WO2015046110A1 - Bladed wheel for fan - Google Patents

Bladed wheel for fan Download PDF

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Publication number
WO2015046110A1
WO2015046110A1 PCT/JP2014/075010 JP2014075010W WO2015046110A1 WO 2015046110 A1 WO2015046110 A1 WO 2015046110A1 JP 2014075010 W JP2014075010 W JP 2014075010W WO 2015046110 A1 WO2015046110 A1 WO 2015046110A1
Authority
WO
WIPO (PCT)
Prior art keywords
blade member
impeller
blade
fitting groove
disk
Prior art date
Application number
PCT/JP2014/075010
Other languages
French (fr)
Japanese (ja)
Inventor
加藤貴久
永田武司
Original Assignee
日清紡メカトロニクス株式会社
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 日清紡メカトロニクス株式会社 filed Critical 日清紡メカトロニクス株式会社
Priority to KR1020167010624A priority Critical patent/KR20160062076A/en
Priority to CN201480065273.2A priority patent/CN105793575A/en
Publication of WO2015046110A1 publication Critical patent/WO2015046110A1/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
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/02Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F04D17/04Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal of transverse-flow 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
    • F04D29/26Rotors 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
    • F04D29/60Mounting; Assembling; Disassembling
    • F04D29/62Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
    • F04D29/624Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/626Mounting or removal of fans
    • 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
    • F04D29/663Sound attenuation
    • 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
    • F04D29/663Sound attenuation
    • F04D29/665Sound attenuation by means of resonance chambers or interference

Definitions

  • the present invention relates to an impeller used for a blower such as a cross-flow blower.
  • the conventional impeller 200 includes a plurality of impeller constituent units 202, a boss-side disk-shaped fixing plate 205, a shaft portion 206, and a boss portion 207.
  • the constituent unit 202 includes a disc-like member 203 and a blade 204.
  • the shaft portion 206 is attached to the disk-like member 203 of the constituent unit 202 at one end of the impeller 200.
  • the boss side disk-shaped fixing plate 205 is attached to the blade member side of the constituent unit at the other end of the impeller 200.
  • the boss portion 207 is provided on the boss side disk-shaped fixing plate 205.
  • this impeller is referred to as a conventional product.
  • the Nz sound is a peak sound generated according to the number of blades and the number of rotations of an impeller for a blower.
  • the Nz sound is generated, it is easy to catch the ear because it has a specific frequency peak.
  • the following impeller is proposed in Patent Document 1.
  • the impeller described in Patent Document 1 will be described.
  • the blades of the impeller 300 have a shape as shown in FIG. 12, and a plurality of blades 304 are arranged in the configuration unit 302 in a cylindrical shape.
  • the impeller of Patent Document 1 has a complicated process and mold for molding a constituent unit including the impeller, which increases the cost of the impeller.
  • this impeller is referred to as an existing product.
  • the present invention has been made in view of the above circumstances, and an object thereof is to provide an inexpensive impeller that is low in noise and that eliminates or reduces Nz noise.
  • the impeller according to the first invention is formed by forming a plurality of blade members into a disk-shaped member in a cylindrical shape to form a structural unit, and connecting the blade member of the structural unit to the disk member of another structural unit.
  • An impeller of a blower formed by providing the same number of fitting grooves as the blade members on the surface of the disk-shaped fixing plate opposite to the side on which the blade members are formed, The position of the fitting groove is shifted with respect to the position of the blade member on the disk-shaped member, the tip of the blade member is fitted into the fitting groove, and each constituent unit is connected.
  • the impeller of the first invention the following effects are manifested.
  • a plurality of constituent units are formed, and the same number of fitting grooves as the blade members are provided on the opposite surface of the constituent unit of the disk-like member on which the blade members are formed, and the positions of the fitting grooves Is shifted with respect to the position of the blade member on the disk-shaped member, the blade member tip is fitted into the fitting groove, and the respective constituent units are connected.
  • the mold for molding the impeller is significantly simpler than the mold for manufacturing the impeller of the existing technology. Therefore, the impeller of the present invention is much cheaper than the impeller of the existing technology.
  • the material of the blade member may be a material having flexibility that does not generate cracks even if deformation such as torsion is applied.
  • the Nz sound can be suppressed to the same level as the existing technology.
  • the impeller of the second invention is the impeller of the first invention, wherein the impeller blade member is made of a composite material of synthetic resin and glass fiber, and the impeller blade member has an average thickness of 0.3 to 0.8 mm. Further, the glass fiber contained in the blade member is oriented in the plane of the surface of the blade member.
  • the material of the blade member is a composite material, and the thickness of the blade member is reduced without causing a decrease in strength.
  • the reduction of the Nz sound was disadvantageous because the thickness of the blade member was reduced.
  • the mold for molding the impeller has a simple structure. Furthermore, the impeller is inexpensive.
  • the material of the blade member is a composite material of a synthetic resin material and glass fiber, and the average thickness of the blade member is reduced to 0.3 to 0.8 mm. For this reason, the glass fiber contained in a blade member is orientated in the surface of the surface of a blade member.
  • the weight can be reduced to half or less compared to the conventional product and the existing product. Even if the blade member is made thinner and lighter, the power for driving the impeller can be reduced without causing a decrease in the performance of the impeller.
  • the thickness of the blade member is less than half that of the conventional material, the cost of material costs is also less than half.
  • the average thickness of the blade member of the present invention is reduced from 0.3 mm to 0.8 mm, and not only the weight reduction but also the glass fiber in the composite material is oriented in the surface of the blade member, and the strength of the blade member Can be further improved. Therefore, in order to express the effect of the present invention, even if the tip of the blade member is twisted into the fitting groove and fitted, there is no problem that the blade member is broken.
  • the impeller of the third invention is the resin composite material according to the second invention, wherein the material of the blade member is a composite material of synthetic resin material and glass fiber, and the glass fiber content is 10% to 40% by weight. It is characterized by that.
  • the impeller of the third invention is a composite material of synthetic resin material and glass fiber, and a resin composite material in which the glass fiber content is 10% to 40% by weight. Therefore, the effects of the second invention can be exhibited, and the following effects are exhibited. Even if the average thickness of the blade member of the impeller is reduced from 0.3 mm to 0.8 mm, the glass fiber can be arranged in the plane of the blade member, so that the strength of the blade member can be improved. .
  • the material of the blade member is a composite material of a synthetic resin material and glass fiber, and the elastic modulus (E ′) in the surface direction of the blade member is 2. It is characterized by being 5 ⁇ 10 9 Pa to 1.2 ⁇ 10 10 Pa.
  • the material of the blade member is a composite material of a synthetic resin material and glass fiber, and the elastic coefficient (E ′) in the surface surface direction of the blade member is 2.5 ⁇ 10 9 Pa to 1..
  • a composite material of 2 ⁇ 10 10 Pa resin material and glass fiber is used. Therefore, the effects of the second invention can be exhibited, and the following effects are exhibited. That is, the impeller of the present invention can be made into an impeller having a high elastic coefficient and easy to return (restorability) characteristics by thinning the blade member as compared with a case where the same composite material is thick. it can.
  • FIG. 9 is a spectrum diagram in which the high spectrum portion of the conventional Nz sound of FIG. 8 is superimposed on FIG. 9. It is explanatory drawing of a conventional product. It is explanatory drawing of the existing goods (impeller of patent document 1).
  • FIG. 1 is a front view of an impeller of the present invention
  • FIG. 2 is an explanatory view of a constituent unit and a fitting groove of the impeller of the present invention
  • FIG. 3 is an explanatory view of Embodiment 1 of a fitting groove of the constituent unit
  • FIG. FIG. 5 is an explanatory diagram of the fitting groove of the constituent unit according to the second embodiment
  • FIG. 5 is an explanatory diagram of the fitting groove of the constituent unit according to the third embodiment
  • FIG. FIG. 7 is a comparison diagram of noise characteristics of the impeller of the present invention, the conventional product and the existing product
  • FIG. 8 is a noise spectrum diagram of the conventional product
  • FIG. 9 is a noise spectrum diagram of the impeller of the present invention
  • FIG. FIG. 9 is a spectrum diagram in which the high spectrum portion of the conventional Nz sound of FIG. 8 is superimposed
  • FIG. 11 is an explanatory diagram of a conventional product
  • FIG. 12 is an explanatory diagram of an existing product (impeller of Patent Document 1).
  • the impeller 1 of FIG. 1 includes a plurality of impeller constituent units 2, a boss-side disk-shaped fixing plate 5, a shaft 6 and a boss 7. It is configured.
  • the shaft portion 6 is attached to the disk-like member 3 of the constituent unit 2 at the end portion on one side of the impeller 1.
  • the boss side disk-shaped fixing plate 5 is attached to the blade member side of the constituent unit at the other end of the impeller 1.
  • the boss portion 7 is provided on the boss side disk-shaped fixing plate 5.
  • the configuration unit 2 of the impeller 1 includes a disk-shaped member 3 and a blade member 4.
  • AS resin, ABS resin or PP resin is used. It is also possible to use a composite material of these resins and glass fibers.
  • the resins and the like described here are only examples, and any synthetic resin that provides a certain strength to a molded product as a commonly used synthetic resin can be used sufficiently.
  • a composite material of the synthetic resin and glass fiber can also be used.
  • the disk-shaped member 3 and the blade member 4 are integrally formed by injection molding, a pressing method, an extrusion method, or the like.
  • Each component unit 2 can be connected by an adhesion method such as an ultrasonic welding method.
  • the boss side disk-shaped fixing plate 5 can be joined to the blade member 4 of the constituent unit 2 at the boss side end of the impeller 1 by an adhesion method such as an ultrasonic welding method.
  • a plurality of component units having the shape of FIG. 2 are formed. That is, unlike the existing product in FIG. 12, the blade member 4 is straight with no twist or the like in the length direction. They are joined by an adhesion method such as ultrasonic welding as described above to form an impeller.
  • the blade member 4 of the component unit 2 of the impeller 1 is provided with a draft angle for molding.
  • the thickness of the blade member 4 is 0.3 to 1.5 mm in average thickness.
  • the thickness is preferably 0.3 to 0.8 mm, and more preferably 0.4 to 0.6 mm. If the average thickness of the blade member is less than 0.3 mm, the moldability by the molding method is deteriorated and there is a risk that a molding defect may occur on the tip side of the blade member. If the average thickness of the blade member is greater than 1.5 mm, the rigidity of the blade member increases, so that a large force is required to deform the blade member, and twisting or the like is applied to the fitting groove provided in the disk-like member described later. It may be difficult to fit.
  • Material of Blade Member (Component Unit 2)
  • the material of the component unit 2 of the impeller 1 and the boss side disk-shaped fixing plate 5 will be described.
  • synthetic resin such as AS resin, ABS resin, or PP resin can be used.
  • the tip of the blade member has an average thickness with flexibility. is there.
  • the average thickness of the blade member is preferably 0.3 to 0.8 mm, and more preferably 0.4 to 0.6 mm. If the average thickness of the blade member is less than 0.3 mm, the moldability by the molding method is deteriorated and there is a risk that a molding defect may occur on the tip side of the blade member. If the average thickness of the blade member is greater than 0.8 mm, the glass fiber in the blade member may not be oriented in the surface of the blade member and the elastic coefficient (E ′) of the blade member may be reduced. The elastic modulus (E ′) will be described later.
  • the glass fiber content is preferably 10% to 40% by weight, and more preferably 10% to 30%. If the weight ratio of the glass fiber content exceeds 40% of the total, there is a risk that defective molding of the blade member of the constituent unit may occur. Moreover, if it is less than 10%, the strength of the blade member may be reduced.
  • the material of the impeller is a composite material of a resin material and glass fiber
  • the elastic modulus (E ′) of the composite material is 2.5 ⁇ 10 9 Pa to 1.2 ⁇ .
  • a composite material of 10 10 Pa can be used. If the elastic modulus (E ′) of the composite material is less than 2.5 ⁇ 10 9 Pa, there is a possibility that the effect of the low elastic modulus and easy return property (restorability) may not appear at all, and 1.2 ⁇ 10 10 If it exceeds Pa, there is a risk that defective formation of the blade member of the constituent unit will occur and the product cannot be produced.
  • the elastic modulus (E ′) was measured with a viscoelasticity measuring instrument (RSA3 manufactured by TA Instruments) after preparing a test piece having a predetermined size from the molded blade member.
  • the elastic modulus was measured at a heating rate of 7.2 ° C./min and a measurement frequency of 1 Hz.
  • the elastic modulus was a measured value at 20 ° C.
  • the elastic modulus (E ′) of the composite material of the resin material and glass fiber used for the blade member of the impeller of the present invention is increased when the thickness of the blade member shown in FIG. 2 is reduced, and the thickness of the blade member is increased. When it is thicker, it tends to be lower. When the wall thickness is increased from 0.5 mm to 2 mm, the elastic modulus (E ′) is approximately halved. Further, when the glass fiber content is increased, the elastic modulus (E ′) also tends to increase. Increasing the glass fiber content from 10% to 40% by weight increases the elastic modulus (E ′) by about 3 times.
  • a configuration unit connection method When connecting the constituent units shown in FIG. 2, a fitting groove 8 for fitting the tip of the blade member is formed on the side of the disk-like member where the blade member is not formed, corresponding to the blade member of the constituent unit to be connected. Provided. The tip of the blade member is fitted into the fitting groove and connected by an adhesive method such as ultrasonic welding to form an impeller.
  • an adhesive method such as ultrasonic welding to form an impeller.
  • the shape of the fitting groove into which the blade member is fitted is devised.
  • FIGS. 3 to 5 As shown in FIG. 2 (c), a plurality of fitting grooves 8 are provided in the disk-like member 3 of the component unit 2, and one of them (M portion in the figure) will be described in detail. .
  • Embodiment 1 of the fitting groove will be described with reference to FIG.
  • the fitting groove 8 in FIG. 3 has the same shape as the tip of the blade member 4 of the constituent unit, and the position of the tip of the blade member of the constituent unit is projected onto the disc-like member 3 at the position to be arranged on the disc-like member 3.
  • the phase is shifted with respect to the position and shape.
  • the way of shifting is as shown in FIGS. 3 (a) and 3 (b).
  • the broken line is a shape obtained by projecting the shape of the tip of the above-described blade member onto a disk-shaped member.
  • the intersections of the broken blade shape and its center line are P1 and P2 in FIG.
  • FIG. 3A shows a shape in which the fitting groove is shifted from the center line P1-P2 by the rotation angle ⁇ in the right direction and the left direction (arrow direction) with P1 as the base point.
  • the center line of the fitting groove shifted to the left is P1-P3, and the center line of the fitting groove shifted to the right is P1-P4.
  • FIG. 3B shows a shape in which the fitting groove is shifted from the center line Q1-Q2 by the rotation angle ⁇ in the right direction and the left direction (arrow direction) with Q1 as a base point.
  • the center line of the fitting groove shifted to the left is Q1-Q3, and the center line of the fitting groove shifted to the right is Q1-Q4.
  • the rotation angle ⁇ is 1 to 15 degrees.
  • Such a blade member 4 is fitted in the fitting groove 8 in a twisted state. Then, it joins by ultrasonic welding etc.
  • the rotation angle ⁇ is less than 1 degree, there is a possibility that the effect of reducing the removal of Nz noise may be lost, and if it exceeds 15 degrees, the blade member may be excessively deformed and the impeller may not be molded.
  • Embodiment 2 of the fitting groove will be described with reference to FIG.
  • the fitting groove 8 in FIG. 4 has the same shape as the tip of the blade member 4 of the constituent unit, and the position at which the fitting groove 8 is arranged on the disc-like member is the position where the shape of the tip of the blade member of the constituent unit is projected onto the disc-like member 3. And slightly shifted inward in the radial direction with respect to the shape.
  • the way of shifting is as shown in FIG.
  • the broken line is a shape obtained by projecting the shape of the tip of the blade member described above onto the disk-shaped fixing plate.
  • the intersections of the broken vane-shaped center lines are R1 and R2.
  • FIG. 4 shows a shape in which the fitting groove is shifted radially inward with respect to the center line R1-R2.
  • the center line of the fitting groove is R3-R4.
  • the amount of displacement of the fitting groove inward in the radial direction is 0.5 mm to 2 mm.
  • Such a blade member is fitted into the fitting groove while being bent slightly in the radial direction. Then, it joins by ultrasonic welding etc.
  • the amount of shift is less than 0.5 mm, the effect of reducing the removal of Nz sound may be lost, and if it exceeds 2 mm, the blade member may be excessively deformed and the impeller may not be molded.
  • Embodiment 3 of the fitting groove will be described with reference to FIG.
  • the fitting groove 8 in FIG. 5 has the same shape as the tip of the blade member 4 of the constituent unit, and the position at which the fitting groove 8 is arranged on the disc-like member is the position where the shape of the tip of the blade member of the constituent unit is projected onto the disc-like member 3.
  • the shape is shifted in the direction of the center line of the shape projected onto the disk-shaped member 3 at the tip of the blade member with respect to the shape.
  • the way of shifting is as shown in FIGS. 5 (a) and 5 (b).
  • 5A and 5B the broken line is a shape obtained by projecting the shape of the tip portion of the above-described blade member onto the disk-shaped member.
  • FIG. 5A The intersections of the broken blade shape and its center line are denoted by S1 and S2 in FIG.
  • FIG. 5B T1 and T2.
  • the fitting groove is shifted in the outer peripheral direction of the impeller along the broken vane-shaped center line S1-S2.
  • the center line of the fitting groove shifted in this direction is S3-S4, which is the same as S1-S2.
  • the fitting groove is shifted in the inner circumferential direction of the impeller along a broken vane-shaped center line T1-T2.
  • T3-T4 The center line of the fitting groove shifted in this direction is T3-T4, which is the same as T1-T2.
  • the shift amount of the fitting groove in the outer circumferential direction or inner circumferential direction of the blade member is 0.5 mm to 2 mm. Therefore, the blade member is fitted in the fitting groove in a state bent slightly along the center line of the shape obtained by projecting the shape of the tip of the blade member onto the disk-shaped member 3. Then, it joins by ultrasonic welding etc.
  • the amount of shift is less than 0.5 mm, the effect of reducing the removal of Nz sound may be lost, and if it exceeds 2 mm, the blade member may be excessively deformed and the impeller may not be molded.
  • Embodiment 4 of the fitting groove 8 will be described. Although this embodiment is not shown, the fitting grooves of the first to third embodiments can be combined and used in combination.
  • the constituent unit and the boss-side disk-shaped fixing plate were made of a composite material of AS resin in which the glass fiber content was 20% by weight.
  • the blade member of the constituent unit has the form shown in FIG. 2, the average thickness is 0.4 mm, the length is 79 mm, and the number is 35.
  • the diameter of the constituent unit was 106 mm at the outermost part of the blade member 4.
  • Such a structural unit was formed by injection molding using the above-mentioned material.
  • eight such constituent units and the boss side disk-shaped fixing plate 5 made of the same material as the constituent unit 2 were joined by an ultrasonic welding method to produce the impeller of FIG.
  • the produced impeller had a total length of 635 mm, a diameter of 106 mm, and a total weight of 385 gr.
  • fitting groove 8 provided in the disk-shaped member in this example is the same as that in FIG.
  • the rotation angle ⁇ of the fitting groove with respect to the blade member of the disk-shaped member was 5 degrees.
  • Example 2 In this example, the fitting groove 8 provided in the disk-shaped member is the second embodiment, and the fitting groove of the disk-shaped member with respect to the blade member is disposed 1 mm inward in the radial direction. Otherwise, the impeller was manufactured in the same manner as in Example 1.
  • Example 3 the fitting groove provided in the disk-shaped member is the third embodiment, and the fitting groove with respect to the blade member of the disk-shaped fixing plate is the center of the broken blade shape according to FIG. It was shifted by 1 mm in the inner circumferential direction of the impeller along the line S1-S2. Otherwise, the impeller was manufactured in the same manner as in Example 1.
  • the impeller of this comparative example is a conventional product (FIG. 11).
  • the material is AS resin and the average thickness of the blades is about 1.8 mm.
  • the wing member is not twisted with the fitting groove on the disk-shaped fixing plate, that is, the wing member 204 of the constituent unit 200 is not twisted and is inserted into the fitting groove and connected.
  • FIG. The weight of the obtained impeller was 733 gr.
  • the impeller of this comparative example is an existing product (FIG. 12).
  • the blade member 304 of the constituent unit 302 shown in FIG. 12A was simulated to have the shape shown in FIG.
  • Each blade was fixedly joined to the disk-shaped fixing plate using a jig so that the tip of each blade was twisted by 5 degrees with respect to the root of the disk-shaped fixing plate.
  • the blade member 304 was connected and fixed to the disk-shaped fixing plate 303 in a state where it was twisted 5 degrees in the directions a and b in FIG.
  • the broken blade member indicates the blade member 204 in FIG. 11 (or the blade member 4 in FIG. 2).
  • the material was AS resin, and the average thickness of the blades was about 1.8 mm.
  • the weight of the obtained impeller was 733 gr.
  • FIG. 6 shows the evaluation results of the blowing efficiency (power consumption).
  • FIG. 6 compares the relationship between the air volume (m 3 / min) and the power consumption (W) for the impellers of the example and the comparative example. As shown in FIG. 6, the power consumption of the impeller of the present invention is reduced by about 5 to 6% when the air volume is 12 m 3 / min.
  • FIG. 7 compares the relationship between the air volume (m 3 / min) and the noise value (dB (A)) for the impellers of the example and the comparative example. From FIG. 7, it can be confirmed that the product of the present invention has the same performance as the conventional product and the existing product.
  • FIG. 8 is a noise spectrum diagram of a conventional impeller.
  • the portions indicated as “Nz sound” and “2Nz” in the figure indicate the strength (level) as the Nz sound.
  • FIG. 9 is a noise spectrum diagram of the invention.
  • the portions indicated as “Nz sound” and “2Nz” in the figure indicate the strength (level) as the Nz sound.
  • FIG. 10 shows a noise spectrum diagram of the present invention product (FIG. 9) at a frequency of 194 Hz to 6100 Hz of FIG. 8 and FIG. A portion having a high level (level) is displayed with an x mark superimposed thereon. From FIG. 10, it was found that the product of the present invention has the Nz sound removed and reduced significantly compared to the conventional product.

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

Abstract

The purpose of the present invention is to provide a low noise, inexpensive bladed wheel that removes or reduces blade-passing frequency noise. A bladed wheel for a fan, which is formed by creating a constituent unit by forming a plurality of blade members in a cylinder on a disc-shaped mounting plate and connecting the blade members of the constituent unit to the disc-shaped mounting plate of another constituent unit, is configured so that: fitting grooves into which the blade member tips fit are provided, in a number equal to the number of blade members, on the face opposite the side where the blade members of the disc-shaped mounting plate are formed; the position of the fitting groove is shifted with respect to the position of the blade member on the disk-shaped mounting plate; and each constituent unit is connected by fitting the blade member tip into the fitting groove.

Description

送風機用羽根車Blower impeller
 本発明は、貫流送風機などの送風機に用いられる羽根車に関するものである。 The present invention relates to an impeller used for a blower such as a cross-flow blower.
 近年の環境問題や省資源への取り組みから送風機の性能向上のため、羽根車を軽量化するとともに、低騒音及び低振動の羽根車の要求が高まっている。 Demand for impellers with low noise and vibration has been increasing in order to reduce the weight of impellers and improve the performance of blowers due to recent environmental issues and resource conservation efforts.
 まず従来技術の羽根車の構成について説明する。従来の羽根車200は、図11に示すように複数の羽根車の構成ユニット202、ボス側円盤状固定板205、及び軸部206とボス部207から構成されている。構成ユニット202は、円盤状部材203と羽根204から構成されている。軸部206は、羽根車200の一方側の端部の構成ユニット202の円盤状部材203に取り付けされている。ボス側円盤状固定板205は、羽根車200の他方側の端部の構成ユニットの羽根部材側に取り付けされている。ボス部207は、ボス側円盤状固定板205に設けられている。以下、この羽根車を従来品と称する。 First, the configuration of a conventional impeller will be described. As shown in FIG. 11, the conventional impeller 200 includes a plurality of impeller constituent units 202, a boss-side disk-shaped fixing plate 205, a shaft portion 206, and a boss portion 207. The constituent unit 202 includes a disc-like member 203 and a blade 204. The shaft portion 206 is attached to the disk-like member 203 of the constituent unit 202 at one end of the impeller 200. The boss side disk-shaped fixing plate 205 is attached to the blade member side of the constituent unit at the other end of the impeller 200. The boss portion 207 is provided on the boss side disk-shaped fixing plate 205. Hereinafter, this impeller is referred to as a conventional product.
 このような従来の羽根車の低騒音を実現するため、特にNz音を除去又は低減する必要がある。Nz音とは、送風機用の羽根車の羽根枚数と回転数に応じて発生するピーク音である。Nz音が発生すると特定の周波数のピークであるため耳につきやすい。このNz音を低減するために以下のような羽根車が特許文献1に提案されている。 In order to realize the low noise of such a conventional impeller, it is particularly necessary to remove or reduce the Nz sound. The Nz sound is a peak sound generated according to the number of blades and the number of rotations of an impeller for a blower. When the Nz sound is generated, it is easy to catch the ear because it has a specific frequency peak. In order to reduce this Nz noise, the following impeller is proposed in Patent Document 1.
 特許文献1に記載の羽根車について説明する。羽根車300の羽根は、図12のような形状を呈し、複数の羽根304が構成ユニット302に円筒状に配置されている。構成ユニットの円盤状固定板303に一体固定されている羽根304の一端とその他端を相対的に角度をずらし捩った状態の羽根を一体成形し、このような構成ユニットを複数接続した羽根車が提案されている。しかしながら特許文献1の羽根車は、その羽根を含む構成ユニットを成形する工程や金型が複雑であり、羽根車のコストが高くなる。以下、この羽根車を現有品と称する。 The impeller described in Patent Document 1 will be described. The blades of the impeller 300 have a shape as shown in FIG. 12, and a plurality of blades 304 are arranged in the configuration unit 302 in a cylindrical shape. An impeller in which one end of a blade 304 integrally fixed to a disk-shaped fixing plate 303 of the constituent unit and the other end are integrally formed with a twisted blade, and a plurality of such constituent units are connected. Has been proposed. However, the impeller of Patent Document 1 has a complicated process and mold for molding a constituent unit including the impeller, which increases the cost of the impeller. Hereinafter, this impeller is referred to as an existing product.
特開平08-049689JP 08-049889
 本発明は、上記の本事情に鑑みてなされたものであり、低騒音でありかつNz音を除去又は低減した安価な羽根車を提供することを目的とする。 The present invention has been made in view of the above circumstances, and an object thereof is to provide an inexpensive impeller that is low in noise and that eliminates or reduces Nz noise.
 上記課題を解決するため、第1発明の羽根車は、複数の羽根部材を円盤状部材に円筒状に成形し構成ユニット化し、前記構成ユニットの羽根部材を別の構成ユニットの前記円盤部材に接続して形成される送風機の羽根車であって、前記円盤状固定板の羽根部材が成形された側と反対面に、羽根部材先端を嵌合する嵌合溝を前記羽根部材と同数設け、前記嵌合溝の位置を前記円盤状部材上における前記羽根部材の位置に対してずらし、前記嵌合溝に前記羽根部材先端部を嵌合し、各構成ユニットを接続したことを特徴とする。 In order to solve the above-described problem, the impeller according to the first invention is formed by forming a plurality of blade members into a disk-shaped member in a cylindrical shape to form a structural unit, and connecting the blade member of the structural unit to the disk member of another structural unit. An impeller of a blower formed by providing the same number of fitting grooves as the blade members on the surface of the disk-shaped fixing plate opposite to the side on which the blade members are formed, The position of the fitting groove is shifted with respect to the position of the blade member on the disk-shaped member, the tip of the blade member is fitted into the fitting groove, and each constituent unit is connected.
 第1発明の羽根車によれば、以下の効果が発現する。複数の構成ユニットを成形し、構成ユニットの円盤状部材の羽根部材が成形された側と反対面に、羽根部材先端を嵌合する嵌合溝を羽根部材と同数設け、前記嵌合溝の位置を前記円盤状部材上における前記羽根部材の位置に対してずらし、前記嵌合溝に前記羽根部材先端部を嵌合し、各構成ユニットを接続した構成とした。これにより羽根車を成形する際の金型は、現有技術の羽根車を製造する金型と比べ格段に構造が簡単となる。従って本発明の羽根車は、現有技術の羽根車に比較して格段に安価となる。 According to the impeller of the first invention, the following effects are manifested. A plurality of constituent units are formed, and the same number of fitting grooves as the blade members are provided on the opposite surface of the constituent unit of the disk-like member on which the blade members are formed, and the positions of the fitting grooves Is shifted with respect to the position of the blade member on the disk-shaped member, the blade member tip is fitted into the fitting groove, and the respective constituent units are connected. As a result, the mold for molding the impeller is significantly simpler than the mold for manufacturing the impeller of the existing technology. Therefore, the impeller of the present invention is much cheaper than the impeller of the existing technology.
 また第1発明の羽根車は、構成ユニットの円盤状部材の嵌合溝が羽根部材先端位置に対してずらして配置しているため、に羽根部材の先端を捩って挿入する。従って羽根部材(構成ユニット)の材質は、捩り等の変形を加えても亀裂等の発生の無い柔軟性を有した素材であれば良い。例えば柔軟性を有する合成樹脂とし、羽根部材の厚さ寸法を現有技術レベルとすることにより、Nz音を現有技術と同レベルに抑えることができる。 In the impeller according to the first aspect of the invention, since the fitting groove of the disk-shaped member of the constituent unit is arranged to be shifted with respect to the tip position of the blade member, the tip of the blade member is twisted and inserted. Therefore, the material of the blade member (component unit) may be a material having flexibility that does not generate cracks even if deformation such as torsion is applied. For example, by using a synthetic resin having flexibility and setting the thickness dimension of the blade member to the existing technology level, the Nz sound can be suppressed to the same level as the existing technology.
 第2発明の羽根車は、第1発明において、羽根車の羽根部材の材質を合成樹脂材料およびガラス繊維の複合材料とし、羽根車の羽根部材の平均肉厚を0.3~0.8mmの範囲にて構成し、さらに羽根部材に含まれるガラス繊維を羽根部材の表面の面内に配向させたことを特徴とする。 The impeller of the second invention is the impeller of the first invention, wherein the impeller blade member is made of a composite material of synthetic resin and glass fiber, and the impeller blade member has an average thickness of 0.3 to 0.8 mm. Further, the glass fiber contained in the blade member is oriented in the plane of the surface of the blade member.
 第2発明の羽根車は、羽根部材の素材を複合材料とし、羽根部材の肉厚を強度低下を招くことなく薄くしている。一方Nz音の低減に関しては、羽根部材の肉厚が薄くなった分不利であった。しかしながら、第1発明の内容を使用しているため、Nz音のレベルを現有技術の羽根車と同等レベルとすることができる。またその羽根車を成形する金型は構造が簡単である。さらに、その羽根車は、安価である。 In the impeller of the second invention, the material of the blade member is a composite material, and the thickness of the blade member is reduced without causing a decrease in strength. On the other hand, the reduction of the Nz sound was disadvantageous because the thickness of the blade member was reduced. However, since the contents of the first invention are used, the level of the Nz sound can be made equal to the impeller of the existing technology. The mold for molding the impeller has a simple structure. Furthermore, the impeller is inexpensive.
 第2発明の羽根車によれば以下の効果も発現する。第2発明の羽根車は、その羽根部材の材質を、合成樹脂材料およびガラス繊維の複合材料としており、羽根部材の平均肉厚を0.3~0.8mmと薄肉化している。このため羽根部材に含まれるガラス繊維を羽根部材の表面の面内に配向させている。羽根車をこのような構成とすることにより、従来品および現有品に比較してその重量を半分以下に軽量化することができる。羽根部材を薄肉化し軽量化しても羽根車としての性能低下を招来することなく、羽根車を駆動するためのパワーを軽減できる。さらに羽根部材の肉厚が従来の半分以下になったことから、材料費のコストも半分以下になっている。また本発明の羽根部材の平均肉厚を0.3mmから0.8mmと薄肉化し、軽量化だけでなく複合材料の中のガラス繊維を羽根部材の表面面内に配向させ、その羽根部材の強度を更に向上させることができる。従って本発明の効果を発現するために、嵌合溝に羽根部材先端を捩って、嵌合しても羽根部材が割れるといような不具合は発生しない。 According to the impeller of the second invention, the following effects are also exhibited. In the impeller of the second invention, the material of the blade member is a composite material of a synthetic resin material and glass fiber, and the average thickness of the blade member is reduced to 0.3 to 0.8 mm. For this reason, the glass fiber contained in a blade member is orientated in the surface of the surface of a blade member. By configuring the impeller with such a configuration, the weight can be reduced to half or less compared to the conventional product and the existing product. Even if the blade member is made thinner and lighter, the power for driving the impeller can be reduced without causing a decrease in the performance of the impeller. Further, since the thickness of the blade member is less than half that of the conventional material, the cost of material costs is also less than half. Moreover, the average thickness of the blade member of the present invention is reduced from 0.3 mm to 0.8 mm, and not only the weight reduction but also the glass fiber in the composite material is oriented in the surface of the blade member, and the strength of the blade member Can be further improved. Therefore, in order to express the effect of the present invention, even if the tip of the blade member is twisted into the fitting groove and fitted, there is no problem that the blade member is broken.
 第3発明の羽根車は、第2発明において、羽根部材の材質を合成樹脂材料およびガラス繊維の複合材料とし、かつガラス繊維の含有率が重量比率で10%から40%となる樹脂複合材料としたことを特徴とする。 The impeller of the third invention is the resin composite material according to the second invention, wherein the material of the blade member is a composite material of synthetic resin material and glass fiber, and the glass fiber content is 10% to 40% by weight. It is characterized by that.
 第3発明の羽根車は、合成樹脂材料およびガラス繊維の複合材料とし、かつガラス繊維の含有率が重量比率で10%から40%となる樹脂複合材料としている。従って第2発明の効果を発現できるとともに以下の効果が発現する。羽根車の羽部部材の平均肉厚を0.3mmから0.8mmと薄肉化しても、ガラス繊維を羽根部材の面内に配置することができるので、羽根部材の強度を向上させることができる。 The impeller of the third invention is a composite material of synthetic resin material and glass fiber, and a resin composite material in which the glass fiber content is 10% to 40% by weight. Therefore, the effects of the second invention can be exhibited, and the following effects are exhibited. Even if the average thickness of the blade member of the impeller is reduced from 0.3 mm to 0.8 mm, the glass fiber can be arranged in the plane of the blade member, so that the strength of the blade member can be improved. .
 第4発明の羽根車は、第2発明または第3発明において、羽根部材の材質を合成樹脂材料およびガラス繊維の複合材料とし、当該羽根部材の表面面方向の弾性係数(E’)が2.5×10Pa~1.2×1010Paであることを特徴とする。 In the impeller of the fourth invention according to the second or third invention, the material of the blade member is a composite material of a synthetic resin material and glass fiber, and the elastic modulus (E ′) in the surface direction of the blade member is 2. It is characterized by being 5 × 10 9 Pa to 1.2 × 10 10 Pa.
 また第4発明の羽根車は、羽根部材の材質を合成樹脂材料およびガラス繊維の複合材料とし、当該羽根部材の表面面方向の弾性係数(E’)が2.5×10Pa~1.2×1010Paの樹脂材料とガラス繊維の複合材料を用いている。従って第2発明の効果を発現できるとともに以下の効果が発現する。すなわち、本発明の羽根車は、羽根部材を薄肉化することにより、同一の複合材料で厚肉とした場合に較べ高弾性係数であり戻り易い(復元性)特性を有する羽根車とすることができる。 In the impeller of the fourth invention, the material of the blade member is a composite material of a synthetic resin material and glass fiber, and the elastic coefficient (E ′) in the surface surface direction of the blade member is 2.5 × 10 9 Pa to 1.. A composite material of 2 × 10 10 Pa resin material and glass fiber is used. Therefore, the effects of the second invention can be exhibited, and the following effects are exhibited. That is, the impeller of the present invention can be made into an impeller having a high elastic coefficient and easy to return (restorability) characteristics by thinning the blade member as compared with a case where the same composite material is thick. it can.
本発明の羽根車の正面図である。It is a front view of the impeller of the present invention. 本発明の羽根車の構成ユニット及び嵌合溝の説明図である。It is explanatory drawing of the structural unit and fitting groove | channel of the impeller of this invention. 構成ユニットの嵌合溝の実施形態1の説明図である。It is explanatory drawing of Embodiment 1 of the fitting groove of a structure unit. 構成ユニットの嵌合溝の実施形態2の説明図である。It is explanatory drawing of Embodiment 2 of the fitting groove of a structure unit. 構成ユニットの嵌合溝の実施形態3の説明図である。It is explanatory drawing of Embodiment 3 of the fitting groove of a structure unit. 本発明の羽根車と従来品及び現有品の送風効率の比較図である。It is a comparison figure of the ventilation efficiency of the impeller of this invention, a conventional product, and the existing product. 本発明の羽根車と従来品及び現有品の騒音特性の比較図である。It is a comparison figure of the noise characteristic of the impeller of this invention, a conventional product, and the existing product. 従来品の騒音スペクトル図である。It is a noise spectrum figure of a conventional product. 本発明の羽根車の騒音スペクトル図である。It is a noise spectrum figure of the impeller of this invention. 図9に図8の従来のNz音の高スペクトル部分を重ね合わせたスペクトル図である。FIG. 9 is a spectrum diagram in which the high spectrum portion of the conventional Nz sound of FIG. 8 is superimposed on FIG. 9. 従来品の説明図である。It is explanatory drawing of a conventional product. 現有品(特許文献1の羽根車)の説明図である。It is explanatory drawing of the existing goods (impeller of patent document 1).
 本発明の実施形態を図により説明する。
 図1は本発明の羽根車の正面図、図2は本発明の羽根車の構成ユニット及び嵌合溝の説明図、図3は構成ユニットの嵌合溝の実施形態1の説明図、図4は 構成ユニットの嵌合溝の実施形態2の説明図、図5は構成ユニットの嵌合溝の実施形態3の説明図、図6は本発明の羽根車と従来品及び現有品の送風効率の比較図、図7は本発明の羽根車と従来品及び現有品の騒音特性の比較図、図8は従来品の騒音スペクトル図、図9は本発明の羽根車の騒音スペクトル図、  図10は図9に図8の従来のNz音の高スペクトル部分を重ね合わせたスペクトル図、図11は従来品の説明図、及び図12は現有品(特許文献1の羽根車)の説明図である。
An embodiment of the present invention will be described with reference to the drawings.
1 is a front view of an impeller of the present invention, FIG. 2 is an explanatory view of a constituent unit and a fitting groove of the impeller of the present invention, FIG. 3 is an explanatory view of Embodiment 1 of a fitting groove of the constituent unit, FIG. FIG. 5 is an explanatory diagram of the fitting groove of the constituent unit according to the second embodiment, FIG. 5 is an explanatory diagram of the fitting groove of the constituent unit according to the third embodiment, and FIG. FIG. 7 is a comparison diagram of noise characteristics of the impeller of the present invention, the conventional product and the existing product, FIG. 8 is a noise spectrum diagram of the conventional product, FIG. 9 is a noise spectrum diagram of the impeller of the present invention, and FIG. FIG. 9 is a spectrum diagram in which the high spectrum portion of the conventional Nz sound of FIG. 8 is superimposed, FIG. 11 is an explanatory diagram of a conventional product, and FIG. 12 is an explanatory diagram of an existing product (impeller of Patent Document 1).
<1>本発明の羽根車の構造
 本発明の図1の羽根車1は、複数の図2の羽根車の構成ユニット2、ボス側円盤状固定板5、及び軸部6とボス部7から構成されている。軸部6は、羽根車1の一方側の端部の構成ユニット2の円盤状部材3に取り付けされている。ボス側円盤状固定板5は、羽根車1の他方側の端部の構成ユニットの羽根部材側に取り付けされている。ボス部7は、ボス側円盤状固定板5に設けられている。
<1> Structure of Impeller of the Present Invention The impeller 1 of FIG. 1 according to the present invention includes a plurality of impeller constituent units 2, a boss-side disk-shaped fixing plate 5, a shaft 6 and a boss 7. It is configured. The shaft portion 6 is attached to the disk-like member 3 of the constituent unit 2 at the end portion on one side of the impeller 1. The boss side disk-shaped fixing plate 5 is attached to the blade member side of the constituent unit at the other end of the impeller 1. The boss portion 7 is provided on the boss side disk-shaped fixing plate 5.
<2>羽根部材(構成ユニット2)の構造
 羽根車1の構成ユニット2は、円盤状部材3と羽根部材4から構成されている。材質は、AS樹脂、ABS樹脂またはPP樹脂が使用される。またこれら樹脂とガラス繊維との複合材料を使用することも可能である。ここに記載した樹脂等は一例であり、通常使われる合成樹脂として成形品に一定の強度をもたらす合成樹脂であれば十分使用することができる。またその合成樹脂とガラス繊維の複合材料も使用することができる。円盤状部材3と羽根部材4は、射出成形、プレス法又は押出法などにより一体で成形されている。各構成ユニット2の接続は、超音波溶着法等の接着法により接合することができる。またボス側円盤状固定板5は、羽根車1のボス側の端部の構成ユニット2の羽根部材4と超音波溶着法等の接着法により接合することができる。
<2> Structure of Blade Member (Configuration Unit 2) The configuration unit 2 of the impeller 1 includes a disk-shaped member 3 and a blade member 4. As the material, AS resin, ABS resin or PP resin is used. It is also possible to use a composite material of these resins and glass fibers. The resins and the like described here are only examples, and any synthetic resin that provides a certain strength to a molded product as a commonly used synthetic resin can be used sufficiently. A composite material of the synthetic resin and glass fiber can also be used. The disk-shaped member 3 and the blade member 4 are integrally formed by injection molding, a pressing method, an extrusion method, or the like. Each component unit 2 can be connected by an adhesion method such as an ultrasonic welding method. The boss side disk-shaped fixing plate 5 can be joined to the blade member 4 of the constituent unit 2 at the boss side end of the impeller 1 by an adhesion method such as an ultrasonic welding method.
 本発明においては、現有品(図12)の構成ユニットの羽根部材とは異なり、図2の形状の構成ユニットを複数成形する。すなわち、図12の現有品と異なり羽根部材4の長さ方向に捩れ等は無く真っ直ぐである。それらを上述のように超音波溶着法等の接着法により接合し、羽根車を形成する。 In the present invention, unlike the blade member of the component unit of the current product (FIG. 12), a plurality of component units having the shape of FIG. 2 are formed. That is, unlike the existing product in FIG. 12, the blade member 4 is straight with no twist or the like in the length direction. They are joined by an adhesion method such as ultrasonic welding as described above to form an impeller.
 羽根車1の構成ユニット2の羽根部材4は、その肉厚は、成型用の抜き勾配が設けられている。羽根部材4の肉厚は、平均肉厚で0.3~1.5mmである。好ましくは0.3~0.8mmであり、さらに好ましくは0.4~0.6mmである。羽根部材の平均肉厚が0.3mmより薄くなると成形法による成形性が悪化し羽根部材の先端側にて成形不良を発生する虞がある。羽根部材の平均肉厚が1.5mmより厚くなると羽根部材の剛性が高くなるので変形させるのに大きな力が必要となり、羽根部材を後述する円盤状部材に設けた嵌合溝に捩り等を加えて嵌合することが困難となる虞がある。 The blade member 4 of the component unit 2 of the impeller 1 is provided with a draft angle for molding. The thickness of the blade member 4 is 0.3 to 1.5 mm in average thickness. The thickness is preferably 0.3 to 0.8 mm, and more preferably 0.4 to 0.6 mm. If the average thickness of the blade member is less than 0.3 mm, the moldability by the molding method is deteriorated and there is a risk that a molding defect may occur on the tip side of the blade member. If the average thickness of the blade member is greater than 1.5 mm, the rigidity of the blade member increases, so that a large force is required to deform the blade member, and twisting or the like is applied to the fitting groove provided in the disk-like member described later. It may be difficult to fit.
<3>羽根部材(構成ユニット2)の材質
 羽根車1の構成ユニット2およびボス側円盤状固定板5の材質について説明する。材質としては、AS樹脂、ABS樹脂またはPP樹脂等の合成樹脂を使用することができる。本発明では、後述するように円盤状固定板に設けた嵌合溝に羽根部材の先端を、変形させて嵌め合わせるため、羽根部材の先端が柔軟性を有する平均肉厚とすることが必要である。
<3> Material of Blade Member (Component Unit 2) The material of the component unit 2 of the impeller 1 and the boss side disk-shaped fixing plate 5 will be described. As a material, synthetic resin such as AS resin, ABS resin, or PP resin can be used. In the present invention, as will be described later, in order to deform and fit the tip of the blade member into the fitting groove provided in the disk-shaped fixing plate, it is necessary that the tip of the blade member has an average thickness with flexibility. is there.
 またこれら合成樹脂とガラス繊維の複合材料を使用することができる。この場合羽根部材の平均肉厚は、好ましくは0.3~0.8mmであり、さらに好ましくは0.4~0.6mmである。羽根部材の平均肉厚が0.3mmより薄くなると成形法による成形性が悪化し羽根部材の先端側にて成形不良を発生する虞がある。羽根部材の平均肉厚が0.8mmより厚くなると羽根部材の中のガラス繊維が羽根部材の表面面内に配向しなくなり羽根部材の弾性係数(E’)が低下する虞がある。尚弾性係数(E’)については後述する。複合材料を使用する場合は、ガラス繊維の含有率が重量比率で全体の10%から40%とすることが好ましく、さらに10%から30%とすることがより好ましい。ガラス繊維の含有率の重量比率が全体の40%を上回ると構成ユニットの羽根部材の成形不良が発生する虞がある。また10%を下回ると羽根部材の強度が低下する虞がある。 Also, composite materials of these synthetic resins and glass fibers can be used. In this case, the average thickness of the blade member is preferably 0.3 to 0.8 mm, and more preferably 0.4 to 0.6 mm. If the average thickness of the blade member is less than 0.3 mm, the moldability by the molding method is deteriorated and there is a risk that a molding defect may occur on the tip side of the blade member. If the average thickness of the blade member is greater than 0.8 mm, the glass fiber in the blade member may not be oriented in the surface of the blade member and the elastic coefficient (E ′) of the blade member may be reduced. The elastic modulus (E ′) will be described later. When the composite material is used, the glass fiber content is preferably 10% to 40% by weight, and more preferably 10% to 30%. If the weight ratio of the glass fiber content exceeds 40% of the total, there is a risk that defective molding of the blade member of the constituent unit may occur. Moreover, if it is less than 10%, the strength of the blade member may be reduced.
 また本発明の羽根車の羽根部材には、羽根部材の材質を樹脂材料およびガラス繊維の複合材料とし、その複合材料の弾性係数(E’)が2.5×10Pa~1.2×1010Paである複合材料を用いることができる。その複合材料の弾性係数(E’)が2.5×10Pa未満であると低弾性係数であり戻り易い(復元性)特性の効果が全く現れない虞があり、1.2×1010Paを超えると構成ユニットの羽根部材の成形不良が発生し製品化出来ない虞がある。
 尚上記の弾性係数(E’)は、成形した羽根部材から所定の寸法の試験片を作成し粘弾性測定機(ティー・エイ・インスツルメント社製のRSA3)により測定した。また弾性係数の測定は、昇温速度、7.2℃/分、および測定周波数は1Hzにて行った。また弾性係数は、20℃における測定値とした。
In the impeller of the impeller of the present invention, the material of the impeller is a composite material of a resin material and glass fiber, and the elastic modulus (E ′) of the composite material is 2.5 × 10 9 Pa to 1.2 ×. A composite material of 10 10 Pa can be used. If the elastic modulus (E ′) of the composite material is less than 2.5 × 10 9 Pa, there is a possibility that the effect of the low elastic modulus and easy return property (restorability) may not appear at all, and 1.2 × 10 10 If it exceeds Pa, there is a risk that defective formation of the blade member of the constituent unit will occur and the product cannot be produced.
The elastic modulus (E ′) was measured with a viscoelasticity measuring instrument (RSA3 manufactured by TA Instruments) after preparing a test piece having a predetermined size from the molded blade member. The elastic modulus was measured at a heating rate of 7.2 ° C./min and a measurement frequency of 1 Hz. The elastic modulus was a measured value at 20 ° C.
 尚本発明の羽根車の羽根部材に使用する樹脂材料とガラス繊維の複合材料の弾性係数(E’)は、図2に示す羽根部材の肉厚を薄くすると高くなり、羽根部材の肉厚を厚くすると低くなる傾向にある。肉厚を0.5mmから2mmに厚くすると弾性係数(E’)は、約半分になる。
 またガラス繊維の含有量を増加させると、弾性係数(E’)も増加する傾向にある。ガラス繊維の含有量を重量比で10%から40%に増加させると弾性係数(E’)は、約3倍になる。
The elastic modulus (E ′) of the composite material of the resin material and glass fiber used for the blade member of the impeller of the present invention is increased when the thickness of the blade member shown in FIG. 2 is reduced, and the thickness of the blade member is increased. When it is thicker, it tends to be lower. When the wall thickness is increased from 0.5 mm to 2 mm, the elastic modulus (E ′) is approximately halved.
Further, when the glass fiber content is increased, the elastic modulus (E ′) also tends to increase. Increasing the glass fiber content from 10% to 40% by weight increases the elastic modulus (E ′) by about 3 times.
<4>構成ユニットの接続方法
 次に構成ユニットの接続方法について説明する。図2に示す構成ユニットを接続する場合、円盤状部材の羽根部材が成形されていない側に、接続する構成ユニットの羽根部材に対応させて、羽根部材の先端を嵌合させる嵌合溝8を設けている。この嵌合溝に羽根部材の先端を嵌合させ、超音波溶着等の接着法で接続し羽根車を成形する。本発明では、羽根車の騒音性能を向上させるために、この羽根部材を嵌合させる嵌合溝の形状を工夫している。以下、嵌合溝8の実施形態について図3から図5により説明する。尚嵌合溝8は、図2(c)に示すように、構成ユニット2の円盤状部材3に複数個設けられているが、その中の一つ(図中のM部)について詳細説明する。
<4> Configuration Unit Connection Method Next, a configuration unit connection method will be described. When connecting the constituent units shown in FIG. 2, a fitting groove 8 for fitting the tip of the blade member is formed on the side of the disk-like member where the blade member is not formed, corresponding to the blade member of the constituent unit to be connected. Provided. The tip of the blade member is fitted into the fitting groove and connected by an adhesive method such as ultrasonic welding to form an impeller. In the present invention, in order to improve the noise performance of the impeller, the shape of the fitting groove into which the blade member is fitted is devised. Hereinafter, an embodiment of the fitting groove 8 will be described with reference to FIGS. 3 to 5. As shown in FIG. 2 (c), a plurality of fitting grooves 8 are provided in the disk-like member 3 of the component unit 2, and one of them (M portion in the figure) will be described in detail. .
 [実施形態1]
 嵌合溝の実施形態1を図3により説明する。図3の嵌合溝8は、構成ユニットの羽根部材4の先端部と同形状とし、円盤状部材3に配置する位置を、構成ユニットの羽根部材先端部の形状を円盤状部材3に投影した位置及び形状に対して位相をずらしたものである。ずらし方は図3(a)および図3(b)のとおりである。図3(a)及び図3(b)において破線は、上述の羽根部材の先端部の形状を円盤状部材に投影した形状である。この破線の羽根形状とその中心線の交点を図3(a)においてP1及びP2とし.図3(b)においてQ1及びQ2とする。図3(a)は、嵌合溝をP1を基点とし嵌合溝を中心線P1-P2に対して右方向及び左方向(矢印方向)に回転角度θずらした形状である。左方向に回転しずらした嵌合溝の中心線は、P1-P3であり、右方向に回転しずらした嵌合溝の中心線は、P1―P4である。図3(b)は、嵌合溝をQ1を基点とし嵌合溝を中心線Q1-Q2に対して右方向及び左方向(矢印方向)に回転角度θずらした形状である。左方向にずらした嵌合溝の中心線は、Q1-Q3であり、右方向にずらした嵌合溝の中心線は、Q1―Q4である。回転角度θは、1度から15度である。このような羽根部材4は、嵌合溝8に捩れた状態で嵌合される。その後、超音波溶着等で接合される。
[Embodiment 1]
Embodiment 1 of the fitting groove will be described with reference to FIG. The fitting groove 8 in FIG. 3 has the same shape as the tip of the blade member 4 of the constituent unit, and the position of the tip of the blade member of the constituent unit is projected onto the disc-like member 3 at the position to be arranged on the disc-like member 3. The phase is shifted with respect to the position and shape. The way of shifting is as shown in FIGS. 3 (a) and 3 (b). In FIG. 3A and FIG. 3B, the broken line is a shape obtained by projecting the shape of the tip of the above-described blade member onto a disk-shaped member. The intersections of the broken blade shape and its center line are P1 and P2 in FIG. In FIG. 3B, it is set as Q1 and Q2. FIG. 3A shows a shape in which the fitting groove is shifted from the center line P1-P2 by the rotation angle θ in the right direction and the left direction (arrow direction) with P1 as the base point. The center line of the fitting groove shifted to the left is P1-P3, and the center line of the fitting groove shifted to the right is P1-P4. FIG. 3B shows a shape in which the fitting groove is shifted from the center line Q1-Q2 by the rotation angle θ in the right direction and the left direction (arrow direction) with Q1 as a base point. The center line of the fitting groove shifted to the left is Q1-Q3, and the center line of the fitting groove shifted to the right is Q1-Q4. The rotation angle θ is 1 to 15 degrees. Such a blade member 4 is fitted in the fitting groove 8 in a twisted state. Then, it joins by ultrasonic welding etc.
 ここで回転角度θは、1度未満となると、Nz音の除去低減の効果がなくなる虞があり、15度を超えると羽根部材が変形過大となり羽根車を成形できない虞がある。 Here, if the rotation angle θ is less than 1 degree, there is a possibility that the effect of reducing the removal of Nz noise may be lost, and if it exceeds 15 degrees, the blade member may be excessively deformed and the impeller may not be molded.
 [実施形態2]
 嵌合溝の実施形態2を図4により説明する。図4の嵌合溝8は、構成ユニットの羽根部材4の先端部と同形状とし、円盤状部材に配置する位置を、構成ユニットの羽根部材先端部の形状を円盤状部材3に投影した位置及び形状に対して半径方向内側にわずかずらしたものである。ずらし方は図4のとおりである。図4において破線は、上述の羽根部材の先端部の形状を円盤状固定板に投影した形状である。この破線の羽根形状の中心線の交点をR1及びR2とする。図4は、嵌合溝を中心線R1―R2に対して半径方向内側に矢印方向にずらした形状である。嵌合溝の中心線は、R3―R4である。嵌合溝の半径方向内側へのずらし量は0.5mmから2mmである。このような羽根部材は、嵌合溝にわずか半径方向に曲げられた状態で嵌合される。その後、超音波溶着等で接合される。
[Embodiment 2]
Embodiment 2 of the fitting groove will be described with reference to FIG. The fitting groove 8 in FIG. 4 has the same shape as the tip of the blade member 4 of the constituent unit, and the position at which the fitting groove 8 is arranged on the disc-like member is the position where the shape of the tip of the blade member of the constituent unit is projected onto the disc-like member 3. And slightly shifted inward in the radial direction with respect to the shape. The way of shifting is as shown in FIG. In FIG. 4, the broken line is a shape obtained by projecting the shape of the tip of the blade member described above onto the disk-shaped fixing plate. The intersections of the broken vane-shaped center lines are R1 and R2. FIG. 4 shows a shape in which the fitting groove is shifted radially inward with respect to the center line R1-R2. The center line of the fitting groove is R3-R4. The amount of displacement of the fitting groove inward in the radial direction is 0.5 mm to 2 mm. Such a blade member is fitted into the fitting groove while being bent slightly in the radial direction. Then, it joins by ultrasonic welding etc.
 ここでずらし量は、0.5mm未満となると、Nz音の除去低減の効果がなくなる虞があり、2mmを超えると羽根部材が変形過大となり羽根車を成形できない虞がある。 Here, if the amount of shift is less than 0.5 mm, the effect of reducing the removal of Nz sound may be lost, and if it exceeds 2 mm, the blade member may be excessively deformed and the impeller may not be molded.
 [実施形態3]
 嵌合溝の実施形態3を図5により説明する。図5の嵌合溝8は、構成ユニットの羽根部材4の先端部と同形状とし、円盤状部材に配置する位置を、構成ユニットの羽根部材先端部の形状を円盤状部材3に投影した位置及び形状に対して、羽根部材先端部の円盤状部材3への投影した形状の中心線方向にずらしたものである。ずらし方は図5(a)および図5(b)のとおりである。図5(a)及び図5(b)において破線は、上述の羽根部材の先端部の形状を円盤状部材に投影した形状である。この破線の羽根形状とその中心線の交点を図5(a)においてS1及びS2とし.図5(b)においてT1及びT2とする。図5(a)は、嵌合溝を破線の羽根形状の中心線S1-S2に沿って羽根車の外周方向にずらしたものである。この方向にずらした嵌合溝の中心線はS3-S4であり、S1-S2と同じである。図5(b)は、嵌合溝を破線の羽根形状の中心線T1-T2に沿って羽根車の内周方向にずらしたものである。この方向にずらした嵌合溝の中心線はT3-T4であり、T1-T2と同じである。嵌合溝の羽根部材の外周方向又は内周方向へのずらし量は0.5mmから2mmである。従って羽根部材は、嵌合溝にわずか羽根部材の先端の形状を円盤状部材3に投影した形状の中心線に沿って曲げられた状態で嵌合される。その後、超音波溶着等で接合される。
[Embodiment 3]
Embodiment 3 of the fitting groove will be described with reference to FIG. The fitting groove 8 in FIG. 5 has the same shape as the tip of the blade member 4 of the constituent unit, and the position at which the fitting groove 8 is arranged on the disc-like member is the position where the shape of the tip of the blade member of the constituent unit is projected onto the disc-like member 3. The shape is shifted in the direction of the center line of the shape projected onto the disk-shaped member 3 at the tip of the blade member with respect to the shape. The way of shifting is as shown in FIGS. 5 (a) and 5 (b). 5A and 5B, the broken line is a shape obtained by projecting the shape of the tip portion of the above-described blade member onto the disk-shaped member. The intersections of the broken blade shape and its center line are denoted by S1 and S2 in FIG. In FIG. 5B, T1 and T2. In FIG. 5A, the fitting groove is shifted in the outer peripheral direction of the impeller along the broken vane-shaped center line S1-S2. The center line of the fitting groove shifted in this direction is S3-S4, which is the same as S1-S2. In FIG. 5B, the fitting groove is shifted in the inner circumferential direction of the impeller along a broken vane-shaped center line T1-T2. The center line of the fitting groove shifted in this direction is T3-T4, which is the same as T1-T2. The shift amount of the fitting groove in the outer circumferential direction or inner circumferential direction of the blade member is 0.5 mm to 2 mm. Therefore, the blade member is fitted in the fitting groove in a state bent slightly along the center line of the shape obtained by projecting the shape of the tip of the blade member onto the disk-shaped member 3. Then, it joins by ultrasonic welding etc.
 ここでずらし量は、0.5mm未満となると、Nz音の除去低減の効果がなくなる虞があり、2mmを超えると羽根部材が変形過大となり羽根車を成形できない虞がある。 Here, if the amount of shift is less than 0.5 mm, the effect of reducing the removal of Nz sound may be lost, and if it exceeds 2 mm, the blade member may be excessively deformed and the impeller may not be molded.
 [実施形態4]
 嵌合溝8の実施形態4について説明する。本実施形態は、図示しないが、実施形態1から実施形態3の嵌合溝を複合化し組み合わせて使用することも可能である。
[Embodiment 4]
Embodiment 4 of the fitting groove 8 will be described. Although this embodiment is not shown, the fitting grooves of the first to third embodiments can be combined and used in combination.
<5>本発明の羽根車の実施例
 以下、実施例および比較例を挙げて、本発明をより具体的に説明するが、本発明は、下記の実施例に限定されるものではない。
<5> Examples of Impeller of the Present Invention Hereinafter, the present invention will be described more specifically with reference to examples and comparative examples. However, the present invention is not limited to the following examples.
 [実施例1]
 本実施例では、ガラス繊維の含有率が重量比率で全体の20%としたAS樹脂の複合材料により、構成ユニットとボス側円盤状固定板を作製した。構成ユニットの羽根部材は、図2に示す形態であり、その平均肉厚は0.4mm、長さは79mmとし、その枚数は35枚とした。また構成ユニットの直径は、羽根部材4の最外部で、106mmとした。このような構成ユニットは、上記材質の素材により射出成形により成形した。さらにこのような構成ユニット8個と、構成ユニット2と同材質のボス側円盤状固定板5とを超音波溶着法により接合し図1の羽根車を作製した。作製した羽根車は、全長635mm、直径106mm、全重量は385grであった。
[Example 1]
In this example, the constituent unit and the boss-side disk-shaped fixing plate were made of a composite material of AS resin in which the glass fiber content was 20% by weight. The blade member of the constituent unit has the form shown in FIG. 2, the average thickness is 0.4 mm, the length is 79 mm, and the number is 35. The diameter of the constituent unit was 106 mm at the outermost part of the blade member 4. Such a structural unit was formed by injection molding using the above-mentioned material. Further, eight such constituent units and the boss side disk-shaped fixing plate 5 made of the same material as the constituent unit 2 were joined by an ultrasonic welding method to produce the impeller of FIG. The produced impeller had a total length of 635 mm, a diameter of 106 mm, and a total weight of 385 gr.
 また本実施例における円盤状部材に設けた嵌合溝8は実施形態1の図3(a)とした。円盤状部材の羽根部材に対する嵌合溝の回転角度θは5度とした。 Further, the fitting groove 8 provided in the disk-shaped member in this example is the same as that in FIG. The rotation angle θ of the fitting groove with respect to the blade member of the disk-shaped member was 5 degrees.
 [実施例2]
 本実施例では、円盤状部材に設けた嵌合溝8は実施形態2とし、円盤状部材の羽根部材に対する嵌合溝は1mm半径方向内側に配置した。それ以外は、実施例1と同様にして羽根車を製作した。
[Example 2]
In this example, the fitting groove 8 provided in the disk-shaped member is the second embodiment, and the fitting groove of the disk-shaped member with respect to the blade member is disposed 1 mm inward in the radial direction. Otherwise, the impeller was manufactured in the same manner as in Example 1.
 [実施例3]
 本実施例では、円盤状部材に設けた嵌合溝は実施形態3とし、円盤状固定板の羽根部材に対する嵌合溝は、図5(a)に従って、嵌合溝を破線の羽根形状の中心線S1-S2に沿って羽根車の内周方向に1mmずらした。それ以外は、実施例1と同様にして羽根車を製作した。
[Example 3]
In this example, the fitting groove provided in the disk-shaped member is the third embodiment, and the fitting groove with respect to the blade member of the disk-shaped fixing plate is the center of the broken blade shape according to FIG. It was shifted by 1 mm in the inner circumferential direction of the impeller along the line S1-S2. Otherwise, the impeller was manufactured in the same manner as in Example 1.
 [比較例1]
 本比較例の羽根車は、従来品(図11)である。材質は、AS樹脂とし羽根の平均肉厚は約1.8mmである。羽部部材は、円盤状固定板に嵌合溝との捩れ等は無く、すなわち構成ユニット200の羽根部材204は捩れ等が無く、嵌合溝に挿入され接続される。それ以外は、実施例1と同様にして図11の羽根車を作製した。得られた羽根車の重量は、733grであった。
[Comparative Example 1]
The impeller of this comparative example is a conventional product (FIG. 11). The material is AS resin and the average thickness of the blades is about 1.8 mm. The wing member is not twisted with the fitting groove on the disk-shaped fixing plate, that is, the wing member 204 of the constituent unit 200 is not twisted and is inserted into the fitting groove and connected. Other than that produced the impeller of FIG. 11 like Example 1. FIG. The weight of the obtained impeller was 733 gr.
 [比較例2]
 本比較例の羽根車は、現有品(図12)である。図12(a)の構成ユニット302の羽根部材304を図12(c)の形状に模擬的に成形した。各羽根の先端を円盤状固定板の羽根の根元に対して5度捩った状態になるように治具を使用し円盤状固定板に固定接合した。図12(c)のa方向及びb方向に捩り5度捩れた状態で羽根部材304を円盤状固定板303に接続固定した。尚図12(c)の中で破線の羽根部材は、図11の羽根部材204(又は図2の羽根部材4)を表示している。材質は、AS樹脂とし羽根の平均肉厚は約1.8mmとした。それ以外は、実施例と同様にして図12の羽根車を作製した。得られた羽根車の重量は、733grであった。
[Comparative Example 2]
The impeller of this comparative example is an existing product (FIG. 12). The blade member 304 of the constituent unit 302 shown in FIG. 12A was simulated to have the shape shown in FIG. Each blade was fixedly joined to the disk-shaped fixing plate using a jig so that the tip of each blade was twisted by 5 degrees with respect to the root of the disk-shaped fixing plate. The blade member 304 was connected and fixed to the disk-shaped fixing plate 303 in a state where it was twisted 5 degrees in the directions a and b in FIG. In FIG. 12C, the broken blade member indicates the blade member 204 in FIG. 11 (or the blade member 4 in FIG. 2). The material was AS resin, and the average thickness of the blades was about 1.8 mm. Other than that produced the impeller of FIG. 12 like the Example. The weight of the obtained impeller was 733 gr.
 実施例1から実施例3および比較例1から比較例2にて作製した羽根車について以下を試験し比較した。
[1]送風効率
 実施例1から実施例3及び比較例1から比較例2で得られた羽根車について、送風効率を以下のように評価した。上記の方法により作製された羽根車をエアコン室内機に組み込み、エアコン実機を風量測定装置に設置して、送風量と、羽根車の駆動に要する消費電力を測定した。
[2]騒音特性
 実施例1から実施例3及び比較例1から比較例2で得られた羽根車について、騒音特性を以下のように評価した。上記の方法により作製された羽根車をエアコン室内機に組み込み、エアコン実機を風量測定装置に設置して、送風量と、羽根車の回転数を測定した。さらにエアコン実機を騒音測定室に壁掛け状態に設置し、騒音値と、羽根車の回転数を測定した。同一回転数での送風量と騒音値の関係をグラフ化した。
[3]Nz音
 上記[2]の騒音特性を測定する際に騒音スペクトル図におけるNz音のレベルを比較評価した。
The following was tested and compared about the impeller produced in Example 1 to Example 3 and Comparative Example 1 to Comparative Example 2.
[1] Blowing efficiency About the impeller obtained in Example 1 to Example 3 and Comparative Example 1 to Comparative Example 2, the blowing efficiency was evaluated as follows. The impeller produced by the above method was incorporated into an air conditioner indoor unit, and the actual air conditioner was installed in the air flow measuring device, and the air flow rate and the power consumption required to drive the impeller were measured.
[2] Noise characteristics The noise characteristics of the impellers obtained in Examples 1 to 3 and Comparative Examples 1 to 2 were evaluated as follows. The impeller produced by the above method was incorporated into an air conditioner indoor unit, the actual air conditioner was installed in an air flow measuring device, and the air flow rate and the rotation speed of the impeller were measured. In addition, the actual air conditioner was installed in the noise measurement room in a wall-mounted state, and the noise level and the rotation speed of the impeller were measured. The relationship between the air flow rate at the same rotation speed and the noise value was graphed.
[3] Nz sound When measuring the noise characteristics of [2] above, the level of the Nz sound in the noise spectrum diagram was compared and evaluated.
<6>実施例と比較例の性能評価
 送風効率(消費電力)の評価結果を図6に示す。図6は、実施例と比較例の羽根車について風量(m/分)と消費電力(W)の関係を比較したものである。図6から風量が12m/分においてその消費電力は、従来品及び現有品に対して本発明の羽根車の方が、その消費電力が約5~6%低減されている。
<6> Performance Evaluation of Examples and Comparative Examples FIG. 6 shows the evaluation results of the blowing efficiency (power consumption). FIG. 6 compares the relationship between the air volume (m 3 / min) and the power consumption (W) for the impellers of the example and the comparative example. As shown in FIG. 6, the power consumption of the impeller of the present invention is reduced by about 5 to 6% when the air volume is 12 m 3 / min.
 騒音特性の評価結果を図7に示す。図7は、実施例と比較例の羽根車について風量(m/分)と騒音値(dB(A))の関係を比較したものである。図7から本発明品は、従来品及び現有品に対して同等の性能であることが確認できる。 The evaluation results of the noise characteristics are shown in FIG. FIG. 7 compares the relationship between the air volume (m 3 / min) and the noise value (dB (A)) for the impellers of the example and the comparative example. From FIG. 7, it can be confirmed that the product of the present invention has the same performance as the conventional product and the existing product.
 Nz音低減の程度は、本発明品と現有品(図12)の羽根車とは同等であることを確認した。またNz音低減の程度を、本発明品と従来品(図11)の羽根車と比較確認した。 It was confirmed that the degree of Nz noise reduction was equivalent to the impeller of the present invention product and the existing product (FIG. 12). The degree of Nz noise reduction was compared with the impeller of the present invention product and the conventional product (FIG. 11).
 図8は、従来品の羽根車の騒音スペクトル図である。図中の「Nz音」と「2Nz」と表記した部分が、Nz音としての強さ(レベル)を表示している。図9は、発明品の騒音スペクトル図である。図中の「Nz音」と「2Nz」と表記した部分が、Nz音としての強さ(レベル)を表示している。図10は、図8及び図9の194Hzから6100Hzの周波数において、本発明品の騒音スペクトル図(図9)に従来品の騒音スペクトル図(図8)のNz音に相当する部分及び騒音の強さ(レベル)が高い部分を×印を付与して重ねて表示したものである。図10より本発明品は、従来品に対してNz音が格段に除去低減されていることが分かった。 FIG. 8 is a noise spectrum diagram of a conventional impeller. The portions indicated as “Nz sound” and “2Nz” in the figure indicate the strength (level) as the Nz sound. FIG. 9 is a noise spectrum diagram of the invention. The portions indicated as “Nz sound” and “2Nz” in the figure indicate the strength (level) as the Nz sound. FIG. 10 shows a noise spectrum diagram of the present invention product (FIG. 9) at a frequency of 194 Hz to 6100 Hz of FIG. 8 and FIG. A portion having a high level (level) is displayed with an x mark superimposed thereon. From FIG. 10, it was found that the product of the present invention has the Nz sound removed and reduced significantly compared to the conventional product.
  1   羽根車(本発明品)
  2   羽根車の構成ユニット
  3   円盤状部材
  4   羽根部材
  5   ボス側円盤状固定板
  6   軸部
  7   ボス部
  8   嵌合溝
  200 従来技術の羽根車(従来品)
  300 現有技術の羽根車(現有品)
1 impeller (product of the present invention)
2 Component unit of impeller 3 Disk-shaped member 4 Blade member 5 Boss side disk-shaped fixing plate 6 Shaft portion 7 Boss portion 8 Fitting groove 200 Conventional impeller (conventional product)
300 Impeller of current technology (current product)

Claims (4)

  1.  複数の羽根部材を円盤状部材に円筒状に成形し構成ユニット化し、前記構成ユニットの羽根部材を別の構成ユニットの前記円盤状部材に接続して形成される送風機の羽根車であって、
     前記円盤状部材の羽根部材が成形された側と反対面に、羽根部材先端を嵌合する嵌合溝を前記羽根部材と同数設け、
     前記嵌合溝の位置を前記円盤状部材上における前記羽根部材の位置に対してずらし、
     前記嵌合溝に前記羽根部材先端部を嵌合し、各構成ユニットを接続したことを特徴とする羽根車。
    A blade impeller of a blower formed by forming a plurality of blade members into a disk-shaped member in a cylindrical shape to form a structural unit, and connecting the blade member of the structural unit to the disk-shaped member of another structural unit,
    On the surface opposite to the side on which the blade member of the disk-shaped member is formed, the same number of fitting grooves as the blade member are fitted to fit the blade member tip,
    Shifting the position of the fitting groove with respect to the position of the blade member on the disk-shaped member,
    The impeller characterized in that the tip of the blade member is fitted into the fitting groove, and each component unit is connected.
  2.  羽根車の羽根部材の材質を合成樹脂材料およびガラス繊維の複合材料とし、羽根車の羽根部材の平均肉厚を0.3~0.8mmの範囲にて構成し、さらに羽根部材に含まれるガラス繊維を羽根部材の表面の面内に配向させたことを特徴とする請求項1に記載の羽根車。 The material of the impeller blade member is a composite material of synthetic resin and glass fiber, and the average thickness of the impeller blade member is in the range of 0.3 to 0.8 mm, and the glass contained in the blade member 2. The impeller according to claim 1, wherein the fibers are oriented in the plane of the surface of the blade member.
  3.  羽根部材の材質を合成樹脂材料およびガラス繊維の複合材料とし、かつガラス繊維の含有率が重量比率で10%から40%となる樹脂複合材料としたことを特徴とする請求項2に記載の羽根車。 3. The blade according to claim 2, wherein the material of the blade member is a composite material of a synthetic resin material and a glass fiber, and a resin composite material having a glass fiber content of 10% to 40% by weight. car.
  4.  羽根部材の材質を合成樹脂材料およびガラス繊維の複合材料とし、当該羽根部材の表面面方向の弾性係数(E’)が2.5×10Pa~1.2×1010Paであることを特徴とする請求項2または請求項3に記載の羽根車。 The blade member is made of a composite material of synthetic resin and glass fiber, and the elastic modulus (E ′) in the surface direction of the blade member is 2.5 × 10 9 Pa to 1.2 × 10 10 Pa. The impeller according to claim 2 or claim 3, characterized by the above.
PCT/JP2014/075010 2013-09-30 2014-09-22 Bladed wheel for fan WO2015046110A1 (en)

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