CN202001369U - Axial-flow pump - Google Patents

Axial-flow pump Download PDF

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Publication number
CN202001369U
CN202001369U CN2010206777001U CN201020677700U CN202001369U CN 202001369 U CN202001369 U CN 202001369U CN 2010206777001 U CN2010206777001 U CN 2010206777001U CN 201020677700 U CN201020677700 U CN 201020677700U CN 202001369 U CN202001369 U CN 202001369U
Authority
CN
China
Prior art keywords
blade
axial
flow pump
apex
size
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
CN2010206777001U
Other languages
Chinese (zh)
Inventor
张辉
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.)
SUZHOU ATHENA TECHNOLOGY Co Ltd
Original Assignee
SUZHOU ATHENA TECHNOLOGY 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 SUZHOU ATHENA TECHNOLOGY Co Ltd filed Critical SUZHOU ATHENA TECHNOLOGY Co Ltd
Priority to CN2010206777001U priority Critical patent/CN202001369U/en
Application granted granted Critical
Publication of CN202001369U publication Critical patent/CN202001369U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to an axial-flow pump which comprises a enclosure, wherein the enclosure is internally provided with an impeller; the size of the gap of a blade apex of the impeller is 0.7-1.6 mm; the size of the gap of the blade apex of a blade near a blade dish is 2-3 times of that of the gap of the blade apex near the rear of the blade; the blade is in a wing shape, and the blade apex part is cut into a pinnacle; and the torsional angle between the apex part of the vane and the middle part of the vane is increased by 5 %. The gap of the blade apex is shorten, and the blade apex adopts a pinnacle structure, so as to effectively reduce the effect from that flow leaks from the blade apex, decrease the loss and improve the work efficiency of the axial-flow pump; in addition, the cut pinnacle structure is rather thin, so as not to cause big damage if the vane wheel collides with the enclosure during the course of the operation; the axial-flow pump has a simple structure, is convenient to implement and improves the property.

Description

Axial-flow pump
Technical field
The utility model relates to field of fluid machinery, especially relates to a kind of axial-flow pump that can increase work efficiency.
Background technique
Pump is widely used in the every field of national economy, and centrifugal pump and axial-flow pump are two kinds of main structural types of pump.The impeller that the blade of centrifugal pump is common and front and rear cover plate formation runner seals all around.The impeller of axial-flow pump only is made up of blade and wheel hub, between blade and frame radial clearance is arranged.In the process of wheel rotation, fluid is revealed from radial clearance, and forms whirlpool, causes bigger hydraulic loss, influences the working efficiency of axial-flow pump.
Summary of the invention
Technical problem to be solved in the utility model provides and a kind ofly can reduce tip leakage stream, the axial-flow pump of increasing work efficiency.
The technical scheme in the invention for solving the technical problem is: a kind of axial-flow pump, comprise casing, casing inside is provided with impeller, the tip clearance size of the blade of described impeller has dwindled 20~30% than stock size, wherein stock size is between 1~2mm, and promptly size is between 0.7~1.6mm.
Owing to rotate shell is caused damage, described blade is of a size of near the tip clearance size of blade back 2~3 times near the tip clearance at leaf basin place in order to reduce blade, and described blade is airfoil, and blade tip is whittled into the pinnacle.
In order to effectively reduce the influence of tip leakage stream, described blade tip improves 5% to blade middle part distortion angle.
Effect intentionally of the present utility model is: dwindle tip clearance and adopt leaf top sharpening roof construction can effectively reduce the influence of tip leakage stream, reduce the loss, improve the working efficiency of axial-flow pump.In addition, because the sharpening roof construction is thinner, if run into casing in the impeller running, also can not cause bigger damage, simple in structure, the convenient realization improved performance.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is an airfoil blade of the present utility model.
Among the figure: 1, blade 2, blade back 3, casing 4, leaf basin
Embodiment
A kind of as depicted in figs. 1 and 2 axial-flow pump comprises casing 3, and casing 3 inside are provided with impeller, and the ratio stock size of the tip clearance size of the blade 1 of described impeller (being the distance between blade tip and the casing 3) has dwindled 20~30%; The tip clearance at described blade 1 close leaf basin 4 places is of a size of 2~3 times near the tip clearance size of blade back 2; Described blade 1 is airfoil, and blade 1 tip is whittled into the pinnacle; Described blade 1 tip improves 5% to blade 1 middle part distortion angle; Circular rector designs such as described blade 1 distortion employing, wherein blade 1 tip amount of finish improves 2% than design load.
By dwindling the influence that the tip clearance size has effectively reduced tip leakage stream, axial-flow pump is improved working power good effect, because the sharpening roof construction is thinner, if run into casing in the impeller running, also can not cause bigger damage.

Claims (4)

1. an axial-flow pump comprises casing, and casing inside is provided with impeller, it is characterized in that: the tip clearance of the blade of described impeller is of a size of between 0.7~1.6mm.
2. axial-flow pump according to claim 1 is characterized in that: the tip clearance at the close leaf basin place of described blade is of a size of 2~3 times near the tip clearance size of blade back.
3. axial-flow pump according to claim 1 is characterized in that: described blade is airfoil, and blade tip is whittled into the pinnacle.
4. axial-flow pump according to claim 1 is characterized in that: described blade tip improves 5% to blade middle part distortion angle.
CN2010206777001U 2010-12-24 2010-12-24 Axial-flow pump Expired - Fee Related CN202001369U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010206777001U CN202001369U (en) 2010-12-24 2010-12-24 Axial-flow pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010206777001U CN202001369U (en) 2010-12-24 2010-12-24 Axial-flow pump

Publications (1)

Publication Number Publication Date
CN202001369U true CN202001369U (en) 2011-10-05

Family

ID=44704112

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2010206777001U Expired - Fee Related CN202001369U (en) 2010-12-24 2010-12-24 Axial-flow pump

Country Status (1)

Country Link
CN (1) CN202001369U (en)

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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: 20111005

Termination date: 20111224