WO2008059775A1 - Impeller for multi-blade fan - Google Patents

Impeller for multi-blade fan Download PDF

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Publication number
WO2008059775A1
WO2008059775A1 PCT/JP2007/071878 JP2007071878W WO2008059775A1 WO 2008059775 A1 WO2008059775 A1 WO 2008059775A1 JP 2007071878 W JP2007071878 W JP 2007071878W WO 2008059775 A1 WO2008059775 A1 WO 2008059775A1
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WO
WIPO (PCT)
Prior art keywords
impeller
end plate
blade
blades
rotation axis
Prior art date
Application number
PCT/JP2007/071878
Other languages
French (fr)
Japanese (ja)
Inventor
Masahito Higashida
Original Assignee
Daikin Industries, Ltd.
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 Daikin Industries, Ltd. filed Critical Daikin Industries, Ltd.
Priority to EP07831608.0A priority Critical patent/EP2096318B1/en
Publication of WO2008059775A1 publication Critical patent/WO2008059775A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • F04D29/282Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis
    • F04D29/283Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis rotors of the squirrel-cage type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/02Selection of particular materials
    • F04D29/023Selection of particular materials especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/50Building or constructing in particular ways
    • F05D2230/53Building or constructing in particular ways by integrally manufacturing a component, e.g. by milling from a billet or one piece construction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/40Organic materials
    • F05D2300/43Synthetic polymers, e.g. plastics; Rubber

Definitions

  • the present invention relates to an impeller of a multiblade blower, and more particularly to an impeller of a multiblade blower that sucks gas from a rotation axis direction and blows out gas in a direction crossing the rotation axis.
  • a multiblade blower that draws gas in the direction of the rotation axis and blows out gas in a direction that intersects the rotation axis is often used in order to blow air.
  • Such an impeller of a multiblade blower is mainly arranged in a substantially circular end plate that rotates about a rotation axis, and is annularly arranged on the end plate with the rotation axis as the center, and each end is disposed on the outer periphery of the main plate.
  • a plurality of wings provided and an end ring connecting the other ends of the plurality of wings are provided.
  • Patent Document 1 JP 2000-320490 A
  • the impeller of the former multiblade fan is rotated at a high speed, the centrifugal force applied to the impeller increases, the concentricity of the impeller cannot be maintained, and the amount of uneven balance increases.
  • the impeller may be greatly deformed and damaged.
  • the latter impeller of the latter multi-blade fan is provided with an intermediate ring, so that the amount of deformation of the impeller due to centrifugal force is larger than that of the former impeller of the multi-blade fan. Becomes smaller and high speed rotation is possible.
  • the intermediate ring provided in this impeller is provided from the outer peripheral edge to the inner peripheral edge of the blade, the ventilation resistance when blowing from the inside of the impeller to the outer peripheral side increases. The problem power.
  • the intermediate ring Since it is provided from the outer peripheral edge to the inner peripheral edge of the blade, it is difficult to mold the resin integrally, and like the impeller of the cross flow fan, the impeller is positioned in the direction of the rotation axis at the position of the intermediate ring. Since it is necessary to mold the resin by dividing it into a part on the end ring side and a part on the end plate side in the rotation axis direction, and joining these parts by ultrasonic welding, etc. There is a problem that it takes time and effort S
  • the problem of the present invention is that the impeller of a multiblade blower suppresses an increase in ventilation resistance when blown from the inside of the impeller to the outer peripheral side as much as possible, and can be integrally molded with a high-speed rotation. It is to realize.
  • An impeller of a multiblade blower that is the power of the first invention is an impeller of a multiblade blower that sucks gas from the direction of the rotation axis and blows out gas in a direction intersecting the rotation axis.
  • a substantially circular end plate that rotates about the center, a plurality of blades, and one or more intermediate rings.
  • the plurality of blades are annularly arranged on one or both sides of the end plate with the rotation axis as the center, and one end is provided on the outer periphery of the end plate.
  • the intermediate ring is located at a position other than the end on the side opposite to the end plate of the plurality of blades! / And connects the outer peripheral edges of the blades so that they do not overlap with the blades when viewed from the rotation axis direction. It is formed as follows.
  • the intermediate ring force provided at a position other than the end on the side opposite to the end plate side of the plurality of blades so that the blades do not overlap with each other when viewed from the direction of the rotation axis.
  • the outer peripheral edge of the impeller is formed so that the increase in ventilation resistance when blown from the inside of the impeller to the outer peripheral side and the resin impregnation of the entire impeller including the intermediate ring are possible, High speed rotation can be realized.
  • the impeller of the multi-blade fan that is powerful in the second invention is the impeller of the multi-blade fan that is powerful in the first invention.
  • At least a part of the intermediate ring is at the end plate side end of the blade. From the position corresponding to 1/4 times the blade length from the end plate side end of the blade to the end plate side end toward the end of the blade opposite to the end plate side. It is formed so as to be included in the range up to the position corresponding to 3/4 times the length!
  • the intermediate ring is directed from the end plate side end of the blade toward the end plate side of the blade toward the end end side of the blade from the end plate side of the blade. From the position corresponding to 1/4 times the blade length to the end, the blade length 3 Because it is formed so as to be included in a range up to a position corresponding to / 4 times the length, deformation of the vane wheel can be effectively suppressed.
  • the impeller of the multi-blade fan which is the power of the third invention, is the blade wheel of the multi-blade fan, the power of the second invention, the intermediate ring is the end plate side end of the blade and the anti-end plate Two pitches are formed between the side edges, and the pitch between the intermediate rings is set within the range of 1/4 times the blade length to 3/4 times the blade length. Yes.
  • the impeller of the multi-blade fan according to the fourth invention is the impeller of the multi-blade fan according to any of the first to third inventions, wherein the cross-sectional shape of the intermediate ring is the rotational axis.
  • the length in the direction is approximately rectangular, which is more than 1/2 the length of protrusion from the outer periphery of the wing.
  • the cross-sectional shape of the intermediate ring is a substantially rectangular shape whose length in the rotation axis direction is 1/2 or more of the protruding length from the outer peripheral edge of the blade, which is sufficient for the intermediate ring. Since it has a thickness in the direction of the rotation axis, deformation of the impeller can be effectively suppressed.
  • the impeller of the multiblade fan according to the fifth invention is the impeller of the multiblade fan according to any of the first to third inventions, wherein the cross-sectional shape of the intermediate ring is substantially L It is a letter shape.
  • the cross-sectional shape of the intermediate ring is substantially L-shaped, and the intermediate ring has a sufficient thickness in the direction of the rotation axis, which effectively suppresses the deformation of the impeller. S can.
  • the impeller of the multiblade fan according to the sixth invention is the impeller of the multiblade fan according to any of the first to third inventions, wherein the cross-sectional shape of the intermediate ring is substantially trapezoidal. Shape.
  • the cross-sectional shape of the intermediate ring has a substantially trapezoidal shape, and the intermediate ring has a sufficient thickness in the direction of the rotation axis, so that it can effectively recognize the deformation of the impeller. That power S.
  • FIG. 1 is a radial cross-sectional view of an impeller of a multiblade blower that is effective in an embodiment of the present invention.
  • FIG. 2 is a radial cross-sectional view of an impeller of a multiblade fan and a shape of a mold corresponding to the cross-sectional view.
  • FIG. 3 is a plan view of an impeller of a multiblade fan and a shape of a mold corresponding to the plan view.
  • FIG. 4 is a radial sectional view of an impeller of a multiblade fan according to Modification 1.
  • FIG. 5 is a radial cross-sectional view of an impeller of a multiblade fan according to Modification 2, showing the vicinity of an intermediate ring.
  • FIG. 6 is a radial cross-sectional view of an impeller of a multiblade fan according to Modification 2, showing the vicinity of an intermediate ring.
  • FIG. 7 is a radial cross-sectional view of an impeller of a multi-blade blower that focuses on another embodiment.
  • FIG. 1 shows an impeller 1 of a multiblade blower according to an embodiment of the present invention.
  • FIG. 1 is a radial sectional view of the impeller 1 of the multiblade fan.
  • Impeller 1 is an impeller of a double-suction type multi-blade fan that sucks gas from both sides of the rotation axis and blows gas in a direction crossing the rotation axis, and is driven to rotate by motor 2. .
  • OO in the figure is the rotational axis of the impeller 1 and the motor 2.
  • the impeller 1 is a resin product that is integrally molded using a mold, and mainly includes an end plate 11, a plurality of blades 12, a undling ring 13, and one or more intermediate rings 14. It is equipped with.
  • the end plate 11 is a substantially circular portion that rotates about the rotation shaft 3 of the motor 2, and a center hole 11 a to which the rotation shaft 3 is coupled is formed.
  • the plurality of blades 12 are annularly arranged on both surfaces of the end plate 11 with the rotation shaft 3 as the center, and each end is disposed on the outer periphery of the end plate 11 and extends without twisting toward both sides in the rotation axis direction. /!
  • the end ring 13 is an annular portion connecting the outer peripheral edges of the opposite end plate 11 side ends of the blades 12 at the position of the other end of the blade (that is, the opposite end plate 11 side end). It is arranged on both sides of the plate 11 in the rotation axis direction. The end ring 13 is formed so as not to overlap the plurality of blades 12 when viewed from the rotation axis direction.
  • the intermediate ring 14 is connected to the outer peripheral edge of each blade 12 so that it does not overlap with the plurality of blades 12 when viewed from the rotational axis direction at a position other than the end on the side opposite to the end plate 11 of the plurality of blades 12.
  • the annular portion is disposed on both sides of the end plate 11 in the rotation axis direction. Further, at least a part of each intermediate ring 14 is directed from the end plate 11 side end of the blade 12 toward the anti-end plate 11 side end of the blade 12 from the end plate 11 side end of the blade 12 as a reference.
  • each intermediate ring 14 is a substantially rectangular shape in which the length L2 in the rotation axis direction is 1/2 or more of the protruding length W from the outer peripheral edge of the blade 12. In the present embodiment, each intermediate ring 14 is approximately 1/2 times the blade length L1 from the end 12 side end of the blade 12 toward the opposite end plate 11 side end of the blade 12.
  • the length L 2 in the direction of the rotation axis has a substantially rectangular (that is, substantially square) cross-sectional shape having a length substantially the same as the protruding length W.
  • FIG. 2 is a diagram showing the radial cross-sectional view of the impeller 1 of the multiblade fan and the shapes of the molds 4, 5, 6, and 7 corresponding to the cross-sectional view.
  • FIG. 3 is a plan view of the bladed wheel 1 of the multiblade fan and the shapes of the molds 4, 6, and 7 corresponding to the plan view.
  • the impeller 1 is formed by integrally molding resin using two pairs of molds 4 and 5 and molds 6 and 7.
  • the end plate forming portion 4a of the mold 4 and the end plate forming portion 5a of the mold 5 include the end plate 11 including the center hole 11a (however, the radial direction).
  • the outer rim forming portions 4c and 5c of the dies 4 and 5 are formed by forming the wing forming portions 4b and 5b of the dies 4 and 5 into the wing 12 (excluding the outer peripheral edge in the radial direction).
  • the illustration of the outer peripheral edge forming portion 5c is omitted) forms the radial inner peripheral edge of the end ring 13 and the radial inner peripheral edge of the intermediate ring 14.
  • the outer peripheral edge forming portions 6 a and 7 a are in the radial outer peripheral edge of the end plate 11.
  • the end ring forming parts 6b and 7b form the end ring 13 (excluding the inner peripheral edge of the end ring 13 in the radial direction)
  • the intermediate ring forming parts 6c and 7c are in the middle Form a ring 14 (except for the radially inner edge of the intermediate ring 14).
  • the impeller 1 of the multiblade fan of the present embodiment can be integrally molded with resin by removing the dies 4 and 5 in the rotational axis direction and dies 6 and 7 in the radial direction. is there.
  • the impeller 1 of the multiblade fan of the present embodiment has the following characteristics.
  • the intermediate ring 14 provided at a position other than the side end of the anti-end plate 11 of the plurality of blades 12 overlaps the plurality of blades 12 when viewed from the rotation axis direction. It is formed so that the outer peripheral edge of each wing 12 is connected. Therefore, when the airflow F (see FIG. 1) flowing into the impeller 1 from the axially opposite end plate 11 side of the impeller 1 is blown out from the inside of the impeller 1 to the outer peripheral side, the conventional intermediate ring In contrast, the intermediate ring 14 can suppress an increase in draft resistance. Moreover, the resin impregnation of the entire impeller 1 including the intermediate ring 14 is possible.
  • the impeller 1 of the multiblade blower of the present embodiment including the suppression of the increase in ventilation resistance when blown from the inside of the impeller 1 to the outer peripheral side and the intermediate ring 14 is included.
  • the entire High-speed rotation can be realized while making the resin integral molding possible.
  • the intermediate ring 14 is directed toward the opposite end plate 11 side end of the blade 12 with respect to the end plate 11 side end of the blade 12. From the position corresponding to 1/4 of the blade length L1 from the end plate 11 side end to the end plate 11 side end of the end plate to the position corresponding to 3/4 times the blade length L1 Since it is formed so as to be included in the range, the deformation of the impeller 1 can be effectively suppressed.
  • the cross-sectional shape of the intermediate ring 14 is a substantially rectangular shape in which the length L2 in the rotation axis direction is 1/2 or more of the projection length W from the outer peripheral edge of the blade 12. Since the intermediate ring 14 has a sufficient thickness in the rotational axis direction, deformation of the impeller 1 can be effectively suppressed.
  • one intermediate ring 14 is formed between the end plate 11 side end of the wing 12 and the opposite end plate 11 side end of the wing 12! /, But a plurality of intermediate rings are formed. In addition, the amount of deformation of the impeller caused by centrifugal force may be further reduced.
  • two intermediate rings 15 can be formed between an end plate 11 side end of the blade 12 and an end plate 11 side end of the blade 12.
  • at least a part of the blades 12 of each intermediate ring 15 is provided so that deformation of the impeller 1 can be effectively suppressed.
  • the blade length from the end plate 11 side end of the blade 12 to the anti-end plate 11 side end is 1/4 times longer than the end plate 11 side end of the blade 12 toward the anti-end plate 11 side end of the blade 12 It is desirable to form it within the range from the position corresponding to the height to the position corresponding to 3/4 times the blade length L1.
  • the pitch P between the two intermediate rings 15 formed between the end 12 of the blade 12 on the side of the end plate 11 and the end of the blade 12 on the side of the end plate 11 is 1/4 times the length L1 of the blade.
  • the deformation of the impeller 1 can be more effectively suppressed by setting it within the range of 3/4 times the blade length.
  • the impeller 1 of the multiblade blower of this modification it corresponds to the formation position of the intermediate ring 15 in the molds (molds 6 and 7 shown in FIGS. 2 and 3) that are pulled out in the radial direction.
  • the cross-sectional shape of the intermediate rings 14 and 15 is substantially rectangular.
  • a mold the mold shown in FIGS. 2 and 3
  • intermediate rings with various cross-sectional shapes can be used.
  • the cross-sectional shape of the intermediate rings 14 and 15 may be substantially L-shaped so as to have a sufficient thickness in the rotational axis direction.
  • the intermediate rings 14 and 15 have portions 14a and 15a extending in the rotation axis direction, and portions 14b and 15b projecting toward the outer peripheral side in the radial direction from the portions 14a and 15a.
  • the force that passes through the impeller 1 It is desirable to form the parts 14b and 15b so that they are placed on the end plate 11 side so that the airflow F can flow smoothly.
  • the cross-sectional shape of the intermediate rings 14 and 15 may be substantially trapezoidal so as to have a sufficient thickness in the direction of the rotation axis.
  • the intermediate rings 14 and 15 are directed to the radially outer peripheral side of the blade 12, and the force formed so that the thickness in the rotational axis direction decreases accordingly.
  • the surface on the side opposite to the end ring 11 is inclined toward the end ring 11 side as it is directed toward the radially outer peripheral side of the blade 12. It is desirable to form.
  • the present invention is applied to the impeller of a single-suction type multi-blade fan, which explains an example in which the present invention is applied to the impeller of a double-suction type multi-blade fan
  • the invention may be applied.
  • an impeller 101 of a multiblade blower that includes an end plate 11, a plurality of blades 12, and an end ring 13, and is driven to rotate by a motor 2, the end plate 11 1
  • the blade 12 can be connected to the blade 12 from the end plate 11 side end similarly to the above-described embodiment.
  • a configuration in which one intermediate ring 14 is formed between the end plate 11 and the end of the end plate 11 is possible.
  • the specific shape of the mold is different from the above-described embodiment and its modifications.
  • the impeller 101 of the multi-blade fan of the configuration as in the above-described embodiment and its modified examples, the impeller including the intermediate ring is used by using the die that is extracted in the rotational axis direction and the die that is extracted in the radial direction.
  • the resin 101 can be integrally molded.
  • each of the plurality of blades 12 is provided with the end plate 11 and the other end is connected with the end ring 13, and the intermediate rings 14 and 15 are provided.
  • the present invention is not limited to this, and the intermediate rings 14 and 15 may be provided in a configuration in which each other end is not connected by the end ring 13.

Abstract

An impeller for a multi-blade fan, in which increase in resistance of the flow of air ejected from the inside to the outer peripheral side of the impeller is suppressed as far as possible and that is integrally formed of a resin to realize high speed rotation of the impeller. The impeller (1) is an impeller for a multi-blade fan for sucking gas from the direction of the rotating shaft and ejecting it to the direction crossing the rotating shaft. The impeller (1) has a substantially circular end plate (11) rotating about the rotating shaft (3) and one or more intermediate rings (14). The blades (12) are annularly arranged about the rotating shaft (3), on one side or both sides of the end plate (11), and one end of each blade is on the outer peripheral section of the end plate (11). The intermediate rings (14) are formed such that, at those positions of the blades (12) that are other than ends on the side opposite the end plate (11), they are not superposed on the blades (12) when viewed in the direction of the rotating shaft and that they connect the outer peripheral edges of the blades (12).

Description

明 細 書  Specification
多翼送風機の羽根車  Impeller of multiblade blower
技術分野  Technical field
[0001] 本発明は、多翼送風機の羽根車、特に、回転軸方向から気体を吸入して回転軸に 交差する方向に気体を吹き出す多翼送風機の羽根車に関する。  TECHNICAL FIELD [0001] The present invention relates to an impeller of a multiblade blower, and more particularly to an impeller of a multiblade blower that sucks gas from a rotation axis direction and blows out gas in a direction crossing the rotation axis.
背景技術  Background art
[0002] 空気清浄機やエアコン等においては、送風を行うために、回転軸方向から気体を 吸入して回転軸に交差する方向に気体を吹き出す多翼送風機がよく用いられている 。このような多翼送風機の羽根車は、主として、回転軸を中心として回転する略円形 のエンドプレートと、エンドプレートに回転軸を中心として環状に配置されており各一 端が主板の外周部に設けられる複数の翼と、複数の翼の他端を結ぶエンドリングとを 備えている。  In air cleaners, air conditioners, and the like, a multiblade blower that draws gas in the direction of the rotation axis and blows out gas in a direction that intersects the rotation axis is often used in order to blow air. Such an impeller of a multiblade blower is mainly arranged in a substantially circular end plate that rotates about a rotation axis, and is annularly arranged on the end plate with the rotation axis as the center, and each end is disposed on the outer periphery of the main plate. A plurality of wings provided and an end ring connecting the other ends of the plurality of wings are provided.
また、このような多翼送風機の羽根車において、エンドプレートとエンドリングと回転 軸方向間に中間リングをさらに設けたものもある(特許文献 1参照。)。  In addition, in such an impeller of a multiblade blower, there is an impeller further provided with an intermediate ring between the end plate, the end ring, and the rotation axis direction (see Patent Document 1).
特許文献 1 :特開 2000— 320490号公報  Patent Document 1: JP 2000-320490 A
発明の開示  Disclosure of the invention
[0003] 上述の多翼送風機の羽根車において、羽根車の小型化や送風能力の向上等を実 現するために、羽根車を高速回転させて使用することが望まれている。  [0003] In the above-described impeller of a multiblade blower, it is desired to use the impeller while rotating the impeller at high speed in order to realize downsizing of the impeller and improvement of the blowing capability.
しかし、上述の前者の多翼送風機の羽根車を高速回転させると、羽根車にかかる 遠心力が大きくなり、羽根車の同心度が保つことができなくなり、また、偏バランス量 が大きくなるため、羽根車が大きく変形し、破損するおそれがある。  However, if the impeller of the former multiblade fan is rotated at a high speed, the centrifugal force applied to the impeller increases, the concentricity of the impeller cannot be maintained, and the amount of uneven balance increases. The impeller may be greatly deformed and damaged.
これに対して、上述の後者の多翼送風機の羽根車においては、中間リングが設けら れているため、上述の前者の多翼送風機の羽根車に比べて、遠心力による羽根車 の変形量が小さくなり、高速回転化が可能となる。しかし、この羽根車において設けら れている中間リングは、翼の外周縁から内周縁の位置にわたって設けられていること から、羽根車の内部から外周側に吹き出される際の通風抵抗が大きくなるという問題 力 る。また、この羽根車を樹脂製品として製造する場合においては、中間リングが 翼の外周縁から内周縁の位置にわたって設けられていることから、樹脂一体成形す ることが困難であり、クロスフローファンの羽根車と同様に、羽根車を中間リングの位 置で回転軸方向エンドリング側の部分と回転軸方向エンドプレート側の部分とに分割 する等して樹脂成形し、これらの複数の部分を超音波溶着により接合する等によって 製造する必要があるため、羽根車の製造に手間力 Sかかるという問題がある。 On the other hand, the latter impeller of the latter multi-blade fan is provided with an intermediate ring, so that the amount of deformation of the impeller due to centrifugal force is larger than that of the former impeller of the multi-blade fan. Becomes smaller and high speed rotation is possible. However, since the intermediate ring provided in this impeller is provided from the outer peripheral edge to the inner peripheral edge of the blade, the ventilation resistance when blowing from the inside of the impeller to the outer peripheral side increases. The problem power. When manufacturing this impeller as a resin product, the intermediate ring Since it is provided from the outer peripheral edge to the inner peripheral edge of the blade, it is difficult to mold the resin integrally, and like the impeller of the cross flow fan, the impeller is positioned in the direction of the rotation axis at the position of the intermediate ring. Since it is necessary to mold the resin by dividing it into a part on the end ring side and a part on the end plate side in the rotation axis direction, and joining these parts by ultrasonic welding, etc. There is a problem that it takes time and effort S
本発明の課題は、多翼送風機の羽根車において、羽根車の内部から外周側に吹 き出される際の通風抵抗の増加を極力抑え、かつ、樹脂一体成形が可能な形で、高 速回転化を実現することにある。  The problem of the present invention is that the impeller of a multiblade blower suppresses an increase in ventilation resistance when blown from the inside of the impeller to the outer peripheral side as much as possible, and can be integrally molded with a high-speed rotation. It is to realize.
[0004] 第 1の発明に力、かる多翼送風機の羽根車は、回転軸方向から気体を吸入して回転 軸に交差する方向に気体を吹き出す多翼送風機の羽根車であって、回転軸を中心 として回転する略円形のエンドプレートと、複数の翼と、 1以上の中間リングとを備え ている。複数の翼は、エンドプレートの片面又は両面に回転軸を中心として環状に配 置されており、各一端がエンドプレートの外周部に設けられている。中間リングは、複 数の翼の反エンドプレート側端以外の位置にお!/、て、回転軸方向から見た際に複数 の翼に重ならないように、かつ、各翼の外周縁を結ぶように形成されている。 [0004] An impeller of a multiblade blower that is the power of the first invention is an impeller of a multiblade blower that sucks gas from the direction of the rotation axis and blows out gas in a direction intersecting the rotation axis. A substantially circular end plate that rotates about the center, a plurality of blades, and one or more intermediate rings. The plurality of blades are annularly arranged on one or both sides of the end plate with the rotation axis as the center, and one end is provided on the outer periphery of the end plate. The intermediate ring is located at a position other than the end on the side opposite to the end plate of the plurality of blades! / And connects the outer peripheral edges of the blades so that they do not overlap with the blades when viewed from the rotation axis direction. It is formed as follows.
この多翼送風機の羽根車では、複数の翼の反エンドプレート側端以外の位置に設 けられた中間リング力 回転軸方向から見た際に複数の翼に重ならないように、かつ 、各翼の外周縁を結ぶように形成されているため、羽根車の内部から外周側に吹き 出される際の通風抵抗の増加の抑制や中間リングを含めた羽根車全体の樹脂一体 成形を可能にしつつ、高速回転化を実現することができる。  In the impeller of this multiblade blower, the intermediate ring force provided at a position other than the end on the side opposite to the end plate side of the plurality of blades so that the blades do not overlap with each other when viewed from the direction of the rotation axis. The outer peripheral edge of the impeller is formed so that the increase in ventilation resistance when blown from the inside of the impeller to the outer peripheral side and the resin impregnation of the entire impeller including the intermediate ring are possible, High speed rotation can be realized.
[0005] 第 2の発明に力、かる多翼送風機の羽根車は、第 1の発明に力、かる多翼送風機の羽 根車において、中間リングの少なくとも一部は、翼のエンドプレート側端を基準として 、翼の反エンドプレート側端に向かって、翼のエンドプレート側端から反エンドプレー ト側端までの翼長さの 1/4倍の長さに対応する位置から翼長さの 3/4倍の長さに 対応する位置までの範囲内に含まれるように形成されて!/、る。 [0005] The impeller of the multi-blade fan that is powerful in the second invention is the impeller of the multi-blade fan that is powerful in the first invention. At least a part of the intermediate ring is at the end plate side end of the blade. From the position corresponding to 1/4 times the blade length from the end plate side end of the blade to the end plate side end toward the end of the blade opposite to the end plate side. It is formed so as to be included in the range up to the position corresponding to 3/4 times the length!
この多翼送風機の羽根車では、中間リングの少なくとも一部が、翼のエンドプレート 側端を基準として、翼の反エンドプレート側端に向かって、翼のエンドプレート側端か ら反エンドプレート側端までの翼長さの 1/4倍の長さに対応する位置から翼長さの 3 /4倍の長さに対応する位置までの範囲内に含まれるように形成されているため、羽 根車の変形を効果的に抑えることができる。 In the impeller of this multiblade blower, at least a part of the intermediate ring is directed from the end plate side end of the blade toward the end plate side of the blade toward the end end side of the blade from the end plate side of the blade. From the position corresponding to 1/4 times the blade length to the end, the blade length 3 Because it is formed so as to be included in a range up to a position corresponding to / 4 times the length, deformation of the vane wheel can be effectively suppressed.
[0006] 第 3の発明に力、かる多翼送風機の羽根車は、第 2の発明に力、かる多翼送風機の羽 根車において、中間リングは、翼のエンドプレート側端と反エンドプレート側端との間 に 2つ形成されており、中間リング間のピッチは、翼長さの 1/4倍の長さから翼長さ の 3/4倍の長さの範囲内に設定されている。 [0006] The impeller of the multi-blade fan, which is the power of the third invention, is the blade wheel of the multi-blade fan, the power of the second invention, the intermediate ring is the end plate side end of the blade and the anti-end plate Two pitches are formed between the side edges, and the pitch between the intermediate rings is set within the range of 1/4 times the blade length to 3/4 times the blade length. Yes.
この多翼送風機の羽根車では、翼のエンドプレート側端と反エンドプレート側端との 間に中間リング力 ¾つ設けられる場合において、中間リング間のピッチが、翼長さの 1 In the impeller of this multiblade blower, when an intermediate ring force is provided between the end plate side end and the opposite end plate side end of the blade, the pitch between the intermediate rings is 1 of the blade length.
/4倍の長さから翼長さの 3/4倍の長さの範囲内に設定されているため、羽根車の 変形を効果的に抑えることができる。 Since it is set within the range of / 4 times the length to 3/4 times the blade length, the deformation of the impeller can be effectively suppressed.
[0007] 第 4の発明に力、かる多翼送風機の羽根車は、第 1〜第 3の発明のいずれかにかか る多翼送風機の羽根車において、中間リングの断面形状は、回転軸方向の長さが翼 の外周縁からの突出長さの 1/2倍以上の略長方形状である。 [0007] The impeller of the multi-blade fan according to the fourth invention is the impeller of the multi-blade fan according to any of the first to third inventions, wherein the cross-sectional shape of the intermediate ring is the rotational axis. The length in the direction is approximately rectangular, which is more than 1/2 the length of protrusion from the outer periphery of the wing.
この多翼送風機の羽根車では、中間リングの断面形状を、回転軸方向の長さが翼 の外周縁からの突出長さの 1/2倍以上の略長方形状としており、中間リングに十分 な回転軸方向の厚みを持たしているため、羽根車の変形を効果的に抑えることがで きる。  In the impeller of this multiblade blower, the cross-sectional shape of the intermediate ring is a substantially rectangular shape whose length in the rotation axis direction is 1/2 or more of the protruding length from the outer peripheral edge of the blade, which is sufficient for the intermediate ring. Since it has a thickness in the direction of the rotation axis, deformation of the impeller can be effectively suppressed.
[0008] 第 5の発明に力、かる多翼送風機の羽根車は、第 1〜第 3の発明のいずれかにかか る多翼送風機の羽根車において、中間リングの断面形状は、略 L字形状である。 この多翼送風機の羽根車では、中間リングの断面形状を略 L形状としており、中間 リングに十分な回転軸方向の厚みを持たしているため、羽根車の変形を効果的に抑 えること力 Sできる。  [0008] The impeller of the multiblade fan according to the fifth invention is the impeller of the multiblade fan according to any of the first to third inventions, wherein the cross-sectional shape of the intermediate ring is substantially L It is a letter shape. In the impeller of this multiblade blower, the cross-sectional shape of the intermediate ring is substantially L-shaped, and the intermediate ring has a sufficient thickness in the direction of the rotation axis, which effectively suppresses the deformation of the impeller. S can.
[0009] 第 6の発明に力、かる多翼送風機の羽根車は、第 1〜第 3の発明のいずれかにかか る多翼送風機の羽根車において、中間リングの断面形状は、略台形形状である。 この多翼送風機の羽根車では、中間リングの断面形状を略台形形状としており、中 間リングに十分な回転軸方向の厚みを持たしているため、羽根車の変形を効果的に 才卬えること力 Sできる。  [0009] The impeller of the multiblade fan according to the sixth invention is the impeller of the multiblade fan according to any of the first to third inventions, wherein the cross-sectional shape of the intermediate ring is substantially trapezoidal. Shape. In this impeller of a multiblade blower, the cross-sectional shape of the intermediate ring has a substantially trapezoidal shape, and the intermediate ring has a sufficient thickness in the direction of the rotation axis, so that it can effectively recognize the deformation of the impeller. That power S.
図面の簡単な説明 [0010] [図 1]本発明の一実施形態に力、かる多翼送風機の羽根車の径方向断面図である。 Brief Description of Drawings FIG. 1 is a radial cross-sectional view of an impeller of a multiblade blower that is effective in an embodiment of the present invention.
[図 2]多翼送風機の羽根車の径方向断面図と、この断面図に対応する部分の金型の 形状を示す図である。  FIG. 2 is a radial cross-sectional view of an impeller of a multiblade fan and a shape of a mold corresponding to the cross-sectional view.
[図 3]多翼送風機の羽根車の平面図と、この平面図に対応する部分の金型の形状を 示す図である。  FIG. 3 is a plan view of an impeller of a multiblade fan and a shape of a mold corresponding to the plan view.
[図 4]変形例 1にかかる多翼送風機の羽根車の径方向断面図である。  FIG. 4 is a radial sectional view of an impeller of a multiblade fan according to Modification 1.
[図 5]変形例 2にかかる多翼送風機の羽根車の径方向断面図であって、中間リング付 近を示す図である。  FIG. 5 is a radial cross-sectional view of an impeller of a multiblade fan according to Modification 2, showing the vicinity of an intermediate ring.
[図 6]変形例 2にかかる多翼送風機の羽根車の径方向断面図であって、中間リング付 近を示す図である。  FIG. 6 is a radial cross-sectional view of an impeller of a multiblade fan according to Modification 2, showing the vicinity of an intermediate ring.
[図 7]他の実施形態に力、かる多翼送風機の羽根車の径方向断面図である。  FIG. 7 is a radial cross-sectional view of an impeller of a multi-blade blower that focuses on another embodiment.
符号の説明  Explanation of symbols
[0011] 1、 101 多翼送風機の羽根車 [0011] 1, 101 Impeller of multi-blade fan
11 エンドプレート  11 End plate
12 翼  12 wings
14、 15 中間リング  14, 15 Intermediate ring
発明を実施するための最良の形態  BEST MODE FOR CARRYING OUT THE INVENTION
[0012] 以下、図面に基づいて、本発明にかかる多翼送風機の羽根車の実施形態につい て説明する。 Hereinafter, an embodiment of an impeller of a multiblade blower according to the present invention will be described based on the drawings.
(1)多翼送風機の羽根車の構成  (1) Configuration of impeller of multiblade fan
図 1に、本発明の一実施形態にかかる多翼送風機の羽根車 1を示す。ここで、図 1 は、多翼送風機の羽根車 1の径方向断面図である。  FIG. 1 shows an impeller 1 of a multiblade blower according to an embodiment of the present invention. Here, FIG. 1 is a radial sectional view of the impeller 1 of the multiblade fan.
羽根車 1は、回転軸方向両側から気体を吸入して回転軸に交差する方向に気体を 吹き出す両吸込タイプの多翼送風機の羽根車であり、モータ 2によって回転駆動され るようになっている。ここで、図中の O— Oは、羽根車 1及びモータ 2の回転軸線であ る。羽根車 1は、後述のように、金型を用いて一体成形される樹脂製品であり、主とし て、エンドプレート 11と、複数の翼 12と、ユンドリング 13と、 1以上の中間リング 14とを 備えている。 [0013] エンドプレート 11は、モータ 2の回転軸 3を中心として回転する略円形の部分であり 、回転軸 3が連結される中心孔 11aが形成されている。 Impeller 1 is an impeller of a double-suction type multi-blade fan that sucks gas from both sides of the rotation axis and blows gas in a direction crossing the rotation axis, and is driven to rotate by motor 2. . Here, OO in the figure is the rotational axis of the impeller 1 and the motor 2. As will be described later, the impeller 1 is a resin product that is integrally molded using a mold, and mainly includes an end plate 11, a plurality of blades 12, a undling ring 13, and one or more intermediate rings 14. It is equipped with. The end plate 11 is a substantially circular portion that rotates about the rotation shaft 3 of the motor 2, and a center hole 11 a to which the rotation shaft 3 is coupled is formed.
複数の翼 12は、エンドプレート 11の両面に回転軸 3を中心として環状に配置されて おり、各一端がエンドプレート 11の外周部に配置され、そこから回転軸方向両側に 向かってねじれなく延びて!/、る。  The plurality of blades 12 are annularly arranged on both surfaces of the end plate 11 with the rotation shaft 3 as the center, and each end is disposed on the outer periphery of the end plate 11 and extends without twisting toward both sides in the rotation axis direction. /!
エンドリング 13は、翼の他端 (すなわち、反エンドプレート 11側端)の位置において 、各翼 12の反エンドプレート 11側端の外周縁を結ぶ環状の部分であり、本実施形態 において、エンドプレート 11の回転軸方向両側に配置されている。エンドリング 13は 、回転軸方向から見た際に、複数の翼 12に重ならないように形成されている。  The end ring 13 is an annular portion connecting the outer peripheral edges of the opposite end plate 11 side ends of the blades 12 at the position of the other end of the blade (that is, the opposite end plate 11 side end). It is arranged on both sides of the plate 11 in the rotation axis direction. The end ring 13 is formed so as not to overlap the plurality of blades 12 when viewed from the rotation axis direction.
中間リング 14は、複数の翼 12の反エンドプレート 11側端以外の位置において、回 転軸方向から見た際に複数の翼 12に重ならないように、かつ、各翼 12の外周縁を結 ぶように形成された環状の部分であり、本実施形態において、エンドプレート 11の回 転軸方向両側に配置されている。また、各中間リング 14の少なくとも一部は、翼 12の エンドプレート 11側端を基準として、翼 12の反エンドプレート 11側端に向かって、翼 12のエンドプレート 11側端から反エンドプレート 11側端までの翼長さ(以下、この長 さを翼長さ L1とする)の 1 /4倍の長さに対応する位置から翼長さ L1の 3/4倍の長さ に対応する位置までの範囲内に含まれるように形成されている。さらに、各中間リング 14の断面形状は、回転軸方向の長さ L2が翼 12の外周縁からの突出長さ Wの 1/2 倍以上の略長方形状である。尚、本実施形態において、各中間リング 14は、翼 12の エンドプレート 11側端を基準として、翼 12の反エンドプレート 11側端に向かって、翼 長さ L1のほぼ 1/2倍の長さに対応する位置に形成されており、回転軸方向の長さ L 2が突出長さ Wとほぼ同じの長さの略長方形状 (すなわち、略正方形状)の断面形状 を有している。  The intermediate ring 14 is connected to the outer peripheral edge of each blade 12 so that it does not overlap with the plurality of blades 12 when viewed from the rotational axis direction at a position other than the end on the side opposite to the end plate 11 of the plurality of blades 12. In the present embodiment, the annular portion is disposed on both sides of the end plate 11 in the rotation axis direction. Further, at least a part of each intermediate ring 14 is directed from the end plate 11 side end of the blade 12 toward the anti-end plate 11 side end of the blade 12 from the end plate 11 side end of the blade 12 as a reference. A position corresponding to a quarter length of the blade length L1 from a position corresponding to a quarter length of the blade length to the side edge (hereinafter referred to as the blade length L1). It is formed to be included in the range up to. Further, the cross-sectional shape of each intermediate ring 14 is a substantially rectangular shape in which the length L2 in the rotation axis direction is 1/2 or more of the protruding length W from the outer peripheral edge of the blade 12. In the present embodiment, each intermediate ring 14 is approximately 1/2 times the blade length L1 from the end 12 side end of the blade 12 toward the opposite end plate 11 side end of the blade 12. The length L 2 in the direction of the rotation axis has a substantially rectangular (that is, substantially square) cross-sectional shape having a length substantially the same as the protruding length W.
[0014] (2)多翼送風機の羽根車の成形  [0014] (2) Molding of impeller of multiblade fan
次に、本実施形態の多翼送風機の羽根車 1の成形について、図 2及び図 3を用い て説明する。ここで、図 2は、多翼送風機の羽根車 1の径方向断面図と、この断面図 に対応する部分の金型 4、 5、 6、 7の形状を示す図である。図 3は、多翼送風機の羽 根車 1の平面図と、この平面図に対応する部分の金型 4、 6、 7の形状を示す図である 羽根車 1は、 2対の金型 4、 5及び金型 6、 7を用いて樹脂一体成形して形作るもの である。 Next, molding of the impeller 1 of the multiblade fan according to the present embodiment will be described with reference to FIGS. Here, FIG. 2 is a diagram showing the radial cross-sectional view of the impeller 1 of the multiblade fan and the shapes of the molds 4, 5, 6, and 7 corresponding to the cross-sectional view. FIG. 3 is a plan view of the bladed wheel 1 of the multiblade fan and the shapes of the molds 4, 6, and 7 corresponding to the plan view. The impeller 1 is formed by integrally molding resin using two pairs of molds 4 and 5 and molds 6 and 7.
金型 4、 5は、回転軸方向に合わさった際に、金型 4のエンドプレート形成部 4a及び 金型 5のエンドプレート形成部 5aが中心孔 11aを含むエンドプレート 11 (但し、径方 向外周縁を除く)を形作り、金型 4、 5の翼形成部 4b、 5bが翼 12 (但し、径方向外周 縁を除く)を形作り、金型 4、 5の外周縁形成部 4c、 5c (但し、外周縁形成部 5cの図 示は省略)がエンドリング 13の径方向内周縁及び中間リング 14の径方向内周縁を形 作る。  When the molds 4 and 5 are aligned in the rotation axis direction, the end plate forming portion 4a of the mold 4 and the end plate forming portion 5a of the mold 5 include the end plate 11 including the center hole 11a (however, the radial direction The outer rim forming portions 4c and 5c of the dies 4 and 5 are formed by forming the wing forming portions 4b and 5b of the dies 4 and 5 into the wing 12 (excluding the outer peripheral edge in the radial direction). However, the illustration of the outer peripheral edge forming portion 5c is omitted) forms the radial inner peripheral edge of the end ring 13 and the radial inner peripheral edge of the intermediate ring 14.
[0015] また、金型 6、 7は、回転軸線 O— Oに直交する方向(すなわち、径方向)に合わさつ た際に、外周縁形成部 6a、 7aがエンドプレート 11の径方向外周縁及び翼 12の径方 向外周縁を形作り、エンドリング形成部 6b、 7bがエンドリング 13 (但し、エンドリング 1 3の径方向内周縁を除く)を形作り、中間リング形成部 6c、 7cが中間リング 14 (但し、 中間リング 14の径方向内周縁を除く)を形作る。  In addition, when the molds 6 and 7 are aligned in a direction orthogonal to the rotation axis O—O (ie, in the radial direction), the outer peripheral edge forming portions 6 a and 7 a are in the radial outer peripheral edge of the end plate 11. And the outer peripheral edge of the blade 12 in the radial direction, the end ring forming parts 6b and 7b form the end ring 13 (excluding the inner peripheral edge of the end ring 13 in the radial direction), and the intermediate ring forming parts 6c and 7c are in the middle Form a ring 14 (except for the radially inner edge of the intermediate ring 14).
このように、本実施形態の多翼送風機の羽根車 1は、回転軸方向に金型 4、 5を抜 き、径方向に金型 6、 7を抜くことによって樹脂一体成形することが可能である。  Thus, the impeller 1 of the multiblade fan of the present embodiment can be integrally molded with resin by removing the dies 4 and 5 in the rotational axis direction and dies 6 and 7 in the radial direction. is there.
(3)本実施形態の多翼送風機の羽根車の特徴  (3) Features of the impeller of the multiblade fan of this embodiment
本実施形態の多翼送風機の羽根車 1には、以下のような特徴がある。  The impeller 1 of the multiblade fan of the present embodiment has the following characteristics.
(A)  (A)
本実施形態の多翼送風機の羽根車 1では、複数の翼 12の反エンドプレート 11側 端以外の位置に設けられた中間リング 14が、回転軸方向から見た際に複数の翼 12 に重ならないように、かつ、各翼 12の外周縁を結ぶように形成されている。このため、 羽根車 1の軸方向反エンドプレート 11側から羽根車 1の内部に流入する気流 F (図 1 参照)が羽根車 1の内部から外周側に吹き出される際において、従来の中間リングと 比べて、中間リング 14によって通風抵抗が増加するのを抑えることができる。しかも、 中間リング 14を含めた羽根車 1全体の樹脂一体成形が可能である。  In the impeller 1 of the multiblade blower of the present embodiment, the intermediate ring 14 provided at a position other than the side end of the anti-end plate 11 of the plurality of blades 12 overlaps the plurality of blades 12 when viewed from the rotation axis direction. It is formed so that the outer peripheral edge of each wing 12 is connected. Therefore, when the airflow F (see FIG. 1) flowing into the impeller 1 from the axially opposite end plate 11 side of the impeller 1 is blown out from the inside of the impeller 1 to the outer peripheral side, the conventional intermediate ring In contrast, the intermediate ring 14 can suppress an increase in draft resistance. Moreover, the resin impregnation of the entire impeller 1 including the intermediate ring 14 is possible.
[0016] このように、本実施形態の多翼送風機の羽根車 1では、羽根車 1の内部から外周側 に吹き出される際の通風抵抗の増加の抑制や中間リング 14を含めた羽根車 1全体 の樹脂一体成形を可能にしつつ、高速回転化を実現することができる。 [0016] Thus, in the impeller 1 of the multiblade blower of the present embodiment, the impeller 1 including the suppression of the increase in ventilation resistance when blown from the inside of the impeller 1 to the outer peripheral side and the intermediate ring 14 is included. The entire High-speed rotation can be realized while making the resin integral molding possible.
(B)  (B)
本実施形態の多翼送風機の羽根車 1では、中間リング 14の少なくとも一部が、翼 1 2のエンドプレート 11側端を基準として、翼 12の反エンドプレート 11側端に向かって 、翼 12のエンドプレート 11側端から反エンドプレート 11側端までの翼長さ L1の 1/4 倍の長さに対応する位置から翼長さ L1の 3/4倍の長さに対応する位置までの範囲 内に含まれるように形成されているため、羽根車 1の変形を効果的に抑えることがで きる。  In the impeller 1 of the multiblade fan according to the present embodiment, at least a part of the intermediate ring 14 is directed toward the opposite end plate 11 side end of the blade 12 with respect to the end plate 11 side end of the blade 12. From the position corresponding to 1/4 of the blade length L1 from the end plate 11 side end to the end plate 11 side end of the end plate to the position corresponding to 3/4 times the blade length L1 Since it is formed so as to be included in the range, the deformation of the impeller 1 can be effectively suppressed.
(C)  (C)
本実施形態の多翼送風機の羽根車 1では、中間リング 14の断面形状を、回転軸方 向の長さ L2が翼 12の外周縁からの突出長さ Wの 1/2倍以上の略長方形状として おり、中間リング 14に十分な回転軸方向の厚みを持たしているため、羽根車 1の変 形を効果的に抑えることができる。  In the impeller 1 of the multiblade blower of the present embodiment, the cross-sectional shape of the intermediate ring 14 is a substantially rectangular shape in which the length L2 in the rotation axis direction is 1/2 or more of the projection length W from the outer peripheral edge of the blade 12. Since the intermediate ring 14 has a sufficient thickness in the rotational axis direction, deformation of the impeller 1 can be effectively suppressed.
(4)変形例 1  (4) Modification 1
上述の実施形態においては、中間リング 14を、翼 12のエンドプレート 11側端から 翼 12の反エンドプレート 11側端までの間に 1つ形成して!/、るが、中間リングを複数形 成して、さらに、遠心力による羽根車の変形量を小さくするようにしてもよい。  In the above-described embodiment, one intermediate ring 14 is formed between the end plate 11 side end of the wing 12 and the opposite end plate 11 side end of the wing 12! /, But a plurality of intermediate rings are formed. In addition, the amount of deformation of the impeller caused by centrifugal force may be further reduced.
例えば、図 4に示されるように、中間リング 15を、翼 12のエンドプレート 11側端から 翼 12の反エンドプレート 11側端までの間に 2つ形成することができる。また、この場 合において、各中間リング 15については、上述の実施形態と同様、羽根車 1の変形 を効果的に抑えることができるように、各中間リング 15の少なくとも一部力 翼 12のェ ンドプレート 11側端を基準として、翼 12の反エンドプレート 11側端に向かって、翼 12 のエンドプレート 11側端から反エンドプレート 11側端までの翼長さ L1の 1/4倍の長 さに対応する位置から翼長さ L1の 3/4倍の長さに対応する位置までの範囲内に含 まれるように形成することが望ましい。また、翼 12のエンドプレート 11側端から翼 12 の反エンドプレート 11側端までの間に形成された 2つの中間リング 15間のピッチ Pを 、翼長さ L1の 1/4倍の長さから翼長さの 3/4倍の長さの範囲内に設定することで、 羽根車 1の変形をさらに効果的に抑えることができる。 [0018] また、本変形例の多翼送風機の羽根車 1においても、径方向に抜く金型(図 2及び 図 3に示される金型 6、 7)に中間リング 15の形成位置に対応するように中間リング形 成部を設けることで、上述の実施形態と同様に、羽根車 1全体の樹脂一体成形が可 能である。 For example, as shown in FIG. 4, two intermediate rings 15 can be formed between an end plate 11 side end of the blade 12 and an end plate 11 side end of the blade 12. Further, in this case, for each intermediate ring 15, as in the above-described embodiment, at least a part of the blades 12 of each intermediate ring 15 is provided so that deformation of the impeller 1 can be effectively suppressed. The blade length from the end plate 11 side end of the blade 12 to the anti-end plate 11 side end is 1/4 times longer than the end plate 11 side end of the blade 12 toward the anti-end plate 11 side end of the blade 12 It is desirable to form it within the range from the position corresponding to the height to the position corresponding to 3/4 times the blade length L1. Also, the pitch P between the two intermediate rings 15 formed between the end 12 of the blade 12 on the side of the end plate 11 and the end of the blade 12 on the side of the end plate 11 is 1/4 times the length L1 of the blade. The deformation of the impeller 1 can be more effectively suppressed by setting it within the range of 3/4 times the blade length. [0018] Also, in the impeller 1 of the multiblade blower of this modification, it corresponds to the formation position of the intermediate ring 15 in the molds (molds 6 and 7 shown in FIGS. 2 and 3) that are pulled out in the radial direction. By providing the intermediate ring forming portion in this way, resin impregnation of the entire impeller 1 is possible as in the above-described embodiment.
(5)変形例 2  (5) Modification 2
上述の実施形態及び変形例 1においては、中間リング 14、 15の断面形状が略長 方形状であるが、羽根車を樹脂一体成形する際に、金型(図 2及び図 3に示される金 型 6、 7)を径方向に抜くことが困難な断面形状でなければ、種々の断面形状を有す る中間リングを用いることが可能である。  In the above-described embodiment and Modification 1, the cross-sectional shape of the intermediate rings 14 and 15 is substantially rectangular. However, when the impeller is integrally molded with resin, a mold (the mold shown in FIGS. 2 and 3) is used. If it is difficult to remove the dies 6 and 7) in the radial direction, intermediate rings with various cross-sectional shapes can be used.
例えば、図 5に示されるように、中間リング 14、 15の断面形状を略 L字形状として、 十分な回転軸方向の厚みを持たせるようにしてもよい。また、この場合において、中 間リング 14、 15は、回転軸方向に延びる部分 14a、 15aと、部分 14a、 15aよりも径方 向外周側に向かって突出する部分 14b、 15bとを有している力 羽根車 1を通過する 気流 Fをスムーズに流すことができるように、部分 14b、 15bがエンドプレート 11側に 酉己置されるように形成することが望ましレ、。  For example, as shown in FIG. 5, the cross-sectional shape of the intermediate rings 14 and 15 may be substantially L-shaped so as to have a sufficient thickness in the rotational axis direction. Further, in this case, the intermediate rings 14 and 15 have portions 14a and 15a extending in the rotation axis direction, and portions 14b and 15b projecting toward the outer peripheral side in the radial direction from the portions 14a and 15a. The force that passes through the impeller 1 It is desirable to form the parts 14b and 15b so that they are placed on the end plate 11 side so that the airflow F can flow smoothly.
[0019] また、図 6に示されるように、中間リング 14、 15の断面形状を略台形形状として、十 分な回転軸方向の厚みを持たせるようにしてもよい。また、この場合において、中間リ ング 14、 15は、図 6に示されるように、翼 12の径方向外周側に向力、うにつれて回転 軸方向の厚みが小さくなるように形成されている力 羽根車 1を通過する気流 Fをスム ーズに流すことができるように、翼 12の径方向外周側に向力、うにつれて、反エンドリ ング 11側の面がエンドリング 11側に傾斜するように形成することが望ましい。 In addition, as shown in FIG. 6, the cross-sectional shape of the intermediate rings 14 and 15 may be substantially trapezoidal so as to have a sufficient thickness in the direction of the rotation axis. Further, in this case, as shown in FIG. 6, the intermediate rings 14 and 15 are directed to the radially outer peripheral side of the blade 12, and the force formed so that the thickness in the rotational axis direction decreases accordingly. In order to allow the air flow F passing through the impeller 1 to flow smoothly, the surface on the side opposite to the end ring 11 is inclined toward the end ring 11 side as it is directed toward the radially outer peripheral side of the blade 12. It is desirable to form.
(6)他の実施形態  (6) Other embodiments
以上、本発明の実施形態及びその変形例について図面に基づいて説明したが、 具体的な構成は、これらの実施形態及びその変形例に限られるものではなぐ発明 の要旨を逸脱しなレ、範囲で変更可能である。  As mentioned above, although embodiment of this invention and its modification were demonstrated based on drawing, specific structure is not restricted to these embodiment and its modification, the range which does not deviate from the summary of invention. Can be changed.
[0020] (A) [0020] (A)
上述の実施形態及びその変形例にお!/、ては、両吸込タイプの多翼送風機の羽根 車に本発明を適用した例を説明した力 片吸込タイプの多翼送風機の羽根車に本 発明を適用してもよい。 In the above-described embodiment and its modifications, the present invention is applied to the impeller of a single-suction type multi-blade fan, which explains an example in which the present invention is applied to the impeller of a double-suction type multi-blade fan The invention may be applied.
例えば、図 7に示されるように、エンドプレート 11と、複数の翼 12と、エンドリング 13 とを備えており、モータ 2によって回転駆動される多翼送風機の羽根車 101において 、エンドプレート 1 1とエンドリング 13との回転軸方向間に、上述の実施形態と同様の 中間リング 14を 1つ形成することで、上述の実施形態と同様に、翼 12のエンドプレー ト 11側端から翼 12の反エンドプレート 11側端までの間に 1つ中間リング 14が形成さ れた構成とすることができる。  For example, as shown in FIG. 7, in an impeller 101 of a multiblade blower that includes an end plate 11, a plurality of blades 12, and an end ring 13, and is driven to rotate by a motor 2, the end plate 11 1 By forming one intermediate ring 14 similar to that of the above-described embodiment between the rotation axis directions of the blade 12 and the end ring 13, the blade 12 can be connected to the blade 12 from the end plate 11 side end similarly to the above-described embodiment. A configuration in which one intermediate ring 14 is formed between the end plate 11 and the end of the end plate 11 is possible.
[0021] また、本実施形態の羽根車 101においては、中間リング 14を 1つ形成する構成だ けでなぐ上述の変形例 1と同様に、翼 12のエンドプレート 11側端から翼 12の反ェ ンドプレート 11側端までの間に 2つの中間リング 15が形成された構成としたり、上述 の変形例 2と同様に、翼 12のエンドプレート 11側端から翼 12の反エンドプレート 11 側端までの間に L字形状や台形形状の中間リング 14、 15が形成された構成とするこ と力 Sできる。 In addition, in the impeller 101 of the present embodiment, as in the above-described modification 1 in which only one intermediate ring 14 is formed, the end of the blade 12 opposite the end of the blade 12 is counteracted. Two intermediate rings 15 are formed between the end plate 11 and the end plate 11 side end, or in the same manner as in the above-described modified example 2, the blade 12 end plate 11 side end to the blade 12 counter end plate 11 side end In the meantime, it is possible to create a structure in which L-shaped or trapezoidal intermediate rings 14 and 15 are formed.
さらに、エンドプレート 11の片面のみに複数の翼 12の一端が設けられていることか ら、金型の具体的な形状が上述の実施形態及びその変形例とは異なることになるが 、本実施形態の多翼送風機の羽根車 101においても、上述の実施形態及びその変 形例と同様に、回転軸方向に抜く金型ゃ径方向に抜く金型を用いて、中間リングを 含めた羽根車 101全体の樹脂一体成形が可能である。  Furthermore, since one end of the plurality of blades 12 is provided only on one side of the end plate 11, the specific shape of the mold is different from the above-described embodiment and its modifications. In the impeller 101 of the multi-blade fan of the configuration, as in the above-described embodiment and its modified examples, the impeller including the intermediate ring is used by using the die that is extracted in the rotational axis direction and the die that is extracted in the radial direction. The resin 101 can be integrally molded.
[0022] (B) [0022] (B)
上述の実施形態及びその変形例においては、複数の翼 12の各一端がエンドプレ ート 11に設けられており、各他端がエンドリング 13で結ばれた構成に、中間リング 14 、 15を設けている力 これに限定されず、各他端がエンドリング 13で結ばれていない 構成に、中間リング 14、 15を設けてもよい。  In the above-described embodiment and its modification, each of the plurality of blades 12 is provided with the end plate 11 and the other end is connected with the end ring 13, and the intermediate rings 14 and 15 are provided. However, the present invention is not limited to this, and the intermediate rings 14 and 15 may be provided in a configuration in which each other end is not connected by the end ring 13.
産業上の利用可能性  Industrial applicability
[0023] 本発明を利用すれば、多翼送風機の羽根車において、羽根車の内部から外周側 に吹き出される際の通風抵抗の増加を極力抑え、かつ、樹脂一体成形が可能な形 で、高速回転化を実現することができる。 [0023] If the present invention is used, in an impeller of a multiblade blower, an increase in ventilation resistance when blown from the inside of the impeller to the outer peripheral side is suppressed as much as possible, and resin integral molding is possible. High speed rotation can be realized.

Claims

請求の範囲  The scope of the claims
回転軸方向から気体を吸入して前記回転軸に交差する方向に気体を吹き出す多 翼送風機の羽根車であって、  An impeller of a multi-blade blower that sucks gas from a rotation axis direction and blows out gas in a direction intersecting the rotation axis,
前記回転軸を中心として回転する略円形のエンドプレート(11)と、  A substantially circular end plate (11) rotating about the rotation axis;
前記エンドプレートの片面又は両面に前記回転軸を中心として環状に配置されて おり、各一端が前記エンドプレートの外周部に設けられる複数の翼(12)と、  A plurality of blades (12) disposed on one or both sides of the end plate in an annular shape around the rotation axis, each end being provided on the outer periphery of the end plate;
前記複数の翼の前記反エンドプレート側端以外の位置にお!/、て、前記回転軸方向 から見た際に前記複数の翼に重ならないように、かつ、前記各翼の外周縁を結ぶよう に形成された 1以上の中間リング(14、 15)と、  At a position other than the opposite end plate side edge of the plurality of blades, the outer peripheral edges of the blades are connected so as not to overlap the plurality of blades when viewed from the rotational axis direction. One or more intermediate rings (14, 15) formed as follows:
を備えた多翼送風機の羽根車(1、 101)。 Multi-blade fan impeller equipped with (1, 101).
前記中間リング(14、 15)の少なくとも一部は、前記翼(12)の前記エンドプレート側 端を基準として、前記翼(12)の前記反エンドプレート側端に向かって、前記翼の前 記エンドプレート側端から前記反エンドプレート側端までの翼長さ(L1)の 1/4倍の 長さに対応する位置から前記翼長さの 3/4倍の長さに対応する位置までの範囲内 に含まれるように形成されている、請求項 1に記載の多翼送風機の羽根車(1、 101) At least a part of the intermediate ring (14, 15) is directed toward the opposite end plate side end of the blade (12) with reference to the end plate side end of the blade (12). From a position corresponding to 1/4 times the blade length (L1) from the end plate side edge to the opposite end plate side edge to a position corresponding to 3/4 times the blade length The impeller (1, 101) of the multiblade fan according to claim 1, wherein the impeller (1, 101) is formed to be included in a range.
Yes
前記中間リング(14、 15)は、前記翼(12)の前記エンドプレート側端と前記反ェン ドプレート側端との間に 2つ形成されており、  Two intermediate rings (14, 15) are formed between the end plate side end and the end plate side end of the wing (12),
前記中間リング間のピッチ (P)は、前記翼長さ(L1)の 1/4倍の長さから前記翼長 さの 3/4倍の長さの範囲内に設定されている、  The pitch (P) between the intermediate rings is set within a range of 1/4 times the blade length (L1) to 3/4 times the blade length,
請求項 2に記載の多翼送風機の羽根車(1、 101)。 The impeller (1, 101) of the multiblade fan according to claim 2.
前記中間リング(14、 15)の断面形状は、前記回転軸方向の長さ(L2)が前記翼(1 2)の外周縁からの突出長さ (W)の 1/2倍以上の略長方形状である、請求項;!〜 3 のいずれかに記載の多翼送風機の羽根車(1、 101)。  The cross-sectional shape of the intermediate ring (14, 15) is a substantially rectangular shape in which the length (L2) in the rotation axis direction is 1/2 or more of the protruding length (W) from the outer peripheral edge of the wing (12). The impeller (1, 101) of the multiblade blower according to any one of claims 1 to 3, wherein the impeller (1, 101) is in the shape of a blade.
前記中間リング(14、 15)の断面形状は、略 L字形状である、請求項;!〜 3のいずれ かに記載の多翼送風機の羽根車(1、 101)。  The impeller (1, 101) of the multiblade blower according to any one of claims 1 to 3, wherein a cross-sectional shape of the intermediate ring (14, 15) is substantially L-shaped.
前記中間リング(14、 15)の断面形状は、略台形形状である、請求項;!〜 3のいず れかに記載の多翼送風機の羽根車(1、 101)。  The impeller (1, 101) of the multiblade fan according to any one of claims 1 to 3, wherein a cross-sectional shape of the intermediate ring (14, 15) is a substantially trapezoidal shape.
PCT/JP2007/071878 2006-11-14 2007-11-12 Impeller for multi-blade fan WO2008059775A1 (en)

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EP2096318A1 (en) 2009-09-02
EP2096318B1 (en) 2020-01-01
JP2008121611A (en) 2008-05-29
EP2096318A4 (en) 2013-02-06

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