CN219064708U - Gas temperature sensor for aerospace - Google Patents
Gas temperature sensor for aerospace Download PDFInfo
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- CN219064708U CN219064708U CN202320140538.7U CN202320140538U CN219064708U CN 219064708 U CN219064708 U CN 219064708U CN 202320140538 U CN202320140538 U CN 202320140538U CN 219064708 U CN219064708 U CN 219064708U
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- gas temperature
- temperature sensor
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- connecting plate
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Abstract
The utility model relates to the technical field of sensors, in particular to a gas temperature sensor for aerospace, which comprises a sensor body and a mounting shell coated on the outer surface of the sensor body, wherein a mounting annular plate is arranged on the surface of the mounting shell in a ring manner, and one end of the mounting annular plate is provided with a first connecting plate used for being connected with a vertical surface and a second connecting plate used for being connected with a horizontal surface. The utility model enables the gas temperature sensor to be installed on various planes by arranging the first connecting plate and the second connecting plate instead of being limited to one installation environment, and in addition, the positions of the first connecting plate and the second connecting plate can be adjusted by installing the plurality of sliding grooves on the surface of the shell, so that the gas temperature sensor is applicable to various installation environments.
Description
Technical Field
The utility model relates to the technical field of sensors, in particular to a gas temperature sensor for aerospace.
Background
The gas temperature sensor can convert the temperature of gas into an available output signal so as to monitor the gas safety condition of equipment, and is widely applied to the field of aerospace. At present, when the gas temperature sensor is installed, most of the gas temperature sensor is installed only by the installation plate at the side edge of the gas temperature sensor, and the installation mode is limited by the installation environment and cannot be suitable for various different installation environments.
Therefore, designing a gas temperature sensor for aerospace is a technical problem to be solved urgently by those skilled in the art.
Disclosure of Invention
The utility model aims to solve the technical problem of overcoming the defects in the prior art and providing a gas temperature sensor for aerospace.
The utility model is realized by the following technical scheme: the utility model provides an aerospace is with gas temperature sensor, includes sensor body and cladding at the installation shell of sensor body surface, and the surface ring of installation shell is equipped with the installation annular plate, and the one end of installation annular plate is equipped with and is used for the first connecting plate that links to each other with vertical face and is used for the second connecting plate that links to each other with the horizontal plane.
According to the technical scheme, preferably, the inner surface of the installation ring plate is fixedly provided with the sliding blocks, the surface of the installation shell is provided with the sliding grooves arranged along the edge of the installation shell, the installation ring plate slides in the sliding grooves through the sliding blocks, and the sliding grooves are communicated through the communication grooves, so that the installation ring plate moves among different sliding grooves.
According to the above technical scheme, preferably, the first connecting plate and the second connecting plate are both detachably connected with the mounting ring plate.
According to the above technical scheme, preferably, the first connecting plate is a vertical connecting plate, the second connecting plate comprises a connecting part connected with the mounting ring plate and a fixing part used for being connected with a horizontal plane, and the connecting part and the fixing part are integrally formed.
According to the above technical scheme, preferably, the vertical connecting plate and the fixing part are provided with fixing holes.
According to the above technical scheme, preferably, a gap is formed between the central axis of the fixing hole on the vertical connecting plate and the mounting ring plate.
According to the above technical scheme, preferably, the top of the sensor body is provided with a junction box, and the bottom is provided with a detection rod.
The beneficial effects of the utility model are as follows: the utility model enables the gas temperature sensor to be installed on various planes by arranging the first connecting plate and the second connecting plate instead of being limited to one installation environment, and in addition, the positions of the first connecting plate and the second connecting plate can be adjusted by installing the plurality of sliding grooves on the surface of the shell, so that the gas temperature sensor is applicable to various installation environments.
Drawings
Fig. 1 shows a schematic structural view of embodiment 1 of the present utility model;
fig. 2 shows a schematic structural diagram of embodiment 2 of the present utility model.
In the figure: 1. a sensor body; 2. mounting a shell; 3. installing a ring plate; 4. a first connection plate; 5. a second connecting plate; 6. a connection part; 7. a fixing part; 8. a fixing hole; 9. a junction box; 10. a detection rod; 11. a slide block; 12. a chute; 13. and a communication groove.
Detailed Description
The present utility model will be described in further detail below with reference to the drawings and preferred embodiments, so that those skilled in the art can better understand the technical solutions of the present utility model.
Example 1
As shown in fig. 1, the utility model provides a gas temperature sensor for aerospace, which comprises a sensor body 1 and a mounting shell 2 coated on the outer surface of the sensor body 1, wherein a mounting annular plate 3 is arranged on the surface of the mounting shell 2 in a ring manner, and one end of the mounting annular plate 3 is provided with a first connecting plate 4 used for being connected with a vertical surface and a second connecting plate 5 used for being connected with a horizontal surface.
The staff selects to use first connecting plate or second connecting plate to fix gas temperature sensor according to the installation environment at that time, when the installation face is the vertical face, then use first connecting plate to fix gas temperature sensor, when the installation face is the horizontal plane, then use the second connecting plate to fix gas temperature sensor.
According to the above embodiment, preferably, the first connecting plate 4 and the second connecting plate 5 are detachably connected with the mounting ring plate 3, so that the first connecting plate and the second connecting plate can be conveniently replaced by a worker, and when the common working environment is changed, the first connecting plate and the second connecting plate with different sizes can be replaced by the worker, so that the working environment is more suitable for the current working environment.
According to the above embodiment, preferably, the first connection plate 4 is a vertical connection plate, and the second connection plate 5 includes a connection portion 6 connected to the mounting ring plate 3 and a fixing portion 7 for connection to a horizontal plane, and the connection portion 6 is integrally formed with the fixing portion 7. The vertical connecting plate is simple in structure, and the effect of being parallel to the vertical surface can be easily achieved, so that the gas temperature sensor can be more conveniently fixed by a worker; the fixing part and the connecting part form an L-shaped plate, so that a sufficient working space is reserved for a worker when the gas temperature sensor is connected with a horizontal plane, and the worker can conveniently construct.
According to the above embodiment, it is preferable that the vertical connection plate and the fixing portion 7 are provided with the fixing hole 8. The staff uses fixing bolts to pass through the fixing holes to finish the installation and the fixation of the gas temperature sensor.
According to the above embodiment, it is preferable that there is a gap between the central axis of the fixing hole 8 on the vertical connection plate and the mounting ring plate 3. When preventing that the staff from fixing gas temperature sensor on vertical face, the installation deflector prevents that the staff from tightening fixing bolt.
According to the above embodiment, the sensor body 1 is preferably provided with a junction box 9 at the top and a detection rod 10 at the bottom.
Example 2
On the basis of embodiment 1, as shown in fig. 2, preferably, the inner surface of the installation ring plate 3 is fixedly provided with a sliding block 11, the surface of the installation shell 2 is provided with a plurality of sliding grooves 12 arranged along the edge of the installation shell 2, the installation ring plate 3 slides in the sliding grooves 12 through the sliding block 11, and the sliding grooves 12 are communicated through a communication groove 13, so that the installation ring plate 3 moves between different sliding grooves 12.
When the position of the installation annular plate relative to the gas temperature sensor needs to be adjusted, the installation annular plate is rotated to drive the sliding block to move to the intersection of the sliding groove and the communication groove, the installation annular plate is moved upwards or downwards according to the needs, the sliding block is moved to the intersection of other sliding grooves and the communication groove, the installation annular plate is rotated again, the sliding block is moved to the sliding groove, and the adjustment of the position of the installation annular plate can be completed.
The beneficial effects of the utility model are as follows: the utility model enables the gas temperature sensor to be installed on various planes by arranging the first connecting plate and the second connecting plate instead of being limited to one installation environment, and in addition, the positions of the first connecting plate and the second connecting plate can be adjusted by installing the plurality of sliding grooves on the surface of the shell, so that the gas temperature sensor is applicable to various installation environments.
The foregoing is merely a preferred embodiment of the present utility model and it should be noted that modifications and adaptations to those skilled in the art may be made without departing from the principles of the present utility model, which are intended to be comprehended within the scope of the present utility model.
Claims (7)
1. The utility model provides an aerospace gas temperature sensor, its characterized in that includes sensor body and cladding at the installation shell of sensor body surface, the surface ring of installation shell is equipped with the installation annular plate, the one end of installation annular plate is equipped with and is used for the first connecting plate that links to each other with the vertical face and is used for the second connecting plate that links to each other with the horizontal plane.
2. The gas temperature sensor for aerospace according to claim 1, wherein the inner surface of the mounting ring plate is fixedly provided with a sliding block, the surface of the mounting shell is provided with a plurality of sliding grooves arranged along the edge of the mounting shell, the mounting ring plate slides in the sliding grooves through the sliding block, and the sliding grooves are communicated through the communicating grooves, so that the mounting ring plate moves among different sliding grooves.
3. The aerospace gas temperature sensor of claim 1, wherein the first and second connection plates are removably connected to the mounting ring plate.
4. The aerospace gas temperature sensor of claim 1, wherein the first connection plate is a vertical connection plate, the second connection plate comprises a connection portion connected to the mounting ring plate and a fixing portion for connection to a horizontal plane, and the connection portion and the fixing portion are integrally formed.
5. The aerospace gas temperature sensor of claim 4, wherein the vertical connection plate and the fixing portion are provided with fixing holes.
6. The aerospace gas temperature sensor of claim 4, wherein a gap is provided between a central axis of the fixing hole in the vertical connection plate and the mounting ring plate.
7. The aerospace gas temperature sensor of claim 1, wherein the sensor body has a junction box at the top and a probe at the bottom.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320140538.7U CN219064708U (en) | 2023-02-07 | 2023-02-07 | Gas temperature sensor for aerospace |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320140538.7U CN219064708U (en) | 2023-02-07 | 2023-02-07 | Gas temperature sensor for aerospace |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219064708U true CN219064708U (en) | 2023-05-23 |
Family
ID=86375484
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320140538.7U Active CN219064708U (en) | 2023-02-07 | 2023-02-07 | Gas temperature sensor for aerospace |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219064708U (en) |
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2023
- 2023-02-07 CN CN202320140538.7U patent/CN219064708U/en active Active
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