 2 and an upper edge 27B extending in the radial direction of the fan 2.
- the stepped portion 27 may be formed as an arcuate edge in which the side edge 27A and the upper edge 27B are continuously formed integrally.
- the outer diameter of the blade formed by the outer peripheral end 24 of each of the plurality of blades 2d is larger than the inner diameter of the bell mouth 3. That is, in the multi-blade centrifugal blower 1 according to the second embodiment, when viewed in the axial direction of the rotation axis RA, the outer peripheral end 24 of the blade 2d is aligned with the inner peripheral end 35 of the bell mouth 3 in the radial direction of the fan 2. It is formed so as to be located on the outer peripheral side.
- At least a portion of the leading edge 25a of the blade 2d is inside the bell mouth 3 in the radial direction of the fan 2 when viewed in the axial direction of the rotation axis RA. It is formed so as to be located on the inner circumferential side of the circumferential end portion 35 .
- the boundary between the tip 2g and the stepped portion 27 is referred to as a stepped starting point 27C.
- the step starting point 27C is the boundary between the tip 2g of the blade 2d and the side edge 27A in the blade 2d.
- the step starting point 27C is a corner portion of the blade 2d formed by the tip portion 2g and the side edge portion 27A.
- the multi-blade centrifugal blower 1 according to the second embodiment is formed such that the step start point 27C of the blade 2d is located closer to the outer circumferential side than the inner circumferential end 35 of the bell mouth 3 in the radial direction of the fan 2. .
- the inner peripheral end portion 35 of the bell mouth 3 is arranged above the stepped portion 27.
- the multi-blade centrifugal blower 1 according to the second embodiment is configured such that the inner peripheral end portion 35 of the bell mouth 3 faces the stepped portion 27 in the axial direction of the rotation axis RA. More specifically, the multi-blade centrifugal blower 1 according to the second embodiment is arranged such that the inner peripheral end 35 of the bell mouth 3 faces the upper edge 27B in the axial direction of the rotation axis RA. .
- the multi-blade centrifugal blower 1 according to the second embodiment forms a gap between the inner peripheral end 35 of the bell mouth 3 and the upper edge 27B.
- the multi-blade centrifugal blower 1 according to the second embodiment may further be arranged such that the inner peripheral end 35 of the bell mouth 3 faces the side edge 27A in the radial direction of the fan 2.
- the multi-blade centrifugal blower 1 according to the second embodiment forms a gap between the inner peripheral end 35 and the upper edge 27B of the bell mouth 3 in the axial direction of the rotation axis RA, and also forms a gap in the radial direction of the rotation axis RA.
- a gap may be formed between the inner peripheral end 35 of the bell mouth 3 and the side edge 27A.
- Each of the plurality of blades 2d has a notch-shaped stepped portion 27 formed on a leading edge 25a on the side plate 2c side.
- the step starting point 27C is located on the outer circumferential side of the inner circumferential end 35 of the bell mouth 3 in the radial direction of the fan 2. is formed.
- the blade 2d does not fit inside the bell mouth 3 due to the stepped portion 27. It does not interfere with the peripheral end portion 35.
- the multi-blade centrifugal blower 1 is formed such that the step starting point 27C is located on the outer peripheral side of the inner peripheral end 35 of the bell mouth 3, so that the inner peripheral end 35 of the bell mouth 3 and the blade 2d are The height of the blade 2d in the axial direction of the rotation axis RA can be increased while maintaining the interval .
- the multi-blade centrifugal blower 1 according to the second embodiment can bring the tips 2g of the blades 2d closer to the side walls 4a and increase the blade area compared to the blades 2d without the stepped portion 27. You can get the air volume.
- FIG. 8 is a partial cross-sectional view of the multi-blade centrifugal blower 1 according to the third embodiment.
- FIG. 8 is a cross-sectional view taken along line AA of the multi-blade centrifugal blower 1 in FIG. 1, viewed in the direction of the arrows.
- Components having the same configuration as the multi-blade centrifugal blower 1 shown in FIGS. 1 to 6 are designated by the same reference numerals, and the description thereof will be omitted.
- the multi-blade centrifugal blower 1 according to the third embodiment specifies the positional relationship between the blades 2d and the bell mouth 3.
- the configuration of the other parts other than the positional relationship between the blades 2d and the bell mouth 3 is the same as that of the multi-blade centrifugal blower 1 according to the first embodiment. Therefore, in the following explanation, the configurations of the blades 2d and the bell mouth 3 of the multi-blade centrifugal blower 1 according to the third embodiment will be mainly explained using FIG.
- the outer diameter of the blade formed by the outer peripheral end 24 of each of the plurality of blades 2d is larger than the inner diameter of the bell mouth 3. That is, in the multi-blade centrifugal blower 1 according to the third embodiment, when viewed in the axial direction of the rotation axis RA, the outer peripheral end 24 of the blade 2d is aligned with the inner peripheral end 35 of the bell mouth 3 in the radial direction of the fan 2. It is formed so as to be located on the outer peripheral side.
- the multi-blade centrifugal blower 1 according to the third embodiment when viewed in the axial direction of the rotation axis RA, in the radial direction of the fan 2, a part of the leading edge 25a of the blade 2d is located at the inner peripheral end of the bell mouth 3. It is formed so as to be located on the inner circumferential side than 35.
- the backward blade portion 22 when viewed in the axial direction of the rotation axis RA, is located further inward than the inner circumferential end portion 35 of the bell mouth 3 in the radial direction of the fan 2. It is formed so as to be located on the circumferential side.
- the leading edge 25a located at the boundary between the leading edge 25a of the blade 2d and the tip 2g is referred to as a side plate side leading edge 25b.
- the side plate side leading edge portion 25b constitutes a part of the corner portion of the wing 2d formed by the tip portion 2g and the leading edge 25a.
- the multi-blade centrifugal blower 1 according to Embodiment 3 is formed such that the front edge portion 25b of the blade 2d on the side plate side is located on the outer peripheral side than the inner peripheral end portion 35 of the bell mouth 3 in the radial direction of the fan 2. ing.
- the inner peripheral end 35 of the bell mouth 3 is formed so as to face a part of the leading edge 25a of the blade 2d in the axial direction of the rotation axis RA. ing.
- the multi-blade centrifugal blower 1 according to the third embodiment is formed such that the front edge portion 25b on the side plate side is located on the outer peripheral side than the inner peripheral end portion 35 of the bell mouth 3 in the radial direction of the fan 2.
- the front edge 25b on the side plate side is closer to the outer periphery than the inner periphery end 35 of the bell mouth 3.
- the multi-blade centrifugal blower 1 is formed such that the front edge portion 25b on the side plate side is located on the outer peripheral side than the inner peripheral end portion 35 of the bell mouth 3, so that the inner peripheral end portion 35 of the bell mouth 3 and the blade
- the height of the blade 2d in the axial direction of the rotation axis RA can be increased while maintaining the distance from the blade 2d.
- the multi-blade centrifugal blower 1 has a tip portion 2g of the blade 2d that is formed such that the front edge portion 25b on the side plate side is located on the inner peripheral side of the inner peripheral end portion 35 of the bell mouth 3. Since it can be brought close to the side wall 4a and the blade area can be increased, a large amount of air can be obtained.
- FIG. 9 is a partially enlarged view of the fan 2 in the multi-blade centrifugal blower 1 according to the fourth embodiment.
- FIG. 9 is an enlarged view of the fan 2 viewed in the axial direction of the rotation axis RA.
- the wing 2d is shown with the bell mouth 3 transparent in order to show the shape of the wing 2d.
- Components having the same configuration as the multi-blade centrifugal blower 1 shown in FIGS. 1 to 8 are denoted by the same reference numerals, and the description thereof will be omitted.
- the shape of the blades 2d is further specified.
- the configuration other than the shape of the blade 2d described below is the same as that of the multi-blade centrifugal blower 1 according to the first embodiment. Therefore, in the following explanation, the shape of the blade 2d of the multi-blade centrifugal blower 1 according to the fourth embodiment will be mainly explained using FIG.
- the arc-shaped portion of the blade 2d is referred to as an arc portion AR.
- the portion from the inflection point 26 to the trailing edge 24a (see FIG. 3) of the blade 2d is one arcuate portion AR, as shown in FIG. Alternatively, it is composed of a plurality of arcuate portions AR. That is, in the blade 2d of the multi-blade centrifugal blower 1 according to the fourth embodiment, the forward vane portion 21 is composed of one circular arc portion AR or a plurality of circular arc portions AR, as shown in FIG.
- the portion from the inflection point 26 to the trailing edge 24a (see FIG. 3) of the blade 2d is composed of at least one arcuate portion AR. There is.
- the arc portion AR is a portion formed in an arc shape in the blade 2d when viewed in the axial direction of the rotation axis RA.
- the rear edge 24a is formed at the outer peripheral end 24.
- the outer peripheral end 24 is an end on the outer peripheral side of the blade 2d in a cross section perpendicular to the rotation axis RA, and the trailing edge 24a is a part where the outer peripheral end 24 is continuous in the axial direction of the rotation axis.
- a portion from the inflection point portion 26 to the trailing edge 24a of the blade 2d is constituted by at least one or more circular arc portions AR.
- the portion from the inflection point 26 of the blade 2d to the trailing edge 24a of the blade is configured with at least one arcuate portion AR, so that the fan 2 This suppresses sudden angle changes of the blade 2d in the radial direction. Therefore, the multi-blade centrifugal blower 1 can suppress separation of airflow on the negative pressure surface 2d2 and suppress a decrease in air volume.
- a main plate having a circular shape when viewed in the axial direction of the rotating shaft, a plurality of blades installed on the peripheral edge of the main plate, and a side opposite to the main plate of the plurality of blades in the axial direction of the rotating shaft.
- a fan having an annular side plate fixing an end; It has a peripheral wall formed in a spiral shape and at least one side wall having a bell mouth forming an inlet, forming an outlet from which airflow generated by the fan is discharged, and housing the fan.
- the fan is In the radial direction of the fan, a rearward blade portion that constitutes a rearward blade at an inner peripheral side portion of each of the plurality of blades; In the radial direction of the fan, a forward blade portion that constitutes a forward blade at an outer peripheral side portion of each of the plurality of blades; an inflection point portion that forms an inflection point between the backward blade portion and the forward blade portion when viewed in the axial direction of the rotating shaft; has The inflection point portion is In the axial direction of the rotating shaft, the inflection point is formed over the entire length of the blade, which is a portion between the base end on the main plate side and the tip end on the side plate side of each of the plurality of blades.
- a multi-blade centrifugal blower wherein all portions in the axial direction of the fan are located on the inner peripheral side of an inner peripheral end forming an inner edge of the bell mouth in the radial direction of the fan.
- the fan is An imaginary line formed by the inflection point from the base end on the main plate side to the tip end on the side plate side of each of the plurality of wings is formed so as to be parallel to the rotation axis.
- Each of the plurality of wings is A notch-like stepped portion is formed on the front edge of the side plate, When the boundary between the tip end and the stepped portion is defined as a step starting point, the step starting point is located on the outer peripheral side of the inner peripheral end of the bell mouth in the radial direction of the fan.
- the multi-blade centrifugal blower according to supplementary note 1 or 2, which is formed.
- Each of the plurality of wings is The multi-blade centrifugal blower according to any one of appendices 1 to 4, wherein a portion from the inflection point to the trailing edge of the blade is constituted by at least one or more circular arc portions.
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Abstract
This multi-blade centrifugal blower comprises: a fan that includes a main plate, a plurality of blades, and a ring-shaped side plate that secures an end section of the plurality of blades on the opposite side from the main plate; and a scroll casing that houses the fan and that includes a peripheral wall formed in a spiral shape and at least one side wall including a bellmouth which forms an intake port. The fan comprises: rear-facing vane sections on the inner peripheral sides of the plurality of blades that serve as rearward blades; front-facing vane sections on the outer peripheral side of the plurality of blades that serve as front-facing blades; and inflection point sections that form inflection points between the rear-facing blade sections and the front-facing blade sections. The inflection point sections are formed along the entire length of each of the plurality of blades, that is, the portion between a base section on the main plate side and a tip section on the side plate side, and all portions of the inflection point sections in an axial direction are formed so as to be located, in the radial direction of the fan, further to the inner peripheral side than an inner peripheral end section that forms an inner edge of the bellmouth.
Description
本開示は、スクロールケーシングを有する多翼遠心送風機に関するものである。
The present disclosure relates to a multi-blade centrifugal blower with a scroll casing.
従来の多翼遠心送風機は、円盤状の主板と、主板の周縁部に設置される複数枚の翼と、翼の端部を固定する側板とを有するファンを備えている。また、従来の多翼遠心送風機は、ファンを覆う渦巻き型の周壁を有するスクロールケーシングを備えており、スクロールケーシングの吸込口には気流を滑らかにファンに誘引するためのベルマウスが設けられている。従来の多翼遠心送風機は、ファンの回転によって翼間から流出した気流をスクロールケーシング内部の拡大風路によって昇圧させるため、翼はファンの回転方向に傾いている前向羽根になっていることが多い。しかし、ベルマウスに沿ってスクロールケーシングの内部に誘引された気流は、翼に向かう気流の角度が、前向羽根の入口角と合わないことが多く、従来の多翼遠心送風機は、翼の前縁側の負圧面で気流の剥離が生じ風量が低下する恐れがある。そこで、前向羽根の内周側にファン回転方向とは逆向きの後向羽根を設けることによって、ベルマウスから誘引された気流を滑らかに翼に導き、翼の前縁側の負圧面で生じる気流の剥離を抑制し、風量の低減を抑制する多翼遠心送風機が提案されている(例えば、特許文献1参照)。
A conventional multi-blade centrifugal blower includes a fan having a disc-shaped main plate, a plurality of blades installed on the peripheral edge of the main plate, and side plates that fix the ends of the blades. In addition, conventional multi-blade centrifugal blowers are equipped with a scroll casing that has a spiral peripheral wall that covers the fan, and a bell mouth is provided at the suction port of the scroll casing to smoothly draw airflow to the fan. . In conventional multi-blade centrifugal blowers, the airflow that flows out between the blades as the fan rotates is boosted by the expanded air passage inside the scroll casing, so the blades are forward-facing blades that are inclined in the direction of fan rotation. many. However, the angle of the airflow drawn inside the scroll casing along the bell mouth often does not match the inlet angle of the forward vane, and conventional multi-blade centrifugal blowers Separation of airflow may occur on the negative pressure surface on the edge side, resulting in a decrease in air volume. Therefore, by providing a rear vane facing opposite to the fan rotation direction on the inner circumferential side of the forward vane, the airflow induced from the bell mouth is smoothly guided to the vane, and the airflow generated on the negative pressure surface on the leading edge side of the vane. A multi-blade centrifugal blower has been proposed that suppresses separation of air and reduces air volume (for example, see Patent Document 1).
しかしながら、特許文献1の多翼遠心送風機は、翼の内周側が後向羽根、翼の外周側が前向羽根となり、翼の内周側の部分と外周側の部分との間において翼面の角度変化が大きいため、翼の負圧面で新たに気流の剥離が生じ、風量が低下する恐れがある。
However, in the multi-blade centrifugal blower of Patent Document 1, the inner circumferential side of the blade is the backward-facing blade, and the outer circumferential side of the blade is the forward-facing blade, and the angle of the blade surface between the inner circumferential side and the outer circumferential side of the blade is Because the change is large, there is a risk that new separation of airflow will occur on the suction surface of the blade, resulting in a decrease in air volume.
本開示は、上記のような課題を解決するためのものであり、翼の負圧面における気流の剥離を抑制し風量の低下を抑制できる多翼遠心送風機を提供するものである。
The present disclosure is intended to solve the above-mentioned problems, and provides a multi-blade centrifugal blower that can suppress separation of airflow on the negative pressure surface of the blade and suppress a decrease in air volume.
本開示に係る多翼遠心送風機は、回転軸の軸方向に見た場合に円形状の主板と、主板の周縁部に設置される複数枚の翼と、回転軸の軸方向において複数枚の翼の主板と反対側の端部を固定する環状の側板と、を有するファンと、渦巻形状に形成された周壁と、吸込口を形成するベルマウスを有する少なくとも1つの側壁と、を有し、ファンが発生させた気流が吐出される吐出口を形成し、ファンを収納するスクロールケーシングと、を備え、ファンは、ファンの径方向において、複数枚の翼のそれぞれの内周側の部分において後向羽根を構成する後向羽根部と、ファンの径方向において、複数枚の翼のそれぞれの外周側の部分において前向羽根を構成する前向羽根部と、回転軸の軸方向に見た場合に、後向羽根部と前向羽根部との変曲点を形成する変曲点部と、を有し、変曲点部は、回転軸の軸方向において、複数枚の翼のそれぞれの主板側の基端部と側板側の先端部との間の部分である翼の全長にわたって形成されており、変曲点部の軸方向の全ての部分が、ファンの径方向において、ベルマウスの内縁を形成する内周端部よりも内周側に位置するように形成されているものである。
A multi-blade centrifugal blower according to the present disclosure includes a main plate that is circular when viewed in the axial direction of the rotating shaft, a plurality of blades installed on the peripheral edge of the main plate, and a plurality of blades in the axial direction of the rotating shaft. an annular side plate fixing an end opposite to the main plate of the fan, a peripheral wall formed in a spiral shape, and at least one side wall having a bell mouth forming a suction port; a scroll casing that forms a discharge port through which airflow generated by the fan is discharged and houses a fan, the fan having a rearward direction at the inner peripheral side of each of the plurality of blades in the radial direction of the fan. When viewed in the axial direction of the rotating shaft, the rearward blade part that constitutes the blade, the forward blade part that constitutes the forward blade at the outer peripheral side of each of the plurality of blades in the radial direction of the fan, , an inflection point part forming an inflection point between the rearward blade part and the forward blade part, and the inflection point part is located on the main plate side of each of the plurality of blades in the axial direction of the rotation shaft. It is formed over the entire length of the blade, which is the part between the base end of the fan and the tip of the side plate, and the entire axial part of the inflection point extends along the inner edge of the bell mouth in the radial direction of the fan. It is formed so as to be located on the inner peripheral side of the inner peripheral end portion to be formed.
本開示に係る多翼遠心送風機のファンは、後向羽根部と、前向羽根部と、後向羽根部と前向羽根部との変曲点を形成する変曲点部と、を有する。変曲点部は、回転軸の軸方向において、複数枚の翼のそれぞれの主板側の基端部と側板側の先端部との間の部分である翼の全長にわたって形成されている。また、変曲点部の、回転軸の軸方向の全ての部分が、ファンの径方向において、ベルマウスの内縁を形成する内周端部よりも内周側に位置するように形成されている。変曲点部の全ての部分が、ベルマウスの内周端部よりも内周側に位置する構成では、変曲点部の少なくとも一部あるいは全ての部分が、内周端部よりも外周側に位置する構成と比較して、翼における前向羽根部の占める割合が大きくなる。そのため、多翼遠心送風機は、前縁側の部分から後縁側の部分に向かって翼角度の変化をなだらかにすることができ、負圧面における気流の剥離を抑制し風量の低下を抑制できる。
The fan of the multi-blade centrifugal blower according to the present disclosure includes a backward blade portion, a forward blade portion, and an inflection point portion that forms an inflection point between the rearward blade portion and the forward blade portion. The inflection point portion is formed over the entire length of the blade, which is a portion between the base end portion on the main plate side and the tip portion on the side plate side of each of the plurality of blades in the axial direction of the rotating shaft. Further, all portions of the inflection point portion in the axial direction of the rotation shaft are formed so as to be located on the inner circumferential side of the inner circumferential end forming the inner edge of the bell mouth in the radial direction of the fan. . In a configuration in which all parts of the inflection point are located on the inner side of the inner circumferential end of the bell mouth, at least part or all of the inflection point part is located on the outer circumferential side of the inner circumferential end. Compared to a configuration in which the wing is located at Therefore, the multi-blade centrifugal blower can gradually change the blade angle from the leading edge side toward the trailing edge side, suppressing separation of airflow on the negative pressure surface and suppressing a decrease in air volume.
以下、実施の形態に係る多翼遠心送風機について図面等を参照しながら説明する。なお、図1を含む以下の図面では、各構成部材の相対的な寸法の関係及び形状等が実際のものとは異なる場合がある。また、以下の図面において、同一の符号を付したものは、同一又はこれに相当するものであり、このことは明細書の全文において共通することとする。また、理解を容易にするために方向を表す用語(例えば「上」、「下」、「右」、「左」、「前」、「後」など)を適宜用いるが、それらの表記は、説明の便宜上、そのように記載しているだけであって、装置あるいは部品の配置及び向きを限定するものではない。
Hereinafter, a multi-blade centrifugal blower according to an embodiment will be described with reference to the drawings and the like. Note that in the following drawings including FIG. 1, the relative dimensional relationships, shapes, etc. of each component may differ from the actual ones. In addition, in the following drawings, parts with the same reference numerals are the same or equivalent, and this is common throughout the entire specification. In addition, to facilitate understanding, we use terms that indicate directions (for example, "top", "bottom", "right", "left", "front", "back", etc.), but these notations are as follows: This is only described for convenience of explanation, and does not limit the arrangement or orientation of the device or parts.
実施の形態1.
[多翼遠心送風機1]
図1は、実施の形態1に係る多翼遠心送風機1を回転軸RAと平行に見た構成を模式的に示す外観図である。図2は、実施の形態1に係る多翼遠心送風機1の斜視図である。図1の矢印Rは、ファン2の回転方向を示し、破線矢印CDは、ファン2の周方向を示している。また、図2は、多翼遠心送風機1の外観を説明するものであり、多翼遠心送風機1の内部の構成は簡略化して示している。図1及び図2を用いて、多翼遠心送風機1の基本的な構造について説明する。Embodiment 1.
[Multi-blade centrifugal blower 1]
FIG. 1 is an external view schematically showing the configuration of a multi-bladecentrifugal blower 1 according to Embodiment 1, viewed parallel to the rotation axis RA. FIG. 2 is a perspective view of the multi-blade centrifugal blower 1 according to the first embodiment. The arrow R in FIG. 1 indicates the rotation direction of the fan 2, and the broken line arrow CD indicates the circumferential direction of the fan 2. Moreover, FIG. 2 explains the external appearance of the multi-blade centrifugal blower 1, and the internal configuration of the multi-blade centrifugal blower 1 is shown in a simplified manner. The basic structure of the multi-blade centrifugal blower 1 will be explained using FIGS. 1 and 2.
[多翼遠心送風機1]
図1は、実施の形態1に係る多翼遠心送風機1を回転軸RAと平行に見た構成を模式的に示す外観図である。図2は、実施の形態1に係る多翼遠心送風機1の斜視図である。図1の矢印Rは、ファン2の回転方向を示し、破線矢印CDは、ファン2の周方向を示している。また、図2は、多翼遠心送風機1の外観を説明するものであり、多翼遠心送風機1の内部の構成は簡略化して示している。図1及び図2を用いて、多翼遠心送風機1の基本的な構造について説明する。
[Multi-blade centrifugal blower 1]
FIG. 1 is an external view schematically showing the configuration of a multi-blade
多翼遠心送風機1は、ファン2の回転による遠心力で風を送る機器であり、例えば、シロッコファン等である。多翼遠心送風機1は、ファン2の仮想の回転軸RAの軸方向においてスクロールケーシング4の片側から空気が吸い込まれる片吸込型の遠心送風機である。なお、多翼遠心送風機1は、片吸込型の遠心送風機に限定されるものではなく、回転軸RAの軸方向においてスクロールケーシング4の両側から空気が吸い込まれる両吸込型の遠心送風機でもよい。多翼遠心送風機1は、図1及び図2に示すように、気流を発生させるファン2と、ファン2を内部に収納するスクロールケーシング4とを有する。
The multi-blade centrifugal blower 1 is a device that sends air using centrifugal force generated by the rotation of the fan 2, and is, for example, a sirocco fan. The multi-blade centrifugal blower 1 is a single-suction type centrifugal blower in which air is sucked in from one side of the scroll casing 4 in the axial direction of the imaginary rotational axis RA of the fan 2 . Note that the multi-blade centrifugal blower 1 is not limited to a single suction type centrifugal blower, but may be a double suction type centrifugal blower in which air is sucked in from both sides of the scroll casing 4 in the axial direction of the rotation axis RA. As shown in FIGS. 1 and 2, the multi-blade centrifugal blower 1 includes a fan 2 that generates airflow and a scroll casing 4 that houses the fan 2 therein.
(ファン2)
図3は、実施の形態1に係る多翼遠心送風機1のファン2の斜視図である。図4は、実施の形態1に係る多翼遠心送風機1のファン2の平面図である。なお、図4は、回転軸RAの軸方向に見たファン2の図面である。図1~図4を用いてファン2について説明する。 (Fan 2)
FIG. 3 is a perspective view of thefan 2 of the multi-blade centrifugal blower 1 according to the first embodiment. FIG. 4 is a plan view of the fan 2 of the multi-blade centrifugal blower 1 according to the first embodiment. Note that FIG. 4 is a diagram of the fan 2 viewed in the axial direction of the rotation axis RA. The fan 2 will be explained using FIGS. 1 to 4.
図3は、実施の形態1に係る多翼遠心送風機1のファン2の斜視図である。図4は、実施の形態1に係る多翼遠心送風機1のファン2の平面図である。なお、図4は、回転軸RAの軸方向に見たファン2の図面である。図1~図4を用いてファン2について説明する。 (Fan 2)
FIG. 3 is a perspective view of the
ファン2は、遠心式のファンである。ファン2は、駆動軸を有するモータ(図示は省略)に接続される。ファン2は、モータによって回転駆動され、回転で生じる遠心力により、径方向外方へ空気を強制的に送出させる。ファン2は、モータ等によって、矢印Rで示す回転方向に向かって回転する。
The fan 2 is a centrifugal fan. The fan 2 is connected to a motor (not shown) having a drive shaft. The fan 2 is rotationally driven by a motor, and uses centrifugal force generated by the rotation to forcibly send air outward in the radial direction. The fan 2 is rotated in the direction of rotation indicated by an arrow R by a motor or the like.
ファン2は、図1に示すように、回転軸RA方向に見た場合に、円形状の主板2aと、円環状の側板2cと、主板2aの周縁部2a1において、回転軸RAを中心に放射状に配置された複数枚の翼2dと、を有する。ファン2は、主板2aと、主板2aに配置された複数枚の翼2dとにより、有底の円筒形状に形成されている。
As shown in FIG. 1, when viewed in the direction of the rotation axis RA, the fan 2 has a circular main plate 2a, an annular side plate 2c, and a peripheral edge 2a1 of the main plate 2a. It has a plurality of wings 2d arranged at. The fan 2 is formed into a bottomed cylindrical shape by a main plate 2a and a plurality of blades 2d arranged on the main plate 2a.
ファン2は、回転軸RAの軸方向において、主板2aと反対側の側板2c側の部分にファン吸込口2eが形成されている。ファン吸込口2eは、ファン2の内部に流れ込む空気が流入するファン2の開口部であり、主板2aと複数枚の翼2dとで囲まれた空間に気体を流入させる。
The fan 2 has a fan suction port 2e formed in a portion on the side plate 2c side opposite to the main plate 2a in the axial direction of the rotation axis RA. The fan suction port 2e is an opening of the fan 2 through which air flows into the fan 2, and allows gas to flow into a space surrounded by the main plate 2a and the plurality of blades 2d.
(主板2a)
主板2aは、回転軸RAの軸方向に見た場合に円形状に形成されている。回転軸RAを中心とした径方向において、外周側の部分に形成された周縁部2a1と、内周側の部分に形成された中央部2a2とを有する。 (Main plate 2a)
Themain plate 2a is formed into a circular shape when viewed in the axial direction of the rotation axis RA. In the radial direction centered on the rotation axis RA, it has a peripheral portion two a1 formed on the outer circumferential side and a central portion two a2 formed on the inner circumferential side.
主板2aは、回転軸RAの軸方向に見た場合に円形状に形成されている。回転軸RAを中心とした径方向において、外周側の部分に形成された周縁部2a1と、内周側の部分に形成された中央部2a2とを有する。 (
The
周縁部2a1は、中央部2a2に対して外周側の部分に形成されており、回転軸RAの軸方向に見た場合に円環状に形成されている。周縁部2a1は、板状に形成されている。中央部2a2は、周縁部2a1に対して内周側の部分に形成されており、周縁部2a1の内周側の縁部分から突出するように形成されている。中央部2a2は、山状に形成された板状の部材で形成されている。中央部2a2は、複数の翼2dの内側に形成されている。
The peripheral portion two a1 is formed on the outer peripheral side of the central portion two a2, and is formed in an annular shape when viewed in the axial direction of the rotation axis RA. The peripheral portion two a1 is formed into a plate shape. The central portion two a2 is formed on the inner peripheral side of the peripheral edge two a1, and is formed to protrude from the inner peripheral edge portion of the peripheral edge two a1. The central portion 2a2 is formed of a plate-like member formed in a mountain shape. The central portion 2a2 is formed inside the plurality of wings 2d.
主板2aは、周縁部2a1と中央部2a2とが一体に形成されてもよい。主板2aは、全体として平板状に形成されてもよい。主板2aは、円盤状あるいは多角形状等に形成されてもよい。主板2aの厚さは、回転軸RAを中心とする径方向において、中心に向かって壁の厚さが厚くなるように形成されてもよく、回転軸RAを中心とする径方向において一定の厚さに形成されてもよい。また、主板2aは一枚の板状部材で構成されたものに限らず、複数枚の板状部材を一体的に固定して構成されたものでもよい。なお、回転軸RAを中心とする径方向とは、回転軸RAの軸方向に対して垂直な方向である。
The main plate 2a may have a peripheral portion two a1 and a central portion two a2 integrally formed. The main plate 2a may be formed into a flat plate shape as a whole. The main plate 2a may be formed into a disk shape, a polygonal shape, or the like. The thickness of the main plate 2a may be formed such that the thickness of the wall becomes thicker toward the center in the radial direction centered on the rotation axis RA, or a constant thickness in the radial direction centered on the rotation axis RA. It may be formed in the same way. Further, the main plate 2a is not limited to being composed of a single plate-like member, but may be composed of a plurality of plate-like members fixed integrally. Note that the radial direction centered on the rotation axis RA is a direction perpendicular to the axial direction of the rotation axis RA.
主板2aの中心部には、モータの駆動軸が接続されるボス部2bが設けられている。ボス部2bには、モータの駆動軸が挿入される軸穴が形成されている。ボス部2bは、例えば、円柱形状に形成されているが、ボス部2bの形状は円柱形状に限定されるものではない。ボス部2bは、柱状に形成されていればよく、例えば多角柱状に形成されてもよい。主板2aは、ボス部2bを介してモータによって回転駆動される。
A boss portion 2b to which the drive shaft of the motor is connected is provided at the center of the main plate 2a. A shaft hole into which the drive shaft of the motor is inserted is formed in the boss portion 2b. The boss portion 2b is formed, for example, in a cylindrical shape, but the shape of the boss portion 2b is not limited to the cylindrical shape. The boss portion 2b may be formed into a columnar shape, for example, a polygonal columnar shape. The main plate 2a is rotationally driven by a motor via the boss portion 2b.
(側板2c)
ファン2は、回転軸RAの軸方向において、複数枚の翼2dの主板2aと反対側の端部に取り付けられた環状の側板2cを有している。側板2cは、回転軸RAの軸方向において、複数枚の翼2dの主板2aと反対側の端部を固定する。側板2cは、ファン2の外周面2fに設けられている。側板2cは、回転軸RAを中心とする径方向において翼2dの外側の部分に設けられている。側板2cは、主板2aから回転軸RA方向に突出する複数枚の翼2dの先端部2gに設けられてもよい。側板2cは、複数枚の翼2dを連結することで、各翼2dの先端の位置関係を維持する。また、側板2cは、複数枚の翼2dを連結することで、複数枚の翼2dの強度を補強している。 (Side plate 2c)
Thefan 2 has an annular side plate 2c attached to an end of a plurality of blades 2d opposite to the main plate 2a in the axial direction of the rotation axis RA. The side plate 2c fixes the ends of the plurality of blades 2d on the side opposite to the main plate 2a in the axial direction of the rotation axis RA. The side plate 2c is provided on the outer peripheral surface 2f of the fan 2. The side plate 2c is provided on the outer side of the blade 2d in the radial direction centered on the rotation axis RA. The side plate 2c may be provided at the tip portion 2g of a plurality of blades 2d that protrude from the main plate 2a in the direction of the rotation axis RA. The side plate 2c maintains the positional relationship of the tips of each wing 2d by connecting the plurality of wings 2d. Moreover, the side plate 2c reinforces the strength of the plurality of wings 2d by connecting the plurality of wings 2d.
ファン2は、回転軸RAの軸方向において、複数枚の翼2dの主板2aと反対側の端部に取り付けられた環状の側板2cを有している。側板2cは、回転軸RAの軸方向において、複数枚の翼2dの主板2aと反対側の端部を固定する。側板2cは、ファン2の外周面2fに設けられている。側板2cは、回転軸RAを中心とする径方向において翼2dの外側の部分に設けられている。側板2cは、主板2aから回転軸RA方向に突出する複数枚の翼2dの先端部2gに設けられてもよい。側板2cは、複数枚の翼2dを連結することで、各翼2dの先端の位置関係を維持する。また、側板2cは、複数枚の翼2dを連結することで、複数枚の翼2dの強度を補強している。 (
The
(翼2d)
複数枚の翼2dは、主板2aの周縁部2a1に設置されている。複数枚の翼2dは、一端が主板2aと接続され、他端が側板2cと接続されており、回転軸RAを中心とする周方向上に配列されている。複数枚の翼2dのそれぞれは、少なくとも主板2aと側板2cとの間に配置されている。複数枚の翼2dは、ボス部2bを中心とする円周状に配置され、基端が主板2aの板面上に固定されている。図3に示すように、翼2dにおいて、回転方向側の面が正圧面2d1であり、回転方向とは反対側の面が負圧面2d2である。 (wing 2d)
The plurality ofwings 2d are installed on the peripheral edge portion two a1 of the main plate 2a. The plurality of blades 2d have one end connected to the main plate 2a, the other end connected to the side plate 2c, and are arranged in a circumferential direction centered on the rotation axis RA. Each of the plurality of wings 2d is arranged at least between the main plate 2a and the side plate 2c. The plurality of wings 2d are arranged circumferentially around the boss portion 2b, and their base ends are fixed on the surface of the main plate 2a. As shown in FIG. 3, in the blade 2d, the surface on the rotation direction side is a pressure surface 2d1, and the surface on the opposite side to the rotation direction is a suction surface 2d2.
複数枚の翼2dは、主板2aの周縁部2a1に設置されている。複数枚の翼2dは、一端が主板2aと接続され、他端が側板2cと接続されており、回転軸RAを中心とする周方向上に配列されている。複数枚の翼2dのそれぞれは、少なくとも主板2aと側板2cとの間に配置されている。複数枚の翼2dは、ボス部2bを中心とする円周状に配置され、基端が主板2aの板面上に固定されている。図3に示すように、翼2dにおいて、回転方向側の面が正圧面2d1であり、回転方向とは反対側の面が負圧面2d2である。 (
The plurality of
各翼2dは、主板2aの周縁部2a1において、互いに一定の間隔をあけて周方向に配置されている。各翼2dは、主板2aから立ち上がるように設けられており、板状に形成されている。各翼2dは、主板2aに対してほぼ垂直に立ち上がるように設けられているが、特にこれに限定されず、各翼2dは、主板2aの垂直方向に対して傾斜して設けられてもよい。
The blades 2d are arranged circumferentially at a constant interval from each other on the peripheral edge 2a1 of the main plate 2a. Each wing 2d is provided so as to rise from the main plate 2a, and is formed in a plate shape. Each wing 2d is provided so as to stand up almost perpendicularly to the main plate 2a, but the invention is not limited to this, and each wing 2d may be provided at an angle with respect to the vertical direction of the main plate 2a. .
図3に示すように、翼2dは、主板2a側の部分から側板2c側の部分に向かうにつれて、前縁25aが回転軸RAから離れるように傾斜している。前縁25aは、翼2dの内周端25により形成されている。内周端25は、回転軸RAに垂直な断面における翼2dの内周側の端部であり、前縁25aは、内周端25が回転軸の軸方向に連なった部分である。翼2dの前縁25aは、主板2a側の部分から側板2c側の部分に向かうにつれて、羽根内径が大きくなるように傾斜している。
As shown in FIG. 3, the blade 2d is inclined such that the leading edge 25a moves away from the rotation axis RA as it goes from the main plate 2a side to the side plate 2c side. The leading edge 25a is formed by the inner peripheral end 25 of the blade 2d. The inner peripheral end 25 is an end on the inner peripheral side of the blade 2d in a cross section perpendicular to the rotation axis RA, and the leading edge 25a is a part where the inner peripheral end 25 is continuous in the axial direction of the rotation axis. The leading edge 25a of the blade 2d is inclined such that the inner diameter of the blade increases from the main plate 2a side toward the side plate 2c side.
図5は、実施の形態1に係る多翼遠心送風機1におけるファン2の部分拡大図である。図5は、回転軸RAの軸方向に見たファン2の拡大図である。図5では、翼2dの形状を示すため、ベルマウス3を透過させて翼2dを示している。図5に示すように、翼2dの内周側の一部は、ベルマウス3の内周端部35の内側に位置するように形成されている。ファン2の翼2dは、図5に示すように前向羽根部21と後向羽根部22とが一体に形成されている。
FIG. 5 is a partially enlarged view of the fan 2 in the multi-blade centrifugal blower 1 according to the first embodiment. FIG. 5 is an enlarged view of the fan 2 viewed in the axial direction of the rotation axis RA. In FIG. 5, the wing 2d is shown with the bell mouth 3 transparent in order to show the shape of the wing 2d. As shown in FIG. 5, a part of the inner circumferential side of the wing 2d is formed to be located inside the inner circumferential end portion 35 of the bell mouth 3. As shown in FIG. As shown in FIG. 5, the blade 2d of the fan 2 has a forward blade portion 21 and a backward blade portion 22 integrally formed.
翼2dは、外周端24を含み前向羽根として構成された前向羽根部21と、内周端25を含み後向羽根として構成された後向羽根部22とを有する。また、翼2dは、ファン2の回転軸RAの軸方向に見た場合に、後向羽根部22と前向羽根部21との変曲点を形成する変曲点部26を有する。翼2dは、ファン2の径方向において、回転軸RAから外周側に向かって、後向羽根部22、変曲点部26、前向羽根部21の順に連続して一体に形成されている。
The blade 2d has a forward blade portion 21 that includes an outer peripheral end 24 and is configured as a forward blade, and a backward blade portion 22 that includes an inner peripheral end 25 and is configured as a backward blade. Further, the blade 2 d has an inflection point portion 26 that forms an inflection point between the backward blade portion 22 and the forward blade portion 21 when viewed in the axial direction of the rotation axis RA of the fan 2 . In the radial direction of the fan 2, the blades 2d are integrally formed in the order of the backward blade portion 22, the inflection point portion 26, and the forward blade portion 21 from the rotation axis RA toward the outer circumferential side.
後向羽根部22は、ファン2の径方向において、複数枚の翼2dのそれぞれの内周側の部分において後向羽根を構成する部分である。前向羽根部21は、ファン2の径方向において、複数枚の翼2dのそれぞれの外周側の部分において前向羽根を構成する部分である。
The backward blade portion 22 is a portion that constitutes a backward blade in the inner peripheral side of each of the plurality of blades 2d in the radial direction of the fan 2. The forward blade portion 21 is a portion that constitutes a forward blade on the outer peripheral side of each of the plurality of blades 2d in the radial direction of the fan 2.
変曲点部26は、内周側の部分が後向羽根で形成され、外周側の部分が前向羽根で形成された翼2dにおいて、後向羽根部22から前向羽根部21に変化する部分を形成する。すなわち、変曲点部26は、ファン2の回転軸RAの軸方向に見た場合に、内周側の部分が後向羽根で形成され、外周側の部分が前向羽根で形成された翼2dにおいて、後向羽根部22と前向羽根部21との変曲点を形成する。換言すれば、変曲点部26は、ファン2の回転軸RAの軸方向に見た場合に、後向羽根部22と前向羽根部21との接続点を形成する。変曲点部26は、回転軸RAの軸方向において、後向羽根部22と前向羽根部21との境界の変曲点が連なった部分であり、後向羽根部22と前向羽根部21との接続点が連なった部分である。
The inflection point portion 26 changes from the backward blade portion 22 to the forward blade portion 21 in the blade 2d, in which the inner peripheral side portion is formed by the backward blade and the outer peripheral side portion is formed by the forward blade. form part. That is, when viewed in the axial direction of the rotation axis RA of the fan 2, the inflection point portion 26 is a blade in which the inner circumferential side portion is formed by backward-facing blades, and the outer circumferential side portion is formed by forward-facing blades. At 2d, an inflection point between the backward blade portion 22 and the forward blade portion 21 is formed. In other words, the inflection point portion 26 forms a connection point between the backward blade portion 22 and the forward blade portion 21 when viewed in the axial direction of the rotation axis RA of the fan 2 . The inflection point portion 26 is a portion where inflection points at the boundary between the backward blade portion 22 and the forward blade portion 21 are connected in the axial direction of the rotation axis RA, and the backward blade portion 22 and the forward blade portion This is a part where connection points with 21 are connected.
ファン2は、モータ(図示は省略)が駆動することにより、回転軸RAを中心に回転駆動される。ファン2が回転することで、多翼遠心送風機1の外部の気体が、図1に示すスクロールケーシング4に形成された吸込口5と、ファン2のファン吸込口2eとを通り、主板2aと複数枚の翼2dとで囲まれる空間に吸い込まれる。そして、ファン2が回転することで、主板2aと複数枚の翼2dとで囲まれる空間に吸込まれた空気が、翼2dと隣接する翼2dとの間の空間を通り、ファン2の径方向外方に送り出される。
The fan 2 is driven to rotate around the rotation axis RA by being driven by a motor (not shown). As the fan 2 rotates, gas outside the multi-blade centrifugal blower 1 passes through the suction port 5 formed in the scroll casing 4 shown in FIG. It is sucked into the space surrounded by the two wings 2d. As the fan 2 rotates, the air sucked into the space surrounded by the main plate 2a and the plurality of blades 2d passes through the space between the blade 2d and the adjacent blade 2d, and passes in the radial direction of the fan 2. sent outward.
(スクロールケーシング4)
図1及び図2を用いて、スクロールケーシング4について説明する。スクロールケーシング4は、ファン2を内部に収納し、ファン2から吹き出された空気を整流する。スクロールケーシング4は、回転軸RAの軸方向において、主板2aの片側に、後述する吸込口5が形成された側壁4aを有する片吸込タイプのケーシングである。スクロールケーシング4は、片吸込タイプのケーシングに限定されるものではなく、回転軸RAの軸方向において、主板2aの両側に、後述する吸込口5が形成された側壁4aを有する両吸込タイプのケーシングでもよい。 (Scroll casing 4)
Thescroll casing 4 will be explained using FIGS. 1 and 2. The scroll casing 4 houses the fan 2 therein and rectifies the air blown out from the fan 2. The scroll casing 4 is a single suction type casing that has a side wall 4a in which a suction port 5 (described later) is formed on one side of the main plate 2a in the axial direction of the rotation axis RA. The scroll casing 4 is not limited to a single suction type casing, but may be a double suction type casing having side walls 4a in which suction ports 5, which will be described later, are formed on both sides of the main plate 2a in the axial direction of the rotation axis RA. But that's fine.
図1及び図2を用いて、スクロールケーシング4について説明する。スクロールケーシング4は、ファン2を内部に収納し、ファン2から吹き出された空気を整流する。スクロールケーシング4は、回転軸RAの軸方向において、主板2aの片側に、後述する吸込口5が形成された側壁4aを有する片吸込タイプのケーシングである。スクロールケーシング4は、片吸込タイプのケーシングに限定されるものではなく、回転軸RAの軸方向において、主板2aの両側に、後述する吸込口5が形成された側壁4aを有する両吸込タイプのケーシングでもよい。 (Scroll casing 4)
The
スクロールケーシング4は、スクロール部41と、吐出部42と、を有する。スクロールケーシング4は、渦巻形状に形成された周壁4cと、回転軸RAの軸方向において、ファン2の両側に設けられた側壁4aと、を有する。
The scroll casing 4 has a scroll part 41 and a discharge part 42. The scroll casing 4 has a peripheral wall 4c formed in a spiral shape and side walls 4a provided on both sides of the fan 2 in the axial direction of the rotation axis RA.
(スクロール部41)
スクロール部41は、ファン2が発生させた気流の動圧を静圧に変換する風路を形成する。スクロール部41は、回転軸RAの軸方向からファン2を覆う側壁4aと、ファン2をボス部2bの回転軸RAの径方向からファン2を囲む周壁4cと、を有する。 (Scroll part 41)
Thescroll portion 41 forms an air path that converts the dynamic pressure of the airflow generated by the fan 2 into static pressure. The scroll portion 41 has a side wall 4a that covers the fan 2 from the axial direction of the rotation axis RA, and a peripheral wall 4c that surrounds the fan 2 from the radial direction of the rotation axis RA of the boss portion 2b.
スクロール部41は、ファン2が発生させた気流の動圧を静圧に変換する風路を形成する。スクロール部41は、回転軸RAの軸方向からファン2を覆う側壁4aと、ファン2をボス部2bの回転軸RAの径方向からファン2を囲む周壁4cと、を有する。 (Scroll part 41)
The
また、スクロール部41は、吐出部42との間に位置して曲面を構成し、ファン2が発生させた気流を、スクロール部41を介して吐出口42aに導く舌部43を有する。周壁4c及び側壁4aにより構成されるスクロール部41の内部空間は、ファン2から吹き出された空気が周壁4cに沿って流れる空間となっている。
Further, the scroll portion 41 has a tongue portion 43 that is located between the scroll portion 41 and the discharge portion 42 and forms a curved surface, and that guides the airflow generated by the fan 2 to the discharge port 42a via the scroll portion 41. The internal space of the scroll portion 41 constituted by the peripheral wall 4c and the side wall 4a is a space through which air blown out from the fan 2 flows along the peripheral wall 4c.
(側壁4a)
実施の形態1では、スクロールケーシング4は、2つの側壁4aを含んでいる。2つの側壁4aのうち、吸込口5を形成するベルマウス3を有する側壁4aを第1側壁4a1と称し、吸込口5及びベルマウス3が形成されていない側壁4aを第2側壁4a2と称する。ファン2の両側に配置されている2つの側壁4aは、周壁4cを介してそれぞれ対向するように形成されている。 (Side wall 4a)
In the first embodiment, thescroll casing 4 includes two side walls 4a. Of the two side walls 4a, the side wall 4a having the bell mouth 3 forming the suction port 5 is referred to as a first side wall 4a1, and the side wall 4a without the suction port 5 and the bell mouth 3 is referred to as a second side wall 4a2. Two side walls 4a arranged on both sides of the fan 2 are formed to face each other with a peripheral wall 4c interposed therebetween.
実施の形態1では、スクロールケーシング4は、2つの側壁4aを含んでいる。2つの側壁4aのうち、吸込口5を形成するベルマウス3を有する側壁4aを第1側壁4a1と称し、吸込口5及びベルマウス3が形成されていない側壁4aを第2側壁4a2と称する。ファン2の両側に配置されている2つの側壁4aは、周壁4cを介してそれぞれ対向するように形成されている。 (
In the first embodiment, the
実施の形態1のスクロールケーシング4は、図2に示すように、側壁4aとして、第1側壁4a1と、第2側壁4a2とを含んでいる。すなわち、スクロールケーシング4は、主板2aと複数枚の翼2dとによって形成される空間に連通する吸込口5を形成するベルマウス3を備えた少なくとも1つの側壁4aを有する。
As shown in FIG. 2, the scroll casing 4 of the first embodiment includes a first side wall 4a1 and a second side wall 4a2 as the side walls 4a. That is, the scroll casing 4 has at least one side wall 4a provided with a bell mouth 3 that forms a suction port 5 that communicates with the space formed by the main plate 2a and the plurality of blades 2d.
第1側壁4a1は、主板2aに対して側板2cが配置された側に位置にする側壁4aである。第2側壁4a2は、側板2cに対して主板2aが配置された側に位置にする側壁4aである。側壁4aは、第1側壁4a1及び第2側壁4a2の総称である。
The first side wall 4a1 is a side wall 4a located on the side where the side plate 2c is arranged with respect to the main plate 2a. The second side wall 4a2 is a side wall 4a located on the side where the main plate 2a is disposed with respect to the side plate 2c. The side wall 4a is a general term for the first side wall four a1 and the second side wall four a2.
スクロールケーシング4の第1側壁4a1には、ファン2とスクロールケーシング4の外部との間を空気が流通できるように、吸込口5が形成されている。吸込口5は、ファン吸込口2eと連通しており、主板2aと複数枚の翼2dとで囲まれた空間に気体を流入させる空気の取り込み口である。吸込口5は、主板2aの板面と対向する位置に形成されている。
A suction port 5 is formed in the first side wall 4a1 of the scroll casing 4 so that air can flow between the fan 2 and the outside of the scroll casing 4. The suction port 5 communicates with the fan suction port 2e, and is an air intake port that allows gas to flow into the space surrounded by the main plate 2a and the plurality of blades 2d. The suction port 5 is formed at a position facing the plate surface of the main plate 2a.
第1側壁4a1に設けられた吸込口5は、ベルマウス3によって形成されている。すなわち、ベルマウス3は、スクロールケーシング4の外部の空間と、主板2aと複数枚の翼2dとによって形成される空間とを連通させる吸込口5を形成している。ベルマウス3は、ファン2に吸入される気体を整流してファン2のファン吸込口2eに流入させる。
The suction port 5 provided in the first side wall 4a1 is formed by the bell mouth 3. That is, the bell mouth 3 forms a suction port 5 that communicates the space outside the scroll casing 4 with the space formed by the main plate 2a and the plurality of blades 2d. The bell mouth 3 rectifies the gas sucked into the fan 2 and causes it to flow into the fan suction port 2e of the fan 2.
ベルマウス3は、スクロールケーシング4の外部から内部に向けて開口径が次第に小さくなるように形成されている。ベルマウス3は、回転軸RAの軸方向に延びるように形成されている。ベルマウス3の内縁を形成する内周端部35は、スクロールケーシング4の内部に位置している。吸込口5近傍の空気は、ベルマウス3に沿って滑らかに流動し、吸込口5からファン2に効率よく流入する。
The bell mouth 3 is formed so that the opening diameter gradually decreases from the outside to the inside of the scroll casing 4. The bell mouth 3 is formed to extend in the axial direction of the rotation axis RA. An inner circumferential end portion 35 forming an inner edge of the bell mouth 3 is located inside the scroll casing 4. Air near the suction port 5 flows smoothly along the bell mouth 3 and efficiently flows into the fan 2 from the suction port 5.
(周壁4c)
周壁4cは、ファン2が発生させた気流を、湾曲する壁面に沿わせて吐出口42aに導く壁である。周壁4cは、渦巻形状に形成されている。周壁4cは、回転軸RAからの距離が、舌部43を始点として、ファン2の回転方向に進むに従い次第に遠くなるように形成されている。周壁4cは、ファン2の回転方向において、舌部43から吐出部42にかけて、周壁4cとファン2の外周との間隙が予め定められた割合で拡大し、また、空気の流路面積が次第に大きくなるように形成されている。 (peripheral wall 4c)
Theperipheral wall 4c is a wall that guides the airflow generated by the fan 2 to the discharge port 42a along the curved wall surface. The peripheral wall 4c is formed in a spiral shape. The circumferential wall 4c is formed such that the distance from the rotation axis RA gradually increases in the rotational direction of the fan 2, starting from the tongue portion 43. In the rotation direction of the fan 2, the gap between the peripheral wall 4c and the outer periphery of the fan 2 increases at a predetermined rate from the tongue portion 43 to the discharge portion 42, and the air flow path area gradually increases. It is formed to be.
周壁4cは、ファン2が発生させた気流を、湾曲する壁面に沿わせて吐出口42aに導く壁である。周壁4cは、渦巻形状に形成されている。周壁4cは、回転軸RAからの距離が、舌部43を始点として、ファン2の回転方向に進むに従い次第に遠くなるように形成されている。周壁4cは、ファン2の回転方向において、舌部43から吐出部42にかけて、周壁4cとファン2の外周との間隙が予め定められた割合で拡大し、また、空気の流路面積が次第に大きくなるように形成されている。 (
The
周壁4cの渦巻形状としては、例えば、対数螺旋、アルキメデス螺旋、あるいは、インボリュート曲線等に基づく形状がある。周壁4cの内周面は、渦巻形状の巻始めとなる舌部43から渦巻形状の巻終りとなる巻終部41bまでファン2の周方向に沿って滑らかに湾曲する湾曲面を構成する。このような構成により、ファン2から送り出された空気は、ファン2から吐出部42の方向へファン2と周壁4cとの間隙を滑らかに流動する。このため、スクロールケーシング4内では、舌部43から吐出部42へ向かって空気の静圧が効率よく上昇する。
The spiral shape of the peripheral wall 4c includes, for example, a logarithmic spiral, an Archimedean spiral, or a shape based on an involute curve. The inner circumferential surface of the peripheral wall 4c constitutes a curved surface that curves smoothly along the circumferential direction of the fan 2 from the tongue portion 43 where the spiral winding begins to the winding end portion 41b where the spiral winding ends. With this configuration, the air sent out from the fan 2 smoothly flows through the gap between the fan 2 and the peripheral wall 4c from the fan 2 toward the discharge portion 42. Therefore, within the scroll casing 4, the static pressure of air increases efficiently from the tongue portion 43 toward the discharge portion 42.
周壁4cは、互いに対向する側壁4aの間に設けられた壁であり、ファン2の回転方向に沿った湾曲面を構成する。周壁4cは、回転軸RAの軸方向と平行に配置されてファン2を覆う。なお、周壁4cは、ファン2の回転軸RAの軸方向に対して傾斜した形態であってもよく、回転軸RAの軸方向と平行に配置される形態に限定されるものではない。
The peripheral wall 4c is a wall provided between the side walls 4a facing each other, and forms a curved surface along the rotation direction of the fan 2. The peripheral wall 4c is arranged parallel to the axial direction of the rotation axis RA and covers the fan 2. Note that the peripheral wall 4c may have a form that is inclined with respect to the axial direction of the rotation axis RA of the fan 2, and is not limited to a form that is arranged parallel to the axial direction of the rotation axis RA.
周壁4cは、ファン2の外周面2fと対向する内壁面を構成する。周壁4cは、ファン2の外周面2fを構成する複数枚の翼2dの外周側の端部と対向する。周壁4cは、ファン2の翼2dの空気の吹き出し側と対向する。周壁4cは、図1に示すように、渦巻形状の巻始め部分となる舌部43から、舌部43から離れた側の吐出部42とスクロール部41との境界に位置する巻終部41bまで、ファン2の回転方向に沿って設けられている。
The peripheral wall 4c constitutes an inner wall surface facing the outer peripheral surface 2f of the fan 2. The peripheral wall 4c faces the outer peripheral side ends of the plurality of blades 2d that constitute the outer peripheral surface 2f of the fan 2. The peripheral wall 4c faces the air blowing side of the blades 2d of the fan 2. As shown in FIG. 1, the peripheral wall 4c extends from a tongue portion 43 that is a spiral-shaped winding start portion to a winding end portion 41b that is located at the boundary between the discharge portion 42 and the scroll portion 41 on the side away from the tongue portion 43. , are provided along the rotation direction of the fan 2.
舌部43は、ファン2の回転によって、スクロールケーシング4の内部空間を周壁4cに沿って流れる気体の流れる方向において、湾曲面を構成する周壁4cにおける上流側の端部である。巻終部41bは、ファン2の回転によって、スクロールケーシング4の内部空間を周壁4cに沿って流れる気体の流れる方向において、湾曲面を構成する周壁4cにおける下流側の端部である。
The tongue portion 43 is an upstream end of the peripheral wall 4c that forms a curved surface in the direction in which gas flows through the internal space of the scroll casing 4 along the peripheral wall 4c due to the rotation of the fan 2. The winding end portion 41b is a downstream end of the peripheral wall 4c that forms a curved surface in the direction in which gas flows through the internal space of the scroll casing 4 along the peripheral wall 4c due to the rotation of the fan 2.
(舌部43)
スクロールケーシング4は、周壁4cのファン2の回転軸RAに近い巻始め部分において曲面を構成し、ファン2が発生させた気流を吐出口42aに導く舌部43を有する。周壁4cは、吐出部42側の端部に舌部43を含んでいる。舌部43は、渦巻形状に形成された周壁4cの巻始め部分に形成されている。 (Tongue 43)
Thescroll casing 4 forms a curved surface at a winding start portion of the peripheral wall 4c near the rotation axis RA of the fan 2, and has a tongue portion 43 that guides the airflow generated by the fan 2 to the discharge port 42a. The peripheral wall 4c includes a tongue portion 43 at the end on the discharge portion 42 side. The tongue portion 43 is formed at the beginning of the spiral-shaped peripheral wall 4c.
スクロールケーシング4は、周壁4cのファン2の回転軸RAに近い巻始め部分において曲面を構成し、ファン2が発生させた気流を吐出口42aに導く舌部43を有する。周壁4cは、吐出部42側の端部に舌部43を含んでいる。舌部43は、渦巻形状に形成された周壁4cの巻始め部分に形成されている。 (Tongue 43)
The
舌部43は、後述する吐出部42のディフューザ板42cとの境界部分に設けられている。舌部43は、曲面を有するように形成されており、回転軸RAの軸方向から見た場合に弧状に形成されている。舌部43は、予め定められた曲率半径で形成されており、周壁4cは、舌部43を介してディフューザ板42cと滑らかに接続されている。舌部43は、吐出口42aから見た場合に回転軸RAの軸方向において略同じ形状であり、回転軸RAの軸方向に沿った形状である。
The tongue portion 43 is provided at the boundary between the discharge portion 42 and the diffuser plate 42c, which will be described later. The tongue portion 43 is formed to have a curved surface, and is formed in an arc shape when viewed from the axial direction of the rotation axis RA. The tongue portion 43 is formed with a predetermined radius of curvature, and the peripheral wall 4c is smoothly connected to the diffuser plate 42c via the tongue portion 43. The tongue portion 43 has substantially the same shape in the axial direction of the rotation axis RA when viewed from the discharge port 42a, and has a shape along the axial direction of the rotation axis RA.
舌部43は、スクロールケーシング4の内部において、渦巻状流路の巻き終わりから巻き始めへの空気の流入を抑制する。舌部43は、通風路の上流部に設けられ、ファン2の回転方向に向かう空気の流れと、通風路の下流部から吐出口42aに向かう吐出方向の空気の流れと、を分流させる役割を有する。また、吐出部42に流入する空気流れは、スクロールケーシング4を通過する間に静圧が上昇して高圧となる。そのため、舌部43は、このような圧力差を仕切る機能を有する。舌部43は、圧力差を仕切る機能を有すると共に、曲面により、吐出部42に流入する空気を各流路へ導く機能を備えている。
The tongue portion 43 suppresses the inflow of air from the end of the spiral flow path to the beginning of the winding inside the scroll casing 4. The tongue portion 43 is provided at the upstream portion of the ventilation path, and has the role of separating the air flow in the rotation direction of the fan 2 and the air flow in the discharge direction from the downstream portion of the ventilation path toward the discharge port 42a. have Further, the static pressure of the air flowing into the discharge portion 42 increases while passing through the scroll casing 4, and becomes high pressure. Therefore, the tongue portion 43 has a function of partitioning off such a pressure difference. The tongue portion 43 has a function of partitioning a pressure difference, and also has a function of guiding air flowing into the discharge portion 42 to each flow path due to its curved surface.
(吐出部42)
吐出部42は、ファン2が発生させ、スクロール部41を通過した気流が吐出される吐出口42aを形成する。吐出部42は、周壁4cに沿って流動する空気の流れる方向に直交する断面が、矩形状となる中空の管で構成されている。なお、吐出部42の断面形状は、矩形に限定されるものではない。吐出部42は、ファン2から送り出されて周壁4cとファン2との間隙を流動する空気を、スクロールケーシング4の外部へ排出するように案内する流路を形成する。 (Discharge part 42)
Thedischarge part 42 forms a discharge port 42a through which the airflow generated by the fan 2 and passed through the scroll part 41 is discharged. The discharge portion 42 is constituted by a hollow tube having a rectangular cross section perpendicular to the direction in which air flows along the peripheral wall 4c. Note that the cross-sectional shape of the discharge portion 42 is not limited to a rectangle. The discharge part 42 forms a flow path that guides the air sent out from the fan 2 and flowing through the gap between the peripheral wall 4c and the fan 2 so as to be discharged to the outside of the scroll casing 4.
吐出部42は、ファン2が発生させ、スクロール部41を通過した気流が吐出される吐出口42aを形成する。吐出部42は、周壁4cに沿って流動する空気の流れる方向に直交する断面が、矩形状となる中空の管で構成されている。なお、吐出部42の断面形状は、矩形に限定されるものではない。吐出部42は、ファン2から送り出されて周壁4cとファン2との間隙を流動する空気を、スクロールケーシング4の外部へ排出するように案内する流路を形成する。 (Discharge part 42)
The
吐出部42の一方の端部は、スクロールケーシング4から吐出部42に空気が流入する流入口(図示は省略)を形成する。また、吐出部42の他方の端部は、吐出部42内の流路を流れた空気が外気へ排出される吐出口42aを形成する。
One end of the discharge section 42 forms an inlet (not shown) through which air flows into the discharge section 42 from the scroll casing 4. Further, the other end of the discharge section 42 forms a discharge port 42a through which the air that has flowed through the flow path within the discharge section 42 is discharged to the outside air.
吐出部42は、図2に示すように、延設板42bと、ディフューザ板42cと、第1側板部42dと、第2側板部42eとを有する。延設板42bは、周壁4cの下流側の巻終部41bに滑らかに連続して、周壁4cと一体に形成されている。ディフューザ板42cは、スクロールケーシング4の舌部43と一体に形成されており、延設板42bと対向する。ディフューザ板42cは、例えば、吐出部42内の空気の流れる方向に沿って流路の断面積が次第に拡大するように、延設板42bに対して所定の角度を有して形成されているが当該構成に限定されるものではない。
As shown in FIG. 2, the discharge part 42 has an extension plate 42b, a diffuser plate 42c, a first side plate part 42d, and a second side plate part 42e. The extension plate 42b is formed integrally with the peripheral wall 4c so as to smoothly continue to the winding end portion 41b on the downstream side of the peripheral wall 4c. The diffuser plate 42c is formed integrally with the tongue portion 43 of the scroll casing 4, and faces the extension plate 42b. For example, the diffuser plate 42c is formed at a predetermined angle with respect to the extension plate 42b so that the cross-sectional area of the flow path gradually expands along the direction in which air flows in the discharge portion 42. It is not limited to this configuration.
第1側板部42dは、スクロールケーシング4の第1側壁4a1と一体に形成されており、第2側板部42eは、スクロールケーシング4の反対側の第2側壁4a2と一体に形成されている。そして、第1側板部42dと第2側板部42eとは、延設板42bとディフューザ板42cとの間に形成されている。このように、吐出部42は、延設板42b、ディフューザ板42c、第1側板部42d及び第2側板部42eにより、断面矩形状の流路が形成されている。
The first side plate portion 42d is formed integrally with the first side wall 4a1 of the scroll casing 4, and the second side plate portion 42e is formed integrally with the second side wall 4a2 of the scroll casing 4 on the opposite side. The first side plate portion 42d and the second side plate portion 42e are formed between the extension plate 42b and the diffuser plate 42c. Thus, in the discharge section 42, a flow path having a rectangular cross section is formed by the extension plate 42b, the diffuser plate 42c, the first side plate part 42d, and the second side plate part 42e.
(ファン2とスクロールケーシング4との関係)
図6は、実施の形態1に係る多翼遠心送風機1の部分断面図である。図6は、図1の多翼遠心送風機1のA-A線位置の断面を矢視方向に見た図である。図6は、回転軸RAの径方向に見た多翼遠心送風機1の断面図である。変曲点部26は、翼2dの全長にわたって形成されている。翼2dの全長とは、回転軸RAの軸方向に沿った翼2dの長さであり、翼2dの主板2a側の基端部2hと翼2dの側板2c側の先端部2gとの間の部分の長さである。基端部2hは、回転軸RAの軸方向において、翼2dにおける一方の端部であり、主板2a側の端部である。先端部2gは、回転軸RAの軸方向において、翼2dにおける他方の端部であり、主板2aとは反対側の端部である。 (Relationship betweenfan 2 and scroll casing 4)
FIG. 6 is a partial cross-sectional view of the multi-bladecentrifugal blower 1 according to the first embodiment. FIG. 6 is a cross-sectional view taken along line AA of the multi-blade centrifugal blower 1 in FIG. 1, viewed in the direction of the arrows. FIG. 6 is a sectional view of the multi-blade centrifugal blower 1 viewed in the radial direction of the rotation axis RA. The inflection point portion 26 is formed over the entire length of the blade 2d. The total length of the blade 2d is the length of the blade 2d along the axial direction of the rotation axis RA, and is the length between the base end 2h of the blade 2d on the main plate 2a side and the tip 2g of the blade 2d on the side plate 2c side. is the length of the part. The base end portion 2h is one end portion of the blade 2d in the axial direction of the rotation axis RA, and is an end portion on the main plate 2a side. The tip portion 2g is the other end of the blade 2d in the axial direction of the rotation axis RA, and is the end on the opposite side from the main plate 2a.
図6は、実施の形態1に係る多翼遠心送風機1の部分断面図である。図6は、図1の多翼遠心送風機1のA-A線位置の断面を矢視方向に見た図である。図6は、回転軸RAの径方向に見た多翼遠心送風機1の断面図である。変曲点部26は、翼2dの全長にわたって形成されている。翼2dの全長とは、回転軸RAの軸方向に沿った翼2dの長さであり、翼2dの主板2a側の基端部2hと翼2dの側板2c側の先端部2gとの間の部分の長さである。基端部2hは、回転軸RAの軸方向において、翼2dにおける一方の端部であり、主板2a側の端部である。先端部2gは、回転軸RAの軸方向において、翼2dにおける他方の端部であり、主板2aとは反対側の端部である。 (Relationship between
FIG. 6 is a partial cross-sectional view of the multi-blade
多翼遠心送風機1は、図6に示すように、回転軸RAの径方向に見た場合に、変曲点部26の全ての部分が、ベルマウス3の内縁を形成する内周端部35よりも内周側に位置するように形成されている。すなわち、多翼遠心送風機1は、図6に示すように、回転軸RAの径方向に見た場合に、変曲点部26の全ての部分が、ベルマウス3の内周端部35よりも回転軸RA側に位置するように形成されている。多翼遠心送風機1は、変曲点部26の、回転軸RAの軸方向の全ての部分が、ファン2の径方向において、ベルマウス3の内縁を形成する内周端部35よりも内周側に位置するように形成されている。
As shown in FIG. 6, in the multi-blade centrifugal blower 1, when viewed in the radial direction of the rotation axis RA, all parts of the inflection point portion 26 form an inner circumferential end portion 35 that forms the inner edge of the bell mouth 3. It is formed so as to be located on the inner circumferential side. That is, in the multi-blade centrifugal blower 1, as shown in FIG. It is formed so as to be located on the rotation axis RA side. In the multi-blade centrifugal blower 1, all portions of the inflection point portion 26 in the axial direction of the rotation axis RA are inner than the inner peripheral end portion 35 forming the inner edge of the bell mouth 3 in the radial direction of the fan 2. It is formed to be located on the side.
多翼遠心送風機1は、翼2dの主板2a側の基端部2hから側板2c側の先端部2gまでの変曲点部26で構成された仮想線Bがファン2の回転軸RAと平行になるように形成されている。仮想線Bがファン2の回転軸RAと平行になるように形成されているとは、例えば、回転軸RAの径方向に見た場合に、仮想線Bが回転軸RAに対して±1度以内の角度となるように形成されている状態である。
In the multi-blade centrifugal blower 1, an imaginary line B formed by an inflection point 26 from a base end 2h on the main plate 2a side of the blade 2d to a tip end 2g on the side plate 2c side is parallel to the rotation axis RA of the fan 2. It is formed to be. When the imaginary line B is formed to be parallel to the rotation axis RA of the fan 2, for example, when viewed in the radial direction of the rotation axis RA, the imaginary line B is formed to be parallel to the rotation axis RA by ±1 degree. It is in a state where it is formed so that the angle is within the range.
[多翼遠心送風機1の動作]
図2を用いて多翼遠心送風機1の動作について説明する。多翼遠心送風機1は、モータ(図示は省略)が駆動すると、モータシャフトが接続された主板2aが回転し、主板2aを介して、複数枚の翼2dが回転軸RAを中心に回転する。ファン2が回転すると、スクロールケーシング4の外部にある空気が、吸込口5を通じてスクロールケーシング4の内部に吸い込まれる。 [Operation of multi-blade centrifugal blower 1]
The operation of the multi-bladecentrifugal blower 1 will be explained using FIG. 2. In the multi-blade centrifugal blower 1, when a motor (not shown) is driven, a main plate 2a to which a motor shaft is connected rotates, and a plurality of blades 2d rotate around a rotation axis RA via the main plate 2a. When the fan 2 rotates, air outside the scroll casing 4 is sucked into the scroll casing 4 through the suction port 5.
図2を用いて多翼遠心送風機1の動作について説明する。多翼遠心送風機1は、モータ(図示は省略)が駆動すると、モータシャフトが接続された主板2aが回転し、主板2aを介して、複数枚の翼2dが回転軸RAを中心に回転する。ファン2が回転すると、スクロールケーシング4の外部にある空気が、吸込口5を通じてスクロールケーシング4の内部に吸い込まれる。 [Operation of multi-blade centrifugal blower 1]
The operation of the multi-blade
スクロールケーシング4の内部に吸い込まれる空気は、ベルマウス3に案内されてファン2に吸い込まれる。ファン2に吸い込まれた空気は、複数枚の翼2dの間を通る過程で、動圧と静圧とが付加された気流となってファン2の径方向外側に向かって吹き出される。ファン2から吹き出される気流は、ファン2の昇圧作用によりファン2からスクロールケーシング4の内部に吹き出される。
Air sucked into the scroll casing 4 is guided by the bell mouth 3 and sucked into the fan 2. The air sucked into the fan 2 becomes an airflow to which dynamic pressure and static pressure are added during the process of passing between the plurality of blades 2d, and is blown out toward the outside in the radial direction of the fan 2. The airflow blown out from the fan 2 is blown out into the scroll casing 4 from the fan 2 due to the pressure increasing action of the fan 2 .
スクロールケーシング4内を流れる気流は、渦巻形状の周壁4cにより巻始め側から巻終わり側に徐々に拡大する風路を流れることで昇圧される。ファン2からスクロールケーシング4の内部に吹き出された空気は、スクロールケーシング4の周壁4cによって形成される拡大風路で減速されて静圧を回復し、図1に示す吐出口42aから外部に吹き出される。
The airflow flowing inside the scroll casing 4 is pressurized by flowing through an air path that gradually expands from the winding start side to the winding end side by the spiral-shaped peripheral wall 4c. The air blown into the scroll casing 4 from the fan 2 is decelerated in the enlarged air path formed by the peripheral wall 4c of the scroll casing 4, recovers static pressure, and is blown out from the discharge port 42a shown in FIG. Ru.
[多翼遠心送風機1の作用効果]
多翼遠心送風機1のファン2は、後向羽根部22と、前向羽根部21と、後向羽根部22と前向羽根部21との変曲点を形成する変曲点部26と、を有する。変曲点部26は、回転軸RAの軸方向において、複数枚の翼2dのそれぞれの主板2a側の基端部2hと側板2c側の先端部2gとの間の部分である翼2dの全長にわたって形成されている。また、変曲点部26の、回転軸RAの軸方向の全ての部分が、ファン2の径方向において、ベルマウス3の内縁を形成する内周端部35よりも内周側に位置するように形成されている。 [Effects of multi-blade centrifugal blower 1]
Thefan 2 of the multi-blade centrifugal blower 1 includes a backward blade portion 22, a forward blade portion 21, an inflection point portion 26 forming an inflection point between the backward blade portion 22 and the forward blade portion 21, has. The inflection point portion 26 is the entire length of the blade 2d, which is a portion between the base end 2h on the main plate 2a side and the tip end 2g on the side plate 2c side of each of the plurality of blades 2d in the axial direction of the rotation axis RA. It is formed over a period of time. Further, all portions of the inflection point portion 26 in the axial direction of the rotation axis RA are located on the inner circumferential side of the inner circumferential end portion 35 forming the inner edge of the bell mouth 3 in the radial direction of the fan 2. is formed.
多翼遠心送風機1のファン2は、後向羽根部22と、前向羽根部21と、後向羽根部22と前向羽根部21との変曲点を形成する変曲点部26と、を有する。変曲点部26は、回転軸RAの軸方向において、複数枚の翼2dのそれぞれの主板2a側の基端部2hと側板2c側の先端部2gとの間の部分である翼2dの全長にわたって形成されている。また、変曲点部26の、回転軸RAの軸方向の全ての部分が、ファン2の径方向において、ベルマウス3の内縁を形成する内周端部35よりも内周側に位置するように形成されている。 [Effects of multi-blade centrifugal blower 1]
The
ここで、変曲点部26の全ての部分が、ベルマウス3の内周端部35よりも内周側に位置するように形成されている場合を構成Aとし、変曲点部26の少なくとも一部あるいは全部が、内周端部35よりも外周側に位置するように形成されている場合を構成Bとする。同じ直径のファン2において構成Aと構成Bとを比較した場合、構成Aは、構成Bと比較して、翼2dにおいて、ファン2の径方向の距離における前向羽根部21の占める割合が大きくなる。そのため、多翼遠心送風機1は、変曲点部26の少なくとも一部あるいは全部が、内周端部35よりも外周側に位置するように形成されている構成と比較して、前縁25a側の部分から後縁24a側の部分に向かって翼角度の変化をなだらかにすることができ、負圧面2d2における気流の剥離を抑制し風量の低下を抑制できる。
Here, the case where all parts of the inflection point part 26 are formed so as to be located on the inner peripheral side than the inner peripheral end part 35 of the bell mouth 3 is referred to as configuration A, and at least the inflection point part 26 is A case in which a part or all of the inner circumferential end portion 35 is located on the outer circumferential side is referred to as configuration B. When comparing configuration A and configuration B for fans 2 of the same diameter, configuration A has a larger proportion of the forward blade portion 21 in the radial distance of the fan 2 in the blade 2d than configuration B. Become. Therefore, in the multi-blade centrifugal blower 1, compared to a configuration in which at least a part or all of the inflection point portion 26 is located on the outer peripheral side than the inner peripheral end portion 35, the multi-blade centrifugal blower 1 is closer to the leading edge 25a. It is possible to make the change in the blade angle gentle from the part toward the part on the trailing edge 24a side, and it is possible to suppress the separation of the airflow on the negative pressure surface 2d2 and suppress the decrease in the air volume.
また、ファン2は、複数枚の翼2dのそれぞれの主板2a側の基端部2hから側板2c側の先端部2gまでの変曲点部26で構成された仮想線Bが、回転軸RAと平行になるように形成されている。多翼遠心送風機1は、仮想線Bと回転軸RAとが平行に形成されているため、仮想線Bと回転軸RAとが平行でない場合と比較して、ファン2の製造時にファン2を金型から抜きやすく製造が容易となる。
Further, in the fan 2, a virtual line B formed by an inflection point 26 from a base end 2h on the main plate 2a side to a tip 2g on the side plate 2c side of each of the plurality of blades 2d is aligned with the rotation axis RA. They are formed to be parallel. In the multi-blade centrifugal blower 1, since the imaginary line B and the rotation axis RA are formed parallel to each other, compared to the case where the imaginary line B and the rotation axis RA are not parallel to each other, the fan 2 is made of metal during manufacturing. Easy to pull out from the mold and easy to manufacture.
実施の形態2.
図7は、実施の形態2に係る多翼遠心送風機1の部分断面図である。図7は、図1の多翼遠心送風機1のA-A線位置の断面を矢視方向に見た図である。図1~図6の多翼遠心送風機1と同一の構成を有する部位には同一の符号を付してその説明を省略する。Embodiment 2.
FIG. 7 is a partial cross-sectional view of the multi-bladecentrifugal blower 1 according to the second embodiment. FIG. 7 is a cross-sectional view taken along line AA of the multi-blade centrifugal blower 1 in FIG. 1, viewed in the direction of the arrows. Components having the same configuration as the multi-blade centrifugal blower 1 shown in FIGS. 1 to 6 are designated by the same reference numerals, and the description thereof will be omitted.
図7は、実施の形態2に係る多翼遠心送風機1の部分断面図である。図7は、図1の多翼遠心送風機1のA-A線位置の断面を矢視方向に見た図である。図1~図6の多翼遠心送風機1と同一の構成を有する部位には同一の符号を付してその説明を省略する。
FIG. 7 is a partial cross-sectional view of the multi-blade
実施の形態2に係る多翼遠心送風機1は、翼2dの形状の関係を更に特定するものである。また、実施の形態2に係る多翼遠心送風機1は、翼2dとベルマウス3との位置関係を更に特定するものである。翼2dの形状及び翼2dとベルマウス3との位置関係以外の他の部分の構成は、実施の形態1に係る多翼遠心送風機1と同様である。従って、以下の説明では、図7を用いて、実施の形態2に係る多翼遠心送風機1の翼2d及びベルマウス3の構成を中心に説明する。
The multi-blade centrifugal blower 1 according to the second embodiment further specifies the relationship between the shapes of the blades 2d. Furthermore, in the multi-blade centrifugal blower 1 according to the second embodiment, the positional relationship between the blades 2d and the bell mouth 3 is further specified. The configuration of other parts other than the shape of the blade 2d and the positional relationship between the blade 2d and the bell mouth 3 is the same as that of the multi-blade centrifugal blower 1 according to the first embodiment. Therefore, in the following description, the configurations of the blades 2d and the bell mouth 3 of the multi-blade centrifugal blower 1 according to the second embodiment will be mainly described using FIG.
実施の形態2に係る多翼遠心送風機1の翼2dは、側板2c側の前縁25aに切欠状の段差部27が形成されている。より詳細には、翼2dは、翼2dの前縁25aにおいて、側板2c側の先端部2gに切欠状の段差部27が形成されている。
The blade 2d of the multi-blade centrifugal blower 1 according to the second embodiment has a notch-shaped stepped portion 27 formed on the leading edge 25a on the side plate 2c side. More specifically, in the leading edge 25a of the blade 2d, a notch-shaped step portion 27 is formed at the tip 2g on the side plate 2c side.
段差部27は、前縁25a及び先端部2gを構成する壁が切り欠かれた状態に形成されている部分である。段差部27は、前縁25aの一部に形成されており、また、先端部2gの一部に形成されている。段差部27は、前縁25aの側板2c側の端部が切り欠かれており、先端部2gの回転軸RA側の端部が切り欠かれている。段差部27は、前縁25aと先端部2gとの連続する角部分が切り欠かれた状態に形成されている部分である。段差部27は、図7に示すように、後向羽根部22及び前向羽根部21の側板2c側の先端部2gに形成されている。
The stepped portion 27 is a portion formed by cutting out the wall that constitutes the front edge 25a and the tip portion 2g. The step portion 27 is formed in a portion of the front edge 25a, and is also formed in a portion of the tip portion 2g. In the step portion 27, the end portion of the front edge 25a on the side plate 2c side is cut out, and the end portion of the tip portion 2g on the rotation axis RA side is cut out. The stepped portion 27 is a portion formed by cutting out a continuous corner portion between the front edge 25a and the tip portion 2g. As shown in FIG. 7, the stepped portion 27 is formed at the tip portion 2g of the rearward blade portion 22 and the forward blade portion 21 on the side plate 2c side.
段差部27は、ファン2の回転軸RAの軸方向に延びる側部縁部27Aと、ファン2の径方向に延びる上部縁部27Bとによって形成されている。ファン2において、上部縁部27Bは、先端部2gよりも主板2a側に位置する縁部である。ファン2は、回転軸RAの軸方向において、上部縁部27Bと先端部2gとの間に段差が形成されている。また、ファン2は、段差部27における前縁25aの仮想の延長線Cに対して、側部縁部27Aがファン2の外周側に位置するように形成されている。ファン2は、回転軸RAの径方向において、前縁25aと側部縁部27Aとの間に段差が形成されている。
The stepped portion 27 is formed by a side edge 27A extending in the axial direction of the rotation axis RA of the fan 2 and an upper edge 27B extending in the radial direction of the fan 2. In the fan 2, the upper edge 27B is an edge located closer to the main plate 2a than the tip 2g. The fan 2 has a step formed between the upper edge 27B and the tip 2g in the axial direction of the rotation axis RA. Further, the fan 2 is formed such that the side edge 27A is located on the outer peripheral side of the fan 2 with respect to an imaginary extension line C of the front edge 25a of the stepped portion 27. The fan 2 has a step formed between the front edge 25a and the side edge 27A in the radial direction of the rotation axis RA.
段差部27は、ファン2の回転軸RAの軸方向に延びる側部縁部27Aと、ファン2の径方向に延びる上部縁部27Bとによって形成されている構成に限定されるものではない。例えば、段差部27は、側部縁部27Aと上部縁部27Bとが連続して一体に形成された弧状の縁部として形成されてもよい。
The stepped portion 27 is not limited to a configuration formed by a side edge 27A extending in the axial direction of the rotation axis RA of the fan 2 and an upper edge 27B extending in the radial direction of the fan 2. For example, the stepped portion 27 may be formed as an arcuate edge in which the side edge 27A and the upper edge 27B are continuously formed integrally.
実施の形態2に係る多翼遠心送風機1は、複数の翼2dのそれぞれの外周端24により構成される羽根外径が、ベルマウス3の内径よりも大きく形成されている。すなわち、実施の形態2に係る多翼遠心送風機1は、回転軸RAの軸方向に見た場合に、ファン2の径方向において、翼2dの外周端24がベルマウス3の内周端部35よりも外周側に位置するように形成されている。また、実施の形態2に係る多翼遠心送風機1は、回転軸RAの軸方向に見た場合に、ファン2の径方向において、翼2dの前縁25aの少なくとも一部がベルマウス3の内周端部35よりも内周側に位置するように形成されている。
In the multi-blade centrifugal blower 1 according to the second embodiment, the outer diameter of the blade formed by the outer peripheral end 24 of each of the plurality of blades 2d is larger than the inner diameter of the bell mouth 3. That is, in the multi-blade centrifugal blower 1 according to the second embodiment, when viewed in the axial direction of the rotation axis RA, the outer peripheral end 24 of the blade 2d is aligned with the inner peripheral end 35 of the bell mouth 3 in the radial direction of the fan 2. It is formed so as to be located on the outer peripheral side. Furthermore, in the multi-blade centrifugal blower 1 according to the second embodiment, at least a portion of the leading edge 25a of the blade 2d is inside the bell mouth 3 in the radial direction of the fan 2 when viewed in the axial direction of the rotation axis RA. It is formed so as to be located on the inner circumferential side of the circumferential end portion 35 .
翼2dにおいて、先端部2gと段差部27との境界部分を段差開始地点27Cと称する。段差開始地点27Cは、翼2dにおいて、翼2dの先端部2gと側部縁部27Aとの境界部分である。段差開始地点27Cは、先端部2gと側部縁部27Aとにより形成される翼2dの角部分である。実施の形態2に係る多翼遠心送風機1は、ファン2の径方向において、翼2dの段差開始地点27Cがベルマウス3の内周端部35よりも外周側に位置するように形成されている。
In the blade 2d, the boundary between the tip 2g and the stepped portion 27 is referred to as a stepped starting point 27C. The step starting point 27C is the boundary between the tip 2g of the blade 2d and the side edge 27A in the blade 2d. The step starting point 27C is a corner portion of the blade 2d formed by the tip portion 2g and the side edge portion 27A. The multi-blade centrifugal blower 1 according to the second embodiment is formed such that the step start point 27C of the blade 2d is located closer to the outer circumferential side than the inner circumferential end 35 of the bell mouth 3 in the radial direction of the fan 2. .
図7に示すように、実施の形態2に係る多翼遠心送風機1は、ベルマウス3の内周端部35が、段差部27の上方に配置される。実施の形態2に係る多翼遠心送風機1は、回転軸RAの軸方向において、ベルマウス3の内周端部35が、段差部27と対向するように構成されている。より詳細には、実施の形態2に係る多翼遠心送風機1は、回転軸RAの軸方向において、ベルマウス3の内周端部35が、上部縁部27Bと対向するように配置されている。実施の形態2に係る多翼遠心送風機1は、ベルマウス3の内周端部35と、上部縁部27Bとの間に隙間を形成している。
As shown in FIG. 7, in the multi-blade centrifugal blower 1 according to the second embodiment, the inner peripheral end portion 35 of the bell mouth 3 is arranged above the stepped portion 27. The multi-blade centrifugal blower 1 according to the second embodiment is configured such that the inner peripheral end portion 35 of the bell mouth 3 faces the stepped portion 27 in the axial direction of the rotation axis RA. More specifically, the multi-blade centrifugal blower 1 according to the second embodiment is arranged such that the inner peripheral end 35 of the bell mouth 3 faces the upper edge 27B in the axial direction of the rotation axis RA. . The multi-blade centrifugal blower 1 according to the second embodiment forms a gap between the inner peripheral end 35 of the bell mouth 3 and the upper edge 27B.
実施の形態2に係る多翼遠心送風機1は、更にファン2の径方向において、ベルマウス3の内周端部35が、側部縁部27Aと対向するように配置されてもよい。実施の形態2に係る多翼遠心送風機1は、回転軸RAの軸方向においてベルマウス3の内周端部35と上部縁部27Bとの間に隙間を形成すると共に、回転軸RAの径方向においてベルマウス3の内周端部35と側部縁部27Aとの間に隙間を形成してもよい。
The multi-blade centrifugal blower 1 according to the second embodiment may further be arranged such that the inner peripheral end 35 of the bell mouth 3 faces the side edge 27A in the radial direction of the fan 2. The multi-blade centrifugal blower 1 according to the second embodiment forms a gap between the inner peripheral end 35 and the upper edge 27B of the bell mouth 3 in the axial direction of the rotation axis RA, and also forms a gap in the radial direction of the rotation axis RA. A gap may be formed between the inner peripheral end 35 of the bell mouth 3 and the side edge 27A.
[多翼遠心送風機1の作用効果]
複数枚の翼2dのそれぞれは、側板2c側の前縁25aに切欠状の段差部27が形成されている。先端部2gと段差部27との境界部分を段差開始地点27Cとした場合に、ファン2の径方向において、段差開始地点27Cがベルマウス3の内周端部35よりも外周側に位置するように形成されている。実施の形態2に係る多翼遠心送風機1は、翼面を広くとるために翼2dの高さを高くしても、段差部27を有していることにより、翼2dがベルマウス3の内周端部35と干渉しない。 [Effects of multi-blade centrifugal blower 1]
Each of the plurality ofblades 2d has a notch-shaped stepped portion 27 formed on a leading edge 25a on the side plate 2c side. When the boundary between the tip portion 2g and the stepped portion 27 is defined as the step starting point 27C, the step starting point 27C is located on the outer circumferential side of the inner circumferential end 35 of the bell mouth 3 in the radial direction of the fan 2. is formed. In the multi-blade centrifugal blower 1 according to the second embodiment, even if the height of the blade 2d is increased to increase the blade surface, the blade 2d does not fit inside the bell mouth 3 due to the stepped portion 27. It does not interfere with the peripheral end portion 35.
複数枚の翼2dのそれぞれは、側板2c側の前縁25aに切欠状の段差部27が形成されている。先端部2gと段差部27との境界部分を段差開始地点27Cとした場合に、ファン2の径方向において、段差開始地点27Cがベルマウス3の内周端部35よりも外周側に位置するように形成されている。実施の形態2に係る多翼遠心送風機1は、翼面を広くとるために翼2dの高さを高くしても、段差部27を有していることにより、翼2dがベルマウス3の内周端部35と干渉しない。 [Effects of multi-blade centrifugal blower 1]
Each of the plurality of
多翼遠心送風機1は、段差開始地点27Cがベルマウス3の内周端部35よりも外周側に位置するように形成されていることで、ベルマウス3の内周端部35と翼2dとの間隔を確保したまま、回転軸RAの軸方向における翼2dの高さを高くすることができる。実施の形態2に係る多翼遠心送風機1は、段差部27を有しない翼2dと比較して、翼2dの先端部2gを側壁4aに近づけることができ、翼面積を大きくできるため、多くの風量を得ることができる。
The multi-blade centrifugal blower 1 is formed such that the step starting point 27C is located on the outer peripheral side of the inner peripheral end 35 of the bell mouth 3, so that the inner peripheral end 35 of the bell mouth 3 and the blade 2d are The height of the blade 2d in the axial direction of the rotation axis RA can be increased while maintaining the interval . The multi-blade centrifugal blower 1 according to the second embodiment can bring the tips 2g of the blades 2d closer to the side walls 4a and increase the blade area compared to the blades 2d without the stepped portion 27. You can get the air volume.
実施の形態3.
図8は、実施の形態3に係る多翼遠心送風機1の部分断面図である。図8は、図1の多翼遠心送風機1のA-A線位置の断面を矢視方向に見た図である。図1~図6の多翼遠心送風機1と同一の構成を有する部位には同一の符号を付してその説明を省略する。Embodiment 3.
FIG. 8 is a partial cross-sectional view of the multi-bladecentrifugal blower 1 according to the third embodiment. FIG. 8 is a cross-sectional view taken along line AA of the multi-blade centrifugal blower 1 in FIG. 1, viewed in the direction of the arrows. Components having the same configuration as the multi-blade centrifugal blower 1 shown in FIGS. 1 to 6 are designated by the same reference numerals, and the description thereof will be omitted.
図8は、実施の形態3に係る多翼遠心送風機1の部分断面図である。図8は、図1の多翼遠心送風機1のA-A線位置の断面を矢視方向に見た図である。図1~図6の多翼遠心送風機1と同一の構成を有する部位には同一の符号を付してその説明を省略する。
FIG. 8 is a partial cross-sectional view of the multi-blade
実施の形態3に係る多翼遠心送風機1は、翼2dとベルマウス3との位置関係を特定するものである。翼2dとベルマウス3との位置関係以外の他の部分の構成は、実施の形態1に係る多翼遠心送風機1と同様である。従って、以下の説明では、図8を用いて、実施の形態3に係る多翼遠心送風機1の翼2d及びベルマウス3の構成を中心に説明する。
The multi-blade centrifugal blower 1 according to the third embodiment specifies the positional relationship between the blades 2d and the bell mouth 3. The configuration of the other parts other than the positional relationship between the blades 2d and the bell mouth 3 is the same as that of the multi-blade centrifugal blower 1 according to the first embodiment. Therefore, in the following explanation, the configurations of the blades 2d and the bell mouth 3 of the multi-blade centrifugal blower 1 according to the third embodiment will be mainly explained using FIG.
実施の形態3に係る多翼遠心送風機1は、複数の翼2dのそれぞれの外周端24により構成される羽根外径が、ベルマウス3の内径よりも大きく形成されている。すなわち、実施の形態3に係る多翼遠心送風機1は、回転軸RAの軸方向に見た場合に、ファン2の径方向において、翼2dの外周端24がベルマウス3の内周端部35よりも外周側に位置するように形成されている。
In the multi-blade centrifugal blower 1 according to the third embodiment, the outer diameter of the blade formed by the outer peripheral end 24 of each of the plurality of blades 2d is larger than the inner diameter of the bell mouth 3. That is, in the multi-blade centrifugal blower 1 according to the third embodiment, when viewed in the axial direction of the rotation axis RA, the outer peripheral end 24 of the blade 2d is aligned with the inner peripheral end 35 of the bell mouth 3 in the radial direction of the fan 2. It is formed so as to be located on the outer peripheral side.
実施の形態3に係る多翼遠心送風機1は、回転軸RAの軸方向に見た場合に、ファン2の径方向において、翼2dの前縁25aの一部がベルマウス3の内周端部35よりも内周側に位置するように形成されている。実施の形態3に係る多翼遠心送風機1は、回転軸RAの軸方向に見た場合に、ファン2の径方向において、後向羽根部22がベルマウス3の内周端部35よりも内周側に位置するように形成されている。
In the multi-blade centrifugal blower 1 according to the third embodiment, when viewed in the axial direction of the rotation axis RA, in the radial direction of the fan 2, a part of the leading edge 25a of the blade 2d is located at the inner peripheral end of the bell mouth 3. It is formed so as to be located on the inner circumferential side than 35. In the multi-blade centrifugal blower 1 according to the third embodiment, when viewed in the axial direction of the rotation axis RA, the backward blade portion 22 is located further inward than the inner circumferential end portion 35 of the bell mouth 3 in the radial direction of the fan 2. It is formed so as to be located on the circumferential side.
ファン2において、翼2dの前縁25aと先端部2gとの境界部分に位置する前縁25aを側板側前縁部25bと称する。側板側前縁部25bは、先端部2gと前縁25aとにより形成される翼2dの角部分の一部を構成する。実施の形態3に係る多翼遠心送風機1は、ファン2の径方向において、翼2dの側板側前縁部25bがベルマウス3の内周端部35よりも外周側に位置するように形成されている。すなわち、実施の形態3に係る多翼遠心送風機1は、回転軸RAの軸方向において、ベルマウス3の内周端部35が、翼2dの前縁25aの一部と対向するように形成されている。
In the fan 2, the leading edge 25a located at the boundary between the leading edge 25a of the blade 2d and the tip 2g is referred to as a side plate side leading edge 25b. The side plate side leading edge portion 25b constitutes a part of the corner portion of the wing 2d formed by the tip portion 2g and the leading edge 25a. The multi-blade centrifugal blower 1 according to Embodiment 3 is formed such that the front edge portion 25b of the blade 2d on the side plate side is located on the outer peripheral side than the inner peripheral end portion 35 of the bell mouth 3 in the radial direction of the fan 2. ing. That is, in the multi-blade centrifugal blower 1 according to the third embodiment, the inner peripheral end 35 of the bell mouth 3 is formed so as to face a part of the leading edge 25a of the blade 2d in the axial direction of the rotation axis RA. ing.
[多翼遠心送風機1の作用効果]
実施の形態3に係る多翼遠心送風機1は、ファン2の径方向において、側板側前縁部25bがベルマウス3の内周端部35よりも外周側に位置するように形成されている。実施の形態3に係る多翼遠心送風機1は、翼面を広くとるために翼2dの高さを高くしても、側板側前縁部25bがベルマウス3の内周端部35よりも外周側に位置するように形成されていることにより、翼2dがベルマウス3の内周端部35と干渉しない。 [Effects of multi-blade centrifugal blower 1]
The multi-bladecentrifugal blower 1 according to the third embodiment is formed such that the front edge portion 25b on the side plate side is located on the outer peripheral side than the inner peripheral end portion 35 of the bell mouth 3 in the radial direction of the fan 2. In the multi-blade centrifugal blower 1 according to Embodiment 3, even if the height of the blade 2d is increased to increase the blade surface, the front edge 25b on the side plate side is closer to the outer periphery than the inner periphery end 35 of the bell mouth 3. By being formed so as to be located on the side, the wings 2d do not interfere with the inner peripheral end portion 35 of the bell mouth 3.
実施の形態3に係る多翼遠心送風機1は、ファン2の径方向において、側板側前縁部25bがベルマウス3の内周端部35よりも外周側に位置するように形成されている。実施の形態3に係る多翼遠心送風機1は、翼面を広くとるために翼2dの高さを高くしても、側板側前縁部25bがベルマウス3の内周端部35よりも外周側に位置するように形成されていることにより、翼2dがベルマウス3の内周端部35と干渉しない。 [Effects of multi-blade centrifugal blower 1]
The multi-blade
多翼遠心送風機1は、側板側前縁部25bがベルマウス3の内周端部35よりも外周側に位置するように形成されていることで、ベルマウス3の内周端部35と翼2dとの間隔を確保したまま、回転軸RAの軸方向における翼2dの高さを高くすることができる。多翼遠心送風機1は、側板側前縁部25bがベルマウス3の内周端部35よりも内周側に位置するように形成された翼2dと比較して、翼2dの先端部2gを側壁4aに近づけることができ、翼面積を大きくできるため、多くの風量を得ることができる。
The multi-blade centrifugal blower 1 is formed such that the front edge portion 25b on the side plate side is located on the outer peripheral side than the inner peripheral end portion 35 of the bell mouth 3, so that the inner peripheral end portion 35 of the bell mouth 3 and the blade The height of the blade 2d in the axial direction of the rotation axis RA can be increased while maintaining the distance from the blade 2d. The multi-blade centrifugal blower 1 has a tip portion 2g of the blade 2d that is formed such that the front edge portion 25b on the side plate side is located on the inner peripheral side of the inner peripheral end portion 35 of the bell mouth 3. Since it can be brought close to the side wall 4a and the blade area can be increased, a large amount of air can be obtained.
実施の形態4.
図9は、実施の形態4に係る多翼遠心送風機1におけるファン2の部分拡大図である。図9は、回転軸RAの軸方向に見たファン2の拡大図である。図9では、翼2dの形状を示すため、ベルマウス3を透過させて翼2dを示している。図1~図8の多翼遠心送風機1と同一の構成を有する部位には同一の符号を付してその説明を省略する。Embodiment 4.
FIG. 9 is a partially enlarged view of thefan 2 in the multi-blade centrifugal blower 1 according to the fourth embodiment. FIG. 9 is an enlarged view of the fan 2 viewed in the axial direction of the rotation axis RA. In FIG. 9, the wing 2d is shown with the bell mouth 3 transparent in order to show the shape of the wing 2d. Components having the same configuration as the multi-blade centrifugal blower 1 shown in FIGS. 1 to 8 are denoted by the same reference numerals, and the description thereof will be omitted.
図9は、実施の形態4に係る多翼遠心送風機1におけるファン2の部分拡大図である。図9は、回転軸RAの軸方向に見たファン2の拡大図である。図9では、翼2dの形状を示すため、ベルマウス3を透過させて翼2dを示している。図1~図8の多翼遠心送風機1と同一の構成を有する部位には同一の符号を付してその説明を省略する。
FIG. 9 is a partially enlarged view of the
実施の形態4に係る多翼遠心送風機1は、翼2dの形状を更に特定するものである。以下に説明する翼2dの形状以外の構成は、実施の形態1に係る多翼遠心送風機1と同様である。従って、以下の説明では、図9を用いて、実施の形態4に係る多翼遠心送風機1の翼2dの形状を中心に説明する。
In the multi-blade centrifugal blower 1 according to the fourth embodiment, the shape of the blades 2d is further specified. The configuration other than the shape of the blade 2d described below is the same as that of the multi-blade centrifugal blower 1 according to the first embodiment. Therefore, in the following explanation, the shape of the blade 2d of the multi-blade centrifugal blower 1 according to the fourth embodiment will be mainly explained using FIG.
翼2dを回転軸RAの軸方向に見た場合に、翼2dにおいて円弧状に形成された部分を円弧部ARと称する。実施の形態4に係る多翼遠心送風機1の翼2dにおいて、変曲点部26から翼2dの後縁24a(図3参照)までの部分が、図9に示すように、1つの円弧部ARまたは複数の円弧部ARで構成されている。すなわち、実施の形態4に係る多翼遠心送風機1の翼2dは、前向羽根部21が、図9に示すように、1つの円弧部ARまたは複数の円弧部ARで構成されている。実施の形態4に係る多翼遠心送風機1の翼2dは、変曲点部26から翼2dの後縁24a(図3参照)までの部分が、少なくとも1つ以上の円弧部ARで構成されている。
When the blade 2d is viewed in the axial direction of the rotation axis RA, the arc-shaped portion of the blade 2d is referred to as an arc portion AR. In the blade 2d of the multi-blade centrifugal blower 1 according to the fourth embodiment, the portion from the inflection point 26 to the trailing edge 24a (see FIG. 3) of the blade 2d is one arcuate portion AR, as shown in FIG. Alternatively, it is composed of a plurality of arcuate portions AR. That is, in the blade 2d of the multi-blade centrifugal blower 1 according to the fourth embodiment, the forward vane portion 21 is composed of one circular arc portion AR or a plurality of circular arc portions AR, as shown in FIG. In the blade 2d of the multi-blade centrifugal blower 1 according to the fourth embodiment, the portion from the inflection point 26 to the trailing edge 24a (see FIG. 3) of the blade 2d is composed of at least one arcuate portion AR. There is.
円弧部ARは、回転軸RAの軸方向に見た場合に、翼2dにおいて円弧状に形成された部分である。後縁24aは、外周端24で形成されている。外周端24は、回転軸RAに垂直な断面における翼2dの外周側の端部であり、後縁24aは、外周端24が回転軸の軸方向に連なった部分である。
The arc portion AR is a portion formed in an arc shape in the blade 2d when viewed in the axial direction of the rotation axis RA. The rear edge 24a is formed at the outer peripheral end 24. The outer peripheral end 24 is an end on the outer peripheral side of the blade 2d in a cross section perpendicular to the rotation axis RA, and the trailing edge 24a is a part where the outer peripheral end 24 is continuous in the axial direction of the rotation axis.
[多翼遠心送風機1の作用効果]
複数枚の翼2dのそれぞれは、変曲点部26から翼2dの後縁24aまでの部分が、少なくとも1つ以上の円弧部ARで構成されている。実施の形態4に係る多翼遠心送風機1は、翼2dの変曲点部26から翼の後縁24aまでの部分が、少なくとも1つ以上の円弧部ARで構成されていることで、ファン2の径方向における翼2dの急な角度変更を抑えている。そのため、多翼遠心送風機1は、負圧面2d2における気流の剥離を抑制し風量の低下を抑制できる。 [Effects of multi-blade centrifugal blower 1]
In each of the plurality ofblades 2d, a portion from the inflection point portion 26 to the trailing edge 24a of the blade 2d is constituted by at least one or more circular arc portions AR. In the multi-blade centrifugal blower 1 according to the fourth embodiment, the portion from the inflection point 26 of the blade 2d to the trailing edge 24a of the blade is configured with at least one arcuate portion AR, so that the fan 2 This suppresses sudden angle changes of the blade 2d in the radial direction. Therefore, the multi-blade centrifugal blower 1 can suppress separation of airflow on the negative pressure surface 2d2 and suppress a decrease in air volume.
複数枚の翼2dのそれぞれは、変曲点部26から翼2dの後縁24aまでの部分が、少なくとも1つ以上の円弧部ARで構成されている。実施の形態4に係る多翼遠心送風機1は、翼2dの変曲点部26から翼の後縁24aまでの部分が、少なくとも1つ以上の円弧部ARで構成されていることで、ファン2の径方向における翼2dの急な角度変更を抑えている。そのため、多翼遠心送風機1は、負圧面2d2における気流の剥離を抑制し風量の低下を抑制できる。 [Effects of multi-blade centrifugal blower 1]
In each of the plurality of
以上、好ましい実施の形態等について詳説したが、上述した実施の形態等に制限されることはなく、特許請求の範囲に記載された範囲を逸脱することなく、上述した実施の形態等に種々の変形及び置換を加えることができる。
Although the preferred embodiments have been described in detail above, they are not limited to the embodiments described above, and various modifications may be made to the embodiments described above without departing from the scope of the claims. Variations and substitutions can be made.
以下、本開示の諸態様を付記としてまとめて記載する。
Hereinafter, various aspects of the present disclosure will be collectively described as supplementary notes.
(付記1)
回転軸の軸方向に見た場合に円形状の主板と、前記主板の周縁部に設置される複数枚の翼と、前記回転軸の軸方向において前記複数枚の翼の前記主板と反対側の端部を固定する環状の側板と、を有するファンと、
渦巻形状に形成された周壁と、吸込口を形成するベルマウスを有する少なくとも1つの側壁と、を有し、前記ファンが発生させた気流が吐出される吐出口を形成し、前記ファンを収納するスクロールケーシングと、
を備え、
前記ファンは、
前記ファンの径方向において、前記複数枚の翼のそれぞれの内周側の部分において後向羽根を構成する後向羽根部と、
前記ファンの径方向において、前記複数枚の翼のそれぞれの外周側の部分において前向羽根を構成する前向羽根部と、
前記回転軸の軸方向に見た場合に、前記後向羽根部と前記前向羽根部との変曲点を形成する変曲点部と、
を有し、
前記変曲点部は、
前記回転軸の軸方向において、前記複数枚の翼のそれぞれの前記主板側の基端部と前記側板側の先端部との間の部分である翼の全長にわたって形成されており、前記変曲点部の前記軸方向の全ての部分が、前記ファンの径方向において、前記ベルマウスの内縁を形成する内周端部よりも内周側に位置するように形成されている多翼遠心送風機。
(付記2)
前記ファンは、
前記複数枚の翼のそれぞれの前記主板側の前記基端部から前記側板側の前記先端部までの前記変曲点部で構成された仮想線が、前記回転軸と平行になるように形成されている付記1に記載の多翼遠心送風機。
(付記3)
前記複数枚の翼のそれぞれは、
前記側板側の前縁に切欠状の段差部が形成されており、
前記先端部と前記段差部との境界部分を段差開始地点とした場合に、前記ファンの径方向において、前記段差開始地点が前記ベルマウスの前記内周端部よりも外周側に位置するように形成されている付記1又は2に記載の多翼遠心送風機。
(付記4)
前記ファンにおいて、前記複数枚の翼のそれぞれの前縁と前記先端部との境界部分に位置する前記前縁を側板側前縁部とした場合に、
前記ファンの径方向において、前記側板側前縁部が前記ベルマウスの前記内周端部よりも外周側に位置するように形成されている付記1~3のいずれか1つに記載の多翼遠心送風機。
(付記5)
前記回転軸の軸方向に見た場合に、翼において円弧状に形成された部分を円弧部とした場合に、
前記複数枚の翼のそれぞれは、
前記変曲点部から翼の後縁までの部分が、少なくとも1つ以上の前記円弧部で構成されている付記1~4のいずれか1つに記載の多翼遠心送風機。 (Additional note 1)
A main plate having a circular shape when viewed in the axial direction of the rotating shaft, a plurality of blades installed on the peripheral edge of the main plate, and a side opposite to the main plate of the plurality of blades in the axial direction of the rotating shaft. a fan having an annular side plate fixing an end;
It has a peripheral wall formed in a spiral shape and at least one side wall having a bell mouth forming an inlet, forming an outlet from which airflow generated by the fan is discharged, and housing the fan. scroll casing;
Equipped with
The fan is
In the radial direction of the fan, a rearward blade portion that constitutes a rearward blade at an inner peripheral side portion of each of the plurality of blades;
In the radial direction of the fan, a forward blade portion that constitutes a forward blade at an outer peripheral side portion of each of the plurality of blades;
an inflection point portion that forms an inflection point between the backward blade portion and the forward blade portion when viewed in the axial direction of the rotating shaft;
has
The inflection point portion is
In the axial direction of the rotating shaft, the inflection point is formed over the entire length of the blade, which is a portion between the base end on the main plate side and the tip end on the side plate side of each of the plurality of blades. A multi-blade centrifugal blower, wherein all portions in the axial direction of the fan are located on the inner peripheral side of an inner peripheral end forming an inner edge of the bell mouth in the radial direction of the fan.
(Additional note 2)
The fan is
An imaginary line formed by the inflection point from the base end on the main plate side to the tip end on the side plate side of each of the plurality of wings is formed so as to be parallel to the rotation axis. The multi-blade centrifugal blower described inSupplementary Note 1.
(Additional note 3)
Each of the plurality of wings is
A notch-like stepped portion is formed on the front edge of the side plate,
When the boundary between the tip end and the stepped portion is defined as a step starting point, the step starting point is located on the outer peripheral side of the inner peripheral end of the bell mouth in the radial direction of the fan. The multi-blade centrifugal blower according to supplementary note 1 or 2, which is formed.
(Additional note 4)
In the fan, when the front edge located at the boundary between the front edge of each of the plurality of blades and the tip portion is a side plate side front edge,
The multi-blade according to any one ofSupplementary Notes 1 to 3, wherein the front edge on the side plate side is formed to be located on the outer peripheral side of the inner peripheral end of the bell mouth in the radial direction of the fan. Centrifugal blower.
(Appendix 5)
When viewed in the axial direction of the rotating shaft, when the arc-shaped portion of the blade is defined as the arc portion,
Each of the plurality of wings is
The multi-blade centrifugal blower according to any one ofappendices 1 to 4, wherein a portion from the inflection point to the trailing edge of the blade is constituted by at least one or more circular arc portions.
回転軸の軸方向に見た場合に円形状の主板と、前記主板の周縁部に設置される複数枚の翼と、前記回転軸の軸方向において前記複数枚の翼の前記主板と反対側の端部を固定する環状の側板と、を有するファンと、
渦巻形状に形成された周壁と、吸込口を形成するベルマウスを有する少なくとも1つの側壁と、を有し、前記ファンが発生させた気流が吐出される吐出口を形成し、前記ファンを収納するスクロールケーシングと、
を備え、
前記ファンは、
前記ファンの径方向において、前記複数枚の翼のそれぞれの内周側の部分において後向羽根を構成する後向羽根部と、
前記ファンの径方向において、前記複数枚の翼のそれぞれの外周側の部分において前向羽根を構成する前向羽根部と、
前記回転軸の軸方向に見た場合に、前記後向羽根部と前記前向羽根部との変曲点を形成する変曲点部と、
を有し、
前記変曲点部は、
前記回転軸の軸方向において、前記複数枚の翼のそれぞれの前記主板側の基端部と前記側板側の先端部との間の部分である翼の全長にわたって形成されており、前記変曲点部の前記軸方向の全ての部分が、前記ファンの径方向において、前記ベルマウスの内縁を形成する内周端部よりも内周側に位置するように形成されている多翼遠心送風機。
(付記2)
前記ファンは、
前記複数枚の翼のそれぞれの前記主板側の前記基端部から前記側板側の前記先端部までの前記変曲点部で構成された仮想線が、前記回転軸と平行になるように形成されている付記1に記載の多翼遠心送風機。
(付記3)
前記複数枚の翼のそれぞれは、
前記側板側の前縁に切欠状の段差部が形成されており、
前記先端部と前記段差部との境界部分を段差開始地点とした場合に、前記ファンの径方向において、前記段差開始地点が前記ベルマウスの前記内周端部よりも外周側に位置するように形成されている付記1又は2に記載の多翼遠心送風機。
(付記4)
前記ファンにおいて、前記複数枚の翼のそれぞれの前縁と前記先端部との境界部分に位置する前記前縁を側板側前縁部とした場合に、
前記ファンの径方向において、前記側板側前縁部が前記ベルマウスの前記内周端部よりも外周側に位置するように形成されている付記1~3のいずれか1つに記載の多翼遠心送風機。
(付記5)
前記回転軸の軸方向に見た場合に、翼において円弧状に形成された部分を円弧部とした場合に、
前記複数枚の翼のそれぞれは、
前記変曲点部から翼の後縁までの部分が、少なくとも1つ以上の前記円弧部で構成されている付記1~4のいずれか1つに記載の多翼遠心送風機。 (Additional note 1)
A main plate having a circular shape when viewed in the axial direction of the rotating shaft, a plurality of blades installed on the peripheral edge of the main plate, and a side opposite to the main plate of the plurality of blades in the axial direction of the rotating shaft. a fan having an annular side plate fixing an end;
It has a peripheral wall formed in a spiral shape and at least one side wall having a bell mouth forming an inlet, forming an outlet from which airflow generated by the fan is discharged, and housing the fan. scroll casing;
Equipped with
The fan is
In the radial direction of the fan, a rearward blade portion that constitutes a rearward blade at an inner peripheral side portion of each of the plurality of blades;
In the radial direction of the fan, a forward blade portion that constitutes a forward blade at an outer peripheral side portion of each of the plurality of blades;
an inflection point portion that forms an inflection point between the backward blade portion and the forward blade portion when viewed in the axial direction of the rotating shaft;
has
The inflection point portion is
In the axial direction of the rotating shaft, the inflection point is formed over the entire length of the blade, which is a portion between the base end on the main plate side and the tip end on the side plate side of each of the plurality of blades. A multi-blade centrifugal blower, wherein all portions in the axial direction of the fan are located on the inner peripheral side of an inner peripheral end forming an inner edge of the bell mouth in the radial direction of the fan.
(Additional note 2)
The fan is
An imaginary line formed by the inflection point from the base end on the main plate side to the tip end on the side plate side of each of the plurality of wings is formed so as to be parallel to the rotation axis. The multi-blade centrifugal blower described in
(Additional note 3)
Each of the plurality of wings is
A notch-like stepped portion is formed on the front edge of the side plate,
When the boundary between the tip end and the stepped portion is defined as a step starting point, the step starting point is located on the outer peripheral side of the inner peripheral end of the bell mouth in the radial direction of the fan. The multi-blade centrifugal blower according to
(Additional note 4)
In the fan, when the front edge located at the boundary between the front edge of each of the plurality of blades and the tip portion is a side plate side front edge,
The multi-blade according to any one of
(Appendix 5)
When viewed in the axial direction of the rotating shaft, when the arc-shaped portion of the blade is defined as the arc portion,
Each of the plurality of wings is
The multi-blade centrifugal blower according to any one of
1 多翼遠心送風機、2 ファン、2a 主板、2a1 周縁部、2a2 中央部、2b ボス部、2c 側板、2d 翼、2d1 正圧面、2d2 負圧面、2e ファン吸込口、2f 外周面、2g 先端部、2h 基端部、3 ベルマウス、4 スクロールケーシング、4a 側壁、4a1 第1側壁、4a2 第2側壁、4c 周壁、5 吸込口、21 前向羽根部、22 後向羽根部、24 外周端、24a 後縁、25 内周端、25a 前縁、25b 側板側前縁部、26 変曲点部、27 段差部、27A 側部縁部、27B 上部縁部、27C 段差開始地点、35 内周端部、41 スクロール部、41b 巻終部、42 吐出部、42a 吐出口、42b 延設板、42c ディフューザ板、42d 第1側板部、42e 第2側板部、43 舌部、AR 円弧部、B 仮想線。
1 Multi-blade centrifugal blower, 2 Fan, 2a Main plate, 2a1 Periphery, 2a2 Center, 2b Boss, 2c Side plate, 2d Wing, 2d1 Positive pressure surface, 2d2 Negative pressure surface, 2e Fan suction port, 2f Outer surface, 2g Tip , 2h base end, 3 bell mouth, 4 scroll casing, 4a side wall, 4a1 first side wall, 4a2 second side wall, 4c peripheral wall, 5 suction port, 21 forward blade part, 22 backward blade part, 24 outer peripheral end, 24a rear edge, 25 inner peripheral end, 25a front edge, 25b side plate side front edge, 26 inflection point, 27 step part, 27A side edge, 27B upper edge, 27C step start point, 35 inner peripheral end Part, 41 scroll part, 41b winding end part, 42 discharge part, 42a discharge port, 42b extension plate, 42c diffuser plate, 42d first side plate part, 42e second side plate part, 43 tongue part, AR arc part, B virtual line.
Claims (5)
- 回転軸の軸方向に見た場合に円形状の主板と、前記主板の周縁部に設置される複数枚の翼と、前記回転軸の軸方向において前記複数枚の翼の前記主板と反対側の端部を固定する環状の側板と、を有するファンと、
渦巻形状に形成された周壁と、吸込口を形成するベルマウスを有する少なくとも1つの側壁と、を有し、前記ファンが発生させた気流が吐出される吐出口を形成し、前記ファンを収納するスクロールケーシングと、
を備え、
前記ファンは、
前記ファンの径方向において、前記複数枚の翼のそれぞれの内周側の部分において後向羽根を構成する後向羽根部と、
前記ファンの径方向において、前記複数枚の翼のそれぞれの外周側の部分において前向羽根を構成する前向羽根部と、
前記回転軸の軸方向に見た場合に、前記後向羽根部と前記前向羽根部との変曲点を形成する変曲点部と、
を有し、
前記変曲点部は、
前記回転軸の軸方向において、前記複数枚の翼のそれぞれの前記主板側の基端部と前記側板側の先端部との間の部分である翼の全長にわたって形成されており、前記変曲点部の前記軸方向の全ての部分が、前記ファンの径方向において、前記ベルマウスの内縁を形成する内周端部よりも内周側に位置するように形成されている多翼遠心送風機。 A main plate having a circular shape when viewed in the axial direction of the rotating shaft, a plurality of blades installed on the peripheral edge of the main plate, and a side opposite to the main plate of the plurality of blades in the axial direction of the rotating shaft. a fan having an annular side plate fixing an end;
It has a peripheral wall formed in a spiral shape and at least one side wall having a bell mouth forming an inlet, forming an outlet from which airflow generated by the fan is discharged, and housing the fan. scroll casing;
Equipped with
The fan is
In the radial direction of the fan, a rearward blade portion that constitutes a rearward blade at an inner peripheral side portion of each of the plurality of blades;
In the radial direction of the fan, a forward blade portion that constitutes a forward blade at an outer peripheral side portion of each of the plurality of blades;
an inflection point portion that forms an inflection point between the backward blade portion and the forward blade portion when viewed in the axial direction of the rotating shaft;
has
The inflection point portion is
In the axial direction of the rotating shaft, the inflection point is formed over the entire length of the blade, which is a portion between the base end on the main plate side and the tip end on the side plate side of each of the plurality of blades. A multi-blade centrifugal blower, wherein all portions in the axial direction of the fan are located on the inner peripheral side of an inner peripheral end forming an inner edge of the bell mouth in the radial direction of the fan. - 前記ファンは、
前記複数枚の翼のそれぞれの前記主板側の前記基端部から前記側板側の前記先端部までの前記変曲点部で構成された仮想線が、前記回転軸と平行になるように形成されている請求項1に記載の多翼遠心送風機。 The fan is
An imaginary line formed by the inflection point from the base end on the main plate side to the tip end on the side plate side of each of the plurality of wings is formed so as to be parallel to the rotation axis. The multi-blade centrifugal blower according to claim 1. - 前記複数枚の翼のそれぞれは、
前記側板側の前縁に切欠状の段差部が形成されており、
前記先端部と前記段差部との境界部分を段差開始地点とした場合に、前記ファンの径方向において、前記段差開始地点が前記ベルマウスの前記内周端部よりも外周側に位置するように形成されている請求項1又は2に記載の多翼遠心送風機。 Each of the plurality of wings is
A notch-like stepped portion is formed on the front edge of the side plate,
When a boundary between the tip end portion and the stepped portion is defined as a step starting point, the step starting point is located on the outer peripheral side of the inner peripheral end of the bell mouth in the radial direction of the fan. The multi-blade centrifugal blower according to claim 1 or 2, wherein the multi-blade centrifugal blower is formed. - 前記ファンにおいて、前記複数枚の翼のそれぞれの前縁と前記先端部との境界部分に位置する前記前縁を側板側前縁部とした場合に、
前記ファンの径方向において、前記側板側前縁部が前記ベルマウスの前記内周端部よりも外周側に位置するように形成されている請求項1~3のいずれか1項に記載の多翼遠心送風機。 In the fan, when the front edge located at the boundary between the leading edge of each of the plurality of blades and the tip portion is a side plate side front edge,
The fan according to any one of claims 1 to 3, wherein the front edge on the side plate side is formed to be located on the outer peripheral side of the inner peripheral end of the bell mouth in the radial direction of the fan. Wing centrifugal blower. - 前記回転軸の軸方向に見た場合に、翼において円弧状に形成された部分を円弧部とした場合に、
前記複数枚の翼のそれぞれは、
前記変曲点部から翼の後縁までの部分が、少なくとも1つ以上の前記円弧部で構成されている請求項1~4のいずれか1項に記載の多翼遠心送風機。 When viewed in the axial direction of the rotating shaft, when the arc-shaped portion of the blade is defined as the arc portion,
Each of the plurality of wings is
The multi-blade centrifugal blower according to any one of claims 1 to 4, wherein a portion from the inflection point to the trailing edge of the blade is comprised of at least one or more circular arc portions.
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JP2020204328A (en) * | 2019-04-25 | 2020-12-24 | 三菱電機株式会社 | Impeller, multi-blade blower and air conditioner |
WO2021210201A1 (en) * | 2020-04-16 | 2021-10-21 | 三菱電機株式会社 | Impeller, centrifugal blower, and air-conditioning device |
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JP2020204328A (en) * | 2019-04-25 | 2020-12-24 | 三菱電機株式会社 | Impeller, multi-blade blower and air conditioner |
WO2021210201A1 (en) * | 2020-04-16 | 2021-10-21 | 三菱電機株式会社 | Impeller, centrifugal blower, and air-conditioning device |
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