WO2022085175A1 - 多翼遠心送風機 - Google Patents

多翼遠心送風機 Download PDF

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Publication number
WO2022085175A1
WO2022085175A1 PCT/JP2020/039898 JP2020039898W WO2022085175A1 WO 2022085175 A1 WO2022085175 A1 WO 2022085175A1 JP 2020039898 W JP2020039898 W JP 2020039898W WO 2022085175 A1 WO2022085175 A1 WO 2022085175A1
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WO
WIPO (PCT)
Prior art keywords
blade
inner peripheral
impeller
wing
plate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/JP2020/039898
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
弘恭 林
拓矢 寺本
克洋 藤木
和平 新宮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to US18/043,917 priority Critical patent/US12241477B2/en
Priority to CN202080106321.3A priority patent/CN116348680A/zh
Priority to EP20958725.2A priority patent/EP4234946A4/en
Priority to JP2022556346A priority patent/JP7466683B2/ja
Priority to PCT/JP2020/039898 priority patent/WO2022085175A1/ja
Priority to TW110108114A priority patent/TWI747758B/zh
Publication of WO2022085175A1 publication Critical patent/WO2022085175A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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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
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4226—Fan casings
    • 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
    • F04D29/281—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08—Centrifugal pumps
    • F04D17/16—Centrifugal pumps for displacing without appreciable compression
    • F04D17/162—Double suction pumps
    • 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
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/50—Building or constructing in particular ways
    • F05D2230/54—Building or constructing in particular ways by sheet metal manufacturing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade

Definitions

  • This disclosure relates to a multi-blade centrifugal blower with an impeller.
  • the multi-blade centrifugal blower is equipped with an impeller and a spiral scroll casing in which the impeller is housed.
  • the impeller is composed of a main plate, an annular side plate facing the main plate, and a plurality of blades provided between the main plate and the side plate. Air is sucked from the side plate side by rotation and scrolls through the blades. Let it flow out into the air passage inside the casing. The airflow is boosted in the air passage inside the scroll casing and blown out from the discharge port.
  • a multi-blade centrifugal blower there is a method of increasing the number of blades as a means of increasing the air volume.
  • Patent Document 1 In the multi-blade centrifugal blower disclosed in Patent Document 1, the swept wing provided on the inner peripheral side of the wing is arranged inside the inner peripheral end of the side plate to be exposed, and air is released by the exposed swept wing. It is captured. In the multi-blade centrifugal blower of Patent Document 1, the impeller is injection-molded from a resin material.
  • Patent Document 1 when an impeller is injection-molded from a resin material, the wall thickness of the blade is generally thicker on the main plate side than on the side plate side due to the moldability of the impeller, and the main plate of the impeller is generally thicker. On the side, the gap formed between the wings is narrower than on the side plate side. Therefore, in the multi-blade centrifugal blower of Patent Document 1, although the swept wing is exposed from the inner peripheral end of the side plate, the air that has reached the vicinity of the swept wing cannot be sufficiently taken into the blades on the main plate side, and the blades. The effect of increasing the suction air volume may not be obtained on the main plate side of the car.
  • the present disclosure has been made in order to solve the above-mentioned problems, and it is possible to increase the suction air volume on the main plate side of the impeller as compared with the conventional multi-blade centrifugal blower made of a resin material. It is an object of the present invention to provide a multi-blade centrifugal blower capable of being capable.
  • the multi-blade centrifugal blower has a disk-shaped main plate, a plurality of blades arranged in the circumferential direction on the peripheral edge of the main plate, and arranged so as to face the main plate and fix the plurality of blades. It comprises an impeller having an annular side plate, a spiral scroll casing in which the impeller is housed and air is introduced from the side plate side and blown out to the outer peripheral side, and the impeller is made of metal.
  • the wing has a certain wall thickness from the main plate side to the side plate side, and extends inward from the inner peripheral end of the side plate.
  • the impeller is made of metal and the wall thickness of the blade is constant from the side plate to the main plate side, the blade extends inward from the inner peripheral end of the side plate in the blade.
  • a gap between the blades similar to that on the side plate side of the vehicle can be secured on the main plate side of the impeller. Therefore, the suction air volume can be increased even on the main plate side of the impeller as compared with the conventional multi-blade centrifugal blower made of a resin material.
  • FIG. 5 is an external view schematically showing a configuration in which the multi-blade centrifugal blower according to the first embodiment is viewed in parallel with the axis of rotation. It is sectional drawing which shows typically the AA line cross section of the multi-blade centrifugal blower of FIG. It is a figure which shows typically the structure which saw the impeller of the multi-blade centrifugal blower of FIG. 1 parallel to the axis of rotation. It is sectional drawing which shows the BB line cross section of the impeller of FIG. 3 schematically. It is a figure which shows typically the positional relationship between the bell mouth of FIG. 2 and an impeller. FIG. 3 is an enlarged partial perspective view of a part of the outer peripheral portion of the impeller of FIG. It is a figure which shows typically the structure which saw the blade of the multi-blade centrifugal blower which concerns on Embodiment 2 parallel to the axis of rotation. It is a figure which shows the deformation example of the wing of FIG.
  • FIG. 1 is an external view schematically showing a configuration in which the multi-blade centrifugal blower 100 according to the first embodiment is viewed in parallel with the rotation axis RS.
  • FIG. 2 is a cross-sectional view schematically showing a cross section taken along line AA of the multi-blade centrifugal blower 100 of FIG. The basic structure of the multi-blade centrifugal blower 100 will be described with reference to FIGS. 1 and 2.
  • the multi-blade centrifugal blower 100 is a multi-blade centrifugal blower, and has an impeller 10 for generating an air flow and a scroll casing 20 in which the impeller 10 is housed.
  • the impeller 10 has a disk-shaped main plate 11 as shown in FIG. 1, a plurality of blades 12 having a uniform thickness, and an annular side plate 13 as shown in FIG.
  • the main plate 11 is provided with a shaft portion 11b to which a motor (not shown) is connected.
  • the plurality of wings 12 are arranged in the circumferential direction on the peripheral edge of the main plate 11.
  • the side plate 13 is arranged so as to face the main plate 11 and fixes a plurality of blades 12.
  • the scroll casing 20 has a scroll portion 21 and a discharge portion 22 in which an air discharge port 22b is formed, and rectifies an air flow blown out from the impeller 10 in the centrifugal direction. It is a thing.
  • the scroll casing 20 has a spiral shape, and an air passage 20a that gradually expands toward the discharge port 22b is formed inside.
  • the scroll portion 21 forms an air passage 20a that converts the dynamic pressure of the airflow generated by the rotation of the impeller 10 into static pressure.
  • the scroll portion 21 has a side wall 23 that covers the impeller 10 from the axial direction of the virtual rotating shaft RS of the impeller 10, and a peripheral wall 24 that surrounds the impeller 10 from the radial outside of the rotating shaft RS.
  • a suction port 23b for sucking air is formed on the side wall 23.
  • the scroll portion 21 has a tongue portion 25 located between the discharge portion 22 and the winding start portion 24a of the peripheral wall 24 to form a curved surface.
  • the tongue portion 25 has a configuration in which the airflow blown out from the impeller 10 in the centrifugal direction in the vicinity of the winding start portion 24a is guided to the rotation direction R of the impeller 10 so as to be directed to the discharge port 22b via the scroll portion 21. Will be done.
  • the radial direction of the rotating shaft RS is a direction perpendicular to the axial direction of the rotating shaft RS.
  • the internal space of the scroll portion 21 composed of the peripheral wall 24 and the side wall 23 is the above-mentioned air passage 20a, and the airflow blown from the impeller 10 flows along the peripheral wall 24 in the air passage 20a.
  • the multi-blade centrifugal blower 100 is a double suction type centrifugal blower in which air is sucked from both ends in the axial direction of the virtual rotation axis RS of the impeller 10.
  • the side walls 23 are arranged on both sides of the impeller 10 in the axial direction of the rotation axis RS of the impeller 10.
  • a suction port 23b is formed on the side wall 23 of the scroll casing 20 so that air can flow between the impeller 10 and the outside of the scroll casing 20.
  • the suction port 23b is formed in a circular shape, and the impeller 10 has the center of the suction port 23b and the center of the shaft portion 11b of the impeller 10 substantially coincide with each other in the scroll casing 20. Be placed.
  • the impeller 10 is pivotally supported by the scroll casing 20 so that it can rotate.
  • the scroll casing 20 is a double suction type casing having side walls 23 having suction ports 23b formed on both sides of the main plate 11 in the axial direction of the rotation axis RS of the impeller 10.
  • the two side walls 23 are provided so as to face each other via the peripheral wall 24.
  • the suction port 23b provided on the side wall 23 is formed by the bell mouth 26. That is, the bell mouth 26 forms a suction port 23b that communicates with the space formed by the main plate 11 and the plurality of blades 12 in the impeller 10.
  • the space formed by the main plate 11 and the plurality of blades 12 may be referred to as a flow passage 11a of the impeller 10.
  • the bell mouth 26 rectifies the air sucked from the suction port 23b of the side wall 23 and flows it into the central portion of the impeller 10 through the impeller suction port 10a.
  • the bell mouth 26 is provided so as to project inward from the side wall 23. More specifically, the bell mouth 26 is formed so that the opening diameter gradually decreases from the side wall 23 of the scroll casing 20 toward the inside.
  • the peripheral wall 24 is composed of a curved wall surface in the rotation direction R of the impeller 10.
  • the peripheral wall 24 is between two side walls 23 facing each other in the scroll casing 20, as shown in FIG. 2, and connects a part of the outer peripheral edge of the two side walls 23 as shown in FIG. It is provided as follows.
  • the peripheral wall 24 has a curved inner peripheral surface 24c, and guides the airflow blown from the impeller 10 into the air passage 20a in the scroll portion 21 to the discharge port 22b along the inner peripheral surface 24c.
  • the peripheral wall 24 has a configuration in which a curved wall surface as shown in FIG. 1 extends parallel to the axial direction of the rotation axis RS of the impeller 10 as shown in FIG.
  • the peripheral wall 24 may be inclined with respect to the axial direction of the rotating shaft RS of the impeller 10, and is not limited to the form arranged in parallel with the axial direction of the rotating shaft RS.
  • the peripheral wall 24 covers the impeller 10 from the radial outside of the shaft portion 11b of the impeller 10, the inner peripheral surface 24c thereof, and the outer peripheral side of a plurality of blades 12 described later. Facing the end. That is, the inner peripheral surface 24c of the peripheral wall 24 faces the air blowing side of the blade 12 of the impeller 10.
  • the peripheral wall 24 has an impeller 10 from the winding start portion 24a located at the boundary with the tongue portion 25 to the winding end portion 24b located at the boundary between the discharge portion 22 and the scroll portion 21 on the side away from the tongue portion 25. It is provided along the rotation direction R.
  • the winding start portion 24a is an upstream end portion of the air flow generated by the rotation of the impeller 10 on the peripheral wall 24 composed of a curved wall surface
  • the winding end portion 24b is the end portion 24b of the impeller 10. It is the downstream end of the airflow generated by rotation.
  • the peripheral wall 24 is formed in a spiral shape. Examples of the spiral shape include a logarithmic spiral, an Archimedes spiral, a spiral shape based on an involute curve, and the like.
  • the discharge unit 22 forms a discharge port 22b that is generated by the rotation of the impeller 10 and discharges the airflow that has passed through the air passage 20a of the scroll unit 21.
  • the discharge unit 22 is composed of a hollow pipe having a rectangular cross section orthogonal to the flow direction of the discharged air.
  • the discharge unit 22 is composed of, for example, four plate-shaped side surfaces.
  • the discharge portion 22 has an extension plate 221 that smoothly connects to the winding end portion 24b of the peripheral wall 24, and a diffuser plate 222 that extends from the tongue portion 25 so as to face the extension plate 221.
  • the discharge portion 22 is a first side wall portion and a second side wall extending from each of the two side walls 23 so as to connect both ends of the rotary shaft RS in the axial direction in the extension plate 221 and the diffuser plate 222, respectively. It has a part (not shown).
  • the cross-sectional shape of the discharge unit 22 is not limited to a rectangle.
  • the discharge unit 22 forms a discharge side air passage 22a that guides the airflow discharged from the impeller 10 and flowing in the gap between the peripheral wall 24 and the impeller 10 to the outside of the scroll casing 20.
  • the tongue portion 25 is formed between the diffuser plate 222 of the discharge portion 22 and the winding start portion 24a of the peripheral wall 24.
  • the tongue portion 25 is formed with a predetermined radius of curvature, and the peripheral wall 24 is smoothly connected to the diffuser plate 222 via the tongue portion 25.
  • the tongue portion 25 suppresses the inflow of air from the end of winding to the beginning of winding in the spiral air passage 20a formed inside the scroll casing 20.
  • the tongue portion 25 has a flow of air in the air passage 20a from the upstream portion toward the rotation direction R of the impeller 10 and an air flow in the discharge direction from the downstream portion of the air passage 20a toward the discharge port 22b. It has a role of splitting.
  • the tongue portion 25 is configured to have a function of partitioning such a pressure difference.
  • FIG. 3 is a diagram schematically showing a configuration in which the impeller 10 of the multi-blade centrifugal blower 100 of FIG. 1 is viewed in parallel with the rotation axis RS.
  • the portion of the wing 12 covered by the side plate 13 is indicated by a broken line.
  • FIG. 4 is a cross-sectional view schematically showing a cross section taken along line BB of the impeller 10 of FIG.
  • the impeller 10 is a centrifugal impeller.
  • the impeller 10 is made of metal, for example, a plurality of steel plates and the like.
  • the impeller 10 is rotationally driven by a motor or the like (not shown), and the centrifugal force generated by the rotation forcibly sends out air in the centrifugal direction, that is, outward in the radial direction, and the impeller suction port provided on the side plate 13 side. It is configured to suck in air from 10a.
  • the impeller 10 is rotated in the rotation direction R by a motor or the like.
  • the thickness of the main plate 11 may be formed in a disk shape in which the wall thickness increases toward the center in the radial direction about the rotation axis RS, or the rotation axis. It may be formed to have a constant thickness in the radial direction centered on RS.
  • the main plate 11 may have a plate shape, and the shape of the main plate 11 may be a shape other than a circular shape, such as a polygonal shape.
  • a motor (not shown) is connected to a shaft portion 11b provided at the center of the main plate 11, and the main plate 11 is rotationally driven by the motor via the shaft portion 11b.
  • the plurality of blades 12 are arranged in the circumferential direction on the plate surface 111 of the main plate 11 with the rotation axis RS as the center so as to form a predetermined space between the adjacent blades 12.
  • the impeller 10 has a tubular shape due to a plurality of blades 12 arranged on the main plate 11.
  • the gap G formed between the adjacent blades 12 constitutes the flow passage 11a of the impeller 10.
  • Each of the plurality of radially provided blades 12 has a sirocco blade portion 30 composed of forward blades and a turbo blade portion 40 composed of rearward blades.
  • the turbo blade portion 40 is radially connected to the sirocco blade portion 30, and the blade 12 has a shape curved in the radial direction.
  • the turbo wing portion 40 is provided on the inner peripheral side of the sirocco wing portion 30 in succession with the sirocco wing portion 30. At the blade boundary 12b between the sirocco wing portion 30 and the turbo wing portion 40, the sirocco wing portion 30 and the turbo wing portion 40 are smoothly connected to each other.
  • the end face on the inner peripheral side of the wing 12 is the wing leading edge 12f
  • the end face on the outer peripheral side of the wing 12 is the wing trailing edge.
  • the edge is 12r.
  • the wing leading edge 12f may be referred to as the inner peripheral edge of the wing 12.
  • the turbo blade portion 40 is formed linearly from the blade boundary 12b to the blade leading edge 12f in the radial direction. As shown in FIG.
  • the blade front edge 12f is in the axial direction of the rotation axis RS so that the blade front edge 12f gradually approaches the rotation axis RS from the side plate 13 side to the main plate 11 side in the axial direction of the rotation axis RS. Is tilted against.
  • the blade trailing edge 12r and the blade boundary 12b are respectively made to be substantially parallel to the axis of rotation RS. The detailed configuration of each wing 12 will be described later.
  • each of the plurality of blades 12 is provided between the main plate 11 and the side plate 13 in the axial direction of the rotation axis RS.
  • one end of each blade 12 is connected to the main plate 11, and the other end of each blade 12 is connected to the side plate 13.
  • the other end of each blade 12 extends along the side plate 13 in the radial direction, and further extends inward from the inner peripheral end 13a of the side plate 13. That is, the portion on the inner peripheral side at the other end of each blade 12 is not connected to the side plate 13.
  • one end of the wing 12 connected to the main plate 11 in the axial direction of the rotary shaft RS is referred to as an end portion 12d on the main plate 11 side
  • the other end of the wing 12 on the side plate 13 side is referred to as the side plate 13 side. It may be referred to as an end portion 12u.
  • the portion connected to the end portion 12d on the main plate 11 side at the wing leading edge 12f of each wing 12 is referred to as the main plate side inner peripheral end 12fd
  • the portion connected to 12u is referred to as a side plate side inner peripheral end 12fu.
  • the first virtual circle C1 passing through the inner peripheral end 12fu on the side plate side of the plurality of blades 12 is represented by a alternate long and short dash line.
  • the first virtual circle C1 has a center on the virtual rotation axis RS of the main plate 11.
  • a part of the wing 12 extends from the main plate 11 side to the side plate 13 side and extends inward from the inner peripheral end 13a of the side plate 13.
  • the inner peripheral end 12fd on the main plate side not only the inner peripheral end 12fd on the main plate side but also the inner peripheral end 12fu on the side plate side (indicated by the first virtual circle C1) is the inner peripheral end 13a of the side plate 13.
  • the wing portion including the inner peripheral side portion of the end portion 12u of the wing 12 and the entire wing leading edge 12f is exposed through the inner peripheral end 13a of the side plate 13.
  • the side plate 13 maintains the positional relationship of the tips of the respective wings 12 and reinforces the plurality of wings 12.
  • side plates 13 and a plurality of blades 12 are provided on both sides of the main plate 11 in the axial direction of the rotating shaft RS.
  • the side plate 13 provided so as to face one plate surface 111 of the main plate 11 connects a plurality of blades 12 arranged on one plate surface 111 side of the main plate 11.
  • the side plate 13 provided so as to face the other plate surface 112 of the main plate 11 connects a plurality of blades 12 arranged on the other plate surface 112 side of the main plate 11.
  • the center of the suction port 23b and the center of the shaft portion 11b of the impeller 10 coincide with each other, and the side plate 13 of the impeller 10 and the suction port 23b are formed. It is arranged so as to face the formed side wall 23. In the radial direction, the inner peripheral end of the side wall 23, that is, the opening edge of the suction port 23b in the side wall 23, and the inner peripheral end 13a of the side plate 13 of the impeller 10 substantially coincide with each other. Therefore, in the impeller 10, the blade portion extending inward from the inner peripheral end 13a of the side plate 13 is exposed from the inner peripheral end of the side wall 23 of the scroll casing 20.
  • FIG. 5 is a diagram schematically showing the positional relationship between the bell mouth 26 of FIG. 2 and the impeller 10.
  • the inner peripheral end 13a of the side plate 13 is preferably located on the inner peripheral side of the outer peripheral end 26a of the tip of the bell mouth 26. With this configuration, the radial length of the side plate 13 is secured so that the plurality of blades 12 are sufficiently fixed by the side plate 13.
  • FIG. 6 is an enlarged partial perspective view of a part of the outer peripheral portion of the impeller 10 of FIG.
  • the side plate 13 side is defined as the upper side and the main plate 11 side is defined as the lower side in the axial direction of the rotary shaft RS, and the detailed configuration of the blade 12 will be described.
  • the blade boundary 12b of each blade 12 coincides with the inner peripheral end 13a of the side plate 13 in the radial direction, and the sirocco blade portion 30 of each blade 12 is on the side plate 13. It is covered, and the turbo blade portion 40 of each blade 12 is configured to be exposed from the inner peripheral end 13a of the side plate 13.
  • the distance Ld between the inner peripheral end 13a of the side plate 13 and the inner peripheral end 12fd on the main plate side at the wing leading edge 12f is the side plate side at the inner peripheral end 13a of the side plate 13 and the wing leading edge 12f.
  • the leading edge 12f of the wing is inclined so as to be longer than the distance Lu from the inner peripheral end 12fu. That is, the blade leading edge 12f is inclined from the main plate 11 side toward the side plate 13 side so that the inner diameter formed by the blade leading edges 12f of the plurality of blades 12 is gradually expanded.
  • the turbo wing portion 40 includes a first turbo wing portion 41 connected to the sirocco wing portion 30, and a second turbo wing portion 42 on the inner peripheral side of the first turbo wing portion 41.
  • the first turbo wing portion 41 includes the entire upper surface of the turbo wing portion 40, and has a rectangular shape such as a rectangular shape.
  • the second turbo blade portion 42 includes the entire blade leading edge 12f of the blade 12, and has a triangular shape. That is, the turbo wing portion 40 is formed so that the chord length of the turbo wing portion 40 increases from the side plate 13 side toward the main plate 11 side.
  • the position of the side plate side inner peripheral end 12fu of the blade leading edge 12f is located inside the inner peripheral end 13a of the side plate 13, and is formed by the first virtual circle C1.
  • the blade boundary 12b of the indicated blade 12 is located on the inner peripheral end 13a of the side plate 13. That is, in the example shown in FIG. 6, the entire turbo wing portion 40 including the first turbo wing portion 41 and the second turbo wing portion 42 is arranged inside the inner peripheral end 13a of the side plate 13 and is exposed. Will be done. On the other hand, the entire upper surface of the sirocco wing portion 30 is covered with the side plate 13.
  • the position of the blade boundary 12b of the blade 12 and the position of the inner peripheral end 13a of the side plate 13 do not necessarily have to coincide with each other. If at least a part of the first turbo wing portion 41 extends inward from the inner peripheral end 13a of the side plate 13 in the radial direction, the exposed portion of the turbo wing portion 40 causes the flow passage 11a to extend from the main plate 11 side. Air can be taken in from the side plate 13 side.
  • each wing 12 has a constant wall thickness W in the radial direction. Further, as shown in FIG. 6, each blade 12 has a constant wall thickness W from the main plate 11 side (see FIG. 3) to the side plate 13 side.
  • Each blade 12 can be made of a steel plate having a uniform thickness. That is, the wall thickness W of the blade 12 at the end portion 12u on the side plate 13 side is the same as the wall thickness W of the blade 12 at the end portion 12d (FIG. 6) on the main plate 11 side. Therefore, the gap G formed between the adjacent blades 12 gradually expands from the blade leading edge 12f toward the blade trailing edge 12r, and has the same size from the main plate 11 side to the side plate 13 side.
  • FIG. 1 when the impeller 10 is rotationally driven around the rotary shaft RS by a motor (not shown), the air outside the multi-blade centrifugal blower 100 is introduced to the suction port 23b of the scroll casing 20 and the impeller. It flows into the central portion of the impeller 10 in the axial direction through the suction port 10a. The air that has flowed into the central portion of the impeller 10 is taken into the flow passage 11a of the impeller 10 from the blade leading edge 12f by the rotation of the impeller 10, and flows outward in the flow passage 11a.
  • the portion of the wing 12 including the main plate 11 side and the side plate 13 side is exposed inward from the inner peripheral end of the side wall 23 and the inner peripheral end 13a of the side plate 13. Therefore, as compared with the configuration in which only the main plate 11 side of the blade 12 extends, the air flowing into the central portion of the impeller 10 can be taken into the flow passage 11a from the side plate 13 side of the blade leading edge 12f.
  • the suction air volume can be increased not only on the main plate 11 side but also on the side plate 13 side.
  • the inner peripheral end 13a of the side plate 13 is used.
  • the resistance on the side plate 13 side can be reduced, and the deterioration of noise can be suppressed.
  • the inflow loss of the airflow sucked from the impeller suction port 10a can be reduced and air can be attracted to the main plate 11 side as well.
  • the gap G formed between the adjacent blades 12 is on the main plate 11 side. It is constant from the side to the side plate 13 side. Therefore, the suction air volume can be increased also on the main plate 11 side of the impeller 10 as compared with the impeller which is made of a resin material and has a narrow gap G on the main plate 11 side as in the conventional case.
  • the turbo blade portion 40 is provided on the radial inside of the sirocco blade portion 30 in the blade 12, and the turbo blade portion 40 is exposed from the inner peripheral end 13a of the side plate 13. There is. Therefore, in the flow passage 11a formed by the turbo wing portion 40, which is inclined in the direction opposite to the rotation direction of the impeller and gradually expands toward the sirocco wing portion 30, the air taken in is efficiently boosted and the sirocco wing. It is sent to the unit 30.
  • the airflow that has been boosted and reached the wing boundary 12b with the sirocco wing portion 30 then flows toward the wing trailing edge 12r while changing the traveling direction along the sirocco wing portion 30 in the flow passage 11a. After that, the airflow reaching the trailing edge 12r of the blade is sent out from the flow passage 11a of the impeller 10 to the air passage 20a of the scroll casing 20.
  • the airflow sent from the impeller 10 to the air passage 20a is further boosted as it passes through the spiral air passage 20a expanding toward the discharge port 22b, and is blown out to the outer peripheral side through the discharge port 22b.
  • the multi-blade centrifugal blower 100 may be a single-suction type centrifugal blower.
  • the number of blades 12 is not limited to the number shown in the figure.
  • the multi-blade centrifugal blower 100 of the first embodiment includes an impeller 10 and a spiral scroll casing 20 in which the impeller 10 is housed.
  • the impeller 10 has a disk-shaped main plate 11, a plurality of blades 12 arranged in the circumferential direction on the peripheral edge of the main plate 11, and an annular shape arranged so as to face the main plate 11 and fixing the plurality of blades 12. It has a side plate 13.
  • the scroll casing 20 is configured to introduce air from the side plate 13 side and blow it out to the outer peripheral side.
  • the impeller 10 is made of metal, and the blade 12 has a constant wall thickness W from the main plate 11 side to the side plate 13 side. Further, the wing 12 extends from the main plate 11 side to the side plate 13 side and extends inward from the inner peripheral end 13a of the side plate 13.
  • the impeller 10 is made of metal, and the wall thickness W of the blade 12 is constant from the side plate 13 to the main plate 11 side. Therefore, the same gap G as the side plate 13 side is provided in the impeller 10. It can also be secured on the main plate 11 side. Therefore, the suction air volume can be increased even on the main plate 11 side of the impeller 10 as compared with the conventional multi-blade centrifugal blower made of a resin molded product.
  • the inner peripheral edge of the wing 12 (blade leading edge 12f) is inclined from the side plate 13 side toward the main plate 11 side.
  • the distance Ld between the inner peripheral end 13a of the side plate 13 and the inner peripheral end on the main plate 11 side (main plate side inner peripheral end 12fd) at the wing leading edge 12f is the side plate 13 side at the inner peripheral end 13a of the side plate 13 and the wing leading edge 12f. It is longer than the distance Lu from the inner peripheral end (inner peripheral end 12fu on the side plate side) of.
  • the blade front edge 12f has a radial distance between the main plate side inner peripheral end 12fd and the rotation axis RS of the impeller 10 (or a perpendicular line drawn from the inner peripheral end 13a of the side plate 13 to the main plate 11) on the side plate side. It is inclined so as to be longer than the radial distance between the inner peripheral end 12fu and the rotation axis RS of the impeller 10 (or the perpendicular line drawn from the inner peripheral end 13a of the side plate 13 to the main plate 11).
  • the resistance generated on the side plate 13 side of the blade portion exposed from the inner peripheral end 13a of the side plate 13 can be reduced, and the inflow loss of the air flowing in through the impeller suction port 10a and the generation of noise deterioration due to the resistance are suppressed. can do. Therefore, the air flowing in through the impeller suction port 10a can be attracted to the main plate 11 side as well, and it is possible to prevent the suction air volume from decreasing on the main plate 11 side with respect to the side plate 13 side.
  • the wing 12 has a sirocco wing portion 30 composed of forward-facing blades and a turbo wing portion 40 connected to the inner peripheral side of the sirocco wing portion 30 and composed of rear-facing blades.
  • the turbo blade portion 40 of the blade 12 is provided inside the inner peripheral end 13a of the side plate 13. As a result, the area of the exposed blade portion can be made larger, and more air flowing in through the impeller suction port 10a can be taken into the gap G between the blades 12. Further, in the flow passage 11a formed by the turbo blade portion 40, which is inclined in the direction opposite to the rotation direction R of the impeller 10 and gradually expands outward in the radial direction, the air taken in is boosted and highly efficient. Can be sent to the sirocco wing portion 30.
  • the scroll casing 20 includes an facing side wall 23 provided with a suction port 23a, a peripheral wall 24, and a bell mouth 26 forming the suction port 23a and gradually reducing the opening diameter toward the inside.
  • the inner peripheral end 13a of the side plate 13 is located on the inner peripheral side of the outer peripheral end 26a of the tip of the bell mouth 26.
  • FIG. 7 is a diagram schematically showing a configuration in which the blades of the multi-blade centrifugal blower according to the second embodiment are viewed in parallel with the axis of rotation.
  • the second embodiment when the blade 12 is viewed from the axial direction of the rotation shaft RS of the impeller 10, a part of the first turbo blade portion 41 is covered with the side plate 13, as in the case of the first embodiment. Is different.
  • the position of the inner peripheral end 13a of the side plate 13 with respect to the blade 12 installed on the plate surface 111 (see FIG. 3) of the main plate 11 is shown by a two-dot chain line.
  • the direction of the airflow passing near the negative pressure surface 122 of the blade 12 during the rotation of the impeller 10 is indicated by the arrow F1.
  • the first turbo wing portion 41 includes the entire upper surface of the turbo wing portion 40 and has a square shape
  • the second turbo wing portion 42 has a quadrangular shape.
  • All of the wing leading edges 12f of the wing 12 are included, and have a triangular shape.
  • the side plate side inner peripheral end 12fu of the blade leading edge 12f which is the boundary between the first turbo wing portion 41 and the second turbo wing portion 42, is inside the position of the inner peripheral end 13a of the side plate 13. It is located in the same as the case of the first embodiment.
  • the blade boundary 12b between the sirocco wing portion 30 and the first turbo wing portion 41 of the turbo wing portion 40 is located outside the position of the inner peripheral end 13a of the side plate 13, and the sirocco wing portion is located.
  • 30 and a part of the outer peripheral side of the first turbo blade portion 41 are covered with the side plate 13.
  • the portion of the blade 12 covered by the side plate 13 is composed of a sirocco blade portion 30 and a part on the outer peripheral side of the first turbo blade portion 41.
  • the portion of the turbo wing portion 40 exposed from the side plate 13 is intended to increase the amount of air sucked into the flow passage 11a, and the portion of the turbo wing portion 40 covered with the side plate 13 is sucked into the flow passage 11a.
  • the airflow can be boosted efficiently.
  • the ratio of the long L2 is preferably larger than 0% and 30% or less.
  • FIG. 8 is a diagram showing a modified example of the wing 12 of FIG.
  • the ratio of the chord length L2 of the portion of the first turbo blade portion 41 covered by the side plate 13 to the chord length L1 of the portion of the blade 12 covered by the side plate 13 is 30. It is larger than% and is 40%.
  • the ratio of the chord length L2 to the chord length L1 is made larger than 30% as in the modified example, if the chord length of the wing 12 is constant, the chord length of the sirocco wing portion 30 is shortened and the turbo wing portion is used. It is necessary to make the 40 more inclined in the rotation direction R.
  • a peeling vortex Fa may be generated on the negative pressure surface 122 side of the sirocco wing portion 30, which may cause a decrease in air volume due to the airflow separating from the negative pressure surface 122 and an increase in noise due to the generation of the peeling vortex Fa.
  • the wing 12 has a sirocco wing portion 30 composed of forward blades and a turbo wing portion 40 connected to the inner peripheral side of the sirocco wing portion 30 and composed of rearward blades.
  • the portion of the blade 12 covered with the side plate 13 is composed of a sirocco blade portion 30 and a part of the turbo blade portion 40.
  • the chord length of the sirocco wing portion 30, that is, the difference between the chord length L1 and the chord length L2 is longer than that of a part of the chord length L2 of the turbo wing portion 40.
  • the ratio of the chord length L2 of the portion of the turbo wing portion 40 covered by the side plate 13 (a part of the turbo wing portion 40 described above) to the chord length L1 of the portion of the wing 12 covered by the side plate 13. Is greater than 0% and less than or equal to 30%.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
PCT/JP2020/039898 2020-10-23 2020-10-23 多翼遠心送風機 Ceased WO2022085175A1 (ja)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US18/043,917 US12241477B2 (en) 2020-10-23 2020-10-23 Multi-blade centrifugal air-sending device
CN202080106321.3A CN116348680A (zh) 2020-10-23 2020-10-23 多翼离心送风机
EP20958725.2A EP4234946A4 (en) 2020-10-23 2020-10-23 MULTIPLE BLADE CENTRIFUGAL FLOWER
JP2022556346A JP7466683B2 (ja) 2020-10-23 2020-10-23 多翼遠心送風機
PCT/JP2020/039898 WO2022085175A1 (ja) 2020-10-23 2020-10-23 多翼遠心送風機
TW110108114A TWI747758B (zh) 2020-10-23 2021-03-08 多葉離心式送風機

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2020/039898 WO2022085175A1 (ja) 2020-10-23 2020-10-23 多翼遠心送風機

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WO2022085175A1 true WO2022085175A1 (ja) 2022-04-28

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PCT/JP2020/039898 Ceased WO2022085175A1 (ja) 2020-10-23 2020-10-23 多翼遠心送風機

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US (1) US12241477B2 (https=)
EP (1) EP4234946A4 (https=)
JP (1) JP7466683B2 (https=)
CN (1) CN116348680A (https=)
TW (1) TWI747758B (https=)
WO (1) WO2022085175A1 (https=)

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WO2024038573A1 (ja) * 2022-08-19 2024-02-22 三菱電機株式会社 送風機用ファン、多翼遠心送風機、及び、空調室内機

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WO2024038573A1 (ja) * 2022-08-19 2024-02-22 三菱電機株式会社 送風機用ファン、多翼遠心送風機、及び、空調室内機

Also Published As

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JP7466683B2 (ja) 2024-04-12
EP4234946A1 (en) 2023-08-30
JPWO2022085175A1 (https=) 2022-04-28
CN116348680A (zh) 2023-06-27
EP4234946A4 (en) 2023-12-20
US12241477B2 (en) 2025-03-04
TW202217151A (zh) 2022-05-01
US20240026899A1 (en) 2024-01-25
TWI747758B (zh) 2021-11-21

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