CN106762828A - Fan leaf annular multistage blade structure - Google Patents

Fan leaf annular multistage blade structure Download PDF

Info

Publication number
CN106762828A
CN106762828A CN201710044450.4A CN201710044450A CN106762828A CN 106762828 A CN106762828 A CN 106762828A CN 201710044450 A CN201710044450 A CN 201710044450A CN 106762828 A CN106762828 A CN 106762828A
Authority
CN
China
Prior art keywords
blade
axle center
group
flabellum axle
blade group
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.)
Pending
Application number
CN201710044450.4A
Other languages
Chinese (zh)
Inventor
梁耀文
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201710044450.4A priority Critical patent/CN106762828A/en
Publication of CN106762828A publication Critical patent/CN106762828A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/38Blades
    • F04D29/384Blades characterised by form

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention discloses a kind of fan leaf annular multistage blade structure, including flabellum axle center and at least two grade blade groups, the blade group includes the blade that multi-disc is set around flabellum axle center, connection ring is provided between adjacent two grade blades group, the distance in blade to the flabellum axle center in same grade blade group is equal, blade in same blade group has identical established angle, near the established angle of the established angle more than the blade group away from flabellum axle center of the blade group in flabellum axle center, near the axial projective area of the axial projective area less than the blade group away from flabellum axle center of the blade group in flabellum axle center, the ratio of the axial projective area between adjacent two grade blades group is 1:1.1~4.The connection ring effectively shares blade pressure, there can be bigger overall front face area, even if reducing rotating speed can cause that fan static pressure is reduced, but enhanced dynamic pressure effectively compensate for hydrostatic pressures losses, and reduction of speed noise reduction is realized while original operating efficiency is kept so as to reach.

Description

Fan leaf annular multistage blade structure
Technical field
The present invention relates to aeration technology field, particularly a kind of fan leaf annular multistage blade structure.
Background technology
The blower fan of cooling tower, its flabellum is to be arranged to form around axis for the blade ring of aerofoil profile or plate shape by multi-disc section, by It is relatively large in diameter in flabellum(0.5 to 6.5 meter), to keep flabellum stress relative equilibrium everywhere, the structure of each blade to be designed It is smaller into its width of blade further away from axis.All it is by increasing leaf arc angle to reach Wind Volume when a diameter of fixed value of flabellum The modes such as degree, increase width of blade, increase blade quantity, raising rotating speed are realized.Due to foregoing blade design principle, the number of blade Measuring at most can be so that the projected area of adjacent blades overlaps, and instead resulting in air cannot circulate.And increase leaf arc angle Fan energy consumption requirement is limited to increase width of blade, limiting value is there is also.Therefore method the most feasible is to improve blower fan Rotating speed, but high-revolving blower fan can produce the noise of high-decibel so that and cooling tower cannot meet the standard of environmental monitoring evaluation.
The content of the invention
The invention provides a kind of fan leaf annular multistage blade structure, which employs brand-new blade design principle, So that the overall front face area of flabellum is greatly increased, in the case of equivalent diameter, even if reduce rotation speed of fan can also keep filling The ventilation of foot.
A kind of fan leaf annular multistage blade structure, including flabellum axle center and at least two grade blade groups, the blade group Including the blade that multi-disc is set around flabellum axle center, connection ring is provided between adjacent two grade blades group, in same grade blade group The distance in blade to flabellum axle center is equal, and the blade in same blade group has identical established angle, and the established angle is acute angle, Near the established angle of the established angle more than the blade group away from flabellum axle center of the blade group in flabellum axle center, near the leaf in flabellum axle center The axial projective area of piece group is less than the axial projective area of the blade group away from flabellum axle center, between adjacent two grade blades group The ratio of axial projective area is 1:1.1~4.
Further, to be flexibly connected between the blade and flabellum axle center/connection ring, its established angle is solid by locking member It is fixed.
Conventional fan flabellum is relatively large in diameter due to flabellum, to keep flabellum stress relative equilibrium everywhere, the knot of each blade It is smaller that structure is both designed to its width of blade further away from axis.If flabellum is divided into multiple concentric annular regions at equal intervals, Then further away from axis, the ratio that its blade area accounts for the concentric annular regions gross area can be substantially reduced.If the fan of conventional fan Leaf rotating speed is reduced, then its rate of air circulation for driving also can be reduced accordingly.
Due to needing to need the blast in pipeline everywhere as uniform as possible during blower fan discharge quantity of fan, and away from flabellum axle center Blade group has linear velocity higher, to avoid blower fan discharge quantity of fan uneven, so being needed away from the blade group in flabellum axle center Less established angle is set, with reduce in pipeline it is each between pressure difference.
Fan leaf annular multistage blade structure disclosed by the invention, it passes through to change blade structure, has abolished traditional fan The technology chains of leaf " its width of blade is smaller further away from axis ", the connection ring that it is set up effectively is shared blade pressure, is made It can have bigger overall front face area, even if reducing rotating speed can cause that fan static pressure is reduced, but enhanced dynamic pressure is effectively more Hydrostatic pressures losses are mended, reduction of speed noise reduction has been realized while original operating efficiency is kept so as to reach.
Brief description of the drawings
Technical scheme in order to illustrate more clearly the embodiments of the present invention, below will be to that will make needed for embodiment description Accompanying drawing is briefly described.Obviously, described accompanying drawing is a part of embodiment of the invention, rather than whole implementations Example, those skilled in the art on the premise of not paying creative work, can also obtain other designs according to these accompanying drawings Scheme and accompanying drawing.
Fig. 1 is the top view of the fan leaf annular multistage blade structure;
Fig. 2 is the side view of the fan leaf annular multistage blade structure;
Fig. 3 is the three-dimensional view of the fan leaf annular multistage blade structure.
Specific embodiment
The technique effect of design of the invention, concrete structure and generation is carried out clearly below with reference to embodiment and accompanying drawing Chu, it is fully described by, to be completely understood by the purpose of the present invention, feature and effect.Obviously, described embodiment is this hair Bright a part of embodiment, rather than whole embodiments, based on embodiments of the invention, those skilled in the art is not paying The other embodiment obtained on the premise of creative work, belongs to the scope of protection of the invention.In addition, be previously mentioned in text All connection/annexations, not singly refer to that component directly connects, and refer to that can be added deduct by adding according to specific implementation situation Lack couple auxiliary to constitute more excellent draw bail.Each technical characteristic in the invention, in not conflicting conflict Under the premise of can be with combination of interactions.
Embodiment 1
As shown in Figures 1 to 3, a kind of fan leaf annular multistage blade structure, including the grade blade group of flabellum axle center 1 and three, it is described Blade group is respectively primary blades group, secondary blades group and exhaust stage blade group from inside to outside, and each blade group includes multi-disc around fan The blade 2 that the rachis heart 1 is set, is provided with connection ring 3 between adjacent two grade blades group, the blade 2 in same grade blade group arrives flabellum The distance in axle center 1 is equal.Blade 2 in same blade group has identical established angle, and the established angle is acute angle, primary blades The established angle of group is more than the established angle of secondary blades group, the established angle of the established angle more than exhaust stage blade group of secondary blades group, institute State to be flexibly connected between blade 2 and the connection ring 3 of flabellum axle center 1/, its established angle is fixed by locking member.Due to cooling tower wind The working environment of machine is different, so the established angle of each blade group is adjustable design, it is specific only to meet above-mentioned size pass System.Near the axis projection of the axial projective area less than the blade group away from flabellum axle center 1 of the blade group in flabellum axle center 1 Area, the ratio of the axial projective area of primary blades group, secondary blades group and exhaust stage blade group is 1:1.5:3.5.
Embodiment 2
Conventional fan flabellum is as follows with the fan leaf of the present invention annular multistage blade structure table of comparisons:
The table of comparisons
Better embodiment of the invention is illustrated above, but the invention is not limited to the embodiment, Those of ordinary skill in the art can also make a variety of equivalent modifications or replacements on the premise of without prejudice to spirit of the invention, this A little equivalent modifications or replacement are all contained in the application claim limited range.

Claims (2)

1. a kind of fan leaf annular multistage blade structure, it is characterised in that:Including flabellum axle center(1)At least two grade blades Group, the blade group includes multi-disc around flabellum axle center(1)The blade of setting(2), connection is provided between adjacent two grade blades group Ring(3), the blade in same grade blade group(2)To flabellum axle center(1)Distance it is equal, the blade in same blade group(2)Tool There is identical established angle, the established angle is acute angle, near flabellum axle center(1)Blade group established angle be more than away from flabellum axle The heart(1)Blade group established angle, near flabellum axle center(1)Blade group axial projective area be less than away from flabellum axle center (1)Blade group axial projective area, the ratio of the axial projective area between adjacent two grade blades group is 1:1.1~4.
2. fan leaf according to claim 1 annular multistage blade structure, it is characterised in that:The blade(2)With fan The rachis heart(1)/ connection ring(3)Between to be flexibly connected, its established angle fixed by locking member.
CN201710044450.4A 2017-01-19 2017-01-19 Fan leaf annular multistage blade structure Pending CN106762828A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710044450.4A CN106762828A (en) 2017-01-19 2017-01-19 Fan leaf annular multistage blade structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710044450.4A CN106762828A (en) 2017-01-19 2017-01-19 Fan leaf annular multistage blade structure

Publications (1)

Publication Number Publication Date
CN106762828A true CN106762828A (en) 2017-05-31

Family

ID=58945042

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710044450.4A Pending CN106762828A (en) 2017-01-19 2017-01-19 Fan leaf annular multistage blade structure

Country Status (1)

Country Link
CN (1) CN106762828A (en)

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6348997U (en) * 1986-09-17 1988-04-02
US5755557A (en) * 1995-08-03 1998-05-26 Valeo Thermique Moteur Axial flow fan
CN2323183Y (en) * 1997-08-26 1999-06-09 吴凤清 Multiblade vane
JP2008064011A (en) * 2006-09-07 2008-03-21 Calsonic Kansei Corp Motor cooling structure of motor fan
US20100260608A1 (en) * 2008-04-18 2010-10-14 Mitsubishi Heavy Industries, Ltd. Propeller fan
CN102227562A (en) * 2009-06-28 2011-10-26 博姆达株式会社 Axial fan
CN102465917A (en) * 2010-11-05 2012-05-23 台达电子工业股份有限公司 Fan structure
CN202418034U (en) * 2011-11-28 2012-09-05 深圳兴奇宏科技有限公司 Axial fan and blade structure thereof
US20130149115A1 (en) * 2011-12-09 2013-06-13 Delta Electronics, Inc. Recirculation fan and wind-guiding device thereof
CN204371777U (en) * 2014-12-29 2015-06-03 广东美的环境电器制造有限公司 Fan blade and there is its fan
CN206449015U (en) * 2017-01-19 2017-08-29 梁耀文 Fan leaf annular multistage blade structure

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6348997U (en) * 1986-09-17 1988-04-02
US5755557A (en) * 1995-08-03 1998-05-26 Valeo Thermique Moteur Axial flow fan
CN2323183Y (en) * 1997-08-26 1999-06-09 吴凤清 Multiblade vane
JP2008064011A (en) * 2006-09-07 2008-03-21 Calsonic Kansei Corp Motor cooling structure of motor fan
US20100260608A1 (en) * 2008-04-18 2010-10-14 Mitsubishi Heavy Industries, Ltd. Propeller fan
CN102227562A (en) * 2009-06-28 2011-10-26 博姆达株式会社 Axial fan
CN102465917A (en) * 2010-11-05 2012-05-23 台达电子工业股份有限公司 Fan structure
CN202418034U (en) * 2011-11-28 2012-09-05 深圳兴奇宏科技有限公司 Axial fan and blade structure thereof
US20130149115A1 (en) * 2011-12-09 2013-06-13 Delta Electronics, Inc. Recirculation fan and wind-guiding device thereof
CN204371777U (en) * 2014-12-29 2015-06-03 广东美的环境电器制造有限公司 Fan blade and there is its fan
CN206449015U (en) * 2017-01-19 2017-08-29 梁耀文 Fan leaf annular multistage blade structure

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
王海宁: "《矿井风流流动与控制》", 冶金工业出版社, pages: 218 - 219 *

Similar Documents

Publication Publication Date Title
CN104930604A (en) Air outlet protective structure, air conditioner outdoor unit and design method of air outlet protective structure
CN108678994B (en) A kind of efficient diagonal flow fan
CN206449015U (en) Fan leaf annular multistage blade structure
CN104061187A (en) Axial-flow fan blade, axial-flow fan and air conditioner
CN106662117A (en) Centrifugal impeller and centrifugal compressor
CN105008723A (en) Propeller fan and air conditioner equipped with same
CN106122092A (en) A kind of novel blade and use the impeller of this fan blade
CN106895027A (en) A kind of axial flow fan vane wheel
CN107965467B (en) Centrifugal fan impeller for range hood
CN207195307U (en) Blower fan structure and there is its air conditioner
CN106762828A (en) Fan leaf annular multistage blade structure
CN104653515A (en) Double-suction type centrifugal ventilation fan
CN203756586U (en) Sealing part and centrifugal compressor
CN206144845U (en) Axial compressor wind wheel and air conditioner that has axial compressor wind wheel
CN204458535U (en) A kind of return channel and centrifugal compressor
CN205064332U (en) Fan and have its air conditioning system
CN205779897U (en) Centrifugal blower
CN210509719U (en) Fan assembly and cabinet air conditioner with same
CN211874764U (en) Large-flow high-full-pressure reloading centrifugal cross-flow fan
CN104685218A (en) Propeller fan
CN207349164U (en) Centrifugation blade and there is its centrifugal blower
CN106321510A (en) Backward centrifugal impeller
CN206449014U (en) Axial-flow leaf and blower fan, air-conditioner outdoor unit with it
CN208380923U (en) S type vanes close formula impeller for Small Centrifugal Fan
CN207161381U (en) Aerofoil fan

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20170531