CN201358951Y - Multistage low-speed centrifugal blower - Google Patents

Multistage low-speed centrifugal blower Download PDF

Info

Publication number
CN201358951Y
CN201358951Y CNU2009200630212U CN200920063021U CN201358951Y CN 201358951 Y CN201358951 Y CN 201358951Y CN U2009200630212 U CNU2009200630212 U CN U2009200630212U CN 200920063021 U CN200920063021 U CN 200920063021U CN 201358951 Y CN201358951 Y CN 201358951Y
Authority
CN
China
Prior art keywords
impeller
speed centrifugal
impellers
utility
centrifugal blower
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
CNU2009200630212U
Other languages
Chinese (zh)
Inventor
苏春模
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.)
Changsha Aerturbo Compressor Co Ltd
Original Assignee
Changsha Aerturbo 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 Changsha Aerturbo Compressor Co Ltd filed Critical Changsha Aerturbo Compressor Co Ltd
Priority to CNU2009200630212U priority Critical patent/CN201358951Y/en
Application granted granted Critical
Publication of CN201358951Y publication Critical patent/CN201358951Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The utility model discloses a multistage low-speed centrifugal blower, which comprises multistage impellers, and each stage of the impellers adopts a ternary impeller. As the impellers provided by the utility model adopt the impellers with the most advanced ternary flow theory at present, and the shape of the blades of the impeller is designed according to the vorticity distribution of fluid particles inside the impeller, the blower approximates the real flowing state of the air inside the impeller, resulting small flow loss and high thermodynamic efficiency. Compared with the prior similar multistage low-speed centrifugal blowers, the utility model can reduce the energy consumption by 2 to 10 percent.

Description

Multistage low-speed centrifugal blower
Technical field
The utility model relates to a kind of multistage low-speed centrifugal blower.
Background technique
Centrifugal blower is a kind of turbomachinery that is used for conveying gas, and impeller is the core part of centrifugal blower, is the key point of its complete machine performance quality.Gas is three-dimensional space motion at the mobile of impeller inside, present state-of-the-art Theory of Three-dimensional Flowing designing technique is also come out, but multistage low-speed centrifugal blower still adopts the impeller according to the mobile Design Theory of monobasic, be binary impeller (see figure 3), make that present multistage low-speed centrifugal blower efficiency is low, energy consumption is big.
The model utility content
The purpose of this utility model is to provide a kind of and can cuts down the consumption of energy, the multistage low-speed centrifugal blower of raising the efficiency.
This multistage low-speed centrifugal blower that the utility model provides comprises multi-stage impeller, and every grade is all adopted 3 d impeller.
The multistage low-speed centrifugal blower of the utility model adopts present state-of-the-art Theory of Three-dimensional Flowing design impeller, every grade of impeller all adopts 3 d impeller, the time of day that the moulding of its ternary twisted blade is flowed near the impeller internal gas more, flow losses are little, the thermodynamic efficiency height.The utility model is compared with existing similar multistage low-speed centrifugal blower, and energy consumption reduces by 2~10%.
Description of drawings
Fig. 1 is a structural representation of the present utility model.
Fig. 2 is a ternary twisted blade structural representation.
Fig. 3 is the structural representation of impeller in the prior art multistage centrifugal blower.
Embodiment
The multistage low-speed centrifugal blower of the utility model has intake grill 1, multi-stage impeller 2 as can be seen from Figure 1, and wherein every grade of impeller employing all is 3 d impellers.This impeller designs with at present existing state-of-the-art centrifugal impeller Theory of Three-dimensional Flowing, it is with the mobile inverse proposition formula of ternary, " whirlpool " (velocity circulation RCu) of input impeller inner fluid particle distributes, directly obtain ternary twisted blade type shape (as shown in Figure 2) by numerical calculation, compare with traditional monobasic flow design, near the mobile time of day of impeller internal gas, flow losses are little, the thermodynamic efficiency height more.During work, gas flows into the multi-stage impeller 2 that is made of the ternary twisted blade by intake grill 1, by these impeller 2 rotations, make gas be subjected to action of centrifugal force and produce pressure, meanwhile gas obtains speed, and gas stream is when expanding channel, and gas flow speed progressively slows down again and becomes the raising of gas pressure.

Claims (1)

1, a kind of multistage low-speed centrifugal blower comprises multi-stage impeller (2), it is characterized in that every grade of impeller (2) all adopts 3 d impeller.
CNU2009200630212U 2009-01-21 2009-01-21 Multistage low-speed centrifugal blower Expired - Fee Related CN201358951Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2009200630212U CN201358951Y (en) 2009-01-21 2009-01-21 Multistage low-speed centrifugal blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2009200630212U CN201358951Y (en) 2009-01-21 2009-01-21 Multistage low-speed centrifugal blower

Publications (1)

Publication Number Publication Date
CN201358951Y true CN201358951Y (en) 2009-12-09

Family

ID=41424714

Family Applications (1)

Application Number Title Priority Date Filing Date
CNU2009200630212U Expired - Fee Related CN201358951Y (en) 2009-01-21 2009-01-21 Multistage low-speed centrifugal blower

Country Status (1)

Country Link
CN (1) CN201358951Y (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103423171A (en) * 2013-07-10 2013-12-04 王雁南 Turbine compressor
CN104963876A (en) * 2015-08-05 2015-10-07 江苏涞森环保设备有限公司 Efficient and energy-saving three-dimensional-flow multi-stage centrifugal blower

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103423171A (en) * 2013-07-10 2013-12-04 王雁南 Turbine compressor
CN103423171B (en) * 2013-07-10 2016-01-20 王雁南 Turbocompressor
CN104963876A (en) * 2015-08-05 2015-10-07 江苏涞森环保设备有限公司 Efficient and energy-saving three-dimensional-flow multi-stage centrifugal blower

Similar Documents

Publication Publication Date Title
CN100485194C (en) Centrifugal impeller
CN104405685A (en) Self-circulation and circumferential groove hybrid treater box for improving performance of air compressor
CN202284569U (en) Improved fan blade structure of centrifugal fan
CN109578085B (en) Method for weakening unsteady acting force of turbine movable blade through guide blade inclination
CN109915407A (en) Centrifugal pump impeller and its efficiency and the noise collaboration of a kind of non-smooth surface promote design method
CN105179322B (en) Blade root opens up the Profile For Compressor Stator leaf grating of wide straight-line groove
CN201358951Y (en) Multistage low-speed centrifugal blower
CN204921480U (en) Centrifugal compressor model level
CN102889237B (en) Blade wheel with large blades and small blades applying front edges with sharp corners and air compressor
CN104806571A (en) Efficient centrifugal air blower based on computational fluid dynamic simulation
CN203230624U (en) Centrifugal fan rotor, centrifugal fan and air cooling refrigerator
CN208605394U (en) With the centrifugal impeller for increasing function decreasing loss
CN202579249U (en) Centrifugal compressor with multiple shafts
CN204239331U (en) One improves Capability of Compressor self-loopa and the hybrid processor box of peripheral groove
CN201582215U (en) Width adjusting mechanism of vaneless diffuser of turbocharger
CN202628612U (en) Axial flow fan blade, fan and air conditioner outdoor machine
CN102182519A (en) Self-jet flow secondary flow control structure of turbine stator vane
CN203717450U (en) Novel air inlet structure of air compressor of turbocharger for automobile
CN201358953Y (en) Single-stage low-speed centrifugal blower
CN202360458U (en) Multi-wing centrifugal fan with reinforced air inlet function
CN204677459U (en) For the mesohigh centrifugal blower of high-pressure delivery material
CN201696309U (en) High speed air centrifugal blower used for coal chemical industry
CN204493271U (en) A kind of centrifugal blower fan blade wheel
CN204200671U (en) The turbo-charger blower impeller that runoff and oblique flow combine
CN201865751U (en) Air inlet channel of supercharger

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20091209

Termination date: 20160121

EXPY Termination of patent right or utility model