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CN201152279Y - Single-stage low speed blast engine blade wheel device - Google Patents

Single-stage low speed blast engine blade wheel device Download PDF

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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
Application number
CNU2007200866762U
Other languages
Chinese (zh)
Inventor
杨建明
杨先驹
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
HUBEI SHUANGJIAN BLOWER PRODUCTION CO Ltd
Original Assignee
HUBEI SHUANGJIAN BLOWER PRODUCTION CO Ltd
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 HUBEI SHUANGJIAN BLOWER PRODUCTION CO Ltd filed Critical HUBEI SHUANGJIAN BLOWER PRODUCTION CO Ltd
Priority to CNU2007200866762U priority Critical patent/CN201152279Y/en
Application granted granted Critical
Publication of CN201152279Y publication Critical patent/CN201152279Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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

The impeller unit of single-stage low speed blower
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.
CNU2007200866762U 2007-08-23 2007-08-23 Single-stage low speed blast engine blade wheel device Expired - Fee Related CN201152279Y (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (4)

* Cited by examiner, † Cited by third party
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

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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