CN102989404B - A kind of impact flow reactor - Google Patents
A kind of impact flow reactor Download PDFInfo
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- CN102989404B CN102989404B CN201210502537.9A CN201210502537A CN102989404B CN 102989404 B CN102989404 B CN 102989404B CN 201210502537 A CN201210502537 A CN 201210502537A CN 102989404 B CN102989404 B CN 102989404B
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Abstract
The invention discloses a kind of impact flow reactor, described reactor is provided with charging aperture and discharge port, two guide shells are provided with in reactor, fluid impingement zone is formed between the outlet of guide shell, in each guide shell, correspondence is provided with screw, the hand of spiral of described screw is contrary, is respectively used to propelling fluid and flows to fluid impingement zone through guide shell from charging aperture, it is characterized in that being provided with spiral diversion sheet on each guide shell inwall.The present invention had both remained strong microcosmic mixing and the flowing of liquid continuous circulation, enhance again the mixing outside knockout process and impingement region, make the fluid in reactor reach mixed uniformly time shorten, increase substantially production efficiency, can good economic performance be obtained.
Description
Technical field
The present invention relates to the reactor in a kind of chemical production field, particularly a kind of impact flow reactor.
Background technology
Chemical reaction process is the core of Chemical Manufacture and key, and for most of liquid phase reaction course, reaction (device) device mass transfer and mixed effect affect great on reaction mass and efficiency.Using maximum in current reactor is stirred tank reactor (Stirred Tank Reactor is called for short STR), but STR mixed effect is unsatisfactory for fast reaction process, even has a negative impact to reaction mass and efficiency in some cases.Therefore, research and develop new and effective mixing reactor and become current chemical field strengthening fast reaction process problem demanding prompt solution, many impact flow reactor patents are arisen at the historic moment thus, its principal character reaches the objects such as strengthening mass transfer by the high-speed impact of two strands of fluids in opposite directions, through studying for many years, percussion flow shows good mixed characteristic, especially significantly can strengthen microcosmic mixing.But in numerous impact flow reactor patent, if patent " a kind of for liquid reactive impact flow reactor " (patent No.: CN200510045866.5) is by the effect of pump, the speed that liquid is certain, it is made to clash in opposite directions, another patent " irrotationality vertical circulation impact flow reactor " (patent No.: CN200720083472.3) is by the effect of guide shell internal propeller, impel fluid-phase to shock, both can reach the object of strengthening mixing, but group always tends to stream line motion due to stream, be in divided stream group between contact with each other very difficult, and above-mentioned patent all only focuses on two fluid-phases to shock, in addition, seldom relate to the flow field mixture situation outside the motion mode of fluid mass and impingement region, therefore the strengthening mixing of impingement region has certain limit, and the strengthening mixing except impingement region, the mixing of other region is more weak.
Summary of the invention
Technical problem to be solved by this invention is to provide a kind of knockout process can not only strengthening percussion flow for above-mentioned the deficiencies in the prior art, and can strengthen the impact flow reactor of the flow field mixture outside impingement region.
The present invention for solving the problems of the technologies described above adopted technical scheme is: a kind of impact flow reactor, described reactor is provided with charging aperture and discharge port, two guide shells are provided with in reactor, fluid impingement zone is formed between the outlet of guide shell, in each guide shell, correspondence is provided with screw, the hand of spiral of described screw is contrary, be respectively used to propelling fluid flow to fluid impingement zone through guide shell from charging aperture, it is characterized in that being provided with spiral diversion sheet on each guide shell inwall.
By technique scheme, the hand of spiral of each spiral diversion sheet is identical with the hand of spiral of its corresponding screw.
By technique scheme, the outlet of the spiral diversion sheet in two guide shells is in being dislocatedly distributed.
By technique scheme, the exit position of two spiral diversion sheets is 135 ° ~ 225 °.
By technique scheme, described reactor is vertical reactor, and two guide shells are vertically coaxial to be installed in reactor, being installed in corresponding guide shell of described two propeller coaxials.
By technique scheme, described reactor is horizontal reactor, the left and right symmetric coaxial of two guide shells be installed in reactor, described two screws are installed in corresponding guide shell.
By technique scheme, 15 ° ~ 60 °, the blade inclination angle of described screw.
By technique scheme, the thickness of described spiral diversion sheet is 1/12 ~ 1/10 of guide shell internal diameter.
By technique scheme, the pitch of described spiral diversion sheet is 1/3 ~ 1 of guide shell internal diameter.
Beneficial effect acquired by the present invention is:
1, this reactor is by arranging spiral diversion sheet on guide shell inwall, fluid in guide shell is flowed along with strong rotation, the interaction of turbulent flow and spiral flow, turbulence intensity is increased greatly, and then mutually clash on impingement region, thus strengthen knockout process further, obtain higher strengthening mixed effect, and the fluid rotated can drive guide shell to enter, outlet fluid around mixes mutually, it entrainments ability, blending effect is larger than acylic motion, make mixing flow field expanded range, simultaneously guide shell is inner there is the bending and flowing oblique of streamline due to arranging of spiral diversion sheet, improve the anisotropy in flow field, make flow field medium velocity layering obvious, to push the speed gradient, thus the flow field mixture enhanced outside impingement region,
2, the present invention had both remained strong microcosmic mixing and the flowing of liquid continuous circulation, enhance again the mixing outside knockout process and impingement region, make the fluid in reactor reach mixed uniformly time shorten, increase substantially production efficiency, can good economic performance be obtained.
Accompanying drawing explanation
Fig. 1 is the structural representation of the impact flow reactor of vertical structure.
Fig. 2 is that the A-A of Fig. 1 is to sectional view.
Fig. 3 is the B partial enlarged drawing of Fig. 1.
Fig. 4 is the inclination angle schematic diagram of propeller blade.
Fig. 5 is the structural representation of guide shell.
Fig. 6 is the structural representation of spiral diversion sheet.
Fig. 7 is the exit position dislocation schematic diagram of spiral diversion sheet.
Fig. 8 is the perspective view of the impact flow reactor of vertical structure.
Fig. 9 is the structural representation of the impact flow reactor of horizontal type structure.
Figure 10 is the perspective view of the impact flow reactor of horizontal type structure.
Detailed description of the invention
Below in conjunction with accompanying drawing, the invention will be further described.
Embodiment 1:
As shown in Figures 1 to 8, a kind of impact flow reactor, it is vertical structure, it comprises reactor bearing 1, barrel type reactor 3, feed pipe 2, blast pipe 5, discharge duct 8, guide shell 4, spiral diversion sheet 7 and screw 6, reactor 3 is fixed on reactor bearing 1, the upper and lower side of reactor 1 is equipped with charging aperture, connected by feed pipe 2, described discharge duct 8 is installed in the lower end of reactor 1, described blast pipe 5 is arranged on the upper end of reactor 3, upper in the inside of reactor 3, lower end is coaxially installed with two guide shells 4, fluid impingement zone IZ is formed between the outlet of guide shell, the screw 6 that two rotation directions are contrary is coaxially arranged with in guide shell 4, be respectively used to propelling fluid flow to fluid impingement zone IZ from top and bottom through guide shell 4, in order to strengthen knockout process, the inwall of each guide shell is provided with spiral diversion sheet 7.
The course of work of the present invention is: the rotation of two screws 6, drive reactor 3 inner fluid respectively from upper, the charging aperture turn of lower end enters guide shell 4, act on because the fluid near guide shell 4 inwall is subject to spiral diversion sheet 7, hinder fluid longitudinal flow, fluid flow line is bent and flowing oblique, and guide it to rotate outflow guide shell 4, clash in opposite directions at impingement region IZ, then the fluid flowed out from impingement region IZ is by turning back to the region between screw 6 and reactor 3 end between guide shell 4 outer wall and reactor 3 inwall, simultaneously, in entering of guide shell 4, exit region, because the turnover of whirl fluid is entrainmented and blending along with strong, the flow direction of fluid is: from the import of guide shell to guide shell inside spin again to impingement region IZ, fluid after impingement region IZ clashes into arrives between guide shell outer wall and inside reactor again, arrive the import of guide shell again, so circulate.
Through test, when the blade inclination alpha of two screws is 15 ° ~ 60 °, can the mixed performance of enhance fluid and circulation ability further.In order to increase impact of the present invention further, the hand of spiral of each spiral diversion sheet can be made identical with the hand of spiral of its corresponding screw.
As shown in Figure 7, due to fluid along 7 outgoing of spiral diversion sheet time, there is certain angle of emergence, therefore the exit position of adjustable spiral diversion sheet between two guide shells, its exit position can be made to be 0 ° ~ 360 ° be dislocatedly distributed, when fluid flows out along spiral diversion sheet from guide shell exit position, different dislocation efflux angle energy enhance fluid is entrainmented, mixing capacity and Shearing Flow, thus enhances the flow field mixture of knockout process.When the exit position of two spiral diversion sheets is β angle, when β angle is 135 ° ~ 225 °, fluid issuing curl obtains superposition and increases, and enhance fluid is entrainmented, blending, and impact effects is relatively good.
The thickness of adjustable spiral diversion sheet 7 of the present invention, when thickness increases, fluid longitudinal flow is obstructed increase, and energy consumption increases, the increase but stream group is disturbed, streamline changes, and speed also changes, cause the layering of guide shell 4 fluid velocity inside obvious, velocity gradient increases, thus the fluid chemical field scope in guide shell 4 is increased and the increase of turbulence intensity, thus enhance the flow field mixture before shock.When the thickness L of spiral diversion sheet 7 is guide shell 4 internal diameter 1/12 ~ 1/10, within the scope of this, fluid longitudinal flow is obstructed less, but velocity gradient is comparatively large, and impingement mix effectiveness comparison is good.
The number of turns of adjustable spiral diversion sheet 7 of the present invention, because guide shell 4 is highly certain, when the number of turns of spiral diversion sheet 7 changes, its pitch also changes, and when the number of turns increases, guide shell 4 inner fluid outlet curl increases, reduce stroke speed, but it is strengthened the entrainmenting of the fluid of guide shell 4 import and export, blending effect, the fluid chemical field scope in reactor is increased and the increase of turbulence intensity, thus enhance knockout process.Due to guide shell 4 height one timing, because the change of guide shell internal diameter (as reduced) can affect the fluid flow (reduction) of reactor impingement region, and then energy per volume dissipative shock wave change (increase) affected in impingement region, and energy per volume dissipative shock wave (increase) is mixed with the impact of important (enhancing) to microcosmic, when the pitch H of spiral diversion sheet 7 is 1/3 ~ 1 of guide shell 4 internal diameter, the fluid angle of emergence is less, its curl is increased, enhance the entrainmenting of fluid outlet, blending, impingement mix effectiveness comparison is good.
Embodiment 2:
As shown in Fig. 9,10, impact flow reactor described in embodiment 2 is substantially identical with the structure of the impact flow reactor in embodiment 1, difference is, it is horizontal type structure, described feed pipe 2 is arranged on the left and right two ends of reactor 3, and described guide shell 4 is arranged on the left and right two ends of reactor 3.
In sum, impact flow reactor of the present invention had both remained strong microcosmic mixing and the flowing of liquid continuous circulation, enhance again the mixing outside knockout process and impingement region, the fluid in reactor is made to reach mixed uniformly time shorten, increase substantially production efficiency, can good economic performance be obtained.
Claims (5)
1. an impact flow reactor, described reactor is provided with charging aperture and discharge port, two guide shells are provided with in reactor, fluid impingement zone is formed between the outlet of guide shell, in each guide shell, correspondence is provided with screw, the hand of spiral of described screw is contrary, be respectively used to propelling fluid flow to fluid impingement zone from charging aperture through guide shell, the hand of spiral of each spiral diversion sheet is identical with the hand of spiral of its corresponding screw, it is characterized in that being provided with spiral diversion sheet on each guide shell inwall, the outlet of the spiral diversion sheet in two guide shells is in being dislocatedly distributed, the exit position of two spiral diversion sheets is 135 ° ~ 225 °, and the thickness of described spiral diversion sheet is 1/12 ~ 1/10 of guide shell internal diameter, and the pitch of described spiral diversion sheet is 1/3 ~ 1 of guide shell internal diameter.
2. a kind of impact flow reactor according to claim 1, is characterized in that: described reactor is vertical reactor, and two guide shells are vertically coaxial to be installed in reactor, being installed in corresponding guide shell of described two propeller coaxials.
3. a kind of impact flow reactor according to claim 1, is characterized in that: described reactor is horizontal reactor, the left and right symmetric coaxial of two guide shells be installed in reactor, described two screws are installed in corresponding guide shell.
4. a kind of impact flow reactor according to claim 2, is characterized in that: 15 ° ~ 60 °, the blade inclination angle of described screw.
5. a kind of impact flow reactor according to claim 3, is characterized in that: 15 ° ~ 60 °, the blade inclination angle of described screw.
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CN201210502537.9A CN102989404B (en) | 2012-11-30 | 2012-11-30 | A kind of impact flow reactor |
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CN102989404B true CN102989404B (en) | 2015-09-09 |
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CN104556174B (en) * | 2013-10-22 | 2016-04-27 | 中国石油化工股份有限公司 | A kind of impact flow reactor |
CN107522591B (en) * | 2016-06-19 | 2020-05-19 | 中国石油化工股份有限公司 | Xylene separation process |
CN108380129B (en) * | 2018-04-02 | 2020-07-10 | 长乐智高生物科技有限公司 | Working method of mixing equipment for liquid materials based on worm and gear self-rotation principle |
CN108435006B (en) * | 2018-04-02 | 2020-07-24 | 浙江兴舟纸业有限公司 | Mixing equipment for liquid material based on worm and gear self-rotation principle |
CN108704599B (en) * | 2018-07-16 | 2024-02-20 | 山东绿色自由基科技研究中心 | Heterogeneous reaction device |
CN108671876B (en) * | 2018-07-16 | 2024-02-20 | 山东绿色自由基科技研究中心 | Heterogeneous catalytic reaction device of multiphase flow |
CN109225117B (en) * | 2018-09-17 | 2024-04-16 | 沈阳化工大学 | Impinging stream reaction kettle for preparing ultrafine powder |
CN109529744A (en) * | 2018-11-26 | 2019-03-29 | 吴小利 | A kind of chemical reaction kettle of convection current mixing |
CN112169736B (en) * | 2020-09-30 | 2022-01-07 | 沈阳化工研究院有限公司 | Micro-collision flow stirring reactor |
CN114762811A (en) * | 2021-01-13 | 2022-07-19 | 南京公汇科技有限公司 | Efficient impinging stream mixing device |
CN113680302B (en) * | 2021-08-11 | 2022-10-14 | 浙江智英石化技术有限公司 | Reaction device for preparing ethylbenzene hydroperoxide |
CN115069205B (en) * | 2022-07-08 | 2024-02-23 | 宁波诺丁汉大学 | Composite vortex reactor |
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CN2659539Y (en) * | 2003-02-20 | 2004-12-01 | 武汉化工学院 | Vertical circulation impacting flow reactor |
CN2810740Y (en) * | 2005-01-05 | 2006-08-30 | 武汉化工学院 | Vertical circulative impinging stream reactor |
WO2007093668A1 (en) * | 2006-02-17 | 2007-08-23 | Outotec Oyj. | Method and mixer apparatus for mixing gas into slurry in a closed reactor |
CN201046396Y (en) * | 2007-02-06 | 2008-04-16 | 伍沅 | Non-rotary vertical cyclic liquid knockout reactor |
CN201593047U (en) * | 2010-01-21 | 2010-09-29 | 伍沅 | Liquid continuous impinging stream multi-phase reaction and aerobic fermentation technical equipment |
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CN2531870Y (en) * | 2002-02-07 | 2003-01-22 | 武汉化工学院 | Injection reactor for liquid-liquid reaction |
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Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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CN2659539Y (en) * | 2003-02-20 | 2004-12-01 | 武汉化工学院 | Vertical circulation impacting flow reactor |
CN2810740Y (en) * | 2005-01-05 | 2006-08-30 | 武汉化工学院 | Vertical circulative impinging stream reactor |
WO2007093668A1 (en) * | 2006-02-17 | 2007-08-23 | Outotec Oyj. | Method and mixer apparatus for mixing gas into slurry in a closed reactor |
CN201046396Y (en) * | 2007-02-06 | 2008-04-16 | 伍沅 | Non-rotary vertical cyclic liquid knockout reactor |
CN201593047U (en) * | 2010-01-21 | 2010-09-29 | 伍沅 | Liquid continuous impinging stream multi-phase reaction and aerobic fermentation technical equipment |
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Effective date of registration: 20160229 Address after: 430223, East Lake hi tech Zone, Hubei, Wuhan No. 18, No. four, Optics Valley Huijin center, 6B Patentee after: Hubei Hengxin Petrochemical Equipment Co., Ltd. Address before: 430074 Wuhan, Hongshan Province District, hung Chu street, No. 693 Patentee before: Wuhan Institute of Technology |
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Granted publication date: 20150909 Termination date: 20181130 |