CN203011587U - Aviation plug output type pressure sensor - Google Patents
Aviation plug output type pressure sensor Download PDFInfo
- Publication number
- CN203011587U CN203011587U CN 201220719884 CN201220719884U CN203011587U CN 203011587 U CN203011587 U CN 203011587U CN 201220719884 CN201220719884 CN 201220719884 CN 201220719884 U CN201220719884 U CN 201220719884U CN 203011587 U CN203011587 U CN 203011587U
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- CN
- China
- Prior art keywords
- output type
- type pressure
- sensor
- aviation plug
- pressure sensor
- 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
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Abstract
The utility model relates to an aviation plug output type pressure sensor. A current output type pressure sensitive part (2) is installed inside a sensor shell (1). A front end of the sensor shell (1) is a thread interface (3). A rear end of the sensor shell (1) is an aviation plug (4). By the use of a stainless steel metal shell, corrosion resistance and electromagnetic shielding capability of the sensor are enhanced; and by the adoption of the current output type pressure sensitive part, the sensor is endowed with strong antijamming capability and temperature adaptability.
Description
Affiliated technical field
The utility model relates to a kind of sensor, especially a kind of aviation plug output type pressure transducer.
Background technology
At present, pressure transducer is widely used in the fields such as oil, chemical industry, metallurgy, electric power, aviation, but there are the shortcomings such as poor anti jamming capability, the serviceability temperature scope is little, withstand voltage is low mostly in existing pressure transducer.
Summary of the invention
In order to overcome existing pressure transducer poor anti jamming capability, the serviceability temperature scope is little, withstand voltage is low deficiency, the utility model provides a kind of aviation plug output type pressure transducer, this sensor adopts the stainless steel metal shell, the anticorrosive of sensor and electromagnetic screen ability have been strengthened, adopt simultaneously the current-output type pressure-sensitive component, make sensor have very strong antijamming capability and temperature adaptive faculty.
The technical scheme that its technical matters that solves the utility model adopts is: a kind of aviation plug output type pressure transducer is equipped with current-output type pressure-sensitive component (2) in the inside of sensor outer housing (1).Leading section at sensor outer housing (1) is hickey (3).Rearward end at sensor outer housing (1) is aviation plug (4).In use, on this installation of sensors Devices to test, and aviation plug (4) is connected with checkout equipment, so just can have realized the measurement of pressure.
The beneficial effects of the utility model are, utilize the stainless steel metal shell, have strengthened the anticorrosive of sensor and electromagnetic screen ability, adopt simultaneously the current-output type pressure-sensitive component, make sensor have very strong antijamming capability and temperature adaptive faculty.
Description of drawings
Below in conjunction with drawings and Examples, the utility model is further illustrated.
Fig. 1 is the utility model outside drawing.
1. sensor outer housings in figure, 2. current-output type pressure-sensitive component, 3. hickey, 4. aviation plug.
Embodiment
In Fig. 1, a kind of aviation plug output type pressure transducer is equipped with current-output type pressure-sensitive component (2) in the inside of sensor outer housing (1).Leading section at sensor outer housing (1) is hickey (3).Rearward end at sensor outer housing (1) is aviation plug (4).In use, on this installation of sensors Devices to test, and aviation plug (4) is connected with checkout equipment, so just can have realized the measurement of pressure.
Claims (1)
1. an aviation plug output type pressure transducer, is characterized in that: in the inside of sensor outer housing (1), current-output type pressure-sensitive component (2) is installed; Leading section at sensor outer housing (1) is hickey (3); Rearward end at sensor outer housing (1) is aviation plug (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220719884 CN203011587U (en) | 2012-12-23 | 2012-12-23 | Aviation plug output type pressure sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220719884 CN203011587U (en) | 2012-12-23 | 2012-12-23 | Aviation plug output type pressure sensor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203011587U true CN203011587U (en) | 2013-06-19 |
Family
ID=48603170
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220719884 Expired - Fee Related CN203011587U (en) | 2012-12-23 | 2012-12-23 | Aviation plug output type pressure sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203011587U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104931162A (en) * | 2015-06-30 | 2015-09-23 | 安徽智敏电气技术有限公司 | Piezoelectric sensor |
| CN106918848A (en) * | 2015-12-24 | 2017-07-04 | 华云升达(北京)气象科技有限责任公司 | A kind of hail sensor |
-
2012
- 2012-12-23 CN CN 201220719884 patent/CN203011587U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104931162A (en) * | 2015-06-30 | 2015-09-23 | 安徽智敏电气技术有限公司 | Piezoelectric sensor |
| CN106918848A (en) * | 2015-12-24 | 2017-07-04 | 华云升达(北京)气象科技有限责任公司 | A kind of hail sensor |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130619 Termination date: 20171223 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |