CN211099618U - Spiral cooling jacket device for butterfly separator - Google Patents
Spiral cooling jacket device for butterfly separator Download PDFInfo
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- CN211099618U CN211099618U CN201922143878.1U CN201922143878U CN211099618U CN 211099618 U CN211099618 U CN 211099618U CN 201922143878 U CN201922143878 U CN 201922143878U CN 211099618 U CN211099618 U CN 211099618U
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- cooling jacket
- jacket device
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- spiral
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Abstract
The utility model discloses a butterfly separator is with spiral cooling jacket device, including fuselage, frame and cooling jacket device, the fuselage sets up the top at the frame, the bottom surface diameter of fuselage is the twice of frame bottom surface diameter, just the fuselage coincides mutually with the perpendicular bisector of frame, the top of fuselage is equipped with the top cap, the internal weld of fuselage is fixed with the rotary drum, the internal weld of rotary drum is fixed with the plate rail, the last surface weld of plate rail is fixed with the disc group, the fuselage passes through the transmission shaft with the frame and rotates and be connected, be equipped with cooling jacket device around the fuselage, the spiral spacer is the heliciform and revolves around the inside at cooling jacket device. This butterfly separator is with spiral cooling jacket device makes the coolant liquid can fully cool off to every place, does not have the dead angle, has improved cooling efficiency and cooling effect greatly.
Description
Technical Field
The utility model belongs to the technical field of the separating centrifuge, concretely relates to butterfly separator is with spiral cooling jacket device.
Background
The disc separator is a vertical centrifuge, and a rotary drum is arranged at the upper end of a vertical shaft and is driven by a motor through a transmission device to rotate at a high speed. The drum is provided with a group of disk-shaped parts, namely disks, which are mutually sleeved together. A small gap is left between the disks. The suspension (or emulsion) is fed into the drum through a feed pipe located in the center of the drum. As the suspension (or emulsion) flows through the gaps between the discs, the solid particles (or droplets) settle by the centrifuge onto the discs to form a sediment (or liquid layer). The sediment slides along the surface of the disc to be separated from the disc and is accumulated at the part with the largest inner diameter of the rotary drum, and the separated liquid is discharged out of the rotary drum from the liquid outlet. The disc is used for shortening the settling distance of solid particles (or liquid drops) and expanding the settling area of the rotary drum, and the production capacity of the separator is greatly improved due to the disc arranged in the rotary drum. The solids accumulated in the drum are removed manually by disassembling the drum after the separator is shut down, or discharged from the drum through a slag discharge mechanism without shutting down the separator. The butterfly separator needs to use a cooling jacket device in many special industries to rapidly reduce the temperature of a rotary drum, however, most of the existing butterfly separators are not provided with the cooling jacket device or have the defects of insufficient cooling and poor cooling effect.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a butterfly separator is with spiral cooling jacket device to solve the insufficient, poor problem of cooling effect of rotary drum cooling.
In order to achieve the above object, the utility model provides a following technical scheme: a spiral cooling jacket device for a butterfly separator comprises a machine body, a machine base and a cooling jacket device, the machine body is arranged at the top of the machine base, the diameter of the bottom surface of the machine body is twice that of the bottom surface of the machine base, the machine body is coincided with the perpendicular bisector of the machine base, the top of the machine body is provided with a top cover, a rotary drum is welded and fixed in the machine body, a disk frame is welded and fixed in the rotary drum, a disk group is welded and fixed on the upper surface of the disk frame, the machine body is rotationally connected with the machine base through a transmission shaft, cooling jacket devices are arranged around the machine body, the cooling jacket device comprises a cooling liquid inlet, a cooling liquid outlet, cooling liquid and a spiral spacer, the cooling liquid inlet is arranged at the bottom of one side of the cooling jacket device, the cooling liquid outlet is arranged at the top of the other side of the cooling jacket device, and the spiral spacer is spirally wound in the cooling jacket device.
Preferably, the cooling jacket device is in an annular column shape and is fixedly connected with the machine body through welding.
Preferably, the cooling jacket device is made of aluminum alloy, and the cooling liquid inlet, the cooling liquid outlet and the spiral spacer are of an integrated structure with the cooling jacket device.
Preferably, the helical partition divides the inner cavity of the cooling jacket device into a helical channel.
Preferably, the cooling liquid is made of water, enters the cavity of the cooling jacket device from the cooling liquid inlet, moves upwards through the spiral channel, and flows out through the cooling liquid outlet.
The utility model discloses a technological effect and advantage: this butterfly separator is with spiral cooling jacket device adopts spiral blade formula structure, and the spiral spacer begins to be the heliciform from the bottom coolant liquid import and winds to the coolant liquid export around the fuselage for the coolant liquid can fully cool off to every place, does not have the dead angle, has improved cooling efficiency and cooling effect greatly.
Drawings
FIG. 1 is a sectional view of the structure of the present invention;
fig. 2 is a detailed sectional view of the cooling jacket device of the present invention.
In the figure: 1-machine body, 2-machine base, 3-rotary drum, 4-disc group, 5-transmission shaft, 6-disc frame, 7-top cover, 8-cooling jacket device, 81-cooling liquid inlet, 82-cooling liquid outlet, 83-cooling liquid and 84-spiral spacer.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
The utility model provides a spiral cooling jacket device for butterfly separator as shown in the figure, which comprises a machine body 1, a machine base 2 and a cooling jacket device 8, wherein the machine body 1 is arranged at the top of the machine base 2, the diameter of the bottom surface of the machine body 1 is twice of that of the bottom surface of the machine base 2, the machine body 1 coincides with the perpendicular bisector of the machine base 2, the top of the machine body 1 is provided with a top cover 7, the machine body 1 is internally welded and fixed with a rotary drum 3, the rotary drum 3 is internally welded and fixed with a disc frame 6, the upper surface of the disc frame 6 is welded and fixed with a disc group 4, the machine body 1 is rotationally connected with the machine base 2 through a transmission shaft 5, the periphery of the machine body 1 is provided with the cooling jacket device 8, the cooling jacket device 8 comprises a cooling liquid inlet 81, a cooling liquid outlet 82, a cooling liquid 83 and a spiral spacer 84, the cooling liquid inlet 81 is arranged at the, the cooling liquid outlet 82 is arranged at the top of the other side of the cooling jacket device 8, and the spiral partition 84 is spirally wound in the cooling jacket device 8. In addition, cooling jacket device 8 is the annular column and passes through welded fastening with fuselage 1 to be connected, increases the area of contact of coolant liquid 83 with fuselage 1, promotes the cooling effect, and welded structure is firm. The material of cooling jacket device 8 is the aluminum alloy, and coolant liquid import 81, coolant liquid export 82 and spiral spacer 84 all with cooling jacket device 8 formula structure as an organic whole, and the aluminum alloy material has the quality light, advantage such as with low costs and corrosion-resistant, and the integral type structure is more firm and can improve machining efficiency. The spiral partition 84 divides the inner cavity of the cooling jacket device 8 into a spiral channel, so that the cooling liquid 83 flows along the channel, the contact time of the cooling liquid 83 and the machine body 1 is prolonged, and the cooling effect is improved. The cooling liquid 83 is made of water, enters the cavity of the cooling jacket device 8 from the cooling liquid inlet 81, moves upwards through the spiral channel, and flows out through the cooling liquid outlet 82, and the cooling liquid 83 is convenient and easy to obtain, low in cost and recyclable.
The working principle is as follows: when the spiral cooling jacket device for the butterfly separator is used, the cooling liquid 83 is injected from the cooling liquid inlet 81, the cooling liquid 83 enters the cavity of the cooling jacket device 8, spirally rises along a channel isolated by the spiral spacer 84, and is discharged from the cooling liquid outlet 82. This butterfly separator is with spiral cooling jacket device adopts spiral blade formula structure, and spiral spacer 84 begins to be the heliciform from bottom coolant liquid import 81 and winds to coolant liquid outlet 82 around fuselage 1 for coolant liquid 83 can fully cool off to every place, does not have the dead angle, has improved cooling efficiency and cooling effect greatly.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.
Claims (5)
1. The utility model provides a butterfly separator is with spiral cooling jacket device, includes fuselage (1), frame (2) and cooling jacket device (8), its characterized in that: the machine body (1) is arranged at the top of the machine base (2), the diameter of the bottom surface of the machine body (1) is two times of the diameter of the bottom surface of the machine base (2), the machine body (1) coincides with the perpendicular bisector of the machine base (2), the top of the machine body (1) is provided with a top cover (7), the machine body (1) is fixedly welded with a rotary drum (3), the rotary drum (3) is fixedly welded with a disc frame (6), the disc frame (6) is fixedly welded with a disc group (4), the machine body (1) is rotatably connected with the machine base (2) through a transmission shaft (5), cooling jacket devices (8) are arranged around the machine body (1), each cooling jacket device (8) comprises a cooling liquid inlet (81), a cooling liquid outlet (82), cooling liquid (83) and a spiral spacer (84), and the cooling liquid inlet (81) is arranged at the bottom of one side of the cooling jacket device (8), the cooling liquid outlet (82) is arranged at the top of the other side of the cooling jacket device (8), and the spiral partition (84) is spirally wound in the cooling jacket device (8).
2. The spiral cooling jacket device for the butterfly separator according to claim 1, wherein: the cooling jacket device (8) is in an annular column shape and is fixedly connected with the machine body (1) through welding.
3. The spiral cooling jacket device for the butterfly separator according to claim 1, wherein: the cooling jacket device (8) is made of aluminum alloy, and the cooling liquid inlet (81), the cooling liquid outlet (82) and the spiral spacer (84) are all in an integrated structure with the cooling jacket device (8).
4. The spiral cooling jacket device for the butterfly separator according to claim 1, wherein: the helical partition (84) divides the inner cavity of the cooling jacket device (8) into a helical channel.
5. The spiral cooling jacket device for the butterfly separator according to claim 1 or 4, wherein: the cooling liquid (83) is made of water, enters the cavity of the cooling jacket device (8) from the cooling liquid inlet (81), moves upwards through the spiral channel, and flows out through the cooling liquid outlet (82).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922143878.1U CN211099618U (en) | 2019-12-04 | 2019-12-04 | Spiral cooling jacket device for butterfly separator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922143878.1U CN211099618U (en) | 2019-12-04 | 2019-12-04 | Spiral cooling jacket device for butterfly separator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211099618U true CN211099618U (en) | 2020-07-28 |
Family
ID=71712995
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922143878.1U Active CN211099618U (en) | 2019-12-04 | 2019-12-04 | Spiral cooling jacket device for butterfly separator |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211099618U (en) |
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2019
- 2019-12-04 CN CN201922143878.1U patent/CN211099618U/en active Active
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