WO2019082378A1 - Multivane blower - Google Patents

Multivane blower

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Publication number
WO2019082378A1
WO2019082378A1 PCT/JP2017/038914 JP2017038914W WO2019082378A1 WO 2019082378 A1 WO2019082378 A1 WO 2019082378A1 JP 2017038914 W JP2017038914 W JP 2017038914W WO 2019082378 A1 WO2019082378 A1 WO 2019082378A1
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WO
WIPO (PCT)
Prior art keywords
wings
wing
cross
section
rotation axis
Prior art date
Application number
PCT/JP2017/038914
Other languages
French (fr)
Japanese (ja)
Inventor
加藤　康明
拓矢 寺本
亮 堀江
Original Assignee
三菱電機株式会社
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 三菱電機株式会社 filed Critical 三菱電機株式会社
Priority to PCT/JP2017/038914 priority Critical patent/WO2019082378A1/en
Priority to JP2019549964A priority patent/JP6896091B2/en
Publication of WO2019082378A1 publication Critical patent/WO2019082378A1/en

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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
    • F04D29/26—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

Definitions

  • the present invention relates to a multi-blade fan provided with an impeller.
  • Patent Document 1 describes an impeller of a centrifugal fan.
  • the blade of this impeller has a turbofan shape that is convex on the pressure surface side on the inner peripheral side of the impeller, and has a sirocco fan shape that is concave on the pressure surface side on the outer peripheral side of the impeller There is.
  • the present invention has been made to solve the problems as described above, and it is an object of the present invention to provide a multi-blade fan capable of improving the efficiency.
  • the multi-blade fan according to the present invention is a multi-blade fan including an impeller that rotates around a rotation axis, and the impeller includes a plurality of blades arranged in a circumferential direction around the rotation axis, And a plurality of main plates for supporting the plurality of blades from one side in a direction along the rotation axis, wherein the plurality of blades are cut at a first plane cut at a first plane perpendicular to the rotation axis.
  • Each of the wings has an inner peripheral end and an outer peripheral end provided on the outer peripheral side than the inner peripheral end and inclined forward in the rotational direction of the impeller, and the plurality of wings Has a plurality of first wings and a plurality of second wings, and in the first cross section, each of the plurality of first wings is greater than the wing length of each of the plurality of second wings. Also has a long wing length, and in the first cross section, each of the rotation axis and the plurality of first wings The distance between the rotary shaft and the inner peripheral end of each of the plurality of second wings is shorter than the distance between the inner peripheral end of each of the plurality of second wings in the circumferential direction. At least one second wing of the plurality of second wings is disposed between two adjacent first wings.
  • At least one second wing whose wing length is shorter than the first wing is disposed between the two first wings adjacent to each other in the circumferential direction. It is possible to prevent the inlet portion of the air flow passage formed in from becoming narrow. Therefore, since the contraction flow at the inlet of the air flow path between the blades can be alleviated, the efficiency of the multi-blade fan can be improved.
  • FIG. 5 is a cross-sectional view showing a VV cross section of FIG. 2; It is a figure explaining the shape of the 1st wing 12A in the 1st section in the multi-blade fan concerning Embodiment 1 of the present invention.
  • FIG. 1 is an external view schematically showing a configuration in which the multi-blade fan according to the present embodiment is viewed along a rotating shaft 11.
  • FIG. 2 is a view schematically showing the II-II cross section of FIG.
  • the multi-blade fan includes an impeller 10 rotating around a rotating shaft 11, a casing 30 accommodating the impeller 10, and a drive motor 40 driving the impeller 10.
  • the multi-blade fan includes an impeller 10 rotating around a rotating shaft 11, a casing 30 accommodating the impeller 10, and a drive motor 40 driving the impeller 10.
  • a drive motor 40 driving the impeller 10.
  • the casing 30 has a scroll wall 31, an inlet 32, and an outlet 33.
  • the scroll wall 31 has a scroll shape such that an enlarged air passage is formed in a cross section perpendicular to the rotation axis 11.
  • the suction port 32 is an opening formed by a bell-mouth-like annular portion centered on the rotation shaft 11.
  • the suction port 32 is formed on one side surface of the casing 30.
  • the blowout port 33 is an opening formed in a tangential direction of the scroll wall 31 in a cross section perpendicular to the rotation axis 11.
  • the drive motor 40 is disposed adjacent to the side surface of the casing 30 opposite to the side surface on which the suction port 32 is formed.
  • the motor shaft 41 of the drive motor 40 extends on the rotary shaft 11 and is inserted into the inside of the casing 30 through the side of the casing 30.
  • the impeller 10 has a plurality of wings 12 arranged in the circumferential direction around the rotation axis 11 and a main plate 13 supporting the plurality of wings 12 from one side in the direction along the rotation axis 11.
  • the main plate 13 is disposed to be perpendicular to the rotation shaft 11 along the side surface of the casing 30 on the drive motor 40 side.
  • a motor shaft 41 inserted into the inside of the casing 30 is fixed to the central portion of the main plate 13.
  • the plurality of wings 12 rotate around the rotation shaft 11 via the motor shaft 41 and the main plate 13.
  • external air is sucked into the interior of the impeller 10 from the suction port 32 and blown out into the casing 30 by the pressurizing action of the impeller 10.
  • the air blown out into the casing 30 is decelerated in the enlarged air path formed by the scroll wall 31 to recover the static pressure, and blown out from the blowout port 33 to the outside.
  • FIG. 3 is a perspective view showing the configuration of the impeller 10 of the multi-blade fan according to the present embodiment.
  • FIG. 4 is a cross-sectional view showing a IV-IV cross section of FIG.
  • the cross section shown in FIG. 4 is a first cross section of the impeller 10 in which a portion near the main plate 13 of the impeller 10 is cut at a first plane 51 perpendicular to the rotation shaft 11.
  • FIG. 5 is a cross-sectional view showing a VV cross section of FIG.
  • the cross section shown in FIG. 5 is a second cross section of the impeller 10 in which a portion closer to the suction port 32 of the impeller 10 is cut at a second plane 52 perpendicular to the rotation axis 11.
  • the plurality of wings 12 have a plurality of first wings 12A and a plurality of second wings 12B.
  • the first wing 12A has an inner peripheral end 14A and an outer peripheral end 15A provided on the outer peripheral side of the inner peripheral end 14A and inclined forward in the rotation direction of the impeller 10.
  • the inner peripheral end 14A is a front edge of the first wing 12A
  • the outer peripheral end 15A is a rear edge of the first wing 12A.
  • the second wing 12B has an inner peripheral end 14B and an outer peripheral end 15B provided on the outer peripheral side of the inner peripheral end 14B and inclined forward in the rotational direction of the impeller 10.
  • the inner peripheral end 14B is the front edge of the second wing 12B
  • the outer peripheral end 15B is the rear edge of the second wing 12B.
  • the wing length of the first wing 12A is equal to the wing length of the second wing 12B at a portion closer to the suction port 32 in the direction along the rotation axis 11 (see FIG. 5).
  • the wing length of the first wing 12A is longer than the wing length of the second wing 12B (see FIG. 4). It is getting longer.
  • the wing length of the first wing 12A is longer than the wing length of the second wing 12B in at least a part of the direction along the rotation axis 11.
  • the distance between the rotation axis 11 and the inner peripheral end 14A of the first wing 12A, that is, the inner diameter of the first wing 12A is ri_Ab.
  • the distance between the rotation shaft 11 and the outer peripheral end 15A, that is, the outer diameter of the first wing 12A is ro_Ab.
  • the blade length of the blade in a cross section perpendicular to the rotation axis is shorter than the width dimension of the blade in the rotation axis direction.
  • the maximum wing length of the first wing 12A that is, the wing length at the end near the main plate 13 of the first wing 12A is the width dimension W of the first wing 12A in the rotational axis direction (see FIG. 2) It is shorter than that.
  • the distance between the rotation axis 11 and the inner peripheral end 14B of the second wing 12B, that is, the inner diameter of the second wing 12B is ri_Bb larger than the distance ri_Ab (ri_Bb> ri_Ab).
  • the wing length L2b of the second wing 12B in the first cross section is shorter than the wing length L1 b of the first wing 12A in the same cross section (L2 b ⁇ L1 b).
  • the exit angle of the first wing 12A in the first cross section is ⁇ bo_Ab.
  • the exit angle of the second wing 12B in the same cross section is ⁇ bo_Bb.
  • the distance between the rotation shaft 11 and the inner peripheral end 14A of the first wing 12A is ri_Ai.
  • the distance ri_Ai is longer than the distance ri_Ab between the rotation axis 11 and the inner peripheral end 14A of the first wing 12A in the first cross section (ri_Ai> ri_Ab).
  • the distance between the rotation axis 11 and the outer peripheral end 15A of the first wing 12A is ro_Ai.
  • the distance between the rotation axis 11 and the inner peripheral end 14B of the second wing 12B is ri_Bi.
  • the distance between the rotation shaft 11 and the outer peripheral end 15B of the second wing 12B is ro_Bi.
  • the outlet angle of the first wing 12A and the outlet angle of the second wing 12B are equal to each other also in the second cross section.
  • At least one second wing 12B is disposed between two first wings 12A adjacent to each other in the circumferential direction. For this reason, the number of second wings 12B is equal to or greater than the number of first wings 12A. In the present embodiment, since two second wings 12B are disposed between two first wings 12A, the number of second wings 12B is twice the number of first wings 12A. .
  • the first wing 12A in the second cross section shown in FIG. 5 does not protrude from the contour of the first wing 12A in the first cross section shown in FIG. And overlap. Therefore, the relationships of ro_Ai ⁇ ro_Ab, ri_Ai ⁇ ri_Ab, and L1i ⁇ L1b are satisfied.
  • the second wing 12B in the second cross section shown in FIG. 5 does not protrude from the contour of the second wing 12B in the first cross section shown in FIG. It overlaps with 2 wings 12B. Therefore, the relationships of ro_Bi ⁇ ro_Bb, ri_Bi_ri_Bb, and L2i ⁇ L2b are satisfied.
  • FIG. 6 is a view for explaining the shape of the first wing 12A in the first cross section in the multi-blade fan according to the present embodiment.
  • the first wing 12A in the first cross section has an outer circumferential wing portion 12A1 located on the outer circumferential side of a circle C1 contacting the inner circumferential end 14B of the second wing 12B with the rotation axis 11 as a center; And an inner peripheral wing portion 12A2 positioned on the inner peripheral side of the circle C1.
  • the length of the chord line 20 of the outer circumferential wing 12A1 is the chord length L_Ab1 of the outer wing 12A1, and the maximum distance between the chord 20 and the warp line 22 of the outer wing 12A1 is the warpage height d_Ab1 of the outer wing 12A1.
  • the warpage height in the reverse direction of the rotation direction of the impeller 10 is represented by a positive value
  • the warpage height in the rotation direction of the impeller 10 is represented by a negative value. Since the outer peripheral side wing 12A1 is warped in the direction opposite to the rotation direction of the impeller 10, the warpage height d_Ab1 takes a positive value (d_Ab1> 0).
  • the ratio (d_Ab1 / L_Ab1) of the warpage height d_Ab1 to the chord length L_Ab1 is taken as the warpage ratio of the outer peripheral wing 12A1.
  • the length of the chord 21 of the inner wing 12A2 is the chord length L_Ab2 of the inner wing 12A2, and the maximum distance between the chord 21 and the warp line 23 of the inner wing 12A2 is the inner wing 12A2.
  • the warp height is d_Ab2.
  • the warpage height d_Ab2 takes a negative value (d_Ab2 ⁇ 0).
  • the inner peripheral side wing portion 12A2 may be curved in the reverse direction of the rotation direction of the impeller 10.
  • the ratio (d_Ab2 / L_Ab2) of the warpage height d_Ab2 to the chord length L_Ab2 is taken as the warpage ratio of the inner peripheral side wing portion 12A2.
  • the warpage ratio (d_Ab1 / L_Ab1) of the outer peripheral side wing 12A1 is larger than the warpage ratio (d_Ab2 / L_Ab2) of the inner peripheral side wing 12A2 (d_Ab1 / L_Ab1> d_Ab2 / L_Ab2).
  • the multi-blade fan according to the present embodiment is a multi-blade fan provided with the impeller 10 rotating around the rotation shaft 11.
  • the impeller 10 has a plurality of wings 12 arranged in the circumferential direction around the rotation axis 11 and a main plate 13 supporting the plurality of wings 12 from one side in the direction along the rotation axis 11.
  • a first cross section for example, the cross section shown in FIG.
  • each of the plurality of wings 12 has an inner peripheral end (for example, an inner peripheral end 14A) Or the inner peripheral end 14B) and the outer peripheral end (for example, the outer peripheral end 15A or the outer peripheral end 15B) provided on the outer peripheral side than the inner peripheral end and inclined forward in the rotational direction of the impeller 10 ing.
  • the plurality of wings 12 includes a plurality of first wings 12A and a plurality of second wings 12B. In the first cross section, each of the plurality of first wings 12A has a wing length L1b longer than the wing length L2b of each of the plurality of second wings 12B.
  • the distance ri_Ab between the rotary shaft 11 and the respective inner peripheral ends 14A of the plurality of first wings 12A is the distance ri_Bb between the rotary shaft 11 and the respective inner peripheral ends 14B of the plurality of second wings 12B. It is shorter than that.
  • At least one second wing 12B of the plurality of second wings 12B is disposed between the two first wings 12A adjacent to each other in the circumferential direction among the plurality of first wings 12A.
  • the blade length L1b of the first blade 12A is longer than the blade length L2b of the second blade 12B, it is possible to enhance the pressure boosting action by the centrifugal force at least in the first blade 12A.
  • at least one second wing 12B shorter in wing length than the first wing 12A is disposed between two first wings 12A adjacent to each other in the circumferential direction.
  • each of the plurality of first wings 12A is in contact with the inner peripheral end 14B of each of the plurality of second wings 12B around the rotation axis 11. It has an outer peripheral side wing portion 12A1 located on the outer peripheral side than the circle C1, and an inner peripheral side wing portion 12A2 located on the inner peripheral side of the circle C1.
  • the ratio of the warpage height to the chord length is taken as a warpage ratio, and the warpage height in the reverse direction of the rotation direction is represented by a positive value.
  • the warp height is expressed as a negative value.
  • the warpage ratio (d_Ab1 / L_Ab1) of the outer peripheral side wing portion 12A1 is larger than the warpage ratio (d_Ab2 / L_Ab2) of the inner peripheral side wing portion 12A2.
  • the difference in angle between the air flow direction and the wing surface of the first wing 12A can be reduced.
  • separation in the air flow path between the blades can be suppressed, so the efficiency of the multi-blade fan can be further improved.
  • a plane which is a plane perpendicular to the rotation axis 11 and whose distance from the main plate 13 is longer than the distance between the first plane and the main plate 13 is taken as a second plane 52.
  • the distance ri_Ab between the rotation axis 11 and the inner peripheral end 14A of each of the plurality of first wings 12A in one cross section is longer.
  • the inner diameter of the first wing 12A centered on the rotation shaft 11 is larger on the suction port 32 side of the impeller 10 than on the main plate 13 side of the impeller 10. Therefore, on the suction port 32 side of the impeller 10, the flow passage cross-sectional area of the air flowing into the impeller 10 from the suction port 32 and flowing along the rotation shaft 11 can be increased. As a result, the velocity component of the air flowing into the impeller 10 can be reduced in the direction of the rotation shaft 11, so that the loss when the flow of air flowing into the impeller 10 is bent in the radial direction of the impeller 10 Can be reduced. Therefore, the efficiency of the multi-blade fan can be further improved.
  • each of the plurality of wings 12 in the second cross section is derived from the contour of each of the plurality of wings 12 in the first cross section. It overlaps with each of the plurality of wings 12 in the first cross section so as not to go out.
  • the main plate 13 and the plurality of wings 12 can be integrally formed using a simple mold that opens in the direction of the rotation shaft 11. Therefore, the manufacturing cost of the multi-blade fan can be reduced.
  • the distance ro_Ab between the outer peripheral end 15A of each of the plurality of first wings 12A and the rotation shaft 11 is the same as each of the plurality of second wings 12B. It is equal to the distance ro_Bb between the outer peripheral end 15B and the rotation shaft 11.
  • the outlet angle ⁇ bo_Ab of each of the plurality of first wings 12A is equal to the outlet angle ⁇ bo_Bb of each of the plurality of second wings 12B.
  • the direction of the air flow flowing out of the impeller 10 can be made uniform regardless of the circumferential position of the impeller 10. If the direction of the air flow flowing out of the impeller 10 changes depending on the circumferential position of the impeller 10, noise such as rotational noise is generated. Therefore, according to the above configuration, noise such as rotational noise can be suppressed.
  • the multi-blade fan provided with the single-suction type impeller 10 in which the plurality of wings 12 is formed only on one side of the main plate 13 has been described as an example.
  • the present invention is also applicable to a multi-blade fan provided with a double-suction type impeller in which a plurality of blades are formed respectively.
  • SYMBOLS 10 impeller 11 rotating shaft, 12 wings, 12A 1st wing, 12A1 outer peripheral side wing part, 12A 2 inner peripheral side wing part, 12B 2nd wing, 13 main plate, 14A, 14B inner peripheral end, 15A, 15B outer peripheral end, 20, 21 chords, 22 and 23 warp lines, 30 casings, 31 scroll walls, 32 suction ports, 33 outlets, 40 drive motors, 41 motor shafts, 51 first plane, 52 second plane, C1 circle.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

This multivane blower is provided with an impeller. The impeller includes: a plurality of vanes arranged circumferentially; and a main plate which supports the plurality of vanes. In a first cross-section of the impeller, each of the plurality of vanes has an inner circumferential edge and an outer circumferential edge. The plurality of vanes include a plurality of first vanes and a plurality of second vanes. In the first cross-section, the plurality of first vanes each have a vane length greater than the plurality of second vanes. In the first cross-section, the distance between the rotating shaft and the inner circumferential edge of each of the plurality of first vanes is less than the distance between the rotating shaft and the inner circumferential edge of each of the plurality of second vanes. Among the plurality of second vanes, at least one second vane is disposed between two of the first vanes, which are circumferentially adjacent to each other.

Description

多翼送風機Multi-blade fan
　本発明は、羽根車を備えた多翼送風機に関するものである。 The present invention relates to a multi-blade fan provided with an impeller.
　特許文献１には、遠心ファンの羽根車が記載されている。この羽根車の翼は、羽根車の内周側では圧力面側に凸となるターボファン形状を有しており、羽根車の外周側では圧力面側に凹となるシロッコファン形状を有している。 Patent Document 1 describes an impeller of a centrifugal fan. The blade of this impeller has a turbofan shape that is convex on the pressure surface side on the inner peripheral side of the impeller, and has a sirocco fan shape that is concave on the pressure surface side on the outer peripheral side of the impeller There is.
特開２００５－６９１８３号公報JP, 2005-69183, A
　特許文献１に記載されているような羽根車において、空気の流れが翼から大きく剥離しないようにするためには、翼の前縁となる内周端から翼の後縁となる外周端にかけて、翼の反りの曲率半径が小さくならないようにする必要がある。翼の反りの曲率半径を大きく確保すると翼長が長くなるため、羽根車の外径を維持する場合には翼の内周端を回転軸に近づける必要がある。翼の内周端が回転軸に近づけられると、翼の内周端の占める面積比率が増大することにより、翼間の空気流路の入口部が狭まってしまう。したがって、回転軸方向に流通する空気が翼間の空気流路に流入する際、翼間の空気流路の入口部での縮流が過大となるため、ファンの効率が低下してしまうという課題があった。 In the impeller as described in Patent Document 1, in order to prevent the flow of air from being greatly separated from the wing, from the inner circumferential end serving as the leading edge of the wing to the outer circumferential end serving as the trailing edge of the wing, It is necessary to make the radius of curvature of the wing warpage not be small. When the curvature radius of the wing is secured large, the wing length becomes long. Therefore, when maintaining the outer diameter of the impeller, it is necessary to bring the inner peripheral end of the wing close to the rotation axis. When the inner peripheral end of the wing is brought close to the rotation axis, the area ratio occupied by the inner peripheral end of the wing increases, and the inlet of the air flow path between the wings is narrowed. Therefore, when air flowing in the rotational axis direction flows into the air flow path between the blades, the contraction flow at the inlet of the air flow path between the blades becomes excessive, and the efficiency of the fan decreases. was there.
　本発明は、上述のような課題を解決するためになされたものであり、効率を向上できる多翼送風機を提供することを目的とする。 The present invention has been made to solve the problems as described above, and it is an object of the present invention to provide a multi-blade fan capable of improving the efficiency.
　本発明に係る多翼送風機は、回転軸を中心として回転する羽根車を備えた多翼送風機であって、前記羽根車は、前記回転軸を中心とする周方向に配列した複数の翼と、前記複数の翼を前記回転軸に沿う方向の一方側から支持する主板と、を有しており、前記回転軸に垂直な第１平面で切断された前記羽根車の第１断面において、前記複数の翼のそれぞれは、内周端と、前記内周端よりも外周側に設けられ、前記羽根車の回転方向で前方に向かって傾斜した外周端と、を有しており、前記複数の翼は、複数の第１翼と、複数の第２翼と、を有しており、前記第１断面において、前記複数の第１翼のそれぞれは、前記複数の第２翼のそれぞれの翼長よりも長い翼長を有しており、前記第１断面において、前記回転軸と前記複数の第１翼のそれぞれの前記内周端との距離は、前記回転軸と前記複数の第２翼のそれぞれの前記内周端との距離よりも短くなっており、前記複数の第１翼のうち前記周方向で互いに隣り合う２つの第１翼の間には、前記複数の第２翼のうちの少なくとも１つの第２翼が配置されているものである。 The multi-blade fan according to the present invention is a multi-blade fan including an impeller that rotates around a rotation axis, and the impeller includes a plurality of blades arranged in a circumferential direction around the rotation axis, And a plurality of main plates for supporting the plurality of blades from one side in a direction along the rotation axis, wherein the plurality of blades are cut at a first plane cut at a first plane perpendicular to the rotation axis. Each of the wings has an inner peripheral end and an outer peripheral end provided on the outer peripheral side than the inner peripheral end and inclined forward in the rotational direction of the impeller, and the plurality of wings Has a plurality of first wings and a plurality of second wings, and in the first cross section, each of the plurality of first wings is greater than the wing length of each of the plurality of second wings. Also has a long wing length, and in the first cross section, each of the rotation axis and the plurality of first wings The distance between the rotary shaft and the inner peripheral end of each of the plurality of second wings is shorter than the distance between the inner peripheral end of each of the plurality of second wings in the circumferential direction. At least one second wing of the plurality of second wings is disposed between two adjacent first wings.
　本発明によれば、周方向で互いに隣り合う２つの第１翼の間には、第１翼よりも翼長の短い少なくとも１つの第２翼が配置されるため、２つの第１翼の間に形成される空気流路の入口部が狭くなるのを防ぐことができる。したがって、翼間の空気流路の入口部での縮流を緩和することができるため、多翼送風機の効率を向上させることができる。 According to the present invention, at least one second wing whose wing length is shorter than the first wing is disposed between the two first wings adjacent to each other in the circumferential direction. It is possible to prevent the inlet portion of the air flow passage formed in from becoming narrow. Therefore, since the contraction flow at the inlet of the air flow path between the blades can be alleviated, the efficiency of the multi-blade fan can be improved.
本発明の実施の形態１に係る多翼送風機を回転軸１１に沿って見た構成を模式的に示す外観図である。It is an external view which shows typically the structure which looked at the multiblade fan which concerns on Embodiment 1 of this invention along the rotating shaft 11. FIG. 図１のＩＩ－ＩＩ断面を模式的に示す図である。It is a figure which shows typically the II-II cross section of FIG. 本発明の実施の形態１に係る多翼送風機の羽根車１０の構成を示す斜視図である。BRIEF DESCRIPTION OF THE DRAWINGS It is a perspective view which shows the structure of the impeller 10 of the multi-blade fan which concerns on Embodiment 1 of this invention. 図２のＩＶ－ＩＶ断面を示す断面図である。It is sectional drawing which shows the IV-IV cross section of FIG. 図２のＶ－Ｖ断面を示す断面図である。FIG. 5 is a cross-sectional view showing a VV cross section of FIG. 2; 本発明の実施の形態１に係る多翼送風機において第１断面での第１翼１２Ａの形状を説明する図である。It is a figure explaining the shape of the 1st wing 12A in the 1st section in the multi-blade fan concerning Embodiment 1 of the present invention.
実施の形態１．
　本発明の実施の形態１に係る多翼送風機について説明する。図１は、本実施の形態に係る多翼送風機を回転軸１１に沿って見た構成を模式的に示す外観図である。図２は、図１のＩＩ－ＩＩ断面を模式的に示す図である。図１及び図２に示すように、多翼送風機は、回転軸１１を中心として回転する羽根車１０と、羽根車１０を収容するケーシング３０と、羽根車１０を駆動する駆動モータ４０と、を有している。 Embodiment 1
A multi-blade fan according to Embodiment 1 of the present invention will be described. FIG. 1 is an external view schematically showing a configuration in which the multi-blade fan according to the present embodiment is viewed along a rotating shaft 11. FIG. 2 is a view schematically showing the II-II cross section of FIG. As shown in FIG. 1 and FIG. 2, the multi-blade fan includes an impeller 10 rotating around a rotating shaft 11, a casing 30 accommodating the impeller 10, and a drive motor 40 driving the impeller 10. Have.
　ケーシング３０は、スクロール壁３１と、吸込口３２と、吹出口３３と、を有している。スクロール壁３１は、回転軸１１に垂直な断面において拡大風路が形成されるようなスクロール形状を有している。吸込口３２は、回転軸１１を中心としたベルマウス状の環状部により形成された開口である。吸込口３２は、ケーシング３０の一方の側面に形成されている。吹出口３３は、回転軸１１に垂直な断面においてスクロール壁３１の接線方向を向いて形成された開口である。 The casing 30 has a scroll wall 31, an inlet 32, and an outlet 33. The scroll wall 31 has a scroll shape such that an enlarged air passage is formed in a cross section perpendicular to the rotation axis 11. The suction port 32 is an opening formed by a bell-mouth-like annular portion centered on the rotation shaft 11. The suction port 32 is formed on one side surface of the casing 30. The blowout port 33 is an opening formed in a tangential direction of the scroll wall 31 in a cross section perpendicular to the rotation axis 11.
　駆動モータ４０は、吸込口３２の形成された側面とは反対側のケーシング３０の側面に隣接して配置されている。駆動モータ４０のモータシャフト４１は、回転軸１１上に延びており、ケーシング３０の側面を貫通してケーシング３０の内部に挿入されている。 The drive motor 40 is disposed adjacent to the side surface of the casing 30 opposite to the side surface on which the suction port 32 is formed. The motor shaft 41 of the drive motor 40 extends on the rotary shaft 11 and is inserted into the inside of the casing 30 through the side of the casing 30.
　羽根車１０は、回転軸１１を中心とする周方向に配列した複数の翼１２と、複数の翼１２を回転軸１１に沿う方向の一方側から支持する主板１３と、を有している。主板１３は、駆動モータ４０側のケーシング３０の側面に沿って、回転軸１１に垂直となるように配置されている。主板１３の中心部には、ケーシング３０の内部に挿入されたモータシャフト４１が固定されている。 The impeller 10 has a plurality of wings 12 arranged in the circumferential direction around the rotation axis 11 and a main plate 13 supporting the plurality of wings 12 from one side in the direction along the rotation axis 11. The main plate 13 is disposed to be perpendicular to the rotation shaft 11 along the side surface of the casing 30 on the drive motor 40 side. A motor shaft 41 inserted into the inside of the casing 30 is fixed to the central portion of the main plate 13.
　駆動モータ４０が運転されると、モータシャフト４１及び主板１３を介して、複数の翼１２が回転軸１１を中心として回転する。これにより、外部の空気が吸込口３２から羽根車１０の内部に吸い込まれ、羽根車１０の昇圧作用によりケーシング３０内に吹き出される。ケーシング３０内に吹き出された空気は、スクロール壁３１により形成される拡大風路で減速して静圧を回復し、吹出口３３から外部に吹き出される。 When the drive motor 40 is operated, the plurality of wings 12 rotate around the rotation shaft 11 via the motor shaft 41 and the main plate 13. As a result, external air is sucked into the interior of the impeller 10 from the suction port 32 and blown out into the casing 30 by the pressurizing action of the impeller 10. The air blown out into the casing 30 is decelerated in the enlarged air path formed by the scroll wall 31 to recover the static pressure, and blown out from the blowout port 33 to the outside.
　図３は、本実施の形態に係る多翼送風機の羽根車１０の構成を示す斜視図である。図４は、図２のＩＶ－ＩＶ断面を示す断面図である。図４に示す断面は、回転軸１１に垂直な第１平面５１で羽根車１０の主板１３寄りの部分が切断された、羽根車１０の第１断面である。図５は、図２のＶ－Ｖ断面を示す断面図である。図５に示す断面は、回転軸１１に垂直な第２平面５２で羽根車１０の吸込口３２寄りの部分が切断された、羽根車１０の第２断面である。 FIG. 3 is a perspective view showing the configuration of the impeller 10 of the multi-blade fan according to the present embodiment. FIG. 4 is a cross-sectional view showing a IV-IV cross section of FIG. The cross section shown in FIG. 4 is a first cross section of the impeller 10 in which a portion near the main plate 13 of the impeller 10 is cut at a first plane 51 perpendicular to the rotation shaft 11. FIG. 5 is a cross-sectional view showing a VV cross section of FIG. The cross section shown in FIG. 5 is a second cross section of the impeller 10 in which a portion closer to the suction port 32 of the impeller 10 is cut at a second plane 52 perpendicular to the rotation axis 11.
　図３～図５に示すように、複数の翼１２は、複数の第１翼１２Ａと、複数の第２翼１２Ｂと、を有している。第１翼１２Ａは、内周端１４Ａと、内周端１４Ａよりも外周側に設けられ、羽根車１０の回転方向で前方に向かって傾斜した外周端１５Ａと、を有している。内周端１４Ａは第１翼１２Ａの前縁となり、外周端１５Ａは第１翼１２Ａの後縁となる。第２翼１２Ｂは、内周端１４Ｂと、内周端１４Ｂよりも外周側に設けられ、羽根車１０の回転方向で前方に向かって傾斜した外周端１５Ｂと、を有している。内周端１４Ｂは第２翼１２Ｂの前縁となり、外周端１５Ｂは第２翼１２Ｂの後縁となる。 As shown in FIGS. 3 to 5, the plurality of wings 12 have a plurality of first wings 12A and a plurality of second wings 12B. The first wing 12A has an inner peripheral end 14A and an outer peripheral end 15A provided on the outer peripheral side of the inner peripheral end 14A and inclined forward in the rotation direction of the impeller 10. The inner peripheral end 14A is a front edge of the first wing 12A, and the outer peripheral end 15A is a rear edge of the first wing 12A. The second wing 12B has an inner peripheral end 14B and an outer peripheral end 15B provided on the outer peripheral side of the inner peripheral end 14B and inclined forward in the rotational direction of the impeller 10. The inner peripheral end 14B is the front edge of the second wing 12B, and the outer peripheral end 15B is the rear edge of the second wing 12B.
　回転軸１１に沿う方向において吸込口３２寄りの部分では、第１翼１２Ａの翼長は、第２翼１２Ｂの翼長と等しくなっている（図５参照）。一方、回転軸１１に沿う方向において主板１３寄りの部分では、第１翼１２Ａの翼長は、第２翼１２Ｂの翼長よりも長くなっており（図４参照）、かつ主板１３に近づくほど長くなっている。このように、本実施の形態では、第１翼１２Ａの翼長は、回転軸１１に沿う方向の少なくとも一部において、第２翼１２Ｂの翼長よりも長くなっている。 The wing length of the first wing 12A is equal to the wing length of the second wing 12B at a portion closer to the suction port 32 in the direction along the rotation axis 11 (see FIG. 5). On the other hand, at a portion closer to the main plate 13 in the direction along the rotation axis 11, the wing length of the first wing 12A is longer than the wing length of the second wing 12B (see FIG. 4). It is getting longer. Thus, in the present embodiment, the wing length of the first wing 12A is longer than the wing length of the second wing 12B in at least a part of the direction along the rotation axis 11.
　図４に示す主板１３寄りの第１断面において、回転軸１１と第１翼１２Ａの内周端１４Ａとの距離、すなわち第１翼１２Ａの内径は、ｒｉ＿Ａｂである。回転軸１１と外周端１５Ａとの距離、すなわち第１翼１２Ａの外径は、ｒｏ＿Ａｂである。距離ｒｏ＿Ａｂと距離ｒｉ＿Ａｂとの差は、第１断面での第１翼１２Ａの翼長Ｌ１ｂとなる（Ｌ１ｂ＝ｒｏ＿Ａｂ－ｒｉ＿Ａｂ）。ここで、一般的な多翼送風機では、回転軸に垂直な断面における翼の翼長は、回転軸方向での翼の幅寸法よりも短くなっている。本実施の形態においても、第１翼１２Ａの最大翼長、すなわち第１翼１２Ａの主板１３寄り端部での翼長は、第１翼１２Ａの回転軸方向の幅寸法Ｗ（図２参照）よりも短くなっている。 In the first cross section closer to the main plate 13 shown in FIG. 4, the distance between the rotation axis 11 and the inner peripheral end 14A of the first wing 12A, that is, the inner diameter of the first wing 12A is ri_Ab. The distance between the rotation shaft 11 and the outer peripheral end 15A, that is, the outer diameter of the first wing 12A is ro_Ab. The difference between the distance ro_Ab and the distance ri_Ab is the blade length L1b of the first wing 12A in the first cross section (L1b = ro_Ab−ri_Ab). Here, in a general multi-blade fan, the blade length of the blade in a cross section perpendicular to the rotation axis is shorter than the width dimension of the blade in the rotation axis direction. Also in the present embodiment, the maximum wing length of the first wing 12A, that is, the wing length at the end near the main plate 13 of the first wing 12A is the width dimension W of the first wing 12A in the rotational axis direction (see FIG. 2) It is shorter than that.
　また、第１断面において、回転軸１１と第２翼１２Ｂの内周端１４Ｂとの距離、すなわち第２翼１２Ｂの内径は、距離ｒｉ＿Ａｂよりも大きいｒｉ＿Ｂｂである（ｒｉ＿Ｂｂ＞ｒｉ＿Ａｂ）。回転軸１１と外周端１５Ｂとの距離、すなわち第２翼１２Ｂの外径は、距離ｒｏ＿Ａｂと等しいｒｏ＿Ｂｂである（ｒｏ＿Ｂｂ＝ｒｏ＿Ａｂ）。距離ｒｏ＿Ｂｂと距離ｒｉ＿Ｂｂとの差は、第１断面での第２翼１２Ｂの翼長Ｌ２ｂとなる（Ｌ２ｂ＝ｒｏ＿Ｂｂ－ｒｉ＿Ｂｂ）。第１断面での第２翼１２Ｂの翼長Ｌ２ｂは、同断面での第１翼１２Ａの翼長Ｌ１ｂよりも短い（Ｌ２ｂ＜Ｌ１ｂ）。 In the first cross section, the distance between the rotation axis 11 and the inner peripheral end 14B of the second wing 12B, that is, the inner diameter of the second wing 12B is ri_Bb larger than the distance ri_Ab (ri_Bb> ri_Ab). The distance between the rotation axis 11 and the outer peripheral end 15B, that is, the outer diameter of the second wing 12B is ro_Bb equal to the distance ro_Ab (ro_Bb = ro_Ab). The difference between the distance ro_Bb and the distance ri_Bb is the blade length L2b of the second wing 12B in the first cross section (L2b = ro_Bb-ri_Bb). The wing length L2b of the second wing 12B in the first cross section is shorter than the wing length L1 b of the first wing 12A in the same cross section (L2 b <L1 b).
　第１断面における第１翼１２Ａの出口角は、βｂｏ＿Ａｂである。同断面における第２翼１２Ｂの出口角は、βｂｏ＿Ｂｂである。第２翼１２Ｂの出口角βｂｏ＿Ｂｂは、第１翼１２Ａの出口角βｂｏ＿Ａｂと等しい（βｂｏ＿Ｂｂ＝βｂｏ＿Ａｂ）。 The exit angle of the first wing 12A in the first cross section is βbo_Ab. The exit angle of the second wing 12B in the same cross section is βbo_Bb. The exit angle βbo_Bb of the second wing 12B is equal to the exit angle βbo_Ab of the first wing 12A (βbo_Bb = βbo_Ab).
　一方、図５に示す吸込口３２寄りの第２断面において、回転軸１１と第１翼１２Ａの内周端１４Ａとの距離は、ｒｉ＿Ａｉである。距離ｒｉ＿Ａｉは、第１断面での回転軸１１と第１翼１２Ａの内周端１４Ａとの距離ｒｉ＿Ａｂよりも長い（ｒｉ＿Ａｉ＞ｒｉ＿Ａｂ）。回転軸１１と第１翼１２Ａの外周端１５Ａとの距離は、ｒｏ＿Ａｉである。距離ｒｏ＿Ａｉと距離ｒｉ＿Ａｉとの差は、第２断面での第１翼１２Ａの翼長Ｌ１ｉとなる（Ｌ１ｉ＝ｒｏ＿Ａｉ－ｒｉ＿Ａｉ）。 On the other hand, in the second cross section near the suction port 32 shown in FIG. 5, the distance between the rotation shaft 11 and the inner peripheral end 14A of the first wing 12A is ri_Ai. The distance ri_Ai is longer than the distance ri_Ab between the rotation axis 11 and the inner peripheral end 14A of the first wing 12A in the first cross section (ri_Ai> ri_Ab). The distance between the rotation axis 11 and the outer peripheral end 15A of the first wing 12A is ro_Ai. The difference between the distance ro_Ai and the distance ri_Ai is the wing length L1i of the first wing 12A in the second cross section (L1i = ro_Ai-ri_Ai).
　また、第２断面において、回転軸１１と第２翼１２Ｂの内周端１４Ｂとの距離は、ｒｉ＿Ｂｉである。距離ｒｉ＿Ｂｉは、同断面での回転軸１１と第１翼１２Ａの内周端１４Ａとの距離ｒｉ＿Ａｉと等しい（ｒｉ＿Ｂｉ＝ｒｉ＿Ａｉ）。回転軸１１と第２翼１２Ｂの外周端１５Ｂとの距離は、ｒｏ＿Ｂｉである。距離ｒｏ＿Ｂｉは、同断面での回転軸１１と第１翼１２Ａの外周端１５Ａとの距離ｒｏ＿Ａｉと等しい（ｒｏ＿Ｂｉ＝ｒｏ＿Ａｉ）。距離ｒｏ＿Ｂｉと距離ｒｉ＿Ｂｉとの差は、第２断面での第２翼１２Ｂの翼長Ｌ２ｉとなる（Ｌ２ｉ＝ｒｏ＿Ｂｉ－ｒｉ＿Ｂｉ）。第２断面での第２翼１２Ｂの翼長Ｌ２ｉは、同断面での第１翼１２Ａの翼長Ｌ１ｉと等しい（Ｌ２ｉ＝Ｌ１ｉ）。 Further, in the second cross section, the distance between the rotation axis 11 and the inner peripheral end 14B of the second wing 12B is ri_Bi. The distance ri_Bi is equal to the distance ri_Ai between the rotation axis 11 and the inner peripheral end 14A of the first wing 12A in the same section (ri_Bi = ri_Ai). The distance between the rotation shaft 11 and the outer peripheral end 15B of the second wing 12B is ro_Bi. The distance ro_Bi is equal to the distance ro_Ai between the rotation axis 11 and the outer peripheral end 15A of the first wing 12A in the same cross section (ro_Bi = ro_Ai). The difference between the distance ro_Bi and the distance ri_Bi is the wing length L2i of the second wing 12B in the second cross section (L2i = ro_Bi-ri_Bi). The wing length L2i of the second wing 12B in the second cross section is equal to the wing length L1i of the first wing 12A in the same cross section (L2i = L1i).
　図５では図示を省略しているが、第２断面においても、第１翼１２Ａの出口角と第２翼１２Ｂの出口角とは等しい。 Although not shown in FIG. 5, the outlet angle of the first wing 12A and the outlet angle of the second wing 12B are equal to each other also in the second cross section.
　図３～図５に示すように、周方向で互いに隣り合う２つの第１翼１２Ａの間には、少なくとも１つの第２翼１２Ｂが配置されている。このため、第２翼１２Ｂの数は、第１翼１２Ａの数と同数又はそれより多くなっている。本実施の形態では、２つの第１翼１２Ａの間には２つの第２翼１２Ｂが配置されているため、第２翼１２Ｂの数は、第１翼１２Ａの数の２倍となっている。 As shown in FIGS. 3 to 5, at least one second wing 12B is disposed between two first wings 12A adjacent to each other in the circumferential direction. For this reason, the number of second wings 12B is equal to or greater than the number of first wings 12A. In the present embodiment, since two second wings 12B are disposed between two first wings 12A, the number of second wings 12B is twice the number of first wings 12A. .
　回転軸１１と平行に見たとき、図５に示す第２断面での第１翼１２Ａは、図４に示す第１断面での第１翼１２Ａの輪郭からはみ出ないように当該第１翼１２Ａと重なっている。このため、ｒｏ＿Ａｉ≦ｒｏ＿Ａｂ、ｒｉ＿Ａｉ≧ｒｉ＿Ａｂ、及びＬ１ｉ≦Ｌ１ｂの関係が満たされている。 When viewed in parallel with the rotation shaft 11, the first wing 12A in the second cross section shown in FIG. 5 does not protrude from the contour of the first wing 12A in the first cross section shown in FIG. And overlap. Therefore, the relationships of ro_Ai ≦ ro_Ab, ri_Ai ≦ ri_Ab, and L1i ≦ L1b are satisfied.
　同様に、回転軸１１と平行に見たとき、図５に示す第２断面での第２翼１２Ｂは、図４に示す第１断面での第２翼１２Ｂの輪郭からはみ出ないように当該第２翼１２Ｂと重なっている。このため、ｒｏ＿Ｂｉ≦ｒｏ＿Ｂｂ、ｒｉ＿Ｂｉ≧ｒｉ＿Ｂｂ、及びＬ２ｉ≦Ｌ２ｂの関係が満たされている。 Similarly, when viewed in parallel with the rotation axis 11, the second wing 12B in the second cross section shown in FIG. 5 does not protrude from the contour of the second wing 12B in the first cross section shown in FIG. It overlaps with 2 wings 12B. Therefore, the relationships of ro_Bi ≦ ro_Bb, ri_Bi_ri_Bb, and L2i ≦ L2b are satisfied.
　図６は、本実施の形態に係る多翼送風機において第１断面での第１翼１２Ａの形状を説明する図である。図６に示すように、第１断面での第１翼１２Ａは、回転軸１１を中心として第２翼１２Ｂの内周端１４Ｂに接する円Ｃ１よりも外周側に位置する外周側翼部１２Ａ１と、円Ｃ１よりも内周側に位置する内周側翼部１２Ａ２と、を有している。 FIG. 6 is a view for explaining the shape of the first wing 12A in the first cross section in the multi-blade fan according to the present embodiment. As shown in FIG. 6, the first wing 12A in the first cross section has an outer circumferential wing portion 12A1 located on the outer circumferential side of a circle C1 contacting the inner circumferential end 14B of the second wing 12B with the rotation axis 11 as a center; And an inner peripheral wing portion 12A2 positioned on the inner peripheral side of the circle C1.
　外周側翼部１２Ａ１の弦線２０の長さを外周側翼部１２Ａ１の弦長Ｌ＿Ａｂ１とし、弦線２０と外周側翼部１２Ａ１の反り線２２との最大距離を外周側翼部１２Ａ１の反り高さｄ＿Ａｂ１とする。ここで、羽根車１０の回転方向の逆方向への反り高さを正の値で表し、羽根車１０の回転方向への反り高さを負の値で表すものとする。外周側翼部１２Ａ１は羽根車１０の回転方向とは逆方向に反っているため、反り高さｄ＿Ａｂ１は正の値となる（ｄ＿Ａｂ１＞０）。弦長Ｌ＿Ａｂ１に対する反り高さｄ＿Ａｂ１の比（ｄ＿Ａｂ１／Ｌ＿Ａｂ１）を、外周側翼部１２Ａ１の反り比とする。 The length of the chord line 20 of the outer circumferential wing 12A1 is the chord length L_Ab1 of the outer wing 12A1, and the maximum distance between the chord 20 and the warp line 22 of the outer wing 12A1 is the warpage height d_Ab1 of the outer wing 12A1. . Here, the warpage height in the reverse direction of the rotation direction of the impeller 10 is represented by a positive value, and the warpage height in the rotation direction of the impeller 10 is represented by a negative value. Since the outer peripheral side wing 12A1 is warped in the direction opposite to the rotation direction of the impeller 10, the warpage height d_Ab1 takes a positive value (d_Ab1> 0). The ratio (d_Ab1 / L_Ab1) of the warpage height d_Ab1 to the chord length L_Ab1 is taken as the warpage ratio of the outer peripheral wing 12A1.
　また、内周側翼部１２Ａ２の弦線２１の長さを内周側翼部１２Ａ２の弦長Ｌ＿Ａｂ２とし、弦線２１と内周側翼部１２Ａ２の反り線２３との最大距離を内周側翼部１２Ａ２の反り高さｄ＿Ａｂ２とする。本実施の形態では、内周側翼部１２Ａ２は羽根車１０の回転方向に反っているため、反り高さｄ＿Ａｂ２は負の値となる（ｄ＿Ａｂ２＜０）。ただし、内周側翼部１２Ａ２は、羽根車１０の回転方向の逆方向に反っていてもよい。弦長Ｌ＿Ａｂ２に対する反り高さｄ＿Ａｂ２の比（ｄ＿Ａｂ２／Ｌ＿Ａｂ２）を、内周側翼部１２Ａ２の反り比とする。このとき、外周側翼部１２Ａ１の反り比（ｄ＿Ａｂ１／Ｌ＿Ａｂ１）は、内周側翼部１２Ａ２の反り比（ｄ＿Ａｂ２／Ｌ＿Ａｂ２）よりも大きくなっている（ｄ＿Ａｂ１／Ｌ＿Ａｂ１＞ｄ＿Ａｂ２／Ｌ＿Ａｂ２）。 Further, the length of the chord 21 of the inner wing 12A2 is the chord length L_Ab2 of the inner wing 12A2, and the maximum distance between the chord 21 and the warp line 23 of the inner wing 12A2 is the inner wing 12A2. The warp height is d_Ab2. In the present embodiment, since the inner circumferential side wing portion 12A2 is warped in the rotational direction of the impeller 10, the warpage height d_Ab2 takes a negative value (d_Ab2 <0). However, the inner peripheral side wing portion 12A2 may be curved in the reverse direction of the rotation direction of the impeller 10. The ratio (d_Ab2 / L_Ab2) of the warpage height d_Ab2 to the chord length L_Ab2 is taken as the warpage ratio of the inner peripheral side wing portion 12A2. At this time, the warpage ratio (d_Ab1 / L_Ab1) of the outer peripheral side wing 12A1 is larger than the warpage ratio (d_Ab2 / L_Ab2) of the inner peripheral side wing 12A2 (d_Ab1 / L_Ab1> d_Ab2 / L_Ab2).
　以上説明したように、本実施の形態に係る多翼送風機は、回転軸１１を中心として回転する羽根車１０を備えた多翼送風機である。羽根車１０は、回転軸１１を中心とする周方向に配列した複数の翼１２と、複数の翼１２を回転軸１１に沿う方向の一方側から支持する主板１３と、を有している。回転軸１１に垂直な第１平面５１で切断された羽根車１０の第１断面（例えば、図４に示す断面）において、複数の翼１２のそれぞれは、内周端（例えば、内周端１４Ａ又は内周端１４Ｂ）と、内周端よりも外周側に設けられ、羽根車１０の回転方向で前方に向かって傾斜した外周端（例えば、外周端１５Ａ又は外周端１５Ｂ）と、を有している。複数の翼１２は、複数の第１翼１２Ａと、複数の第２翼１２Ｂと、を有している。上記第１断面において、複数の第１翼１２Ａのそれぞれは、複数の第２翼１２Ｂのそれぞれの翼長Ｌ２ｂよりも長い翼長Ｌ１ｂを有している。上記第１断面において、回転軸１１と複数の第１翼１２Ａのそれぞれの内周端１４Ａとの距離ｒｉ＿Ａｂは、回転軸１１と複数の第２翼１２Ｂのそれぞれの内周端１４Ｂとの距離ｒｉ＿Ｂｂよりも短くなっている。複数の第１翼１２Ａのうち周方向で互いに隣り合う２つの第１翼１２Ａの間には、複数の第２翼１２Ｂのうちの少なくとも１つの第２翼１２Ｂが配置されている。 As described above, the multi-blade fan according to the present embodiment is a multi-blade fan provided with the impeller 10 rotating around the rotation shaft 11. The impeller 10 has a plurality of wings 12 arranged in the circumferential direction around the rotation axis 11 and a main plate 13 supporting the plurality of wings 12 from one side in the direction along the rotation axis 11. In a first cross section (for example, the cross section shown in FIG. 4) of the impeller 10 cut at a first plane 51 perpendicular to the rotation axis 11, each of the plurality of wings 12 has an inner peripheral end (for example, an inner peripheral end 14A) Or the inner peripheral end 14B) and the outer peripheral end (for example, the outer peripheral end 15A or the outer peripheral end 15B) provided on the outer peripheral side than the inner peripheral end and inclined forward in the rotational direction of the impeller 10 ing. The plurality of wings 12 includes a plurality of first wings 12A and a plurality of second wings 12B. In the first cross section, each of the plurality of first wings 12A has a wing length L1b longer than the wing length L2b of each of the plurality of second wings 12B. In the first cross section, the distance ri_Ab between the rotary shaft 11 and the respective inner peripheral ends 14A of the plurality of first wings 12A is the distance ri_Bb between the rotary shaft 11 and the respective inner peripheral ends 14B of the plurality of second wings 12B. It is shorter than that. At least one second wing 12B of the plurality of second wings 12B is disposed between the two first wings 12A adjacent to each other in the circumferential direction among the plurality of first wings 12A.
　この構成によれば、第１翼１２Ａの翼長Ｌ１ｂが第２翼１２Ｂの翼長Ｌ２ｂよりも長いため、少なくとも第１翼１２Ａにおいて遠心力による昇圧作用を高めることができる。一方で、周方向で互いに隣り合う２つの第１翼１２Ａの間には、第１翼１２Ａよりも翼長の短い少なくとも１つの第２翼１２Ｂが配置される。これにより、２つの第１翼１２Ａの間に形成される空気流路の入口部が狭くなるのを防ぐことができるため、翼間の空気流路の入口部での縮流を緩和することができる。したがって、上記構成によれば、多翼送風機の効率を向上させることができるとともに、多翼送風機の所要動力を低減することができる。 According to this configuration, since the blade length L1b of the first blade 12A is longer than the blade length L2b of the second blade 12B, it is possible to enhance the pressure boosting action by the centrifugal force at least in the first blade 12A. On the other hand, at least one second wing 12B shorter in wing length than the first wing 12A is disposed between two first wings 12A adjacent to each other in the circumferential direction. As a result, since it is possible to prevent the inlet portion of the air flow passage formed between the two first wings 12A from being narrowed, it is possible to alleviate the contraction flow at the inlet portion of the air flow passage between the wings. it can. Therefore, according to the above configuration, the efficiency of the multi-blade fan can be improved, and the required power of the multi-blade fan can be reduced.
　また、本実施の形態に係る多翼送風機では、上記第１断面において、複数の第１翼１２Ａのそれぞれは、回転軸１１を中心として複数の第２翼１２Ｂのそれぞれの内周端１４Ｂに接する円Ｃ１よりも外周側に位置する外周側翼部１２Ａ１と、円Ｃ１よりも内周側に位置する内周側翼部１２Ａ２と、を有している。外周側翼部１２Ａ１及び内周側翼部１２Ａ２のそれぞれにおいて、弦長に対する反り高さの比を反り比とし、上記回転方向の逆方向への反り高さを正の値で表し、上記回転方向への反り高さを負の値で表す。このとき、外周側翼部１２Ａ１の反り比（ｄ＿Ａｂ１／Ｌ＿Ａｂ１）は、内周側翼部１２Ａ２の反り比（ｄ＿Ａｂ２／Ｌ＿Ａｂ２）よりも大きい。 Further, in the multi-blade fan according to the present embodiment, in the first cross section, each of the plurality of first wings 12A is in contact with the inner peripheral end 14B of each of the plurality of second wings 12B around the rotation axis 11. It has an outer peripheral side wing portion 12A1 located on the outer peripheral side than the circle C1, and an inner peripheral side wing portion 12A2 located on the inner peripheral side of the circle C1. In each of the outer peripheral side wing portion 12A1 and the inner peripheral side wing portion 12A2, the ratio of the warpage height to the chord length is taken as a warpage ratio, and the warpage height in the reverse direction of the rotation direction is represented by a positive value. The warp height is expressed as a negative value. At this time, the warpage ratio (d_Ab1 / L_Ab1) of the outer peripheral side wing portion 12A1 is larger than the warpage ratio (d_Ab2 / L_Ab2) of the inner peripheral side wing portion 12A2.
　この構成によれば、２つの第１翼１２Ａの間に形成される空気流路の入口部において、空気の流れ方向と第１翼１２Ａの翼面との角度差を小さくすることができる。これにより、翼間の空気流路での剥離を抑制できるため、多翼送風機の効率をさらに向上させることができる。 According to this configuration, at the inlet of the air flow path formed between the two first wings 12A, the difference in angle between the air flow direction and the wing surface of the first wing 12A can be reduced. As a result, separation in the air flow path between the blades can be suppressed, so the efficiency of the multi-blade fan can be further improved.
　また、本実施の形態に係る多翼送風機において、回転軸１１に垂直な平面であって主板１３からの距離が上記第１平面と主板１３との距離よりも長い平面を第２平面５２とする。第２平面５２で切断された羽根車１０の第２断面（例えば、図５に示す断面）における回転軸１１と複数の第１翼１２Ａのそれぞれの内周端１４Ａとの距離ｒｉ＿Ａｉは、上記第１断面における回転軸１１と複数の第１翼１２Ａのそれぞれの内周端１４Ａとの距離ｒｉ＿Ａｂよりも長い。 Further, in the multi-blade fan according to the present embodiment, a plane which is a plane perpendicular to the rotation axis 11 and whose distance from the main plate 13 is longer than the distance between the first plane and the main plate 13 is taken as a second plane 52. . The distance ri_Ai between the rotary shaft 11 and the inner peripheral end 14A of each of the plurality of first wings 12A in the second cross section (for example, the cross section shown in FIG. 5) of the impeller 10 cut at the second plane 52 The distance ri_Ab between the rotation axis 11 and the inner peripheral end 14A of each of the plurality of first wings 12A in one cross section is longer.
　この構成によれば、回転軸１１を中心とする第１翼１２Ａの内径は、羽根車１０の主板１３側よりも羽根車１０の吸込口３２側で大きくなる。このため、羽根車１０の吸込口３２側では、吸込口３２から羽根車１０内部に流入し回転軸１１に沿って流れる空気の流路断面積を大きくすることができる。これにより、羽根車１０内部に流入した空気の回転軸１１方向の速度成分を減少させることができるため、羽根車１０内部に流入した空気の流れが羽根車１０の径方向に曲げられるときの損失を低減することができる。したがって、多翼送風機の効率をさらに向上させることができる。一方、羽根車１０内部を流通する空気は、吸込口３２から主板１３に向かう回転軸１１方向の運動量を有している。このため、羽根車１０から流出する空気の風量分布は、回転軸１１方向において主板１３寄りに偏る。上記構成では、第１翼１２Ａの翼長が主板１３寄りの部分で長くなっているため、第１翼１２Ａでの昇圧作用を風量分布が多い部分で高めることができる。したがって、多翼送風機の出力を効果的に向上させることができる。 According to this configuration, the inner diameter of the first wing 12A centered on the rotation shaft 11 is larger on the suction port 32 side of the impeller 10 than on the main plate 13 side of the impeller 10. Therefore, on the suction port 32 side of the impeller 10, the flow passage cross-sectional area of the air flowing into the impeller 10 from the suction port 32 and flowing along the rotation shaft 11 can be increased. As a result, the velocity component of the air flowing into the impeller 10 can be reduced in the direction of the rotation shaft 11, so that the loss when the flow of air flowing into the impeller 10 is bent in the radial direction of the impeller 10 Can be reduced. Therefore, the efficiency of the multi-blade fan can be further improved. On the other hand, air flowing through the inside of the impeller 10 has momentum in the direction of the rotation axis 11 from the suction port 32 toward the main plate 13. Therefore, the air volume distribution of the air flowing out of the impeller 10 is biased toward the main plate 13 in the direction of the rotation shaft 11. In the above-described configuration, since the blade length of the first wing 12A is long in the portion near the main plate 13, the pressurizing action in the first wing 12A can be enhanced in the portion where the air volume distribution is large. Therefore, the output of the multi-blade fan can be effectively improved.
　また、本実施の形態に係る多翼送風機において、回転軸１１と平行に見たとき、上記第２断面における複数の翼１２のそれぞれは、上記第１断面における複数の翼１２のそれぞれの輪郭からはみ出ないように上記第１断面における複数の翼１２のそれぞれと重なっている。 Further, in the multi-blade fan according to the present embodiment, when viewed in parallel with the rotation shaft 11, each of the plurality of wings 12 in the second cross section is derived from the contour of each of the plurality of wings 12 in the first cross section. It overlaps with each of the plurality of wings 12 in the first cross section so as not to go out.
　この構成によれば、回転軸１１方向に開く簡易的な金型を用いて、主板１３と複数の翼１２とを一体的に成形することができる。したがって、多翼送風機の製造コストを削減することができる。 According to this configuration, the main plate 13 and the plurality of wings 12 can be integrally formed using a simple mold that opens in the direction of the rotation shaft 11. Therefore, the manufacturing cost of the multi-blade fan can be reduced.
　また、本実施の形態に係る多翼送風機では、上記第１断面において、複数の第１翼１２Ａのそれぞれの外周端１５Ａと回転軸１１との距離ｒｏ＿Ａｂは、複数の第２翼１２Ｂのそれぞれの外周端１５Ｂと回転軸１１との距離ｒｏ＿Ｂｂと等しい。上記第１断面において、複数の第１翼１２Ａのそれぞれの出口角βｂｏ＿Ａｂは、複数の第２翼１２Ｂのそれぞれの出口角βｂｏ＿Ｂｂと等しい。 Further, in the multi-blade fan according to the present embodiment, in the first cross section, the distance ro_Ab between the outer peripheral end 15A of each of the plurality of first wings 12A and the rotation shaft 11 is the same as each of the plurality of second wings 12B. It is equal to the distance ro_Bb between the outer peripheral end 15B and the rotation shaft 11. In the first cross section, the outlet angle βbo_Ab of each of the plurality of first wings 12A is equal to the outlet angle βbo_Bb of each of the plurality of second wings 12B.
　この構成によれば、羽根車１０から流出する気流の向きを羽根車１０の周方向位置によらず均一にすることができる。仮に、羽根車１０から流出する気流の向きが羽根車１０の周方向位置によって変動する場合、回転音などの騒音が生じる。したがって、上記構成によれば、回転音などの騒音を抑制することができる。 According to this configuration, the direction of the air flow flowing out of the impeller 10 can be made uniform regardless of the circumferential position of the impeller 10. If the direction of the air flow flowing out of the impeller 10 changes depending on the circumferential position of the impeller 10, noise such as rotational noise is generated. Therefore, according to the above configuration, noise such as rotational noise can be suppressed.
　なお、上記実施の形態では、主板１３の一方側のみに複数の翼１２が形成された片吸込型の羽根車１０を備えた多翼送風機を例に挙げたが、本発明は、主板の両側にそれぞれ複数の翼が形成された両吸込型の羽根車を備えた多翼送風機にも適用できる。 In the above embodiment, the multi-blade fan provided with the single-suction type impeller 10 in which the plurality of wings 12 is formed only on one side of the main plate 13 has been described as an example. The present invention is also applicable to a multi-blade fan provided with a double-suction type impeller in which a plurality of blades are formed respectively.
　１０　羽根車、１１　回転軸、１２　翼、１２Ａ　第１翼、１２Ａ１　外周側翼部、１２Ａ２　内周側翼部、１２Ｂ　第２翼、１３　主板、１４Ａ、１４Ｂ　内周端、１５Ａ、１５Ｂ　外周端、２０、２１　弦線、２２、２３　反り線、３０　ケーシング、３１　スクロール壁、３２　吸込口、３３　吹出口、４０　駆動モータ、４１　モータシャフト、５１　第１平面、５２　第２平面、Ｃ１　円。 DESCRIPTION OF SYMBOLS 10 impeller, 11 rotating shaft, 12 wings, 12A 1st wing, 12A1 outer peripheral side wing part, 12A 2 inner peripheral side wing part, 12B 2nd wing, 13 main plate, 14A, 14B inner peripheral end, 15A, 15B outer peripheral end, 20, 21 chords, 22 and 23 warp lines, 30 casings, 31 scroll walls, 32 suction ports, 33 outlets, 40 drive motors, 41 motor shafts, 51 first plane, 52 second plane, C1 circle.

Claims (5)

  1. 　回転軸を中心として回転する羽根車を備えた多翼送風機であって、
    　前記羽根車は、前記回転軸を中心とする周方向に配列した複数の翼と、前記複数の翼を前記回転軸に沿う方向の一方側から支持する主板と、を有しており、
    　前記回転軸に垂直な第１平面で切断された前記羽根車の第１断面において、前記複数の翼のそれぞれは、内周端と、前記内周端よりも外周側に設けられ、前記羽根車の回転方向で前方に向かって傾斜した外周端と、を有しており、
    　前記複数の翼は、複数の第１翼と、複数の第２翼と、を有しており、
    　前記第１断面において、前記複数の第１翼のそれぞれは、前記複数の第２翼のそれぞれの翼長よりも長い翼長を有しており、
    　前記第１断面において、前記回転軸と前記複数の第１翼のそれぞれの前記内周端との距離は、前記回転軸と前記複数の第２翼のそれぞれの前記内周端との距離よりも短くなっており、
    　前記複数の第１翼のうち前記周方向で互いに隣り合う２つの第１翼の間には、前記複数の第２翼のうちの少なくとも１つの第２翼が配置されている多翼送風機。     A multi-blade fan comprising an impeller rotating about a rotation axis, the fan comprising:
    The impeller includes: a plurality of wings arranged in a circumferential direction around the rotation axis; and a main plate supporting the plurality of wings from one side in a direction along the rotation axis,
    In the first cross section of the impeller cut at a first plane perpendicular to the rotation axis, each of the plurality of wings is provided at an inner peripheral end and an outer peripheral side than the inner peripheral end, the impeller And an outer peripheral edge inclined forward in the rotational direction of the
    The plurality of wings includes a plurality of first wings and a plurality of second wings,
    In the first cross section, each of the plurality of first wings has a wing length longer than a wing length of each of the plurality of second wings,
    In the first cross section, the distance between the rotation axis and the inner peripheral end of each of the plurality of first wings is greater than the distance between the rotation axis and each inner peripheral end of the plurality of second wings. It has become shorter
    A multi-blade fan in which at least one second wing of the plurality of second wings is disposed between two first wings adjacent to each other in the circumferential direction among the plurality of first wings.
  2. 　前記第１断面において、前記複数の第１翼のそれぞれは、前記回転軸を中心として前記複数の第２翼のそれぞれの前記内周端に接する円よりも外周側に位置する外周側翼部と、前記円よりも内周側に位置する内周側翼部と、を有しており、
    　前記外周側翼部及び前記内周側翼部のそれぞれにおいて、弦長に対する反り高さの比を反り比とし、前記回転方向の逆方向への反り高さを正の値で表し、前記回転方向への反り高さを負の値で表したとき、
    　前記外周側翼部の反り比は、前記内周側翼部の反り比よりも大きい請求項１に記載の多翼送風機。     In the first cross section, each of the plurality of first wings is an outer circumferential side wing portion located on the outer circumferential side with respect to a circle contacting the inner circumferential end of each of the plurality of second wings with the rotation axis as a center; And an inner peripheral wing portion located on the inner peripheral side of the circle,
    In each of the outer peripheral wing portion and the inner peripheral wing portion, the ratio of the warpage height to the chord length is taken as the warpage ratio, and the warpage height in the reverse direction of the rotation direction is represented by a positive value, When the warp height is expressed as a negative value,
    The multi-blade fan according to claim 1, wherein the warpage ratio of the outer peripheral side wing portion is larger than the warpage ratio of the inner peripheral side wing portion.
  3. 　前記回転軸に垂直な平面であって前記主板からの距離が前記第１平面と前記主板との距離よりも長い平面を第２平面としたとき、
    　前記第２平面で切断された前記羽根車の第２断面における前記回転軸と前記複数の第１翼のそれぞれの前記内周端との距離は、前記第１断面における前記回転軸と前記複数の第１翼のそれぞれの前記内周端との距離よりも長い請求項１又は請求項２に記載の多翼送風機。     When a plane which is a plane perpendicular to the rotation axis and whose distance from the main plate is longer than the distance between the first plane and the main plate is a second plane,
    The distance between the rotation axis in the second cross section of the impeller cut by the second plane and the inner peripheral end of each of the plurality of first wings is the rotation axis and the plurality of the plurality in the first cross section. The multi-blade fan according to claim 1 or 2, wherein the distance is longer than the distance between each of the first wings and the inner circumferential end.
  4. 　前記回転軸と平行に見たとき、前記第２断面における前記複数の翼のそれぞれは、前記第１断面における前記複数の翼のそれぞれの輪郭からはみ出ないように前記第１断面における前記複数の翼のそれぞれと重なっている請求項３に記載の多翼送風機。 When viewed parallel to the rotation axis, each of the plurality of wings in the second cross section does not protrude from the contour of each of the plurality of wings in the first cross section. The multi-blade fan according to claim 3, overlapping with each of the above.
  5. 　前記第１断面において、前記複数の第１翼のそれぞれの前記外周端と前記回転軸との距離は、前記複数の第２翼のそれぞれの前記外周端と前記回転軸との距離と等しく、
    　前記第１断面において、前記複数の第１翼のそれぞれの出口角は、前記複数の第２翼のそれぞれの出口角と等しい請求項１～請求項４のいずれか一項に記載の多翼送風機。     In the first cross section, the distance between the outer peripheral end of each of the plurality of first wings and the rotation axis is equal to the distance between each outer peripheral end of each of the plurality of second wings and the rotation axis,
    The multi-blade fan according to any one of claims 1 to 4, wherein in the first cross section, an outlet angle of each of the plurality of first wings is equal to an outlet angle of each of the plurality of second wings. .
PCT/JP2017/038914 2017-10-27 2017-10-27 Multivane blower WO2019082378A1 (en)

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