CN208937240U - Stove special pressure sensor - Google Patents
Stove special pressure sensor Download PDFInfo
- Publication number
- CN208937240U CN208937240U CN201821823884.0U CN201821823884U CN208937240U CN 208937240 U CN208937240 U CN 208937240U CN 201821823884 U CN201821823884 U CN 201821823884U CN 208937240 U CN208937240 U CN 208937240U
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- CN
- China
- Prior art keywords
- shell
- fuselage
- outside
- pressure sensor
- fixedly connected
- 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
- 238000001514 detection method Methods 0.000 claims abstract description 32
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 31
- 239000000498 cooling water Substances 0.000 claims abstract description 17
- 210000000481 breast Anatomy 0.000 claims abstract description 5
- 238000001816 cooling Methods 0.000 claims description 8
- 239000011248 coating agent Substances 0.000 claims description 5
- 238000000576 coating method Methods 0.000 claims description 5
- 229920000742 Cotton Polymers 0.000 claims description 4
- 238000009413 insulation Methods 0.000 claims description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000017525 heat dissipation Effects 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003129 oil well Substances 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
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- Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)
Abstract
Stove special pressure sensor, it is related to High-temp. kiln detection device technical field.Described includes detection bar containing sensor body, fuselage, detection bar is fixedly connected on the underface middle position of fuselage, and fuselage is located at the bosom position of shell, detection bar runs through the bottom of shell and extends to the outside of shell, water inlet is fixedly connected on the top left side of shell, water outlet is fixedly connected on the top right side of shell, cooling water pipe is wrapped in the outside of fuselage, two binding posts are separately positioned at left and right sides of fuselage roof, and two binding posts extend through the top of shell, fixed plate is fixedly connected on the bottom outside of shell, the top center position of shell is arranged in thermovent, radiator fan is provided with immediately below thermovent, its structure is simple, cooled down in real time by circulating cooling water pipe in shell and exhaust fan to sensor, good working environment is created to sensor, improve sensor detection data Accuracy.
Description
Technical field
The utility model relates to High-temp. kiln detection device technical fields, and in particular to stove special pressure sensor.
Background technique
Pressure sensor is a kind of sensor the most commonly used in industrial practice, is widely used in various industrial automatic control rings
Border, be related to water conservancy and hydropower, railway traffic, intelligent building, production automatic control, aerospace, military project, petrochemical industry, oil well, electric power, ship,
Numerous industries such as lathe, pipeline, pressure sensor (Pressure Transducer) are to experience pressure signal, and can be according to
Pressure signal is converted into the device or device of the electric signal of available output by certain rule, and pressure sensor is usually by pressure
Sensing element and signal processing unit composition.
Temperature inside stove is very high, needs to detect internal pressure in time, traditional pressure sensor is on stove
Service life it is very short, mainly due to itself heat-insulating problem of traditional pressure sensor, and traditional sensor is in hot environment
The data of lower detection are unable to ensure accuracy.
Utility model content
The purpose of this utility model is that it is in view of the drawbacks of the prior art and insufficient, a kind of stove special pressure sensing is provided
Device, its structure is simple, is cooled down in real time by circulating cooling water pipe in shell and exhaust fan to sensor, and sensor wound is given
Good working environment is made, the accuracy of sensor detection data is improved.
To achieve the above object, the utility model is using following technical scheme: it include sensor body 1, shell 2,
Water inlet 3, water outlet 4, cooling water pipe 10, fixed plate 5, binding post 6, radiator fan 7, thermovent 8, the sheet containing sensor
Body 1 includes detection bar 11, fuselage 12, and detection bar 11 is fixedly connected on the underface middle position of fuselage 12, and fuselage 12 is located at
The bosom position of shell 2, detection bar 11 run through the bottom of shell 2 and extend to the outside of shell 2, and water inlet 3 is fixed to be connected
The top left side in shell 2 is connect, water outlet 4 is fixedly connected on the top right side of shell 2, and cooling water pipe 10 is wrapped in fuselage 12
Outside, and the both ends of cooling water pipe 10 respectively correspond and connect with water inlet 3 and water outlet 4, two binding posts 6 are separately positioned on machine
The 12 top left and right sides of body, and two binding posts 6 extend through the top of shell 2, fixed plate 5 is fixedly connected on the bottom of shell 2
On the outside of portion, the top center position of shell 2 is arranged in thermovent 8, and thermovent 8 is located at the middle position of two binding posts 6, dissipates
The underface of hot mouth 8 is provided with radiator fan 7.
The outside surrounding of the fuselage 12 is provided with several cooling fins 121, is provided with heat dissipation on several cooling fins 121
Fin 1211.
The junction of the detection bar 11 and shell 2 is provided with temperature-resistant heat insulating pad 111, the outside setting of detection bar 11
High-temperaure coating 112.
The surrounding of the fixed plate 5 is evenly arranged with connecting hole 51.
The junction of the two piece-root grafting terminals 6 and shell 2 is provided with insulating protection pad 9.
The outside of the shell 2 and the inside of fixed plate 5 are provided with high temperature resistant heat insulation cotton.
Connection relationship between the radiator fan 7 and two piece-root grafting terminals 6 is to be electrically connected.
After adopting the above technical scheme, the utility model has the beneficial effect that its structure is simple, it is cold by the circulation in shell
But water pipe and exhaust fan cool down in real time to sensor, create good working environment to sensor, improve sensor detection
The accuracy of data.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only
It is some embodiments of the utility model, for those of ordinary skill in the art, before not making the creative labor property
It puts, is also possible to obtain other drawings based on these drawings.
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the schematic diagram of internal structure of the utility model；
Fig. 3 is the top view of sensor body 1 in the utility model.
Description of symbols: sensor body 1, water inlet 3, water outlet 4, cooling water pipe 10, fixed plate 5, connects shell 2
Terminal 6, radiator fan 7, thermovent 8, detection bar 11, fuselage 12, cooling fin 121, heat radiating fin 1211, temperature-resistant heat insulating pad 111,
High-temperaure coating 112, connecting hole 51, insulating protection pad 9.
Specific embodiment
Referring to shown in Fig. 1-Fig. 3, present embodiment the technical solution adopted is that: it includes sensor body 1, shell
2, water inlet 3, water outlet 4, cooling water pipe 10, fixed plate 5, binding post 6, radiator fan 7, thermovent 8, described contains sensor
Ontology 1 includes detection bar 11, fuselage 12, and detection bar 11 is fixedly connected on the underface middle position of fuselage 12, and 12, fuselage
In the bosom position of shell 2, detection bar 11 runs through the bottom of shell 2 and extends to the outside of shell 2, and water inlet 3 is fixed
It is connected to the top left side of shell 2, water outlet 4 is fixedly connected on the top right side of shell 2, and cooling water pipe 10 is wrapped in fuselage 12
Outside, and the both ends of cooling water pipe 10 respectively correspond and connect with water inlet 3 and water outlet 4, and two binding posts 6 are separately positioned on
The 12 top left and right sides of fuselage, and two binding posts 6 extend through the top of shell 2, fixed plate 5 is fixedly connected on shell 2
Bottom outside, the top center position of shell 2 is arranged in thermovent 8, and thermovent 8 is located at the middle position of two binding posts 6,
The underface of thermovent 8 is provided with radiator fan 7.
The outside surrounding of the fuselage 12 is provided with several cooling fins 121, is provided with heat dissipation on several cooling fins 121
Fin 1211.Several cooling fins 121 radiate when working for fuselage 12, and accelerate radiating efficiency by heat radiating fin 1211.
The junction of the detection bar 11 and shell 2 is provided with temperature-resistant heat insulating pad 111, the outside setting of detection bar 11
High-temperaure coating 112.Temperature-resistant heat insulating pad 111 is used to separate the contact of fuselage 12 with shell 2, and heat is avoided to be sent to fuselage 12
On, influence working efficiency；Detection bar 11 is placed in the inside of high temperature furnace, and high-temperaure coating 112 is for protecting detection bar 11.
The surrounding of the fixed plate 5 is evenly arranged with connecting hole 51.Sensor is fixedly connected on by connecting hole 51
The outside of high temperature furnace.
The junction of the two piece-root grafting terminals 6 and shell 2 is provided with insulating protection pad 9.Insulating protection pad 9 can be protected
The surface for protecting two piece-root grafting terminals 6 avoids the junction of prolonged use and shell 2 from generating abrasion, and that improves equipment uses the longevity
Life.
The outside of the shell 2 and the inside of fixed plate 5 are provided with high temperature resistant heat insulation cotton.High temperature resistant heat insulation cotton can be with
Effectively by the shield heat away of High-temp. kiln in the outside of shell 2, good working environment is provided to sensor body 1.
Connection relationship between the radiator fan 7 and two piece-root grafting terminals 6 is to be electrically connected.Radiator fan 7 and two
Connection relationship between binding post 6 is to be electrically connected, and provides electric energy to radiator fan 7 by two piece-root grafting terminals 6, will be in shell 2
The heat in portion is discharged by thermovent 8.
Working principle of the utility model is: sensor body 1 includes detection bar 11, fuselage 12, detection bar 11 is fixedly connected
In the underface middle position of fuselage 12, and fuselage 12 is located at the bosom position of shell 2, and detection bar 11 is through shell 2
Bottom and the outside for extending to shell 2, the inside that detection bar 11 enters stove are detected, and water inlet 3 is fixedly connected on shell 2
Top left side, water outlet 4 is fixedly connected on the top right side of shell 2, and cooling water pipe 10 is wrapped in the outside of fuselage 12, and cold
But the both ends of water pipe 10 are respectively corresponded connect with water inlet 3 and water outlet 4, and cooling water enters cooling water pipe 4 by water inlet 3
Inside, then be discharged by water outlet 4, it realizes that cooling water is recycled and cools down to fuselage 12, two binding posts 6 are separately positioned on the top of fuselage 12
At left and right sides of portion, the top center position of shell 2 is arranged in thermovent 8, and thermovent 8 is located at the interposition of two binding posts 6
It sets, the underface of thermovent 8 is provided with radiator fan 7, and the connection relationship between radiator fan 7 and two piece-root grafting terminals 6 is electrically
Connection, provides electric energy to radiator fan 7 by two piece-root grafting terminals 6, and the heat inside shell 2 is discharged by thermovent 8.
After adopting the above technical scheme, the utility model has the beneficial effect that its structure is simple, it is cold by the circulation in shell
But water pipe and exhaust fan cool down in real time to sensor, create good working environment to sensor, improve sensor detection
The accuracy of data.
The above is merely intended for describing the technical solutions of the present application, but not for limiting the present application, those of ordinary skill in the art couple
The other modifications or equivalent replacement that the technical solution of the utility model is made, without departing from technical solutions of the utility model
Spirit and scope should all cover in the scope of the claims of the utility model.
Claims (7)
1. stove special pressure sensor, it is characterised in that: it includes sensor body (1), shell (2), water inlet (3), goes out
The mouth of a river (4), cooling water pipe (10), fixed plate (5), binding post (6), radiator fan (7), thermovent (8), described contains sensor
Ontology (1) includes detection bar (11), fuselage (12), and detection bar (11) is fixedly connected on the underface middle position of fuselage (12),
And fuselage (12) is located at the bosom position of shell (2), detection bar (11) runs through the bottom of shell (2) and extends to shell
(2) outside, water inlet (3) are fixedly connected on the top left side of shell (2), and water outlet (4) is fixedly connected on the top of shell (2)
On the right side of portion, cooling water pipe (10) is wrapped in the outside of fuselage (12), and the both ends of cooling water pipe (10) respectively correspond and water inlet
(3) and water outlet (4) connection, two binding posts (6) are separately positioned on the left and right sides at the top of fuselage (12), and two binding posts
(6) top of shell (2) is extended through, fixed plate (5) is fixedly connected on the bottom outside of shell (2), and thermovent (8) setting exists
The top center position of shell (2), and thermovent (8) is located at the middle position of two binding posts (6), thermovent (8) just under
Side is provided with radiator fan (7).
2. stove special pressure sensor according to claim 1, it is characterised in that: the outside four of the fuselage (12)
It is provided in week several cooling fins (121), is provided with heat radiating fin (1211) on several cooling fins (121).
3. stove special pressure sensor according to claim 1, it is characterised in that: the detection bar (11) and shell
(2) junction is provided with temperature-resistant heat insulating pad (111), and high-temperaure coating (112) are arranged in the outside of detection bar (11).
4. stove special pressure sensor according to claim 1, it is characterised in that: the surrounding of the fixed plate (5)
It is evenly arranged with connecting hole (51).
5. stove special pressure sensor according to claim 1, it is characterised in that: the two piece-root grafting terminals (6) with
The junction of shell (2) is provided with insulating protection pad (9).
6. stove special pressure sensor according to claim 1, it is characterised in that: the outside of the shell (2) and
Fixed plate is provided with high temperature resistant heat insulation cotton on the inside of (5).
7. stove special pressure sensor according to claim 1, it is characterised in that: the radiator fan (7) and two
Connection relationship between piece-root grafting terminal (6) is to be electrically connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821823884.0U CN208937240U (en) | 2018-11-07 | 2018-11-07 | Stove special pressure sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821823884.0U CN208937240U (en) | 2018-11-07 | 2018-11-07 | Stove special pressure sensor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208937240U true CN208937240U (en) | 2019-06-04 |
Family
ID=66727203
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821823884.0U Expired - Fee Related CN208937240U (en) | 2018-11-07 | 2018-11-07 | Stove special pressure sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208937240U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111664967A (en) * | 2020-06-22 | 2020-09-15 | 东风商用车有限公司 | Exhaust manifold thermal stress assessment device and method |
| CN112284604A (en) * | 2020-11-05 | 2021-01-29 | 南京沃天科技有限公司 | High-temperature-resistant pressure transmitter |
-
2018
- 2018-11-07 CN CN201821823884.0U patent/CN208937240U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111664967A (en) * | 2020-06-22 | 2020-09-15 | 东风商用车有限公司 | Exhaust manifold thermal stress assessment device and method |
| CN111664967B (en) * | 2020-06-22 | 2021-05-11 | 东风商用车有限公司 | Exhaust manifold thermal stress assessment device and method |
| CN112284604A (en) * | 2020-11-05 | 2021-01-29 | 南京沃天科技有限公司 | High-temperature-resistant pressure transmitter |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190604 |