WO2016090417A1 - Centrifugal fan - Google Patents
Centrifugal fan Download PDFInfo
- Publication number
- WO2016090417A1 WO2016090417A1 PCT/AU2015/000752 AU2015000752W WO2016090417A1 WO 2016090417 A1 WO2016090417 A1 WO 2016090417A1 AU 2015000752 W AU2015000752 W AU 2015000752W WO 2016090417 A1 WO2016090417 A1 WO 2016090417A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- impeller
- disc
- blades
- previous
- irregular edge
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/281—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/30—Vanes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- 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
- F05D2250/10—Two-dimensional
- F05D2250/18—Two-dimensional patterned
- F05D2250/184—Two-dimensional patterned sinusoidal
Definitions
- This invention concerns centrifugal fans. BACKGROUND
- Centrifugal fans are widely used in industry in a large range of power requirements and performance.
- the tips of blades are invariably disposed at 90° to the sides of the blades which are welded to the circular parts of the impeller. As the impeller rotates gas is drawn through the centre of the impeller and driven by the blades toward the housing and as each blade passes the fan exit a pressure change occurs and noise is generated. If the fan is inside a building and there are personnel in the vicinity, understanding speech may be difficult and the long term effect on people's hearing may become an issue.
- An object of the present invention is to ameliorate the aforementioned disadvantages of the prior art or to at least provide a useful alternative thereto.
- an impeller for a centrifugal fan wherein the impeller has an outer portion that has an irregular edge, the irregular edge forming an outer periphery of impeller.
- the outer edge may comprise a variety of different outlines, including jagged and wavy outlines.
- the outer portion may include at least one projection flanked by a pair of recesses.
- the outer portion may include a plurality of projections.
- the outer portion includes an edge with at least one prominent projections and two side recesses.
- the side recesses have side portions that extend outwardly partially or wholly as far radially as a central projection.
- the projections may be radiussed to minimise turbulence.
- the outline of the tip of the outer portion across its width may be in the form of a sawtooth configuration.
- the outer edge may provide scalloped, sinusoidal or other variants of such patterns or side edge profiles.
- the outer portion is expected to exhibit noise reduction compared to an impeller with straight blade tips or tips with a constant curvature.
- the corners of some prior art blades may be radiussed so as to join the hub at an acute angle rather than 90°. Such variations in the shape of the outer edge are too small to contribute a significant reduction in noise of prior art devices.
- the impeller of the present invention is configured by edge modification to ameliorate wind noise issues.
- An intermediate annular plate parallel to the impeller disc may divide the blades widthwise.
- the impeller blade may be reinforced intermediate the length of the outer edge.
- the reinforcement may include a rib radially aligned and in the form of a hollow disc or a radial band. The reinforcement increases the blade's rigidity.
- Useful noise reduction is measurable when the blade top has a pair of V-shaped excisions. Preferably, these excisions are separated by a V-shaped tooth substantially of the same size as the excision.
- the impeller may include one or more impeller discs configured to lie in a plane transverse to the rotational axis of the fan.
- a first impeller disc may define a rearmost panel of the impeller.
- the rear impeller disc is preferably flat or planar.
- the impeller may include an opposed or frontward disc whereby the rear disc and the opposite disc are longitudinally spaced and lying substantially in parallel planes.
- the front disc may be frusto conical in shape.
- the front disc defines a centre aperture.
- the centre aperture may be bordered by a radially spaced band or circular flange.
- the blades may extend between a first disc with a ratchet edge and the opposed disc in the form of a frusto conical plate.
- the first disc may be the rearmost impeller disc.
- the ratchet edge may define the outer peripheral edge of the first disc and may cooperate with a ratchet pawl or other spring biased detent.
- the ratchet mechanism may be adapted to regulate the rotational speed of the impeller.
- the fan may have 4-70 blades.
- the impeller has between 8 and 20 blades, and still more preferably between 8 - 12 blades.
- the invention is applicable to all centrifugal type fans including impeller blade shapes that are airfoil, backward inclined, flat backward inclined, curved backwardly inclined, radial, radial tip and forward curved, and the like.
- Figure 1 is a plan of an impeller from the inlet end with blades and ratchet disc in broken lines;
- Figure 2 is a mid section on Figure 1 ;
- Figure 3 is a plan of a blade;
- Figure 4 is a perspective from the ratchet disc direction;
- Figure 5 is a perspective from the opposite direction;
- Figure 6 is a side view showing the bush;
- Figure 7 is a plan of a impeller with aerofoil blades.
- an impeller 1 that is part of a centrifugal fan used for pumping fluid, including gas, further including air, where the rotational speed of a tip or corner 22 of a blade 14 is more than 400 k/hr.
- the impeller is made of welded steel components.
- the impeller 1 includes a disc 2 which has a ratchet wheel shape with a steel bush 4 at its centre.
- the bush 4 has a key way 6. This forms a closed face of the impeller 1.
- Bush 4 is preferably braced.
- the brace may include multiple triangular and radially aligned struts or a cone 8.
- the brace 8 extends radially inwardly from disc 2.
- An open face 3 of the impeller 1 is defined by frusto-conical plate 10.
- the plate 10 has an entry aperture 5 which is surrounded by circular flange 12.
- the impeller includes a plurality of blades 14 that each have a side 16 and a root end 18 aligned at substantially and preferably 90° to the side 16.
- the impeller 1 may include more or less blades 14, preferably 10 or 12.
- An opposite edge 20 to the side edge 16 is inclined to match a slope of the frusto-conical plate 10.
- the corner 22 junction between the root end 18 and the side 20 is radiussed advantageously to reduce turbulence.
- the blade 14 has a tip end 25 that has a plurality of teeth, advantageously comprising three teeth 24 and two half teeth 26.
- the tip 25 is cleft by a notch, cut-out or slot 28.
- the root end 18 is cleft by an inclined notch 30.
- the notches 28,30 ideally lie transverse of the tip end 25 and the root end 18 at a location intermediate the length of either end 18,25
- the disc 2 includes a set of ratchet teeth 32.
- the impeller 1 ideally includes twelve blades 14.
- the blades 14 arc arranged around the frusto-conical plate 10 so that a curve of each blade 14 matches the curvature of the ratchet teeth 32.
- the blades 14 are stabilised by a flat outer circumferential ring 34 which projects and inserts into the tip notch 28 of each of the blades 14.
- the blades 14 a re further stabilised by an inner inclined ring 36 which projects into each of the root notches 30 of the blades 14.
- the blades 14 are of ideally of uniform thickness.
- the outer ring 34 divides the tip edge into two side by side arrays of a central V-shaped tooth 24 with a half tooth 26 on both sides (see Figure 4).
- an impeller la is shown having ten blades 38 which a are similarly arranged compared to the embodiment of Figs. 1 - 4, but instead are of aerofoil section in side profile.
- the disc 2 is circular, rather than having radially outwardly extending ratchet teeth 32.
- An air gap 40 or circumferential spacing between the blades 38 is similar to that provided between the blades 14 of Figure 1.
- member may refer to singular or plural items and are terms intended to refer to a set of properties, functions or characteristics performed by one or more items or components having one or more parts. It is envisaged that where an "apparatus”, “means”, “device” or “member” or similar term is described as being a unitary object, then a functionally equivalent object having multiple components is considered to fall within the scope of the term, and similarly, where an "apparatus”, “assembly”, “means”, “device” or “member” is described as having multiple components, a functionally equivalent but unitary object is also considered to fall within the scope of the term, unless the contrary is expressly stated or the context requires otherwise.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
An impeller (1) forms part of a centrifugal fan used for pumping fluid. The impeller (1) includes a disc (2) which has a ratchet wheel shape with a steel bush (4) at its centre. The bush (4) has a keyway (6). This forms a closed face of the impeller (1). Bush (4) is preferably braced. The brace may include multiple triangular and radially aligned struts or a cone (8). The brace (8) extends radially inwardly from disc (2). An open face (3) of the impeller (1) is defined by frusto-conical plate (10). The plate (10) has an entry aperture (5) which is surrounded by circular flange (12).
Description
TI TLE OF INVENTION
Centrifugal Fan
TECHNICAL FIELD
This invention concerns centrifugal fans. BACKGROUND
The following references to and descriptions of prior proposals or products are not intended to be, and are not to be construed as, statements or admissions of common general knowledge in the art. In particular, the following prior art discussion does not relate to what is commonly or well known by the person skilled in the art, but assists in the understanding of the inventive step of the present invention of which the identification of pertinent prior art proposals is but one part.
Centrifugal fans are widely used in industry in a large range of power requirements and performance.
When impellers have forwardly curved blades, the blades curve in the direction of the fans rotation. Backwardly curved blades curve in the opposite direction. Backwardly curved blades may have an aerofoil section. Both types propel gas streams efficiently. A third type has radial blades and of the three tends to be noisiest. It is the noise factor with which this invention is concerned.
Technical Problem The tips of blades are invariably disposed at 90° to the sides of the blades which are welded to the circular parts of the impeller. As the impeller rotates gas is drawn through the centre of the impeller and driven by the blades toward the housing and as each blade passes the fan exit a pressure change occurs and noise is generated. If the fan is inside a building and there are personnel in the vicinity, understanding speech may be difficult and the long term effect on people's hearing may become an issue.
Attempts have been made to modify the airflow through such fans but no worthwhile reduction in noise has resulted.
An object of the present invention is to ameliorate the aforementioned disadvantages
of the prior art or to at least provide a useful alternative thereto. SUMMARY OF I VENTION
The invention according to one or more aspects is as defined in the independent claims. Some optional and/or preferred features of the invention are defined in the dependent claims.
Accordingly, in one aspect of the invention, there is provided an impeller for a centrifugal fan, wherein the impeller has an outer portion that has an irregular edge, the irregular edge forming an outer periphery of impeller.
The outer edge may comprise a variety of different outlines, including jagged and wavy outlines. The outer portion may include at least one projection flanked by a pair of recesses. The outer portion may include a plurality of projections. Preferably, the outer portion includes an edge with at least one prominent projections and two side recesses. Preferably, the side recesses have side portions that extend outwardly partially or wholly as far radially as a central projection. The projections may be radiussed to minimise turbulence.
The outline of the tip of the outer portion across its width may be in the form of a sawtooth configuration. Alternatively, the outer edge may provide scalloped, sinusoidal or other variants of such patterns or side edge profiles.
Advantageously, the outer portion is expected to exhibit noise reduction compared to an impeller with straight blade tips or tips with a constant curvature. The corners of some prior art blades may be radiussed so as to join the hub at an acute angle rather than 90°. Such variations in the shape of the outer edge are too small to contribute a significant reduction in noise of prior art devices. In contrast, the impeller of the present invention is configured by edge modification to ameliorate wind noise issues. An intermediate annular plate parallel to the impeller disc may divide the blades widthwise. Furthermore, the impeller blade may be reinforced intermediate the length of the outer edge. The reinforcement may include a rib radially aligned and in the form of a hollow disc or a radial band. The reinforcement increases the blade's rigidity.
Useful noise reduction is measurable when the blade top has a pair of V-shaped excisions. Preferably, these excisions are separated by a V-shaped tooth substantially of the same size as the excision.
The impeller may include one or more impeller discs configured to lie in a plane transverse to the rotational axis of the fan. A first impeller disc may define a rearmost panel of the impeller. The rear impeller disc is preferably flat or planar. The impeller may include an opposed or frontward disc whereby the rear disc and the opposite disc are longitudinally spaced and lying substantially in parallel planes. The front disc may be frusto conical in shape. Preferably, the front disc defines a centre aperture. The centre aperture may be bordered by a radially spaced band or circular flange.
The blades may extend between a first disc with a ratchet edge and the opposed disc in the form of a frusto conical plate. The first disc may be the rearmost impeller disc.
The ratchet edge may define the outer peripheral edge of the first disc and may cooperate with a ratchet pawl or other spring biased detent. The ratchet mechanism may be adapted to regulate the rotational speed of the impeller.
The fan may have 4-70 blades. Preferably, the impeller has between 8 and 20 blades, and still more preferably between 8 - 12 blades.
Advantageous Effects of Invention
1. Noticeable noise reduction. 2. The invention is applicable to all centrifugal type fans including impeller blade shapes that are airfoil, backward inclined, flat backward inclined, curved backwardly inclined, radial, radial tip and forward curved, and the like.
BRIEF DESCRIPTION OF DRAWINGS
The invention may be better understood from the following non-limiting description of preferred embodiments, in which:
Figure 1 is a plan of an impeller from the inlet end with blades and ratchet disc in broken lines;
Figure 2 is a mid section on Figure 1 ;
Figure 3 is a plan of a blade;
Figure 4 is a perspective from the ratchet disc direction; Figure 5 is a perspective from the opposite direction; Figure 6 is a side view showing the bush; and Figure 7 is a plan of a impeller with aerofoil blades. DETAILED DESCRIPTION OF THE DRAWINGS
Preferred features of the present invention will now be described with particular reference to the accompanying drawings. However, it is to be understood that the features illustrated in and described with reference to the drawings are not to be construed as limiting on the scope of the invention.
Referring firstly to Figures 1-4, there is shown an impeller 1 that is part of a centrifugal fan used for pumping fluid, including gas, further including air, where the rotational speed of a tip or corner 22 of a blade 14 is more than 400 k/hr. The impeller is made of welded steel components. The impeller 1 includes a disc 2 which has a ratchet wheel shape with a steel bush 4 at its centre. The bush 4 has a key way 6. This forms a closed face of the impeller 1. Bush 4 is preferably braced. The brace may include multiple triangular and radially aligned struts or a cone 8. The brace 8 extends radially inwardly from disc 2. An open face 3 of the impeller 1 is defined by frusto-conical plate 10. The plate 10 has an entry aperture 5 which is surrounded by circular flange 12.
The impeller includes a plurality of blades 14 that each have a side 16 and a root end 18 aligned at substantially and preferably 90° to the side 16. The impeller 1 may include more or less blades 14, preferably 10 or 12. An opposite edge 20 to the side edge 16 is inclined to match a slope of the frusto-conical plate 10. The corner 22 junction between the root end 18 and the side 20 is radiussed advantageously to reduce turbulence. The blade 14 has a tip end 25 that has a plurality of teeth, advantageously comprising three teeth 24 and two half teeth 26.
The tip 25 is cleft by a notch, cut-out or slot 28. The root end 18 is cleft by an inclined notch 30. The notches 28,30 ideally lie transverse of the tip end 25 and the root end 18 at a location intermediate the length of either end 18,25
The disc 2 includes a set of ratchet teeth 32. The impeller 1 ideally includes twelve blades 14. The blades 14 arc arranged around the frusto-conical plate 10 so that a curve of each blade 14 matches the curvature of the ratchet teeth 32. The blades 14 are stabilised by a flat outer circumferential ring 34 which projects and inserts into the tip notch 28 of each of the blades 14. The blades 14 a re further stabilised by an inner inclined ring 36 which projects into each of the root notches 30 of the blades 14. The blades 14 are of ideally of uniform thickness. The outer ring 34 divides the tip edge into two side by side arrays of a central V-shaped tooth 24 with a half tooth 26 on both sides (see Figure 4).
In Figure 7, an impeller la is shown having ten blades 38 which a are similarly arranged compared to the embodiment of Figs. 1 - 4, but instead are of aerofoil section in side profile. In another variation of the first embodiment, the disc 2 is circular, rather than having radially outwardly extending ratchet teeth 32.
An air gap 40 or circumferential spacing between the blades 38 is similar to that provided between the blades 14 of Figure 1.
Throughout the specification and claims the word "comprise" and its derivatives are intended to have an inclusive rather than exclusive meaning unless the contrary is expressly stated or the context requires otherwise. That is, the word "comprise" and its derivatives will be taken to indicate the inclusion of not only the listed components, steps or features that it directly references, but also other components, steps or features not specifically listed, unless the contrary is expressly stated or the context requires otherwise.
In the present specification, terms such as "apparatus", "means", "device" and
"member" may refer to singular or plural items and are terms intended to refer to a set of properties, functions or characteristics performed by one or more items or components having one or more parts. It is envisaged that where an "apparatus",
"means", "device" or "member" or similar term is described as being a unitary object, then a functionally equivalent object having multiple components is considered to fall within the scope of the term, and similarly, where an "apparatus", "assembly", "means", "device" or "member" is described as having multiple components, a functionally equivalent but unitary object is also considered to fall within the scope of the term, unless the contrary is expressly stated or the context requires otherwise.
Orientational terms used in the specification and claims such as vertical, horizontal, top, bottom, upper and lower are to be interpreted as relational and are based on the premise that the component, item, article, apparatus, device or instrument will usually be considered in a particular orientation which will be understood by the skilled reader from the context.
The illustrations, photographs and drawings, if any, form part of the disclosure of this specification as does the description, illustrations, photographs and drawings of any associated provisional or parent specification or of any priority document, if any, all of which are imported hereinto as part of the record hereof.
Finally it is to be understood that various alterations, modifications and/or additions may be incorporated into the various constructions and arrangements or parts without departing from the spirit and ambit of the invention.
Claims
An impeller for a centrifugal fan comprising a rear disc and a plurality of impeller blades extending forward of the rear disc,
wherein the impeller blades each have an outer portion that has an irregular edge.
The impeller of Claim 1, wherein the irregular edge forms an outer periphery of impeller spaced radially from a rotational axis of the impeller.
The impeller of Claim 1 or 2, wherein the impeller is aligned at an angle between 0° and an obtuse angle relative to the rotational axis.
The impeller of Claim 3, wherein the angle is between substantially 0° and
10°.
The impeller of any one of previous claims, wherein the rear disc is a planar disc.
The impeller of any one of previous claims, wherein the rear disc has radially extending ratchet teeth.
The impeller of any one of Claims 1- 5, wherein the rear disc is a substantially circular disc.
The impeller of any one of the previous claims, wherein the irregular edge comprises a jagged outlines.
The impeller of any one of the previous claims, wherein the irregular edge comprises a wavy outlines.
The impeller of any one of the previous claims, wherein the irregular edge includes at least one curved projection flanked by a pair of recesses.
The impeller of Claim 10, wherein the projection is radiussed to minimise turbulence.
The impeller of any one of the previous claims, wherein the impeller further includes an intermediate annular plate parallel to the rear impeller disc The impeller of Claim 12, wherein the intermediate annular plate divides each of the blades widthwise.
The impeller of Claim 12 or 13, wherein each impeller blade is reinforced intermediate the length of the outer portion.
15. The impeller of Claim 14, wherein the reinforcement includes a rib radially aligned and in the form of an annular disc.
16. The impeller of any one of Claims 1 - 1 1, wherein the rear disc is a first impeller disc defining a rearmost panel of the impeller and the impeller further includes a second disc whereby the rear disc and the second disc are longitudinally spaced and lying substantially in parallel planes.
17. The impeller of any one of Claims 1 - 1 1, wherein the second disc is a front disc that is frusto conical in shape.
18. The impeller of any one of the previous claims, wherein the number of blades is 8 - 12.
19. The impeller of any one of claims! 6 - 18, wherein the second disc is frusto- conical in shape
20. The impeller of any one of the previous claims, wherein blades are aerofoil in profile.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AU2014905037 | 2014-12-12 | ||
AU2014905037A AU2014905037A0 (en) | 2014-12-12 | Centrifugal Fan |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2016090417A1 true WO2016090417A1 (en) | 2016-06-16 |
Family
ID=56106301
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/AU2015/000752 WO2016090417A1 (en) | 2014-12-12 | 2015-12-14 | Centrifugal fan |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2016090417A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106640752A (en) * | 2016-12-19 | 2017-05-10 | 宁波方太厨具有限公司 | Impeller of kitchen ventilator |
IT201700058843A1 (en) * | 2017-05-30 | 2018-11-30 | Ma Ti Ka S R L | FAN FOR OVENS AND METHOD OF REALIZATION OF THAT FAN |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2546280A1 (en) * | 1975-10-16 | 1977-04-21 | Kodak Ag | Centrifugal fan impeller with blades parallel to axis - has blade edges with sawtooth serrations arranged in comb fashion |
EP0440048A1 (en) * | 1990-02-02 | 1991-08-07 | ELETTROVAGO S.p.A. | Fan impeller |
JPH11141494A (en) * | 1997-11-10 | 1999-05-25 | Daikin Ind Ltd | Impeller structure of multiblade blower |
EP0942175B1 (en) * | 1997-09-30 | 2004-11-24 | Daikin Industries, Limited | Centrifugal blower, method of manufacturing the same, and air-conditioner provided with the same |
CN103696985A (en) * | 2013-11-30 | 2014-04-02 | 宁波方太厨具有限公司 | Centrifugal fan impeller |
-
2015
- 2015-12-14 WO PCT/AU2015/000752 patent/WO2016090417A1/en active Application Filing
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2546280A1 (en) * | 1975-10-16 | 1977-04-21 | Kodak Ag | Centrifugal fan impeller with blades parallel to axis - has blade edges with sawtooth serrations arranged in comb fashion |
EP0440048A1 (en) * | 1990-02-02 | 1991-08-07 | ELETTROVAGO S.p.A. | Fan impeller |
EP0942175B1 (en) * | 1997-09-30 | 2004-11-24 | Daikin Industries, Limited | Centrifugal blower, method of manufacturing the same, and air-conditioner provided with the same |
JPH11141494A (en) * | 1997-11-10 | 1999-05-25 | Daikin Ind Ltd | Impeller structure of multiblade blower |
CN103696985A (en) * | 2013-11-30 | 2014-04-02 | 宁波方太厨具有限公司 | Centrifugal fan impeller |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106640752A (en) * | 2016-12-19 | 2017-05-10 | 宁波方太厨具有限公司 | Impeller of kitchen ventilator |
IT201700058843A1 (en) * | 2017-05-30 | 2018-11-30 | Ma Ti Ka S R L | FAN FOR OVENS AND METHOD OF REALIZATION OF THAT FAN |
EP3410021A1 (en) * | 2017-05-30 | 2018-12-05 | MA.TI.KA. S.r.l. | Fan for ovens, oven and method for making said fan |
US10648677B2 (en) | 2017-05-30 | 2020-05-12 | Ma. Ti.Ka. S.R.L. | Fan for ovens |
RU2761979C2 (en) * | 2017-05-30 | 2021-12-14 | Ма.Ти.Ка. С.Р.Л. | Fan for furnaces and method for manufacturing the specified fan |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3470686B1 (en) | Propeller fan | |
KR102196815B1 (en) | Radial or mixed-flow compressor diffuser having vanes | |
CN201560963U (en) | High-efficiency axial flow fan | |
JP5737666B2 (en) | Impellers used for centrifugal or mixed flow fans | |
JPS5990797A (en) | Centrifugal compressor and compression method | |
US20160076551A1 (en) | Impeller and fluid machine | |
UA92141C2 (en) | Centrifugal fan | |
WO2011062062A1 (en) | Multi-blade fan for centrifugal blower | |
US20170356673A1 (en) | Ventilator Unit | |
JP2018514691A5 (en) | ||
EP2787172A3 (en) | Blade grid with side wall contours and turbomachine | |
DE602007001234D1 (en) | IMPROVED WHEEL AND FAN | |
US8926278B2 (en) | Fan and fan frame thereof | |
JP2015094293A5 (en) | ||
CN102168687B (en) | Compressor first-stage blade with hub diameter of phi 762 | |
US20120121421A1 (en) | Flow vector control for high speed centrifugal pumps | |
US20150152879A1 (en) | Blade structure of axial fan | |
WO2016090417A1 (en) | Centrifugal fan | |
JP2016061241A5 (en) | ||
JP2016102467A (en) | Blower device | |
JP6121046B2 (en) | Axial blower | |
US8313299B2 (en) | Frustoconical centrifugal wheel | |
US9926943B2 (en) | Axial blower | |
CN103161755B (en) | Industrial blower impeller | |
JP5305460B2 (en) | Axial blower |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 15867134 Country of ref document: EP Kind code of ref document: A1 |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 15867134 Country of ref document: EP Kind code of ref document: A1 |