WO2007114090A1 - 多翼ファン - Google Patents
多翼ファン Download PDFInfo
- Publication number
- WO2007114090A1 WO2007114090A1 PCT/JP2007/056148 JP2007056148W WO2007114090A1 WO 2007114090 A1 WO2007114090 A1 WO 2007114090A1 JP 2007056148 W JP2007056148 W JP 2007056148W WO 2007114090 A1 WO2007114090 A1 WO 2007114090A1
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- WO
- WIPO (PCT)
- Prior art keywords
- blade
- fan
- notch
- notches
- multiblade fan
- Prior art date
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/02—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
- F04D17/04—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal of transverse-flow type
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/281—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
- F04D29/282—Rotors 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
- F04D29/283—Rotors 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/30—Vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/663—Sound attenuation
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/666—Combating 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/667—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by influencing the flow pattern, e.g. suppression of turbulence
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F24—HEATING; RANGES; VENTILATING
- F24F—AIR-CONDITIONING; AIR-HUMIDIFICATION; VENTILATION; USE OF AIR CURRENTS FOR SCREENING
- F24F1/00—Room units for air-conditioning, e.g. separate or self-contained units or units receiving primary air from a central station
- F24F1/0007—Indoor units, e.g. fan coil units
- F24F1/0018—Indoor units, e.g. fan coil units characterised by fans
- F24F1/0025—Cross-flow or tangential fans
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2210/00—Working fluids
- F05D2210/10—Kind or type
- F05D2210/12—Kind or type gaseous, i.e. compressible
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/304—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the trailing edge of a rotor blade
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/20—Three-dimensional
- F05D2250/29—Three-dimensional machined; miscellaneous
- F05D2250/294—Three-dimensional machined; miscellaneous grooved
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/711—Shape curved convex
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/70—Shape
- F05D2250/71—Shape curved
- F05D2250/712—Shape curved concave
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/60—Fluid transfer
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
- F05D2260/961—Preventing, counteracting or reducing vibration or noise by mistuning rotor blades or stator vanes with irregular interblade spacing, airfoil shape
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/97—Reducing windage losses
Definitions
- the present invention relates to a blade structure in an impeller of a multiblade fan.
- multi-blade fans such as crossflow fans, sirocco fans, and turbo fans are used as blowers for air conditioners.
- Figure 26 shows a wall-mounted air conditioner A that uses a multiblade fan as a blower.
- the air conditioner A includes a main body casing 1.
- the main casing 1 includes an air suction port 4 on the upper surface and an air outlet 5 on the front portion of the lower surface.
- a heat exchanger 2 and a multiblade fan 3 are provided in the main casing 1.
- the multiblade fan 3 is disposed between the heat exchanger 2 and the air outlet 5.
- the heat exchanger 2 includes a front-side heat exchange part 2a disposed near the front surface of the main body casing 1, and a back-side heat exchange part 2b disposed near the back surface of the main body casing 1.
- the rear side heat exchange part 2b is connected to the upper end of the front side heat exchange part 2a.
- an air passage 6 through which air taken in from the air inlet 4 flows is provided near the front surface thereof.
- a first drain pan 8, a second drain pan 9, a guide portion 10, a backflow preventing tongue portion 11, a vertical blade 12 and a horizontal blade 13 are provided in the main body casing 1.
- the first drain pan 8 is for receiving the drain generated in the front side heat exchange section 2a.
- the second drain pan 9 is for receiving the drain generated in the back side heat exchange section 2b.
- the guide unit 10 is for guiding the air blown from the impeller 7 of the multiblade fan 3 to the air outlet 5.
- the backflow preventing tongue 11 is for preventing backflow of air blown out from the impeller 7.
- the air sucked from the air suction port 4 is cooled or heated when it passes through the heat exchanger 2.
- the air then travels on the impeller 7 of the multiblade fan 3. It flows through in the direction perpendicular to the axis of rotation, and then blows out from the air outlet 5.
- the impeller 7 includes a plurality of circular support plates and a plurality of blades (blades) 15.
- the impeller 7 has a forward wing structure.
- the circular support plates are arranged in parallel to each other at a predetermined interval along the rotation axis of the impeller 7.
- Each blade 15 is arranged at a predetermined blade angle with respect to the rotation axis at the outer peripheral edge of each circular support plate.
- noise is generated when air passes through the blades 15 of the impeller 7.
- the main causes of this noise are separation of the air flow that occurs near the suction surface of the blade 15 and wake vortices that occur near the trailing edge of the blade.
- Patent Document 1 Japanese Patent Laid-Open No. 3-249400
- Patent Document 2 JP-A-11-141494
- the present inventor has proposed a multiblade fan having a blade structure as shown in FIGS. 27 to 30 (for example, Japanese Patent Application No. 2005-269765 (Japanese Patent Application No. 2006-125390)). Publication))).
- the impeller 7 of the multiblade fan 3 shown in FIGS. 27 to 30 has a forward blade structure, and includes a plurality of circular support plates 14 and a plurality of blades 15.
- the circular support plates 14 are arranged in parallel to each other at a predetermined interval along the rotation axis 16.
- Each blade 15 is arranged at a predetermined blade angle with respect to the rotating shaft 16 at the outer peripheral edge of each circular support plate 14!
- a plurality of notches 17 having an equilateral triangle shape are provided on the outer blade tip 15 a of each blade 15 at a predetermined interval along the longitudinal direction of the blade 15. Further, a plurality of smooth portions (non-notched portions) 18 forming part of the blade tip 15a are provided at the blade tip 15a outside each blade 15. Each smooth portion 18 has a predetermined width and is provided between adjacent notches 17.
- the notch 17 is easier to machine than the conventional method of machining the blade tip of the blade into a sawtooth shape. Further, if the smooth portion 18 forms a part of the blade tip, the shape of the blade tip can be maintained. Furthermore, if each notch 17 is formed in an equilateral triangle, the area of one notch 17 can be minimized, and the area of the pressure surface of each blade 15 that receives air pressure by the rotation of the fan can be secured to the maximum.
- the notch 17 is provided in the blade tip 15a outside the blade 15, the blade outlet of the portion of the notch 17 has a portion without the notch 17 (see FIG. 33 (a)). Compared to the circumferential direction, it is open enough. For this reason, at the time of blowing out, the air flow from which the fan force is blown out is not sufficiently directed in the circumferential direction, and deviates as shown by the two-dot chain line in FIG. 33 (b). As a result, the fan pressure is reduced, it becomes weak against the pressure loss of the filter, and the wind is hard to come out.
- FIG. 31 shows the state of air suction and blowing around the impeller 7 when the impeller 7 shown in FIGS. 27 to 30 is applied to the air conditioner A shown in FIG.
- FIG. 32 shows the flow of air flowing through the impeller 7.
- a multi-blade fan such as a cross flow fan has a plurality of blades 15 arranged in the circumferential direction and a plurality of blades 15 in order to secure the strength of the impeller 7. It has side plates 14. Each side plate 14 is provided at each of both ends and the center of the impeller 7 in the longitudinal direction. Therefore, in the vicinity of each side plate 14, as shown in FIG. 34, the side plate 14 is affected, so the air flow velocity FV decreases.
- a sufficiently high wind speed FV can be obtained in a portion without the side plate 14, but the side plate 14
- the wind speed FV is much lower than the wind speed FV.
- An object of the present invention is to provide a multiblade fan in which a plurality of notches are provided at the blade tip outside the blade, and project along the blade thickness direction near the rear of the notch on the blade pressure surface.
- An object of the present invention is to provide a multiblade fan that can effectively increase the fan pressure by providing a convex portion.
- a multiblade fan having a plurality of notches provided on the outer wing tip of a vane is rotated by the rotation of the multiblade fan.
- a protrusion protruding along the thickness direction of the blade is provided at the rear of each notch.
- the blade has a recess on the suction surface opposite to the pressure surface, and the recess is formed by denting a portion corresponding to the protrusion on the suction surface.
- the width between adjacent wings can be increased at the rear of the notch. Therefore, air can easily flow between adjacent blades, and the fan pressure can be further improved.
- the convex portion and the concave portion preferably extend along a single arc.
- a convex part and a recessed part can be processed easily, and cost is reduced.
- the convex portion and the concave portion may each extend along a plurality of arcs having different curvatures. In this case, air can flow more smoothly between adjacent blades, and the fan pressure can be further improved.
- the height of the convex portion becomes smaller as it approaches the blade tip of the blade.
- the depth of the concave portion becomes smaller as it approaches the blade tip of the blade. In these cases, it is possible to effectively suppress the wake vortex generated at the trailing edge of the blade during blowing, and to reduce noise.
- the notches at both ends of the blades are preferably smaller than the notches provided at the center of the blades.
- a multi-blade fan such as a crossflow fan has a plurality of side plates in order to fix a plurality of blades arranged in the circumferential direction and to secure the strength of the impeller.
- Each side plate is provided at both ends and the center of the impeller in the longitudinal direction. In this case, the air flow rate decreases near the side plate. Therefore, if a notch of the same size is provided at the outer edge of the blade, it is much larger than the notch for obtaining a noise reduction effect near both ends of the blade.
- the fan pressure is excessively reduced as in the case where the concave portion is arranged.
- a notch in the vicinity of both ends of the blade is formed smaller than a notch provided in the central portion of the blade.
- the noise reduction effect due to the notch is sufficiently maintained.
- the fan pressure can be further increased and a reduction in air blowing performance can be avoided as compared with a configuration in which notches having the same size are provided.
- the notches at both ends of the multiblade fan are preferably smaller than the notches provided at the center of the multiblade fan.
- a multi-blade fan such as a crossflow fan has a plurality of side plates in order to fix a plurality of blades arranged in the circumferential direction and secure the strength of the impeller. Each side plate is provided at both ends and the center of the impeller. In this case, the air flow velocity decreases in the vicinity of the side plate.
- a sufficiently high wind speed can be obtained at the portion where there is no side plate.
- the air flow rate decreases, and further, the impeller adjacent to both side walls of the main body casing is further reduced. Near the both ends, the air flow rate is greatly reduced.
- the notch in the vicinity of both ends of the impeller (portion close to the side wall of the main body casing) is formed smaller than the notch in the center of the impeller.
- the noise reduction effect due to the notch is sufficiently maintained.
- the fan pressure can be further increased to avoid a reduction in blowing performance.
- the multiblade fan is preferably a blower for an air conditioner.
- a pressure can be raised effectively. Moreover, even when a resistor such as a filter is provided, a desired air volume can be secured.
- a multiblade fan suitable as a blower for an air conditioner such as a crossflow fan can be realized. As a result, it is possible to stabilize the air flow and realize a high-performance air conditioner with high and low noise. wear.
- ⁇ 1 A perspective view of the blades of the multiblade fan according to the first embodiment, in which the pressure surface force is also seen.
- FIG. 2 is an enlarged partial side view showing the vicinity of the outer end of the blade.
- FIG. 4 is a cross-sectional view taken along line 4 4 in FIG.
- FIG. 5 is a cross-sectional view taken along line 5-5 in FIG.
- FIG. 7 A perspective view of the blades of the multi-blade fan of the second embodiment as seen from the pressure surface force.
- FIG. 8 is a partial side view showing the vicinity of the outer end of the blade.
- FIG. 9 A perspective view of the blades of the multiblade fan according to the third embodiment in which the pressure surface force is also seen. [10] Perspective view of blades with negative pressure surface force.
- FIG. 11 is an enlarged partial side view showing the vicinity of the outer end of the blade.
- FIG. 15 is an enlarged partial side view showing the vicinity of the outer end of the blade.
- FIG. 19 A side view of the blade.
- FIG. 20 is a cross-sectional view taken along line 20-20 in FIG.
- FIG. 21 is a cross-sectional view taken along line 21-21 in FIG.
- FIG. 25 A perspective view of the blades of the multiblade fan of the eighth embodiment as seen from the suction surface.
- FIG. 27 is a perspective view showing the overall configuration of the impeller.
- FIG. 28 is a partial perspective view showing an enlarged part of the impeller.
- FIG. 29 is a perspective view showing a conventional blade.
- FIG. 30 is an enlarged partial front view showing the vicinity of the outer end of the blade.
- FIG. 31 is a schematic diagram showing air flow when a conventional impeller is used.
- FIG. 32 is a schematic diagram showing the air flow in the impeller.
- FIG. 33 (a) is a cross section taken along line 33 (a) 33 (a) in FIG. 30, and (b) is a cross section taken along line 33 (b) 33 (b) in FIG.
- FIG. 34 is an explanatory diagram for explaining the relationship between the side plates of the impeller and both side walls of the main casing and the wind speed distribution.
- the impeller of the multiblade fan of the present embodiment has a forward blade structure as in the conventional configuration shown in FIG.
- the impeller includes a plurality of circular support plates 14 and a plurality of blades 15 having an arcuate cross section.
- the circular support plates 14 are arranged in parallel to each other at a predetermined interval along the rotation axis 16.
- Each blade 15 is arranged at a predetermined blade angle with respect to the rotating shaft 16 at the outer peripheral edge of each circular support plate 14! RU
- a plurality of notches 17 forming an equilateral triangle are arranged at predetermined intervals along the longitudinal direction of the blade 15 at the blade tip 15a outside the blade 15. Is provided. Further, a plurality of smooth portions (non-notched portions) 18 forming a part of the blade tip are provided on the blade tip 15a outside each blade 15. Each smoothing portion 18 has a predetermined width and is provided between adjacent notches 17.
- the multi-blade fan having the notch 17 at the blade tip 15a of the blade 15 and the smoothing portion 18 between the adjacent notches 17 is a cross-flow fan (FIGS. 26, 31 and 32).
- a large horizontal vortex released from the tip of the wing is reduced by a vertical vortex formed by the notch 17 in the region on the blowout side. It is subdivided into For this reason, noise is reduced.
- the blade outlet of the portion of the notch 17 is sufficiently larger in the circumferential direction than the portion without the notch 17. It is open without going to.
- the pressure surface (concave surface) of the blade has a notch 17 near the rear portion.
- a triangular pyramid-shaped convex portion 19 is provided.
- the triangular pyramid-shaped convex portion 19 is formed near the rear portion of the notch 17 on the pressure surface of the blade.
- the blade tip 15a of the blade 15 is not planar, the wake vortex generated when the blade is blown out near the trailing edge of the blade can be suppressed, and noise can be further effectively reduced.
- the height of the convex portion 19 is set so as to decrease as it approaches the blade tip 15a in order to smooth the air flow on the pressure surface of the blade.
- the wake vortex generated near the trailing edge of the blade during blowing can be effectively suppressed, and noise can be reduced.
- a multiblade fan according to a second embodiment will be described with reference to FIGS.
- the triangular notch 17 shown in the first embodiment is changed to a square notch 17 and at the pressure surface of the blade 15 near the rear of the notch 17.
- a square-shaped convex portion 20 is provided.
- the blade outlet of the notch 17 can be directed in the circumferential direction. Therefore, the air flow blown from the fan can be directed in the circumferential direction, and the fan pressure can be effectively increased.
- the square-shaped convex portion 20 is provided in the vicinity of the rear portion of the notch 17 on the pressure surface of the blade.
- the blade outlet at the notch 17 can be sufficiently directed in the circumferential direction in the same manner as the part without the notch 17 (indicated by the broken line). Therefore, the fan pressure can be increased.
- the blade tip 15a of the blade 15 is not planar, the wake vortex generated when the blade is blown out near the trailing edge of the blade can be suppressed, and noise can be further effectively reduced.
- a multiblade fan according to a third embodiment will be described with reference to FIGS.
- the blade tip 15a of the blade 15 is provided with the same triangular notch 17 as in the first embodiment, and the notch 17 has a notch 17 on the pressure surface of the blade 15.
- a triangular pyramid-shaped convex part 19 is provided in the vicinity of the rear part.
- the blade outlet of the notch 17 can be directed in the circumferential direction. Therefore, the air flow blown from the fan can be directed in the circumferential direction, and the fan pressure can be effectively increased.
- the blade 15 has a recess 19a on the suction surface opposite to the pressure surface.
- the concave portion 19 a is formed by denting a portion corresponding to the convex portion 19 on the suction surface of the blade 15. As a result, the blade 15 is provided with irregularities in the vicinity of the rear portion of the notch 17.
- the concave portion 19a located on the back side of the convex portion 19 provides a space between adjacent wings in the vicinity of the rear portion of the notch 17. Can be widened. Therefore, air can easily flow between adjacent blades, and the fan pressure can be further improved.
- the convex portion and the concave portion near the rear portion of the notch 17 may extend along an arc having the same curvature. In this case, a convex part and a recessed part can be processed easily, and cost is reduced. Further, the convex portion and the concave portion may extend along a plurality of arcs having different curvatures. In this case, air can flow more easily between adjacent blades, and the fan pressure can be further improved.
- the depth of the recess 19a is set so as to become smaller as it approaches the blade tip 15a of the blade 15. In this way, the wake vortex generated near the trailing edge of the blade during blowing can be more effectively suppressed, and noise can be reduced.
- a multiblade fan according to a fourth embodiment will be described with reference to FIGS.
- a rectangular notch 17 similar to that of the second embodiment is provided at the blade tip 15a on the outer side of the blade 15 and the pressure surface of the blade 15 is near the rear of the notch 17.
- Convex part 20 is provided on.
- the blade outlet at the notch 17 can be directed in the circumferential direction. Therefore, the air flow blown from the fan can be directed in the circumferential direction, and the fan pressure can be effectively increased.
- the blade 15 has a recess 20a on the negative pressure surface opposite to the pressure surface.
- the concave portion 20a is formed by denting a portion corresponding to the convex portion (20) on the suction surface of the blade 15. As a result, the blade 15 is provided with irregularities in the vicinity of the rear portion of the notch 17.
- the concave portion 20a located on the back side of the convex portion 20 widens the width between adjacent wings in the vicinity of the rear portion of the notch 17. can do. Therefore, air can easily flow between adjacent blades, and the fan pressure can be further improved.
- a multiblade fan according to a fifth embodiment will be described with reference to FIGS.
- the width and depth of the notch 17a in the portion adjacent to the plate 14 are set to be smaller than the width and depth of the notch 17 provided in the center of the blade 15.
- a multi-blade fan such as a cross flow fan has a plurality of side plates 14 in order to securely fix a plurality of blades 15 arranged in the circumferential direction and to ensure the strength of the impeller 7.
- Each side plate 14 is provided at both ends and the center of the impeller 7 in the longitudinal direction. Therefore, as shown in FIG. 34, in the vicinity of each side plate 14, since it is affected by the side plate 14, the flow velocity FV of air decreases.
- a sufficiently high wind speed FV can be obtained at the portion where the side plate 14 is not provided.
- the wind speed FV is significantly lower than the wind speed FV.
- the notches 17a (see FIG. 21) at both ends of the blade 15 (portions close to the side plate 14) are notched 17 at the center of the blade 15 (see FIG. 20). ) Smaller than. As a result, the noise reduction effect due to the notches 17, 17a is sufficiently maintained. As compared with a configuration in which notches 17 having the same size are provided intermittently over the entire blade 15, the fan pressure can be further increased and a reduction in the blowing performance can be avoided.
- a multiblade fan according to the sixth embodiment will be described with reference to FIG.
- the width and depth of the notches 17a in the vicinity of both ends of the blades 15 are provided in the center portion of the blades 15. It is set smaller than 17.
- a multi-blade fan such as a crossflow fan has a plurality of side plates 14 in order to fix a plurality of blades 15 arranged in the circumferential direction and to secure the strength of the impeller 7. ing .
- the side plates 14 are provided at both ends and the center of the impeller 7 in the longitudinal direction. Therefore, as shown in FIG. 34, in the vicinity of each side plate 14, since it is affected by the side plate 14, the air flow velocity FV decreases. [0063] Specifically, a sufficiently high wind speed FV can be obtained at the portion where the side plate 14 is empty.
- the wind speed FV is much lower than the wind speed FV.
- the notch 17a in the vicinity of both ends of the blade 15 is formed smaller than the notch 17 provided in the central portion of the blade 15. Yes.
- the noise reduction effect by the notches 17 and 17a is fully maintained.
- the fan pressure can be further increased, and the deterioration of the blowing performance can be avoided.
- a multiblade fan according to a seventh embodiment will be described with reference to FIGS.
- the width and depth of the notches 17a in the vicinity of both ends of the blades 15 are provided in the center portion of the blades 15. It is set to be smaller than 17 width and depth.
- a multi-blade fan such as a crossflow fan has a plurality of side plates 14 in order to securely fix a plurality of blades 15 arranged in the circumferential direction and to ensure the strength of the impeller 7.
- Each side plate 14 is provided at both ends and the center of the impeller 7 in the longitudinal direction. Therefore, as shown in FIG. 34, in the vicinity of each side plate 14, since it is affected by the side plate 14, the flow velocity FV of air decreases.
- a sufficiently high wind speed FV can be obtained at the portion where the side plate 14 is not provided.
- the wind speed FV is much lower than the wind speed FV.
- the notch 17a is formed smaller than the notch 17 provided at the center of the blade 15. Thereby, the noise reduction effect by the notches 17 and 17a is fully maintained.
- the fan pressure can be further increased and the deterioration of the air blowing performance can be avoided as compared with the configuration in which notches 17 having the same size are provided intermittently over the entire blade 15.
- a multiblade fan according to an eighth embodiment will be described with reference to FIG.
- the width and depth of the notches 17a in the vicinity of both ends of the blades 15 are provided in the center portion of the blades 15. It is set smaller than 17.
- a multi-blade fan such as a crossflow fan has a plurality of side plates 14 in order to fix a plurality of blades 15 arranged in the circumferential direction and secure the strength of the impeller 7. ing .
- the side plates 14 are provided at both ends and the center of the impeller 7 in the longitudinal direction. Therefore, as shown in FIG. 34, in the vicinity of each side plate 14, since it is affected by the side plate 14, the air flow velocity FV decreases.
- the wind speed FV is much lower than the wind speed FV.
- the notch 17a in the vicinity of both ends of the blade 15 is formed smaller than the notch 17 provided in the central portion of the blade 15. Yes.
- the noise reduction effect by the notches 17 and 17a is fully maintained.
- the fan pressure can be further increased, and the deterioration of the blowing performance can be avoided.
- the side plate 14 when the side plate 14 is located in the vicinity of both ends of the impeller 7, that is, when the side plate 14 is adjacent to the side walls la and lb of the main casing 1, it is relatively small.
- the force for changing the degree of reduction of the notches 17a to be formed or the number of the notches 17a may be increased as appropriate.
- the air flow rate can be improved, and the blowing performance is improved as much as possible.
- the impeller 7 has side plates 14 at portions excluding both ends thereof.
- one or a plurality of notches 17a are provided at both ends of the impeller 7, and the notches 17a are relatively disposed. It may be formed small.
- the fan pressure can be further increased compared to a configuration in which notches 17 having the same size are provided intermittently.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Air-Conditioning Room Units, And Self-Contained Units In General (AREA)
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/224,724 US8029242B2 (en) | 2006-03-31 | 2007-03-26 | Multi-blade fan |
AU2007233449A AU2007233449B2 (en) | 2006-03-31 | 2007-03-26 | Multi-blade fan |
EP07739587.9A EP2003340B1 (en) | 2006-03-31 | 2007-03-26 | Cross-flow fan |
CN2007800094721A CN101405506B (zh) | 2006-03-31 | 2007-03-26 | 多翼风扇 |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2006-097078 | 2006-03-31 | ||
JP2006097078 | 2006-03-31 | ||
JP2007-062198 | 2007-03-12 | ||
JP2007062198A JP4973249B2 (ja) | 2006-03-31 | 2007-03-12 | 多翼ファン |
Publications (1)
Publication Number | Publication Date |
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WO2007114090A1 true WO2007114090A1 (ja) | 2007-10-11 |
Family
ID=38563359
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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PCT/JP2007/056148 WO2007114090A1 (ja) | 2006-03-31 | 2007-03-26 | 多翼ファン |
Country Status (7)
Country | Link |
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US (1) | US8029242B2 (ja) |
EP (1) | EP2003340B1 (ja) |
JP (1) | JP4973249B2 (ja) |
KR (1) | KR100985958B1 (ja) |
CN (1) | CN101405506B (ja) |
AU (1) | AU2007233449B2 (ja) |
WO (1) | WO2007114090A1 (ja) |
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WO2009136584A1 (ja) * | 2008-05-09 | 2009-11-12 | ダイキン工業株式会社 | クロスフローファン及びこれを備えた空気調和機 |
JP2010014123A (ja) * | 2008-05-09 | 2010-01-21 | Daikin Ind Ltd | クロスフローファン及びこれを備えた空気調和機 |
US20110033307A1 (en) * | 2008-05-09 | 2011-02-10 | Daikin Industries, Ltd. | Cross-flow fan and air conditioner equipped with same |
AU2009245175B2 (en) * | 2008-05-09 | 2011-12-22 | Daikin Industries, Ltd. | Cross-flow fan and air conditioner equipped with same |
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Also Published As
Publication number | Publication date |
---|---|
EP2003340A9 (en) | 2009-04-22 |
US20090028719A1 (en) | 2009-01-29 |
EP2003340A2 (en) | 2008-12-17 |
CN101405506A (zh) | 2009-04-08 |
EP2003340B1 (en) | 2017-08-30 |
CN101405506B (zh) | 2010-09-01 |
JP2007292053A (ja) | 2007-11-08 |
AU2007233449A1 (en) | 2007-10-11 |
AU2007233449B2 (en) | 2010-04-29 |
EP2003340A4 (en) | 2015-12-02 |
KR100985958B1 (ko) | 2010-10-06 |
US8029242B2 (en) | 2011-10-04 |
JP4973249B2 (ja) | 2012-07-11 |
KR20080104169A (ko) | 2008-12-01 |
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