CN208382179U - Oxidator chilling segment structure - Google Patents
Oxidator chilling segment structure Download PDFInfo
- Publication number
- CN208382179U CN208382179U CN201820686393.XU CN201820686393U CN208382179U CN 208382179 U CN208382179 U CN 208382179U CN 201820686393 U CN201820686393 U CN 201820686393U CN 208382179 U CN208382179 U CN 208382179U
- Authority
- CN
- China
- Prior art keywords
- inner cylinder
- outer barrel
- oxidator
- chilling
- perforated plate
- 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.)
- Expired - Fee Related
Links
Landscapes
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
Abstract
The utility model discloses a kind of oxidator chilling segment structures, including outer barrel, the outer barrel upper end is equipped with cone end socket, the cone end socket upper end is welded with upper perforated plate, the upper perforated plate upper end is equipped with inner cylinder, the cone end socket and inner cylinder junction are equipped with ring top board, the inner cylinder side is equipped with the first connecting flange, and the inner cylinder other side is equipped with thermocouple head, the thermocouple head lower end is equipped with minor axis elbow, minor axis elbow one end is welded on ring top board, the inner cylinder lower end is equipped with aviation expansion joint, the inner cylinder bottom is equipped with insulation ring, the insulation ring is equipped with ignition ring, heat exchanger tube is equipped with inside the outer barrel, the heat exchanger tube lower end is equipped with lower perforated plate.The present apparatus can effectively remove the additional stress generated by temperature difference, to increase the service life of the present apparatus by the way that aviation expansion joint is arranged between outer barrel and inner cylinder.
Description
Technical field
The utility model relates to environmental technology field, specially a kind of oxidator chilling segment structure.
Background technique
Thermal oxidizer is a kind of environmental protection equipment.With heat before the waste liquid exhaust gas that various technical process generate is discharged into environment
Oxidator carries out effective destruction processing to it, to greatly reduce the discharge of waste liquid exhaust emission.To destroy waste liquid exhaust gas
Harmful components in pollutant, thermal oxidizer use " thermal oxide " principle." thermal oxide " is a kind of burning process, in thermal oxide
In technical process, under the conditions of certain temperature oxidation reaction occurs for pollutant and oxygen.The product of this chemical reaction is harmless
Substance (carbon dioxide, vapor and heat), can safely discharge.Chilling structure is the important component of oxidator, is passed
Structure is complicated for the oxidator quench zone of system, and not convenient for safeguarding and service life is low.
For this purpose, we release a kind of oxidator chilling segment structure convenient for safeguarding and with long service life.
Utility model content
The purpose of this utility model is to provide a kind of oxidator chilling segment structures, to solve to propose in above-mentioned background technique
The problem of.
To achieve the above object, the utility model provides the following technical solutions: a kind of oxidator chilling segment structure, including outer
Cylinder, the outer barrel upper end are equipped with cone end socket, and the cone end socket upper end is welded with upper perforated plate, and the upper perforated plate upper end is equipped with interior
Cylinder, the cone end socket and inner cylinder junction are equipped with ring top board, and the inner cylinder side is equipped with the first connecting flange, and inner cylinder
The body other side is equipped with thermocouple head, and the thermocouple head lower end is equipped with minor axis elbow, and minor axis elbow one end is welded on ring top
On plate, the inner cylinder lower end is equipped with aviation expansion joint, and the inner cylinder bottom is equipped with insulation ring, and the insulation ring is equipped with point
Pyrosphere, the outer barrel inside are equipped with heat exchanger tube, and the heat exchanger tube lower end is equipped with lower perforated plate, and the lower perforated plate is welded on outer barrel
On, the lower perforated plate upper end is equipped with expansion joint.
Preferably, first connecting flange one end is equipped with visor.
Preferably, gasket is equipped on the outside of the inner cylinder upper end.
Preferably, the internal diameter of the aviation expansion joint is 108mm.
Preferably, the outer barrel bottom side is equipped with lower part equipment flange, and the outer barrel bottom other side is equipped with second
Connecting flange.
Preferably, the internal diameter of the cone end socket is 2800mm, and the internal diameter of the outer barrel is 2300mm, and inner cylinder is interior
Diameter is 2400mm.
Compared with prior art, the utility model has the beneficial effects that the utility model is equal by the both ends in heat exchanger tube
It is provided with tube sheet, when it needs to safeguard, easily heat exchanger tube can be removed and safeguarded；By outer barrel and inner cylinder it
Between be arranged aviation expansion joint, the additional stress generated by temperature difference can be effectively removed, to increase the service life of the present apparatus.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model.
In figure: 1 outer barrel, 2 cone end sockets, 3 upper perforated plates, 4 inner cylinders, 5 ring top boards, 6 first connecting flanges, 7 thermocouple heads,
8 minor axis elbows, 9 aviation expansion joints, 10 insulation rings, 11 ignition rings, 12 heat exchanger tubes, 13 lower perforated plates, 14 expansion joints, 15 visors, 16
Gasket, 17 lower part equipment flanges, 18 second connecting flanges.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Referring to Fig. 1, the utility model provides a kind of oxidator quench zone structure technology scheme, including outer barrel 1, institute
It states 1 upper end of outer barrel and is equipped with cone end socket 2,2 upper end of cone end socket is welded with upper perforated plate 3, and 3 upper end of upper perforated plate is equipped with inner cylinder
Body 4, the cone end socket 2 and 4 junction of inner cylinder are equipped with ring top board 5, and 4 side of inner cylinder is equipped with the first connecting flange 6, and
4 other side of inner cylinder is equipped with thermocouple head 7, and 7 lower end of thermocouple head is equipped with minor axis elbow 8,8 one end of minor axis elbow weldering
It connects on ring top board 5,4 lower end of inner cylinder is equipped with aviation expansion joint 9, and 4 bottom of inner cylinder is equipped with insulation ring 10, described
Insulation ring 10 is equipped with ignition ring 11, and heat exchanger tube 12 is equipped with inside the outer barrel 1, and 12 lower end of heat exchanger tube is equipped with lower perforated plate
13, the lower perforated plate 13 is welded on outer barrel 1, and 13 upper end of lower perforated plate is equipped with expansion joint 14.
Specifically, 6 side of the first connecting flange is welded with visor 15, convenient for observation device inner case.
Specifically, being equipped with gasket 16 on the outside of 4 upper end of inner cylinder, play the role of protection.
Specifically, the internal diameter of the aviation expansion joint 9 is 108mm.
Specifically, 1 bottom side of outer barrel is equipped with lower part equipment flange 17, and the 1 bottom other side of outer barrel is equipped with
Second connecting flange 18.
Specifically, the internal diameter of the cone end socket 2 is 2800mm, the internal diameter of the outer barrel 1 is 2300mm, and inner cylinder 4
Internal diameter be 2400mm.
The utility model is by being provided with upper perforated plate 3 and lower perforated plate 13 at the both ends of heat exchanger tube 12, when it needs to safeguard,
Easily heat exchanger tube 12 can be removed and be safeguarded；By the way that aviation expansion joint 9 is arranged between outer barrel 1 and inner cylinder 4, can have
The additional stress that effect removal is generated by temperature difference, to increase the service life of the present apparatus.By the way that the first connecting flange is arranged
6, the second connecting flange 18 and lower part equipment flange 17 are convenient for connecting with other equipment, are expanded by being arranged on outer barrel 1
Section 14 can effectively remove the influence of the temperature difference generated by heat exchanger tube 12.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of oxidator chilling segment structure, including outer barrel (1), it is characterised in that: outer barrel (1) upper end is equipped with cone envelope
Head (2), cone end socket (2) upper end are welded with upper perforated plate (3), and upper perforated plate (3) upper end is equipped with inner cylinder (4), the cone
End socket (2) and inner cylinder (4) junction are equipped with ring top board (5), and inner cylinder (4) side is equipped with the first connecting flange (6), and
Inner cylinder (4) other side is equipped with thermocouple head (7), and thermocouple head (7) lower end is equipped with minor axis elbow (8), and the minor axis is curved
Head (8) one end is welded on ring top board (5), and inner cylinder (4) lower end is equipped with aviation expansion joint (9), inner cylinder (4) bottom
Portion is equipped with insulation ring (10), and the insulation ring (10) is equipped with ignition ring (11), and heat exchanger tube is equipped with inside the outer barrel (1)
(12), heat exchanger tube (12) lower end is equipped with lower perforated plate (13), and the lower perforated plate (13) is welded on outer barrel (1), under described
Tube sheet (13) upper end is equipped with expansion joint (14).
2. a kind of oxidator chilling segment structure according to claim 1, it is characterised in that: first connecting flange (6)
Side is welded with visor (15).
3. a kind of oxidator chilling segment structure according to claim 1, it is characterised in that: outside inner cylinder (4) upper end
Side is equipped with gasket (16).
4. a kind of oxidator chilling segment structure according to claim 1, it is characterised in that: the aviation expansion joint (9)
Internal diameter is 108mm.
5. a kind of oxidator chilling segment structure according to claim 1, it is characterised in that: outer barrel (1) bottom one
Side is equipped with lower part equipment flange (17), and outer barrel (1) the bottom other side is equipped with the second connecting flange (18).
6. a kind of oxidator chilling segment structure according to claim 1, it is characterised in that: the internal diameter of cone end socket (2)
For 2800mm, the internal diameter of the outer barrel (1) is 2300mm, and the internal diameter of inner cylinder (4) is 2400mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820686393.XU CN208382179U (en) | 2018-05-09 | 2018-05-09 | Oxidator chilling segment structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820686393.XU CN208382179U (en) | 2018-05-09 | 2018-05-09 | Oxidator chilling segment structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208382179U true CN208382179U (en) | 2019-01-15 |
Family
ID=64973896
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820686393.XU Expired - Fee Related CN208382179U (en) | 2018-05-09 | 2018-05-09 | Oxidator chilling segment structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208382179U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113267076A (en) * | 2021-06-04 | 2021-08-17 | 四川能投建工集团设计研究院有限公司 | Hydrocyanic acid oxidation reactor and tube plate cooling structure thereof |
-
2018
- 2018-05-09 CN CN201820686393.XU patent/CN208382179U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113267076A (en) * | 2021-06-04 | 2021-08-17 | 四川能投建工集团设计研究院有限公司 | Hydrocyanic acid oxidation reactor and tube plate cooling structure thereof |
| CN113267076B (en) * | 2021-06-04 | 2022-08-23 | 四川能投建工集团设计研究院有限公司 | Hydrocyanic acid oxidation reactor and tube plate cooling structure thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN208382179U (en) | Oxidator chilling segment structure | |
| CN202638252U (en) | White smoke eliminating system for solid waste incineration | |
| WO2023050702A1 (en) | Low-temperature desulfurization and denitrification method and system for flue gas from rotary kiln combustion furnace of refuse incineration power plant | |
| CN207941313U (en) | A kind of energy-saving and environment-friendly exhaust gas purification and treatment device | |
| CN103994449B (en) | A kind of compound emission-control equipment | |
| CN206709104U (en) | Emission-control equipment with waste heat recovery | |
| CN210568480U (en) | Exhaust-gas treatment recycle utilizes system | |
| CN210602844U (en) | Physical tar removing device for sintering lithium battery powder material | |
| CN210110718U (en) | Be applied to semiconductor exhaust-gas treatment equipment's waste gas reaction cavity | |
| CN209726225U (en) | A kind of catalysis fume afterheat reutilization system removing dioxin, furans, particulate | |
| CN109029048B (en) | Industrial flue gas waste heat recycling system | |
| CN206648050U (en) | A kind of incinerator | |
| CN215112624U (en) | Slag removing device of CO catalytic combustion furnace | |
| CN206175924U (en) | A sleeve type telescopic festival for high temperature exhaust pipe | |
| CN102829654A (en) | Tube plate-tube bundle assembly, tube type heat exchanger and desorption tower | |
| CN214147941U (en) | Organic waste gas environmental protection processing technology device | |
| CN109882873A (en) | A kind of direct combustion apparatus of organic exhaust gas of energy-saving anti-leak | |
| CN218485627U (en) | Environment-friendly flue gas denitration device | |
| CN212618409U (en) | Flue gas CO removing device for gas boiler | |
| CN213777755U (en) | Acid gas incinerator containing hydrogen sulfide | |
| CN207546027U (en) | A kind of noble metal flue dust recovery device | |
| CN219907479U (en) | Device for preventing dust hardening of primary dust removal system of dry quenching furnace | |
| CN213599409U (en) | Industrial waste gas treatment device capable of utilizing waste heat | |
| CN213872764U (en) | Air preheater for waste sulfuric acid cracking and regenerating device | |
| CN217613988U (en) | Hazardous waste disposal engineering tail gas treatment synergistic device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190115 Termination date: 20200509 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |