CN103447173A - Cyclone separator with internally installed vortex core crushing wing - Google Patents

Cyclone separator with internally installed vortex core crushing wing Download PDF

Info

Publication number
CN103447173A
CN103447173A CN2013103595550A CN201310359555A CN103447173A CN 103447173 A CN103447173 A CN 103447173A CN 2013103595550 A CN2013103595550 A CN 2013103595550A CN 201310359555 A CN201310359555 A CN 201310359555A CN 103447173 A CN103447173 A CN 103447173A
Authority
CN
China
Prior art keywords
broken
vortex
cyclone separator
vortex core
fixed axis
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
CN2013103595550A
Other languages
Chinese (zh)
Inventor
王博
陈泊豪
蒋梦婷
刘鹤
蔡圃
王渊
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.)
Lanzhou University
Original Assignee
Lanzhou University
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 Lanzhou University filed Critical Lanzhou University
Priority to CN2013103595550A priority Critical patent/CN103447173A/en
Publication of CN103447173A publication Critical patent/CN103447173A/en
Pending legal-status Critical Current

Links

Images

Landscapes

  • Cyclones (AREA)

Abstract

The invention discloses a cyclone separator with an internally installed vortex core crushing wing. The cyclone separator is characterized in that a fixed shaft is arranged in the traditional cyclone separator along the central shaft position of a cyclone separation chamber; the lower end of the fixed shaft is positioned on the half position of a conical contraction section; the fixed shaft is provided with the vortex core crushing wing sheet of the fixed shaft, so that an immobile body is formed. According to the cyclone separator, because the immobile body is arranged in the center of the cyclone separation chamber, the occupied area of a forced vortex is reduced, the strength of the forced vortex is reduced, so that the pressure loss is reduced, and the energy consumption of the cyclone separator during work is reduced. The cyclone separator disclosed by the invention has the advantages of simple structure, easiness for implementing and convenience for reconstruction on the traditional device.

Description

The cyclone separator of the broken wing of built-in vortex core
Technical field
The present invention relates to a kind of cyclone separator, comprise: a cyclone separating chamber formed by column body segment and cone segments that inside is cavity, the recovering hopper be connected with the cyclone separating chamber cone segments, along column body segment tangential that arrange and the air inlet column body segment intracavity inter-connection, be positioned at the central exhaust outlet on column body segment top.
Background technology
Cyclone separator is a kind of common device separated from the gas of the particle for by gas, its basic structure by: inside is the cyclone separator be comprised of column body segment and cone segments of cavity, the recovering hopper be connected with the cyclone separator cone segments, along column body segment tangential that arrange and the air inlet column body segment intracavity inter-connection, and the central exhaust outlet that is positioned at the column body segment top forms.Cyclone separator is one of most widely used equipment, has a device structure simple, and volume is little, and manufacturing expense is low, safeguard, repair convenient, be easy to lay wear-resisting, corrosion resisting liner, but the purification of corrosive dust, and characteristics such as long service life.But the cyclone separator in use useless pressure loss is larger, affect the effect of its use.The useless pressure loss that how under the prerequisite that guarantees separative efficiency, to reduce separator is the problem that will solve present stage.
Summary of the invention
The invention provides a kind of prior art deficiency that overcomes, can guarantee separative efficiency, reduce the cyclone separator of the useless pressure loss.
The cyclone separator of the broken wing of built-in vortex core of the present invention comprises: the inside be comprised of column body segment and cone segments is cavity, cross section is the cyclone separating chamber of circle, the recovering hopper be connected with the cyclone separating chamber cone segments, along column body segment tangential that arrange and the air inlet column body segment intracavity inter-connection, be positioned at the central exhaust outlet on column body segment top, central shaft position along cyclone separating chamber in cyclone separator is provided with a fixed axis, the lower end of fixed axis is positioned at 1/2 place of taper contraction section, is provided with the broken fin of vortex core of fixed axis on fixed axis.
In the cyclone separator of the broken wing of built-in vortex core of the present invention, the floor projection length of the broken fin of vortex core be approximately equal on cyclone separating chamber's longitudinal profile geometric center to forced vortex the twice with free vortex intersection distance, the product of the broken fin width of vortex core and fin quantity is greater than the zero fixed axis length that is less than.
In the embodiment of the present invention, the broken fin of vortex core that is positioned at separation chamber column body segment part is that length is approximately equal to 1/6 the rectangular block that is approximately equal to the fixed axis diameter for central diameter of outlet, thickness; The broken fin of each vortex core of cyclone separating chamber cone segments part be length be approximately equal to its cross circular section diameter of living in 1/2, width is approximately equal to 1/6 the rectangular block that fixed axis length 1/23, thickness are approximately equal to the fixed axis diameter.Need the present invention of special instruction and the thickness of the broken fin of vortex core to have no special requirements, only require that its thickness can keep certain rigidity, the unlikely failure damage that in use occurs gets final product simultaneously.
In the cyclone separator of the broken wing of built-in vortex core of the present invention, the setting position that is arranged at the broken wing of fixed axis vortex core topmost should, slightly lower than the lower edge of central exhaust outlet, be positioned at the lower end of a little higher than fixed axis of the broken fin setting position of fixed axis vortex core bottom.
In the cyclone separator of the broken wing of built-in vortex core of the present invention, be provided with the broken wing of 8 vortex cores on its fixed axis, and broken interplane every two the equidistant quadrature arrangement of adjacent fin of each vortex core, the diameter of fixed axis is 1/2 of cone segments lower ending opening diameter, and the fixed axis lower end is positioned at 1/2 place of cyclone separator cone segments.
Correlative study shows, in cyclone separator when work, exist the inward eddy air-flow (be also referred to as forced vortex) mobile to central exhaust outlet in heart zone therein, in the cyclone separator central area to existing between the cyclone separator barrel along the outer eddy flow (being also referred to as free vortex) that separates the body wall rotational flow.Research also shows that the pressure loss of cyclone separator is mainly determined by the forced vortex of inward eddy, and separative efficiency is mainly determined by the free vortex of outer eddy flow.The pressure loss and separative efficiency are to weigh the leading indicator of Separation Performance of cyclone Separators, so, under the prerequisite that guarantees separative efficiency, the pressure loss that reduces the separator central area is to improve a key point of cyclone separator.
Technical solution of the present invention is: the built-in not kinetoplast consisted of fixed axis and the broken fin of vortex core that invests in the forced vortex zone of the cyclone separating chamber center of cyclone separator, replace and destroy forced vortex with kinetoplast not, to reduce the pressure loss.The length of the broken wing of the fixed axis in the present invention and vortex core and to be distributed in be to design according to forced vortex and free vortex position and shape in theory, the broken fin length of set vortex core should equal on the cyclone separator longitudinal profile geometric center to the twice of forced vortex and free vortex intersection distance in principle, make the broken fin of fixed axis and vortex core in inward eddy, its effect is both to have destroyed the inward eddy forced vortex, reduce the pressure loss, do not destroy again outer eddy flow free vortex, affect its collection efficiency simultaneously.According to related experiment, the edge of the broken fin of vortex core preferably is positioned at the intersection of forced vortex and free vortex, should retain as far as possible the large shared space of outer eddy flow simultaneously, to reduce, flowing of air-flow formed to obstruction with the whereabouts of particulate matter, meeting under this prerequisite the shape of the broken wing of vortex core and the restriction that setting there is no other.
Just because of this reason, in conjunction with the above-mentioned architectural feature of characteristics formation the present invention of existing cyclone separator.
The present invention by cyclone separator to the interior broken fin of vortex core that arranges, reduced the zone of forced vortex, weakened forced vortex intensity, also reduced the pressure loss simultaneously, energy consumption in the time of can reducing cyclone separator work, and the present invention is simple in structure, easily realize, be convenient to existing apparatus is transformed.
the accompanying drawing explanation
Accompanying drawing 1 is cyclone separator longitudinal profile schematic diagram of the present invention; The generalized section that accompanying drawing 2 is accompanying drawing 1 right apparent place; The schematic diagram that accompanying drawing 3 is accompanying drawing 1 head-down position; The schematic perspective view that accompanying drawing 4 is the broken fin of vortex core; Accompanying drawing 5 is the system schematic that device of the present invention carries out the dusty gas discrete testing; Accompanying drawing 6 is for adopting separative efficiency and the pressure loss comparison diagram of the fixed axis of different length in related experiment of the present invention, fixed axis length shown in figure is that the fixed axis bottom is apart from the distance between central exhaust outlet, abscissa 0cm is not for inserting the situation of the broken wing of fixed axis and vortex core, and 120cm represents that fixed axis is inserted into the situation of recovering hopper bottom.Wherein: with black lattice curve, being the collection efficiency curve of device, is the device falloff curve with the curve of deceiving trigonal lattice; Accompanying drawing 7 is separative efficiency and pressure loss comparison diagrams of the broken fin of vortex core of different length in related experiment of the present invention, and wherein: with black lattice curve, being falloff curve, is the collection efficiency curve with the curve of deceiving trigonal lattice.
In figure: 1, air inlet; 2, central exhaust outlet; 3, fixed axis; 4, recovering hopper; 5, column body segment; 6, cone segments; 7, fin (a, b, c, d are respectively the fin of different length); 8, air inlet; 9, screw(-type) feeder; 10, cyclone separator of the present invention; 11, manometer; 12, valve; 13, sack cleaner; 14, roots blower.
The specific embodiment
Below in conjunction with embodiment, the present invention is explained orally.
The cyclone separator that embodiments of the invention are used is referring to accompanying drawing 1 and accompanying drawing 2, and cyclone separating chamber wherein consists of column body segment 5 and cone segments 6, and wherein: the internal diameter of column body segment 5 is 200mm, and length is 400mm; The internal diameter of central authorities' exhaust outlet 2 is 100mm, and the length that central exhaust outlet 2 stretches into column body segment 5 is 140mm; The length of cone segments 6 is 400mm, and cone segments 6 is 50mm with the internal diameter of recovering hopper 4 connecting places.Fixed axis diameter in the cyclone separator of the embodiment of the present invention is 25mm, and the lower end of fixed axis is positioned at 1/2 place of taper contraction section 6.The equidistant broken fin of eight vortex cores that is provided with on fixed axis, distance is arranged for 50mm between every two fins, and the broken fin quadrature arrangement of two adjacent vortex cores, referring to Fig. 1 and Fig. 2, wherein five broken fins of vortex core are arranged in column body segment, see the 7a in Fig. 1 or Fig. 2, the rectangular block that broken each fin of fin of these five vortex cores is length 100mm, width 18mm, thickness 4mm; The broken fin of its excess-three vortex core respectively is arranged at the taper contraction section, referring to the 7b in Fig. 1 and Fig. 2,7c and 7d.And the broken fin of these three vortex cores is 1/2 rectangular block that length is approximately equal to respectively its cross section, relevant position circular diameter.
For testing device of the present invention, set up test macro as shown in Figure 5, in this test macro, screw(-type) feeder 9 is connected with the pipeline be connected with air inlet 8, and this pipeline is communicated with the air inlet 1 of cyclone separator of the present invention, and the central exhaust outlet 2 use pipeline connection sack cleaners 13 of separator, and sack cleaner 13 is connected with roots blower 14.Be provided with valve 12 on the pipeline that is communicated with 14 of central exhaust outlet 2 and sack cleaners, on cyclone separator air inlet 1 and central exhaust outlet 2, be provided with manometer 11.
Test macro of the present invention be take cement slurry as stand-by dust when being tested, with screw(-type) feeder 9 by cement slurry in respective line is sent into air inlet 1, the dust inlet concentration of take is tested as 66.7g/m3.
Start blower fan 14 while being tested, with valve 12 controlled wind speeds, be 20m/s, dusty gas passes in cyclone separator 10 of the present invention and is separated by 8,9, clean gas is discharged via roots blower 14, the dust granules separated is discharged by recovering hopper 4, obtain separative efficiency by inlet amount and load, with manometer 11 detected pressures losses, the position that stretches to cone in experiment by changing fixed axis obtains the graph of relation of acquisition means pressure drop and collection efficiency under different fixed axis length conditions, sees accompanying drawing 6.As seen from Figure 6, when the fixed axis lower end is about the position that stretches to cone segments 1/2 apart from the distance of central exhaust outlet for 60cm() time, when the broken fin end of vortex core during in forced vortex and free vortex intersection, the pressure loss obviously reduces, and collection efficiency is not obvious for changing, qualitative explanation: illustrate that the broken fin end of vortex core, when cone segments forced vortex and free vortex intersection, can play the effect of protecting the effect drag reduction.
Under condition as hereinbefore, adjust broken chord degree, record separative efficiency and the pressure loss of every group of experiment, see Fig. 7.By Fig. 7, known, when length of blade is 100mm(while approximating cyclone separator central authorities diameter of outlet, when blade during in forced vortex and free vortex intersection, the collection efficiency variation is not obvious, and pressure drop obviously descends.Illustrate when blade during in forced vortex and free vortex intersection, can play the effect of protecting the effect drag reduction.

Claims (5)

1. the cyclone separator of the broken wing of built-in vortex core, comprise: the inside be comprised of column body segment and cone segments is cavity, cross section is the cyclone separating chamber of circle, the recovering hopper be connected with the cone segments of cyclone separating chamber, along column body segment tangential that arrange and the air inlet column body segment intracavity inter-connection, be positioned at the central exhaust outlet on column body segment top, it is characterized in that the central shaft position along cyclone separator is provided with a fixed axis in cyclone separating chamber, the lower end of fixed axis is positioned at 1/2 place of taper contraction section, is provided with the broken fin of vortex core of fixed axis on fixed axis.
2. the cyclone separator of the broken wing of built-in vortex core according to claim 1, the floor projection length that it is characterized in that the broken wing of vortex core be approximately equal on cyclone separating chamber's longitudinal profile geometric center to forced vortex the twice with free vortex intersection distance, the product of the broken fin width of vortex core and fin quantity is greater than the zero length that is less than fixed axis.
3. the cyclone separator of the broken wing of built-in vortex core according to claim 2, is characterized in that the broken fin of vortex core of the column body segment part of cyclone separating chamber is that length is approximately equal to the rectangular block into central diameter of outlet; The broken fin of vortex core that is positioned at cyclone separating chamber's cone segments part is 1/2 rectangular block that length is approximately equal to its present position cross circular section diameter.
4. according to the cyclone separator of the broken wing of the described arbitrary built-in vortex core of claims 1 to 3, it is characterized in that being arranged at the broken wing of fixed axis vortex core topmost slightly lower than the lower edge of central exhaust outlet, be positioned at the lower end of a little higher than fixed axis of the broken fin setting position of fixed axis vortex core bottom.
5. want the cyclone separator of the broken wing of 4 described built-in vortex core according to right, it is characterized in that on fixed axis being provided with the broken wing of 8 vortex cores, and broken interplane every two the equidistant quadrature arrangement of adjacent fin of each vortex core, the diameter of fixed axis is 1/2 of cone segments lower ending opening diameter.
CN2013103595550A 2013-08-18 2013-08-18 Cyclone separator with internally installed vortex core crushing wing Pending CN103447173A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2013103595550A CN103447173A (en) 2013-08-18 2013-08-18 Cyclone separator with internally installed vortex core crushing wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2013103595550A CN103447173A (en) 2013-08-18 2013-08-18 Cyclone separator with internally installed vortex core crushing wing

Publications (1)

Publication Number Publication Date
CN103447173A true CN103447173A (en) 2013-12-18

Family

ID=49730242

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2013103595550A Pending CN103447173A (en) 2013-08-18 2013-08-18 Cyclone separator with internally installed vortex core crushing wing

Country Status (1)

Country Link
CN (1) CN103447173A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104190561A (en) * 2014-08-21 2014-12-10 山东科技大学 Self-driven intensive-separation swirler
CN104437907A (en) * 2014-11-26 2015-03-25 北京贝睿通信息咨询有限公司 Device and method for improving separation efficiency of cyclone separator using gaseous fluid flow
CN107597457A (en) * 2017-10-19 2018-01-19 询莱流体技术(上海)有限公司 A kind of cyclone separator for exempting from flutter valve
CN108245078A (en) * 2018-01-29 2018-07-06 兰州大学 A kind of dust catcher using wet type hypergravity separator

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4094772A (en) * 1976-05-22 1978-06-13 Krauss-Maffei Aktiengesellschaft Method of and apparatus for sorting light refuse fractions
JPH0549972A (en) * 1991-08-09 1993-03-02 Nippondenso Co Ltd Cyclone separator
CN101254489A (en) * 2008-02-29 2008-09-03 华东理工大学 Water cyclone with improved base pipe and overflows structure
CN101516784A (en) * 2006-09-28 2009-08-26 沃雷科有限责任公司 Vortex generator
CN203408805U (en) * 2013-08-18 2014-01-29 兰州大学 Cyclone separator with built-in vortex core breaking wing

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4094772A (en) * 1976-05-22 1978-06-13 Krauss-Maffei Aktiengesellschaft Method of and apparatus for sorting light refuse fractions
JPH0549972A (en) * 1991-08-09 1993-03-02 Nippondenso Co Ltd Cyclone separator
CN101516784A (en) * 2006-09-28 2009-08-26 沃雷科有限责任公司 Vortex generator
CN101254489A (en) * 2008-02-29 2008-09-03 华东理工大学 Water cyclone with improved base pipe and overflows structure
CN203408805U (en) * 2013-08-18 2014-01-29 兰州大学 Cyclone separator with built-in vortex core breaking wing

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104190561A (en) * 2014-08-21 2014-12-10 山东科技大学 Self-driven intensive-separation swirler
CN104437907A (en) * 2014-11-26 2015-03-25 北京贝睿通信息咨询有限公司 Device and method for improving separation efficiency of cyclone separator using gaseous fluid flow
CN104437907B (en) * 2014-11-26 2018-04-03 北京贝睿通信息咨询有限公司 For the apparatus and method for the separative efficiency for improving the cyclone separator using flow of gaseous fluid
CN107597457A (en) * 2017-10-19 2018-01-19 询莱流体技术(上海)有限公司 A kind of cyclone separator for exempting from flutter valve
CN108245078A (en) * 2018-01-29 2018-07-06 兰州大学 A kind of dust catcher using wet type hypergravity separator

Similar Documents

Publication Publication Date Title
CN103447173A (en) Cyclone separator with internally installed vortex core crushing wing
CN203494671U (en) Novel third-grade cyclone separation single tube for catalytically cracking
CN102343310A (en) Shunting core pipe and single-pipe cyclone separator with same
CN203408805U (en) Cyclone separator with built-in vortex core breaking wing
CN204710582U (en) A kind of helical type cyclone separator of improvement
CN203355532U (en) Natural gas filter
CN204789066U (en) Few sampling probe of maintenance is swept in outer blowback of high efficiency filter
CN207951756U (en) Stop cyclone separator
CN207308133U (en) A kind of axial swirler and system for being suitable for gas-solid two phases
CN204710555U (en) A kind of cyclone dust collectors of static electrification
CN203257512U (en) Composite spark arrester
CN101367064A (en) Cyclonic collector
CN104128269A (en) Tangential flow type parallel cyclone separator
CN204220315U (en) A kind of cyclone separator
CN212309892U (en) Cyclone separator, separation device and production line
CN211635874U (en) Filter cylinder type active carbon adsorption device
CN210252733U (en) High-efficiency multi-pipe cyclone separator
CN103691232A (en) Natural gas oil-gas separator with inverted circular truncated cone-shaped filter element
CN208894422U (en) Regenerator cyclone separator
CN203836487U (en) Floor heating blow-down valve
CN203862424U (en) Centrifugal guide vane of efficient double delamination cyclone separator
WO2016193802A1 (en) Cyclone separator
CN201613185U (en) Enhanced pre-filter device of air filter assembly
CN205643378U (en) Cleaning tube velocity of medium detection device
CN202199444U (en) Desulfurization-denitriding cyclone separator

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20131218