CN207297458U - A kind of low noise airfoil type motor centrifugal fan - Google Patents

A kind of low noise airfoil type motor centrifugal fan Download PDF

Info

Publication number
CN207297458U
CN207297458U CN201720930869.5U CN201720930869U CN207297458U CN 207297458 U CN207297458 U CN 207297458U CN 201720930869 U CN201720930869 U CN 201720930869U CN 207297458 U CN207297458 U CN 207297458U
Authority
CN
China
Prior art keywords
wing blades
fixed disc
fixing sleeve
low noise
centrifugal fan
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.)
Active
Application number
CN201720930869.5U
Other languages
Chinese (zh)
Inventor
焦华勇
李学武
赵东娜
柳忠雨
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.)
Wolong Electric Drive Group Co Ltd
Wolong Electric Nanyang Explosion Protection Group Co Ltd
Original Assignee
Wolong Electric Group Co Ltd
Wolong Electric Nanyang Explosion Protection Group 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 Wolong Electric Group Co Ltd, Wolong Electric Nanyang Explosion Protection Group Co Ltd filed Critical Wolong Electric Group Co Ltd
Priority to CN201720930869.5U priority Critical patent/CN207297458U/en
Application granted granted Critical
Publication of CN207297458U publication Critical patent/CN207297458U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The utility model discloses a kind of low noise airfoil type motor centrifugal fan, including the fixed disc being vertically arranged, ring baffle, the perforation for fixing bearing is equipped with the center of fixed disc, it is integrally formed with perforation to the bearing fixing sleeve extended on front side of fixed disc, bearing fixing sleeve is coaxially disposed with fixed disc, circumferencial direction around bearing fixing sleeve on fixed disc is uniformly provided with multiple wing blades, the wing blades width in the front-back direction is more than bearing fixing sleeve length in the front-back direction, the leading flank of the ring baffle and wing blades is integrally formed;Shown as a result, eliminating blade back air-flow using wing blades and separated according to flow field analysis, further reduce eddy current loss, improve vane efficiency, noise reduces notable.According to Experimental Comparison verification is carried out on 2 1250KW 10KV motors of YBXKK630, on the premise of ensureing that aerodynamic parameter is constant, its noise reduces 5db(A);Electromechanics loss reduces 2kw;Purpose of design is reached.

Description

A kind of low noise airfoil type motor centrifugal fan
Technical field
The utility model belongs to technical field of motors, more particularly to a kind of low noise airfoil type motor centrifugal fan.
Background technology
The current existing centrifugal fan applied on motor uses straight-plate-type blade structure more, this straight-plate-type blade There are noise is high, airflow inlet impact is big, vane efficiency is low for centrifugal fan;On the other hand, found after aerodynamics is analyzed, Airflow path is also easy to produce vortex, and flow losses are larger.The development trend of motor requires motor to have low noise, efficient at present Feature, the aerodynamic noise of pot motor are to influence the main reason for noise of motor index is high, thus there is an urgent need to it is a kind of efficiently, The motor centrifugal fan of low noise.
The content of the invention
The utility model aim is to provide a kind of low noise airfoil type motor centrifugal fan, greatly reduces high rotating speed electricity The aerodynamic noise problem of machine;Adopted the technical scheme that to reach above-mentioned purpose:A kind of low noise airfoil type motor centrifuges wind Fan, including fixed disc, the ring baffle being vertically arranged, the perforation for fixing bearing is equipped with the center of fixed disc, The bearing fixing sleeve to extension on front side of fixed disc is integrally formed with perforation, bearing fixing sleeve is coaxially disposed with fixed disc, Circumferencial direction on fixed disc around bearing fixing sleeve is uniformly provided with multiple wing blades, the wing blades anteroposterior direction Width be more than bearing fixing sleeve length in the front-back direction, the leading flank of the ring baffle and wing blades is integrally formed.
Preferably, the wing blades are curved surface column blade, and the contour line of the cross section of wing blades is by interior Contour and outer peripheral lines are connected in sequence, and the interior contour has the spline curve of 17 nodes, the abscissa of interior contour node xIt is interiorWith ordinate yIt is interiorAs shown in following table:
,
The origin of rectangular coordinate system xOy is at the barycenter of wing blades.
Preferably, the outer peripheral lines have the spline curve of 17 nodes, the abscissa x of outer peripheral lines nodeOutsideAnd ordinate yOutsideAs shown in following table:
,
The origin of rectangular coordinate system xOy is at the barycenter of wing blades.
Preferably, the inner of the interior contour and outer peripheral lines is connected smoothly and forms an edge camber line, the head edge arc Line is semicircular arc, and the central coordinate of circle of head edge camber line is (x=-64.5, y=45.6), radius R=2.9, unit:Millimeter, directly The origin of angular coordinate system xOy is at the barycenter of wing blades.
Preferably, the wall thickness of the wing blades is 1.5.
The wing blades of the utility model use newest Theory of Three-dimensional Flowing and airfoil type pneumatic principle, according to reality Structure needs to carry out optimization design repeatedly, reduces inlet air flow impact;Shown according to flow field analysis as a result, using airfoil type leaf Piece eliminates the air-flow separation of blade back, further reduces eddy current loss, improves vane efficiency, and noise reduces notable.Root According on YBXKK630-2 1250KW 10KV motors carry out Experimental Comparison verification, ensure aerodynamic parameter it is constant on the premise of, Its noise reduces 5db (A);Electromechanics loss reduces 2kw;Purpose of design is reached.
Brief description of the drawings
Fig. 1 is the dimensional structure diagram of the utility model;
Fig. 2 be Fig. 1 in along A-A to sectional view;
Fig. 3 is the structure diagram of wing blades.
Embodiment
The utility model is further described below in conjunction with the accompanying drawings.
As depicted in figs. 1 and 2, a kind of low noise airfoil type motor centrifugal fan, including be vertically arranged fixed disc 1, Ring baffle 3, is equipped with the perforation for fixing bearing at the center of fixed disc 1, is integrally formed with perforation to fixed disc 1 The bearing fixing sleeve 4 of front side extension, bearing fixing sleeve 4 are coaxially disposed with fixed disc 1, are fixed on fixed disc 1 around bearing The circumferencial direction of set 4 is uniformly provided with multiple wing blades 2, and 2 width in the front-back direction of wing blades is consolidated more than bearing Surely 4 length in the front-back direction are covered, the leading flank of the ring baffle 3 and wing blades 2 is integrally formed.
As shown in figure 3, the wing blades 2 are curved surface column blade, and the contour line of the cross section of wing blades 2 It is connected in sequence by interior contour 6, head edge camber line 7 and outer peripheral lines 5, the interior contour 6 and outer peripheral lines are with 17 nodes Spline curve, the abscissa x of interior 6 node of contourIt is interiorWith ordinate yIt is interior, 5 node of outer peripheral lines abscissa xOutsideAnd ordinate yOutsideAs shown in following table:
The origin of rectangular coordinate system xOy is at the barycenter of wing blades 2.
The head edge camber line 7 is semicircular arc, and the central coordinate of circle of head edge camber line 7 is (x=-64.5, y=45.6), radius For R=2.9, unit:Millimeter.
Further, the wall thickness of the wing blades 2 is 1.5.
The wing blades 2 of the utility model use newest Theory of Three-dimensional Flowing and airfoil type pneumatic principle, according to reality Border structure needs to carry out optimization design repeatedly, reduces inlet air flow impact;Shown according to flow field analysis as a result, using airfoil type Blade 2 eliminates the air-flow separation of blade back, further reduces eddy current loss, improves vane efficiency, and noise reduces notable. According to Experimental Comparison verification is carried out on YBXKK630-2 1250KW 10KV motors, ensureing the constant premise of aerodynamic parameter Under, its noise reduces 5db (A);Electromechanics loss reduces 2kw;Purpose of design is reached.
Limitation of the present embodiment not to works such as the shape of the utility model, material, structures in any form, every foundation Any simple modification, equivalent change and modification that the technical essence of the utility model makees above example, belongs to this reality With the protection domain of new technique scheme.

Claims (5)

1. a kind of low noise airfoil type motor centrifugal fan, including fixed disc, the ring baffle being vertically arranged, its feature exist In being equipped with the perforation for fixing bearing at the center of fixed disc, be integrally formed with perforation to extending on front side of fixed disc Bearing fixing sleeve, bearing fixing sleeve is coaxially disposed with fixed disc, around the circumferencial direction of bearing fixing sleeve on fixed disc Multiple wing blades are uniformly provided with, the wing blades width in the front-back direction is more than bearing fixing sleeve length in the front-back direction Degree, the leading flank of the ring baffle and wing blades are integrally formed.
2. low noise airfoil type motor centrifugal fan according to claim 1, it is characterised in that the wing blades are Curved surface column blade, and the contour line of the cross section of wing blades is connected in sequence by interior contour and outer peripheral lines, it is described interior Contour has the spline curve of 17 nodes, the abscissa x of interior contour nodeIt is interiorWith ordinate yIt is interiorAs shown in following table:
,
The origin of rectangular coordinate system xOy is at the barycenter of wing blades.
3. low noise airfoil type motor centrifugal fan according to claim 2, it is characterised in that the outer peripheral lines have 17 The spline curve of a node, the abscissa x of outer peripheral lines nodeOutsideWith ordinate yOutsideAs shown in following table:
,
The origin of rectangular coordinate system xOy is at the barycenter of wing blades.
4. low noise airfoil type motor centrifugal fan according to claim 3, it is characterised in that the interior contour and periphery The inner of line is connected smoothly and forms an edge camber line, and the head edge camber line is semicircular arc, the central coordinate of circle of head edge camber line For (x=-64.5, y=45.6), radius R=2.9, unit:Millimeter, the origin of rectangular coordinate system xOy is in wing blades At barycenter.
5. according to claim 2 to 4 any one of them low noise airfoil type motor centrifugal fan, it is characterised in that the machine The wall thickness of airfoil fan is 1.5, unit:Millimeter.
CN201720930869.5U 2017-07-28 2017-07-28 A kind of low noise airfoil type motor centrifugal fan Active CN207297458U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720930869.5U CN207297458U (en) 2017-07-28 2017-07-28 A kind of low noise airfoil type motor centrifugal fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720930869.5U CN207297458U (en) 2017-07-28 2017-07-28 A kind of low noise airfoil type motor centrifugal fan

Publications (1)

Publication Number Publication Date
CN207297458U true CN207297458U (en) 2018-05-01

Family

ID=62447951

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720930869.5U Active CN207297458U (en) 2017-07-28 2017-07-28 A kind of low noise airfoil type motor centrifugal fan

Country Status (1)

Country Link
CN (1) CN207297458U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108390500A (en) * 2018-02-08 2018-08-10 浙江希尔富电气有限公司 One kind being based on brushless motor and the special noise reduction combined mechanism of wind turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108390500A (en) * 2018-02-08 2018-08-10 浙江希尔富电气有限公司 One kind being based on brushless motor and the special noise reduction combined mechanism of wind turbine

Similar Documents

Publication Publication Date Title
CN105736426A (en) Axial flow fan comprising blade pressure surfaces with winglets and blade tops with blowing structures
CN206344995U (en) Ducted fan for aircraft
CN105756975B (en) The axial flow blower that a kind of blade inlet edge is blown with groove structure and blade root
CN104454641A (en) Low-noise axial flow fan impeller for high-speed electric multiple unit cooling system
CN105736425A (en) Axial flow fan comprising blades with wing-type guide plates and guide blades with bionic tail edges
CN205639000U (en) Blade leading edge takes axial fan that groove structure and blade root blew
CN107061329A (en) A kind of axial flow blower
CN101092976A (en) Synergic action device of controlling flow of airbleed inside blades of diffuser in centrifugal compressor
CN104061187A (en) Axial flow fan blade, axial flow fan and air conditioner
JP3204521U (en) fan
CN106939902B (en) Energy-saving straight-wall front and rear disk variable-curvature curve element ternary impeller and centrifugal fan adopting same
CN109667790A (en) A kind of bionical leading edge blade of INVESTIGATION ON A HIGH SPEED CENTRIFUGAL COMPRESSOR
CN103486081B (en) Axial flow fan blade, fan and air conditioner outdoor unit
CN202326414U (en) Axial flow fan
CN207297458U (en) A kind of low noise airfoil type motor centrifugal fan
CN105782090A (en) Noise-lowering and vortex-reducing axial flow fan
CN202628612U (en) Axial flow fan blade, fan and air conditioner outdoor unit
CN201547015U (en) Low-noise centrifugal wind wheel
CN103016401B (en) Novel axial fan for air-conditioner outdoor unit
WO2020042551A1 (en) Axial flow fan wheel and axial flow fan using same
CN103122872A (en) Axial flow fan
CN203584898U (en) Low-noise high-efficiency central air conditioner outdoor machine cooling axial-flow fan
CN104613009A (en) Reversible axial flow fan blade with air blowing grooves
CN205101284U (en) Low noise ceiling fan
CN202659570U (en) Axial wind wheel

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant