CN210674318U - High-efficiency rotational flow aviation kerosene dehydrator - Google Patents
High-efficiency rotational flow aviation kerosene dehydrator Download PDFInfo
- Publication number
- CN210674318U CN210674318U CN201920828127.0U CN201920828127U CN210674318U CN 210674318 U CN210674318 U CN 210674318U CN 201920828127 U CN201920828127 U CN 201920828127U CN 210674318 U CN210674318 U CN 210674318U
- Authority
- CN
- China
- Prior art keywords
- aviation kerosene
- water
- dehydrator
- cyclone
- cavity
- 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
Links
Images
Abstract
The utility model discloses a high-efficient whirl aviation kerosene dehydrator, including the shell body, greasy dirt discharge pipe, sewage feeding reposition of redundant personnel subassembly, cyclone separation subassembly, the drainage subassembly of catchmenting that top-down fixed in the shell body, the aviation kerosene that sets up in the shell body top is collected filtering component and is fixed to be set up the oily water inlet pipe at the shell body lateral part. The utility model has the characteristics of strong dehydration capability, high efficiency and stable water quality of outlet water, and the outside of the dehydrator only needs one path of oil sewage pipeline and one path of water outlet pipeline, thereby solving the problem of the existing sewage pipeline and water outlet pipeline which are distributed and dispersed in a mess; four cyclone separators are distributed in the dehydrator, so that the turbulence of the oil sewage is reduced after the flow is split, the dehydration separation effect is stable, and refined and efficient dehydration is realized; the air outlet pipe provides negative pressure to improve the overflow speed of the separated aviation kerosene, the aviation kerosene enters the grease filter from the air outlet pipe quickly, air is not discharged, and zero emission and no pollution are realized.
Description
Technical Field
The utility model relates to a dehydrator technical field, concretely relates to high-efficient whirl aviation kerosene dehydrator.
Background
The oil-water separation is an important link for sewage discharge standard treatment, the oil-water separator mainly separates oil or other organic matters which are insoluble in water and light in weight from water, and the existing oil-water separator has the problems that the oil-water separator with large treatment capacity has low separation precision, and the oil-water separator with high separation precision has low treatment efficiency; at present adopt cyclone to separate the dehydration more, but every separator of this kind of mode can only separate sewage all the way alone, not only need set up a plurality of sewage pipes, also need be equipped with corresponding outlet conduit, and manufacturing cost is high, and area is big, and sewage directly gets into cyclone moreover and produces high-speed torrent easily, and oil-water separation is unstable because the torrent influences separation effect.
It is therefore desirable to design an efficient and energy-saving apparatus for separating kerosene mixed with sewage.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a high-efficient whirl aviation kerosene dehydrator of dewatering ability reinforce, play water quality of water stability.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
a high-efficiency rotational flow aviation kerosene dehydrator comprises an outer shell, an oil stain discharge pipeline, a sewage feeding and shunting assembly, a rotational flow separation assembly, a water collecting and discharging assembly, an aviation kerosene collecting and filtering assembly and an oil sewage inlet pipe, wherein the oil stain discharge pipeline, the sewage feeding and shunting assembly, the rotational flow separation assembly and the water collecting and discharging assembly are fixed in the outer shell from top to bottom;
the sewage feeding and distributing assembly comprises a rotational flow feeding cavity fixed inside the outer shell and distributing openings circumferentially arrayed on the rotational flow feeding cavity, and the distributing openings are tangentially arranged with the circumference of the rotational flow feeding cavity.
As a further improvement of the present invention, the cyclone feeding cavity comprises an inner circumferential enclosing plate, an outer circumferential enclosing plate concentric with the inner circumferential enclosing plate, and an end plate fixed between the ends of the inner circumferential enclosing plate and the outer circumferential enclosing plate in a sealing manner, and the cyclone feeding cavity is an annular feeding cavity;
the oil sewage inlet pipe is communicated with the rotational flow feeding cavity from the tangential direction of the outer circumference of the rotational flow feeding cavity; each flow dividing port is arranged opposite to the flow direction of the oily water entering the rotational flow feeding cavity.
As a further improvement, the number of the flow dividing ports is four, and the included angle between the central axes of the adjacent flow dividing ports is the degree.
As a further improvement of the utility model, the cyclone separation assembly comprises four cyclone separators respectively communicated with the flow splitting ports, a aviation kerosene discharge port arranged at the top of each cyclone separator and a water discharge port arranged at the bottom of each cyclone separator;
and the oily water is tangentially injected into the corresponding cyclone separator through the flow dividing port.
As a further improvement of the utility model, the water collecting and discharging component comprises a water collecting cavity arranged below the water outlet of the cyclone separator and a water collecting cavity mounting rack fixedly connecting the water collecting cavity and the inner side wall of the outer shell;
the water collecting cavity is funnel-shaped, the upper port of the water collecting cavity collects the drained water of the water outlet, and the lower port of the water collecting cavity penetrates through the lower end of the outer shell.
As a further improvement of the utility model, the greasy dirt discharge pipe is including connecting respectively at the drainage tube of four boat kerosene discharge ports and fixing at the shell body top and converging four drainage tubes together the pressure manifold.
As a further improvement of the utility model, the aviation kerosene collecting and filtering component comprises an air outlet pipe which is horizontally arranged, a fan which is connected to one end of the air outlet pipe and is used for providing air pressure for the air outlet pipe, and a grease filter which is connected to the other end of the air outlet pipe;
and the air outlet of the grease filter is communicated with the air inlet of the fan through an air return pipe.
As a further improvement of the utility model, two sides of the upper end of the outer shell are respectively and fixedly provided with a bearing platform, and the fan and the grease filter are respectively arranged on the bearing platforms at the two sides;
and an inclined strut is fixed between the outer side wall of the outer shell and the lower surface of the bearing platform.
As a further improvement, the grease filter adopts a filter filled with an activated carbon filter material.
As a further improvement of the utility model, the pressure manifold is vertical direction, the pressure manifold communicates out the tuber pipe perpendicularly, aviation kerosene in the pressure manifold is along with the air current negative pressure drainage in the air-out pipe to going out the tuber pipe.
Compared with the prior art, the utility model discloses the beneficial effect who gains as follows:
the utility model has the characteristics of strong dehydration capability, high efficiency and stable water quality of outlet water, and the outside of the dehydrator only needs one path of oil sewage pipeline and one path of water outlet pipeline, thereby solving the problem of the existing sewage pipeline and water outlet pipeline which are distributed and dispersed in a mess; four cyclone separators are distributed in the dehydrator, so that the water flow entering the cyclone separators tangentially is reduced, the turbulence of the oil sewage after the flow splitting is reduced, the dehydration separation effect is stable, and the refined and high-efficiency dehydration is realized; purified water is collected by the funnel-shaped water collecting cavity and then is continuously discharged from the bottom of the outer shell, no water is accumulated in the water collecting cavity, and one path of water discharging pipeline is simple and convenient to arrange; the air outlet pipe provides negative pressure to improve the overflow speed of the separated aviation kerosene, the aviation kerosene rapidly enters the grease filter from the air outlet pipe, air is supplied to the fan after the aviation kerosene is filtered, air is not discharged, and zero emission and no pollution are realized.
Drawings
FIG. 1 is a schematic structural view of the present invention;
figure 2 is the structure sketch map that the utility model discloses cyclone is connected with whirl feeding chamber.
In the attached drawing, 1 outer shell, 2 mount pads, 3 cyclone feeding cavities, 4 oily water inlet pipes, 5 cyclone separators, 6 cyclone separator fixing frames, 7 water collecting cavities, 8 water collecting cavity mounting frames, 9 maintenance sealing doors, 10 drainage pipes, 11 collecting pipes, 12 inclined struts, 13 bearing platforms, 14 grease filters, 15 return air pipes, 16 air outlet pipes and 17 fans.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
As shown in the attached figure 1-2, the high-efficiency cyclone kerosene dehydrator comprises an outer shell 1, an oil stain discharge pipeline, a sewage feeding and shunting assembly, a cyclone separation assembly, a water collecting and discharging assembly, a aviation kerosene collecting and filtering assembly and an oil sewage inlet pipe 4, wherein the oil stain discharge pipeline, the sewage feeding and shunting assembly, the cyclone separation assembly and the water collecting and discharging assembly are fixed in the outer shell 1 from top to bottom;
the sewage feeding and distributing assembly comprises a rotational flow feeding cavity 3 fixed inside the outer shell 1 and distributing ports of a circumferential array on the rotational flow feeding cavity 3, and the distributing ports are tangentially arranged with the circumference of the rotational flow feeding cavity 3.
The cyclone feeding cavity 3 comprises an inner circumferential enclosing plate, an outer circumferential enclosing plate concentric with the inner circumferential enclosing plate and an end plate fixed between the ends of the inner circumferential enclosing plate and the outer circumferential enclosing plate in a sealing way, and the cyclone feeding cavity 3 is an annular feeding cavity;
the oil sewage inlet pipe 4 is communicated with the rotational flow feeding cavity 3 from the tangential direction of the outer circumference of the rotational flow feeding cavity 3; each flow dividing port is arranged opposite to the flow direction of the oily water entering the rotational flow feeding cavity 3.
The quantity of reposition of redundant personnel mouth is four, and the contained angle between the adjacent reposition of redundant personnel mouth axis is 90 degrees.
The cyclone separation assembly comprises four cyclone separators 5 respectively communicated with the flow splitting ports, aviation kerosene discharge ports arranged at the tops of the cyclone separators 5 and water discharge ports arranged at the bottoms of the cyclone separators 5;
the oily water is tangentially injected into the corresponding cyclone separator 5 through the flow dividing port.
The water collecting and discharging assembly comprises a water collecting cavity 7 arranged below the water outlet of the cyclone separator 5 and a water collecting cavity mounting frame 8 fixedly connecting the water collecting cavity 7 with the inner side wall of the outer shell 1;
the water collecting cavity 7 is funnel-shaped, the upper port of the water collecting cavity collects the drainage of the drainage outlet, and the lower port of the water collecting cavity penetrates through the lower end of the outer shell 1.
The oil stain discharge pipeline comprises drainage pipes 10 respectively connected with four aviation kerosene discharge ports and a collecting pipe 11 fixed at the top of the outer shell 1 and used for collecting the four drainage pipes 10 together.
The aviation kerosene collecting and filtering component comprises an air outlet pipe 16 which is horizontally arranged, a fan 17 which is connected with one end of the air outlet pipe 16 and used for providing air pressure for the air outlet pipe 16, and a grease filter 14 which is connected with the other end of the air outlet pipe 16;
the air outlet of the grease filter 14 is communicated with the air inlet of the fan 17 through an air return pipe 15.
and an inclined strut 12 is fixed between the outer side wall of the outer shell 1 and the lower surface of the bearing platform 13.
The grease filter 14 is a filter filled with an activated carbon filter material.
The collecting pipe 11 is in the vertical direction, the collecting pipe 11 is vertically communicated with the air outlet pipe 16, and the aviation kerosene in the collecting pipe 11 is drained to the air outlet pipe 16 along with the airflow negative pressure in the air outlet pipe 16.
The utility model discloses a boat kerosene dehydration working process as follows: oily water enters a cyclone feeding cavity 3 from an oily water inlet pipe 4 in a tangential direction, the oily water forms a flow direction rotating along an annular cavity in the cyclone feeding cavity 3, the oily water in the cyclone feeding cavity 3 is thrown into a cyclone separator 5 from a flow splitting port in the tangential direction, the oily water uniformly enters the cyclone separator 5 for cyclone separation, the cyclone separator 5 is a conical cavity and is provided with a tangential inlet connected with the flow splitting port and two axial outlets, the two axial outlets are respectively a aviation kerosene outlet arranged at the top of each cyclone separator 5 and a water outlet arranged at the bottom of each cyclone separator 5, the heterogeneous phase separation with different densities in a heterogeneous system is carried out by utilizing the centrifugal sedimentation principle, and an oily mixed liquid enters the cyclone separator 5 from the tangential inlet, so that the oily mixed liquid rotates at a high speed in the cyclone separator 5 to generate a centrifugal force field; under the action of the centrifugal force, the phase (water) with high density is thrown to the periphery, moves downwards along the wall surface and is discharged from a water outlet at the bottom; the phase (oil) with low density is brought to the middle and moves upwards, overflows to a aviation kerosene discharge port and is discharged, and the purpose of oil-water separation is achieved by using a cyclone separator 5; aviation kerosene overflowed from the four cyclone separators 5 flows into a collecting pipe 11 after passing through corresponding drainage pipes 10, and the aviation kerosene in the collecting pipe 11 enters the collecting pipe 11 and enters a grease filter 14 along with the wind direction due to negative pressure generated by the airflow direction in an air outlet pipe 16, the grease is filtered and adsorbed on the grease filter, and purified wind flows back to an air inlet of a fan 17; purified water discharged from water outlets at the bottoms of the four cyclone separators 5 is collected to the water collecting cavity 7 and then is uniformly discharged out of the outer shell.
The utility model has the characteristics of strong dehydration capability, high efficiency and stable water quality of outlet water, and the outside of the dehydrator only needs one path of oil sewage pipeline and one path of water outlet pipeline, thereby solving the problem of the existing sewage pipeline and water outlet pipeline which are distributed and dispersed in a mess; four cyclone separators are distributed in the dehydrator, so that the water flow entering the cyclone separators tangentially is reduced, the turbulence of the oil sewage after the flow splitting is reduced, the dehydration separation effect is stable, and the refined and high-efficiency dehydration is realized; purified water is collected by the funnel-shaped water collecting cavity 7 and then is continuously discharged from the bottom of the outer shell 1, no water is accumulated in the water collecting cavity 7, and one path of water discharging pipeline is simple and convenient to arrange; the air outlet pipe 16 provides negative pressure to improve the overflow speed of the separated aviation kerosene, the aviation kerosene rapidly enters the grease filter 14 from the air outlet pipe 16, air is supplied to the fan after the aviation kerosene is filtered, air is not discharged, and zero emission and no pollution are realized.
The above-described embodiments are merely preferred examples of the present invention and are not exhaustive of the possible implementations of the present invention. Any obvious modifications to the above would be obvious to those of ordinary skill in the art, but would not bring the invention so modified beyond the spirit and scope of the present invention.
Claims (10)
1. A high-efficient whirl aviation kerosene dehydrator which characterized in that: the device comprises an outer shell (1), an oil stain discharge pipeline, a sewage feeding and shunting assembly, a cyclone separation assembly, a water collecting and discharging assembly, a aviation kerosene collecting and filtering assembly and an oil sewage inlet pipe (4), wherein the oil stain discharge pipeline, the sewage feeding and shunting assembly, the cyclone separation assembly and the water collecting and discharging assembly are fixed in the outer shell (1) from top to bottom;
the sewage feeding and distributing assembly comprises a rotational flow feeding cavity (3) fixed inside the outer shell (1) and distributing ports of a circumferential array on the rotational flow feeding cavity (3), and the distributing ports are tangentially arranged with the circumference of the rotational flow feeding cavity (3).
2. The high efficiency cyclonic aviation kerosene dehydrator of claim 1, wherein: the cyclone feeding cavity (3) comprises an inner circumferential enclosing plate, an outer circumferential enclosing plate concentric with the inner circumferential enclosing plate and an end plate fixed between the ends of the inner circumferential enclosing plate and the outer circumferential enclosing plate in a sealing way, and the cyclone feeding cavity (3) is an annular feeding cavity;
the oil sewage inlet pipe (4) is communicated with the rotational flow feeding cavity (3) from the tangential direction of the outer circumference of the rotational flow feeding cavity (3); each flow dividing port is arranged opposite to the flow direction of the oily water entering the rotational flow feeding cavity (3).
3. The high efficiency cyclonic aviation kerosene dehydrator of claim 1, wherein: the quantity of reposition of redundant personnel mouth is four, and the contained angle between the adjacent reposition of redundant personnel mouth axis is 90 degrees.
4. The high efficiency cyclonic aviation kerosene dehydrator of claim 3, wherein: the cyclone separation assembly comprises four cyclone separators (5) respectively communicated with the flow splitting ports, a aviation kerosene discharge port arranged at the top of each cyclone separator (5) and a water discharge port arranged at the bottom of each cyclone separator (5);
the oily water is tangentially injected into the corresponding cyclone separator (5) through the flow dividing port.
5. The high efficiency cyclonic aviation kerosene dehydrator of claim 4, wherein: the water collecting and discharging assembly comprises a water collecting cavity (7) arranged below the water outlet of the cyclone separator (5) and a water collecting cavity mounting frame (8) fixedly connecting the water collecting cavity (7) with the inner side wall of the outer shell (1);
the water collecting cavity (7) is funnel-shaped, the upper port of the water collecting cavity collects the drained water of the water outlet, and the lower port of the water collecting cavity penetrates through the lower end of the outer shell (1).
6. The high efficiency cyclonic aviation kerosene dehydrator of claim 4, wherein: the oil stain discharge pipeline comprises drainage pipes (10) which are respectively connected with the four aviation kerosene discharge ports and a collecting pipe (11) which is fixed at the top of the outer shell (1) and used for collecting the four drainage pipes (10) together.
7. The high efficiency cyclonic aviation kerosene dehydrator of claim 6, wherein: the aviation kerosene collecting and filtering component comprises an air outlet pipe (16) which is horizontally arranged, a fan (17) which is connected with one end of the air outlet pipe (16) and used for providing air pressure for the air outlet pipe (16), and a grease filter (14) which is connected with the other end of the air outlet pipe (16);
the air outlet of the grease filter (14) is communicated with the air inlet of the fan (17) through an air return pipe (15).
8. The high efficiency cyclonic aviation kerosene dehydrator of claim 7, wherein: bearing platforms (13) are respectively and fixedly arranged on two sides of the upper end of the outer shell (1), and the fan (17) and the grease filter (14) are respectively arranged on the bearing platforms (13) on the two sides;
and an inclined strut (12) is fixed between the outer side wall of the outer shell (1) and the lower surface of the bearing platform (13).
9. The high efficiency cyclonic aviation kerosene dehydrator of claim 8, wherein: the grease filter (14) is a filter filled with an active carbon filter material.
10. A high efficiency cyclonic aviation kerosene dehydrator as claimed in any one of claims 7-9 wherein: the collecting pipe (11) is in the vertical direction, the collecting pipe (11) is vertically communicated with the air outlet pipe (16), and the aviation kerosene in the collecting pipe (11) is drained to the air outlet pipe (16) along with the negative pressure of air flow in the air outlet pipe (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920828127.0U CN210674318U (en) | 2019-06-04 | 2019-06-04 | High-efficiency rotational flow aviation kerosene dehydrator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920828127.0U CN210674318U (en) | 2019-06-04 | 2019-06-04 | High-efficiency rotational flow aviation kerosene dehydrator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210674318U true CN210674318U (en) | 2020-06-05 |
Family
ID=70891871
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920828127.0U Active CN210674318U (en) | 2019-06-04 | 2019-06-04 | High-efficiency rotational flow aviation kerosene dehydrator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210674318U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112742111A (en) * | 2020-12-24 | 2021-05-04 | 大庆东大盛源科技开发有限公司 | Novel detachable efficient upper water distribution filter for oil field |
-
2019
- 2019-06-04 CN CN201920828127.0U patent/CN210674318U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112742111A (en) * | 2020-12-24 | 2021-05-04 | 大庆东大盛源科技开发有限公司 | Novel detachable efficient upper water distribution filter for oil field |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2018006766A1 (en) | Multi-mechanism wet dust removal apparatus achieving water circulation use and dust removal method | |
| CA2308410A1 (en) | Cyclone separator | |
| CN210674318U (en) | High-efficiency rotational flow aviation kerosene dehydrator | |
| CN201361490Y (en) | Combined filtration and separation device | |
| CN115974357B (en) | Separation device for oil-containing sewage sludge treatment and application method thereof | |
| CN104001630A (en) | Low-resistance cyclone separator of coal bed gas air blower | |
| CN209128172U (en) | A kind of centrifugal oil-water separator | |
| CN203886311U (en) | Device for removing coal ash from coal bed gas | |
| CN100551485C (en) | Drip-irrigation water-current mud-sand separation system | |
| CN101912828B (en) | Whirlwind-type separation device for conveying powder particle materials | |
| CN205856055U (en) | A kind of industrial circulating water is at the monitoring of tape oil, degreasing unit | |
| CN207641672U (en) | A kind of metalloid core cylinder in recirculating fluidized bed whirlwind separator | |
| CN207887348U (en) | A kind of metalloid core cylinder in recirculating fluidized bed whirlwind separator | |
| CN207950957U (en) | Separator for producing krypton xenon | |
| CN206385102U (en) | A kind of dedusting dehydrating tower | |
| CN215784058U (en) | Tailings self-dewatering device of hydraulic classification cyclone | |
| CN105999950A (en) | Novel high-efficiency gas-liquid separating device | |
| CN203170123U (en) | Industrial oil-gas separator | |
| CN212440398U (en) | Oil mist separator liquid recovery device | |
| CN209670036U (en) | Oil-water separation system | |
| CN105087095A (en) | Gas-liquid separator for natural gas | |
| CN206121331U (en) | Centrifugal gas -liquid defroster | |
| CN220697120U (en) | Integrated lotus root starch cyclone device | |
| CN101147663B (en) | Vacuum cleaner | |
| CN220738009U (en) | Wet cyclone separator |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |