CN202209308U - Efficient fully-three-dimensional impeller - Google Patents

Efficient fully-three-dimensional impeller Download PDF

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Publication number
CN202209308U
CN202209308U CN2011203080531U CN201120308053U CN202209308U CN 202209308 U CN202209308 U CN 202209308U CN 2011203080531 U CN2011203080531 U CN 2011203080531U CN 201120308053 U CN201120308053 U CN 201120308053U CN 202209308 U CN202209308 U CN 202209308U
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CN
China
Prior art keywords
impeller
blade
diameter end
blades
dimensional
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Expired - Lifetime
Application number
CN2011203080531U
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Chinese (zh)
Inventor
金炳庆
金华明
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.)
JIANGSU GL-TURBO CORPORATION
Original Assignee
Wuxi GL Turbo Compressor 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 Wuxi GL Turbo Compressor Co Ltd filed Critical Wuxi GL Turbo Compressor Co Ltd
Priority to CN2011203080531U priority Critical patent/CN202209308U/en
Application granted granted Critical
Publication of CN202209308U publication Critical patent/CN202209308U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

The utility model discloses an efficient fully-three-dimensional impeller, which comprises an impeller body. Main blades are evenly distributed on the impeller body and the number of the main blades is from six to twelve. The main blades are all formed by three-dimensional curved surfaces which are recurved towards the direction of turning N from a small diameter end to a large diameter end. The efficient fully-three-dimensional impeller is characterized by further comprising secondary blades. The secondary blades are formed by three-dimensional curved surfaces which are recurved towards the direction of turning from the small diameter end to the large diameter end. One secondary blade is respectively disposed in the middle of every two adjacent main blades, and the axial length Y of each secondary blade is smaller than the axial length X of each main blade. The efficient fully-three-dimensional impeller is compact and reasonable in structure and enables efficiency of the impeller to be further improved due to the adoption of the fully-three-dimensional structure of the main blades and the secondary blades. Meanwhile, the impeller is made of aluminum alloy with small mass, and rotor inertia is small, thereby facilitating maintenance of dynamic balance of a rotor at high speed and also facilitating improvement of efficiency.

Description

A kind of complete efficiently 3 d impeller
Technical field
The utility model relates to a kind of complete efficiently 3 d impeller, specifically after improving on the basis of common 3 d impeller, has more high efficiency a kind of impeller, belongs to the mechanical structure technical field.
Background technique
At present; The major technique that is used for the homemade single-stage high-speed centrifugal blower in the aeration in sewage treatment system comes from the technology of introducing advanced country's the eighties; The impeller that uses on this series products is common 3 d impeller; Except the primary blades that three-dimension curved surface constitutes, do not divide blade, impeller adiabatic efficiency is on the low side relatively, is difficult to satisfy current to energy-conservation increasingly high requirement.
Summary of the invention
The purpose of the utility model is to overcome above-mentioned deficiency, thereby a kind of complete efficiently 3 d impeller is provided, and is convenient to keep the dynamic balancing under the rotor high-speed, and has higher working efficiency.
The technological scheme that provides according to the utility model; A kind of complete efficiently 3 d impeller comprises impeller body; Said impeller body is provided with 6-12 primary blades that is uniformly distributed with, and said primary blades constitutes to the three-dimension curved surface of bigger diameter end to rotation direction N back-flexing by miner diameter end, and characteristic is: also comprise the branch blade; Be provided with a branch blade in the middle of said every two adjacent primary blades, divide the axial length of the axial length of blade less than primary blades.
As the further improvement of the utility model, blade was made up of to the three-dimension curved surface of bigger diameter end to the rotation direction back-flexing miner diameter end in said minute.
As the further improvement of the utility model, said impeller body comprises primary blades, divides blade to be processed by aluminum alloy material integral body.
The utility model compact structure, reasonable; Have primary blades and the full ternary structural that divides blade owing to adopt, impeller adiabatic efficiency is further enhanced; Simultaneously, impeller is processed by the little aluminum alloy of quality, and rotor inertia is little, is convenient to keep the dynamic balancing under the rotor high-speed, helps the raising of efficient equally.
Description of drawings
Fig. 1 is the front view of the utility model.
Fig. 2 is a K-K sectional view among Fig. 1.
Embodiment
Following the utility model will combine accompanying drawing to further describe:
Like Fig. 1, shown in Figure 2: the utility model comprises impeller body 1, primary blades 2, divides blade 3.Said impeller body 1 is provided with primary blades 2 that 6-12 is uniformly distributed with and divides blade 3, and said primary blades 2 is with to divide blade 3 structures identical, by miner diameter end to bigger diameter end to rotation direction N back-flexing and through the three-dimension curved surface formation of optimal design.
Be provided with a branch blade 3 in the middle of said every two adjacent primary blades 2, divide the axial length Y of blade 3 axial length X less than primary blades 2. Y/X=0.5-0.95。
Said impeller body 1 comprises primary blades 2, divides blade 3 to be processed by aluminum alloy material integral body.
When the utility model when diagram arrow N makes high-speed rotation; Air gets into impeller cavity 4 along the arrow A direction; Air under the centrifugal action of the utility model, an edge N direction high-speed rotation, on one side flow to Way out B; And receiving certain diffusion action, pressure ability and kinetic energy are all improved accordingly.Because primary blades 2 and the acting in conjunction that divides blade 3; Make the utility model higher than the efficient of the common 3 d impeller that does not divide blade, impeller is processed by the little aluminum alloy material of quality simultaneously, and rotor inertia is little; Be convenient to keep the dynamic balancing under the rotor high-speed, more help the raising of efficient.

Claims (3)

1. complete efficiently 3 d impeller; Comprise impeller body (1); Be uniformly distributed with on the said impeller body (1) and be provided with 6-12 primary blades (2), said primary blades (2) is made up of to the three-dimension curved surface of bigger diameter end to rotation direction (N) back-flexing miner diameter end, it is characterized in that: also comprise branch blade (3); Be provided with a branch blade (3) in the middle of said every adjacent two primary blades (2), divide the axial length (X) of the axial length (Y) of blade (3) less than primary blades (2).
2. a kind of complete efficiently 3 d impeller as claimed in claim 1 is characterized in that: said minute blade (3) by miner diameter end to the three-dimension curved surface formation of bigger diameter end to rotation direction (N) back-flexing.
3. a kind of complete efficiently 3 d impeller as claimed in claim 1, it is characterized in that: said impeller body comprises primary blades (2), divides blade (3) to be processed by aluminum alloy material integral body.
CN2011203080531U 2011-08-23 2011-08-23 Efficient fully-three-dimensional impeller Expired - Lifetime CN202209308U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011203080531U CN202209308U (en) 2011-08-23 2011-08-23 Efficient fully-three-dimensional impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011203080531U CN202209308U (en) 2011-08-23 2011-08-23 Efficient fully-three-dimensional impeller

Publications (1)

Publication Number Publication Date
CN202209308U true CN202209308U (en) 2012-05-02

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Family Applications (1)

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CN2011203080531U Expired - Lifetime CN202209308U (en) 2011-08-23 2011-08-23 Efficient fully-three-dimensional impeller

Country Status (1)

Country Link
CN (1) CN202209308U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102242731A (en) * 2011-08-23 2011-11-16 无锡杰尔压缩机有限公司 Efficient full-ternary impellor
WO2017133371A1 (en) * 2016-02-01 2017-08-10 宁波方太厨具有限公司 Ceiling-mounted exhaust hood
CN110234886A (en) * 2017-01-27 2019-09-13 赛峰直升机发动机公司 What it is for turbine includes the impeller blade of winglet at the tip of impeller blade and edge
CN111794991A (en) * 2020-09-08 2020-10-20 山东天瑞重工有限公司 Magnetic suspension double round air-blower
WO2021056258A1 (en) 2019-09-25 2021-04-01 协磁股份有限公司 Method for manufacturing three-dimensional plastic impeller of centrifugal pump and structure thereof

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102242731A (en) * 2011-08-23 2011-11-16 无锡杰尔压缩机有限公司 Efficient full-ternary impellor
WO2017133371A1 (en) * 2016-02-01 2017-08-10 宁波方太厨具有限公司 Ceiling-mounted exhaust hood
CN110234886A (en) * 2017-01-27 2019-09-13 赛峰直升机发动机公司 What it is for turbine includes the impeller blade of winglet at the tip of impeller blade and edge
WO2021056258A1 (en) 2019-09-25 2021-04-01 协磁股份有限公司 Method for manufacturing three-dimensional plastic impeller of centrifugal pump and structure thereof
US11739642B2 (en) 2019-09-25 2023-08-29 Assoma Inc. Manufacturing method of 3-dimensional plastic impeller of centrifugal pump and the impeller
EP4345315A2 (en) 2019-09-25 2024-04-03 Assoma Inc. Method for manufacturing three-dimensional plastic impeller of centrifugal pump and structure thereof
CN111794991A (en) * 2020-09-08 2020-10-20 山东天瑞重工有限公司 Magnetic suspension double round air-blower

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C56 Change in the name or address of the patentee
CP03 Change of name, title or address

Address after: 214101 No. 38, Qian Lian Road, Xishan Economic Development Zone, Xishan District, Jiangsu, Wuxi

Patentee after: JIANGSU GL-TURBO CORPORATION

Address before: 214192 Jiangsu Province, Wuxi city Xishan District of Xishan Economic Development Zone in three Furong Road No. 99 building six room 507 zuiun

Patentee before: Wuxi Jieer Compressor Co., Ltd.

CX01 Expiry of patent term
CX01 Expiry of patent term

Granted publication date: 20120502