CN101349282A - Impeller set - Google Patents
Impeller set Download PDFInfo
- Publication number
- CN101349282A CN101349282A CNA200710136070XA CN200710136070A CN101349282A CN 101349282 A CN101349282 A CN 101349282A CN A200710136070X A CNA200710136070X A CN A200710136070XA CN 200710136070 A CN200710136070 A CN 200710136070A CN 101349282 A CN101349282 A CN 101349282A
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- CN
- China
- Prior art keywords
- guide ring
- guide
- impeller
- rib
- impeller sets
- Prior art date
- Legal status (The legal status 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 status listed.)
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Abstract
The invention discloses an impeller assembly, which comprises an impeller and at least one guide ring, the guide ring is provided with a guide surface, the other surface of the guide ring is an inner side surface, the guide ring is equipped with ribs, the guide ring is assembled in a gap arranged behind the rear edges of blades arranged on the circumference of the hub of the impeller to form the impeller assembly, and the ribs are located at an air outlet end of a wind guide groove arranged between two blades, according to this design, ribs, particularly the ribs with wing-shaped cross sections decrease air flow resistance, pressure of blown out air is increased, thereby the flow field is smoothed to save energy, and when the guide ring has more than one , the ribs are connected to support inner guide rings and outer guide rings, which obtains the practical efficiency of simplifying operation.
Description
Technical field
The invention relates to a kind of combination type blade wheel group, it is provided with rib on the guide ring of impeller, can simplify operation to increase smooth and easy flow field of blast and tool connection guide ring.
Background technique
The impeller sets 200 of existing a kind of tool guide ring 25 cooperates referring to shown in Fig. 7,8,9, and the impeller sets 200 of this kind tool guide ring comprises:
At least one guide ring 25, it is arranged in the breach 24 of blade 21 trailing edge air opening ends, guide ring 25 is ring structurees, when having an above guide ring 25, be interior guide ring 25 near wheel hub, then be outer guide ring 25 away from wheel hub, guide ring 25 outer periphery tool guide faces 26, its another side is an inner side surface, and guide face 26 is a hypotenuse type or streamlined, and establishes the usefulness that flange 27 is thought the location in guide ring 25 air opening end inboards;
Again, the electronic equipment arithmetic speed is more and more fast, and the heat that is produced is also many, how to increase heat dissipation, and enhances productivity and be the important topic that industry desires to overcome solution.
Summary of the invention
Because the shortcoming of the impeller sets of existing tool guide ring, the technical problem to be solved in the present invention provides a kind of impeller sets, it utilizes and rib to be set on guide ring to increase the pressure of air-flow that impeller sets blows out and smooth and easy flow field with energy-conservation, the operation when simplification is provided with a plurality of guide ring.
For solving the problems of the technologies described above, the present invention proposes a kind of " impeller sets ", it comprises:
One impeller, and at least one guide ring combine, guide ring is a ring structure, its periphery outside tool guide face, another side is an inner side surface, guide face can be hypotenuse type or streamlined, inner side surface also can be hypotenuse type, streamlined or vertical-type, and the guide face at guide ring is established rib, the section of this rib can be the geometric modeling that airfoil, circle, rectangle, triangle or other tool connect supporting effect, when being more than one guide ring, be connected with rib between interior guide ring and outer guide ring, also can be simultaneously outside the guide face of guide ring be provided with wing leaf;
Impeller, tool one wheel hub, and be located on several pieces blades of wheel hub periphery, and establish and guide ring sectional shape and the same number of breach at this trailing edge.Guide ring is arranged in the default breach of trailing edge and forms impeller sets, and rib then is positioned at the air opening end of air guide channel between two blades.
The advantage of structural design has thus, guide ring and outer guide ring in rib connects, and can simplify the program of making and assembling, thus reach the purpose that saves time; Utilize rib to support, make assembling easy and quick in the outer guide ring locating blade breach; Reach the resistance that more can lower air-flow with the airfoil cross section when rib, and increase the pressure of blow out air and smooth and easy flow field with energy-conservation, so get to when air and to treat that heat-dissipating thing is difficult for rebound back in the air guide channel or between the delay exhaust outlet, the present invention truly has the practical effect that can improve radiating efficiency and simplification operation.
Description of drawings
Fig. 1: the three-dimensional exploded view of first kind of embodiment's impeller sets of the present invention.
Fig. 2: the three-dimensional combination figure of first kind of embodiment's impeller sets of the present invention.
Fig. 3: the combination section of first kind of embodiment's impeller sets of the present invention.
Fig. 4: the three-dimensional combination section of second kind of embodiment's impeller sets of the present invention.
Fig. 5: the three-dimensional combination figure of the third embodiment's impeller sets of the present invention.
Fig. 6: the three-dimensional combination figure of the 4th kind of embodiment's impeller sets of the present invention.
Fig. 7: the three-dimensional combination figure of the impeller sets of existing tool guide ring.
Fig. 8: the three-dimensional exploded view of the impeller sets of existing tool guide ring.
Fig. 9: the sectional drawing of the impeller of existing tool guide ring.
Figure 10: the sectional drawing of the impeller sets of the existing a plurality of guide rings of tool.
Description of reference numerals:
<the present invention 〉
100 impeller sets, 10 impellers
11 blades, 12 wheel hubs
13 air guide channels, 14 breach
15 guide rings, 16 guide faces
17 flanges, 18 ribs
19 wing leaves
<existing
200 impeller sets, 20 impellers
21 blades, 22 wheel hubs
23 air guide channels, 24 breach
25 guide rings, 26 guide faces
27 flanges
Embodiment
Please cooperate referring to shown in 1,2,3 figure, it is first kind of example structure of impeller sets of the present invention, and this impeller sets 100 comprises:
More than one guide ring 15, it is arranged in the breach 14 of the air guide channel 13 trailing edge air opening ends between blade 11 and the blade 11, guide ring 15 is ring structurees, guide ring 15 outer periphery rings are established guide face 16, and its another side is an inner side surface, when being an above guide ring 15, near wheel hub is interior guide ring 15, away from wheel hub then is outer guide ring 15, in the inboard position flange 17 of setting of interior guide ring 15 air opening ends, to locate with wheel hub 12 root edge clips, be connected with rib 18 between the guide face 16 of interior guide ring 15 and the inner side surface of outer guide ring 15, rib 18 is positioned between two blades among the air guide channel 13, and the sectional shape of rib 18 can be rectangle, circular, triangle or airfoil, be airfoil shown in the figure, and on the guide face 16 of outer guide ring 15, establish to wing leaf 19 is arranged;
Please cooperate referring to shown in Figure 4, it is second kind of example structure of impeller sets of the present invention, and this impeller sets 100 comprises:
The more than one guide ring 15 of tool, it is arranged in the breach 14 of the air guide channel 13 trailing edge air opening ends between blade 11 and the blade 11, be connected with rib 18 between the guide face 16 of interior guide ring 15 and the inner side surface of outer guide ring 15, rib 18 is positioned between two blades among the air guide channel, and rib 18 sections are airfoil.
Please cooperate referring to shown in Figure 5, it is for the third example structure of impeller sets of the present invention, this impeller sets 100 and second kind of different being of embodiment: the guide face 16 of this outer guide ring 15 is provided with 2 wing leaves 19, and described wing leaf 19 is arranged in the air guide channel 13 of 11 in two blades.
Please cooperate referring to shown in Figure 6, it is for the 4th kind of example structure of impeller sets of the present invention, this impeller sets 100 is the design of single guide ring 15, and rib 18 sections are airfoil then on the guide face 16 of its guide ring 15, is positioned at 11 air guide channel 13 air opening ends of two blades.
Via the detailed description of said structure feature, can know and find out that characteristics of the present invention are:
1. connect with rib when above when guide ring is one, can simplify and make and the program of assembling, thereby Reach the timesaving purpose.
2. work as the resistance that rib can lower air-flow with the airfoil cross section, the pressure and the tool that more increase blow out air are suitable Channel Group's field effect.
3. the rear rib that connects that utilizes in interior guide ring location supports outer guide ring, makes the easy locating blades of outer guide ring In the breach.
Claims (5)
1. an impeller sets is characterized in that, comprising:
At least one guide ring, this guide ring periphery has guide face and inner side surface, and this guide ring is provided with rib;
One impeller, has a wheel hub, and be located on several pieces blades of this wheel hub periphery, form air guide channel between blade and blade, trailing edge is established sectional shape and the same number of breach with this guide ring, this guide ring is assembled in and forms combination in the breach of trailing edge, and this rib then is positioned at the air opening end of air guide channel between two blades.
2. impeller sets according to claim 1 is characterized in that, when being an above guide ring, and the inner side surface of the guide face of guide ring and outer guide ring in connecting with rib.
3. as impeller sets as described in the claim 2, it is characterized in that the guide face of guide ring is provided with at least one wing leaf outside.
4. as impeller sets as described in the claim 2, it is characterized in that the cross section of this rib is an airfoil.
5. impeller sets according to claim 1 is characterized in that the cross section of this rib is an airfoil.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNA200710136070XA CN101349282A (en) | 2007-07-16 | 2007-07-16 | Impeller set |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CNA200710136070XA CN101349282A (en) | 2007-07-16 | 2007-07-16 | Impeller set |
Publications (1)
Publication Number | Publication Date |
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CN101349282A true CN101349282A (en) | 2009-01-21 |
Family
ID=40268202
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNA200710136070XA Pending CN101349282A (en) | 2007-07-16 | 2007-07-16 | Impeller set |
Country Status (1)
Country | Link |
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CN (1) | CN101349282A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102635571A (en) * | 2012-03-30 | 2012-08-15 | 中山市威宇技研机电有限公司 | Fan blade |
CN103375434A (en) * | 2012-04-20 | 2013-10-30 | 协禧电机股份有限公司 | Cooling fan |
CN105102823A (en) * | 2013-02-08 | 2015-11-25 | 苏尔寿管理有限公司 | Turbomachine, and flow conducting element for turbomachine |
CN106837866A (en) * | 2016-09-12 | 2017-06-13 | 东莞市卓奇电子科技有限公司 | Noise-and-vibration-reduction impeller |
CN110118195A (en) * | 2018-02-07 | 2019-08-13 | 广东美的制冷设备有限公司 | Axial-flow windwheel and air conditioner |
CN110118193A (en) * | 2018-02-07 | 2019-08-13 | 广东美的制冷设备有限公司 | Axial-flow windwheel and air conditioner |
-
2007
- 2007-07-16 CN CNA200710136070XA patent/CN101349282A/en active Pending
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102635571A (en) * | 2012-03-30 | 2012-08-15 | 中山市威宇技研机电有限公司 | Fan blade |
CN103375434A (en) * | 2012-04-20 | 2013-10-30 | 协禧电机股份有限公司 | Cooling fan |
CN103375434B (en) * | 2012-04-20 | 2015-08-12 | 协禧电机股份有限公司 | Radiation fan |
CN105102823A (en) * | 2013-02-08 | 2015-11-25 | 苏尔寿管理有限公司 | Turbomachine, and flow conducting element for turbomachine |
CN106837866A (en) * | 2016-09-12 | 2017-06-13 | 东莞市卓奇电子科技有限公司 | Noise-and-vibration-reduction impeller |
CN110118195A (en) * | 2018-02-07 | 2019-08-13 | 广东美的制冷设备有限公司 | Axial-flow windwheel and air conditioner |
CN110118193A (en) * | 2018-02-07 | 2019-08-13 | 广东美的制冷设备有限公司 | Axial-flow windwheel and air conditioner |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |
Open date: 20090121 |