CN201152279Y - Single-stage low speed blast engine blade wheel device - Google Patents
Single-stage low speed blast engine blade wheel device Download PDFInfo
- Publication number
- CN201152279Y CN201152279Y CNU2007200866762U CN200720086676U CN201152279Y CN 201152279 Y CN201152279 Y CN 201152279Y CN U2007200866762 U CNU2007200866762 U CN U2007200866762U CN 200720086676 U CN200720086676 U CN 200720086676U CN 201152279 Y CN201152279 Y CN 201152279Y
- Authority
- CN
- China
- Prior art keywords
- impeller
- low speed
- stage low
- blade
- wheel device
- 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.)
- Expired - Fee Related
Links
- 238000009434 installation Methods 0.000 claims abstract description 4
- 210000003205 muscle Anatomy 0.000 abstract 1
- 230000003014 reinforcing effect Effects 0.000 abstract 1
- 238000000034 method Methods 0.000 description 2
Images
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The utility model relates to the field of fans, in particular to an impeller device of a single-stage and low-speed fan. A turntable of the impeller is added with reinforcing muscles, the blades in the impeller are composed of half of long pieces and half of short pieces, and the outlet installation angle of the impeller is between 55 and 60 degrees. Adopting the technical proposal, on the basis of former rotary speed and adding blade number of the impeller, the fan performance and efficiency are enhanced, and cost is reduced.
Description
Technical field
The utility model relates to the blower field, is a kind of impeller unit of single-stage low speed blower.
Background technique
Single-stage low speed blower uses widely at each industrial department, according to design theory in the past, along with the increase of blade exit established angle, flow coefficient should increase, like this, the particularly design of chemical industry Intermediate High Pressure small-flow blower, the ratio of blade exit width and impeller cylindrical is very little, and efficient is low, the rev up or increase impeller progression and reach requirement of having to, like this, increased cost of production.
Summary of the invention
The purpose of this utility model is that a kind of new impeller unit will be provided, and need not rev up or increases impeller progression, just can reach designing requirement.
The utility model is achieved in that on the wheel disc of impeller increases strength bar, and the blade in the impeller the inside is that deviated splitter vane is formed, and respectively is half, and the exit installation angle of blade is 55 degree~60 degree.
Owing to adopted technique scheme, at rev up not or increase on the basis of the number of blade of impeller, improved fan performance and efficient, reduced cost.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is a cross-sectional view of the present utility model.
In the drawings: 1, established angle; 2, linear leaf; 3, short blade; 4, strength bar; 5, impeller shroud; 6, hub disk; 7, impeller
Embodiment
Down in that the utility model is further described in conjunction with the accompanying drawings and embodiments.
In Fig. 1 and Fig. 2: increase strength bar 4 on the hub disk 6 of impeller 7, the blade in impeller 7 the insides is that linear leaf 2 and short blade 3 are formed, and respectively is half, and the exit installation angle 1 of blade is 55 degree~60 degree.
Claims (1)
1, the impeller unit of single-stage low speed blower, it is characterized in that going up increase strength bar (4) at the hub disk (6) of impeller (7), blade in impeller (7) the inside is that linear leaf (2) and short blade (3) are formed, and respectively is half, and the exit installation angle of blade (1) is 55 degree~60 degree.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200866762U CN201152279Y (en) | 2007-08-23 | 2007-08-23 | Single-stage low speed blast engine blade wheel device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200866762U CN201152279Y (en) | 2007-08-23 | 2007-08-23 | Single-stage low speed blast engine blade wheel device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201152279Y true CN201152279Y (en) | 2008-11-19 |
Family
ID=40127957
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007200866762U Expired - Fee Related CN201152279Y (en) | 2007-08-23 | 2007-08-23 | Single-stage low speed blast engine blade wheel device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201152279Y (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102797702A (en) * | 2012-08-20 | 2012-11-28 | 上海通用风机股份有限公司 | Narrowly welded impeller of small-flow centrifugal fan and centrifugal fan |
| CN103775377A (en) * | 2013-12-31 | 2014-05-07 | 江苏大学 | Torque flow pump hydraulic design method by adopting long-short vanes |
| CN103850981A (en) * | 2012-12-04 | 2014-06-11 | 杜尔牙科股份有限公司 | Medical or dental fan |
| CN108953222A (en) * | 2018-08-16 | 2018-12-07 | 泛仕达机电股份有限公司 | A kind of centrifugal impeller |
-
2007
- 2007-08-23 CN CNU2007200866762U patent/CN201152279Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102797702A (en) * | 2012-08-20 | 2012-11-28 | 上海通用风机股份有限公司 | Narrowly welded impeller of small-flow centrifugal fan and centrifugal fan |
| CN103850981A (en) * | 2012-12-04 | 2014-06-11 | 杜尔牙科股份有限公司 | Medical or dental fan |
| CN103775377A (en) * | 2013-12-31 | 2014-05-07 | 江苏大学 | Torque flow pump hydraulic design method by adopting long-short vanes |
| CN108953222A (en) * | 2018-08-16 | 2018-12-07 | 泛仕达机电股份有限公司 | A kind of centrifugal impeller |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201297278Y (en) | Closed vane wheel with S-shaped novel vanes dedicated to small high-speed centrifugal fan | |
| CN202091251U (en) | Intermediate blade of compressor with hub with diameter of phi 940 | |
| CN102506029A (en) | Centrifugal fan impeller and centrifugal fan | |
| TWI256441B (en) | Axial flow fan | |
| CN201152279Y (en) | Single-stage low speed blast engine blade wheel device | |
| CN104033422B (en) | A kind of small axial flow fan of band splitterr vanes | |
| CN202937480U (en) | Multistage impeller centrifugal blower | |
| TW200624674A (en) | Axial-flow heat-dissipating fan | |
| KR101817956B1 (en) | Impeller for a blower | |
| CN205173055U (en) | Low noise that trailing edge is buckled does not have spiral case fan wheel | |
| CN203384065U (en) | Multi-vane fan | |
| CN202228423U (en) | Double-suction semi-open type impeller centrifugal blower | |
| CN222797761U (en) | Blade for centrifugal fan, double suction centrifugal impeller using the blade and fan | |
| CN204553344U (en) | Double-sucking type centrifugal blower | |
| CN201696309U (en) | High speed air centrifugal blower for coal chemical industry | |
| CN102979765A (en) | Blower volute with multi-layer guide blade air inlet structure of intermediate plate | |
| CN101334041A (en) | Star-shaped vane closed impeller for small-sized high speed centrifugal blower fan | |
| CN211474517U (en) | High-efficient centrifugal impeller of multistage | |
| CN209959557U (en) | Centrifugal blower impeller and centrifugal blower thereof | |
| CN209959556U (en) | Blade of centrifugal blower impeller | |
| CN205207221U (en) | Fan | |
| CN209959561U (en) | High pneumatic load blade of centrifugal blower impeller | |
| CN205714857U (en) | A kind of antecurvature multiple wing type centrifugal blower fan | |
| CN204828037U (en) | Leafy centrifugal impeller | |
| CN103321955A (en) | Energy-saving fan |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20081119 Termination date: 20100823 |