CN214481742U - Novel mounting structure of aviation plug - Google Patents
Novel mounting structure of aviation plug Download PDFInfo
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- CN214481742U CN214481742U CN202120627366.7U CN202120627366U CN214481742U CN 214481742 U CN214481742 U CN 214481742U CN 202120627366 U CN202120627366 U CN 202120627366U CN 214481742 U CN214481742 U CN 214481742U
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- circuit board
- aviation plug
- installation shell
- aviation
- mounting structure
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Abstract
The utility model relates to an aviation plug technical field discloses a novel mounting structure of aviation plug, including the installation shell, a plurality of perforation have evenly been seted up at the interval on one side of installation shell, pass the perforation and be equipped with aviation plug, aviation plug is in the fixed first circuit board that is equipped with of one side in the installation shell, first circuit board is connected with the second circuit board through the winding displacement, four angle departments of second circuit board are equipped with the fixed orifices, and the second circuit board passes through the fixed orifices to be established on the bottom surface of installation shell, be equipped with the RS485 interface on the installation shell with set up the perforation adjacent one side, the RS485 interface with the second circuit board is connected, aviation plug is equipped with fastening bolt in the outside of installation shell. The mounting shell is provided with a cover plate on the side opposite to the side provided with the through hole in a rotating way. The utility model provides a problem of a plurality of aviation plugs in constrictive space be not convenient for install, very big improvement the efficiency and the convenience of installation, standardized the mode of connection, the practicality is strong.
Description
Technical Field
The utility model relates to an aviation plug technical field especially relates to a novel mounting structure of aviation plug.
Background
When traditional equipment used a plurality of aviation plugs, generally all can be because the space is narrow and small, it is inconvenient to cause a plurality of aviation plug installation to exist the operation, the not high problem of installation effectiveness, traditional equipment fixing shell all need be in the inside and outside of installation shell when installing aviation plug, install the bolt on the aviation plug, when a plurality of aviation plugs are installed side by side, because the inboard space of installation shell is narrow and small, be not convenient for carry out the installation of screwing of inboard bolt, make the installation effectiveness extremely low, and traditional still is connected with inside circuit board through the winding displacement through every aviation plug, cause the crisscross redundancy of a plurality of winding displacements easily, so just need a neotype aviation plug's mounting structure.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model aims at providing a novel mounting structure of aviation plug, the utility model discloses a to the outside aviation plug of installation shell carry on the single face fastening bolt screw can, the installation shell inboard collects the data of a plurality of aviation plug inputs through first circuit board, then carries out unified transmission to the second circuit board through the winding displacement and carries out data processing, then connects other equipment through the RS485 interface. The utility model provides a problem of a plurality of aviation plugs in constrictive space be not convenient for install, very big improvement the efficiency and the convenience of installation, standardized the mode of connection, the practicality is strong.
The utility model discloses an above-mentioned technical problem is solved to following technical means:
the utility model discloses a novel mounting structure of aviation plug includes the installation shell, a plurality of perforation have evenly been seted up at the interval on one side of installation shell, pass the perforation is equipped with the aviation plug, the aviation plug is in the fixed first circuit board that is equipped with of one side in the installation shell, first circuit board is connected with the second circuit board through the winding displacement, four angle departments of second circuit board are equipped with the fixed orifices, the second circuit board passes through the fixed orifices to be established on the bottom surface of installation shell, be equipped with the RS485 interface on the installation shell with set up perforation adjacent one side, the RS485 interface with the second circuit board is connected, the aviation plug is equipped with fastening bolt in the outside of installation shell.
Further, the installation shell is provided with a cover plate on the opposite side of the perforation.
Further, the number of the RS485 interfaces is 2.
Furthermore, the number of the through holes and the number of the aviation plugs are 11.
Furthermore, the first circuit board is used for collecting the pins of the plurality of aviation plugs on the first circuit board, and the second circuit board is used for processing data transmission of the plurality of aviation plugs.
The utility model has the advantages that: through carrying out the fastening bolt of single face to the outside aviation plug of installation shell and tighten can, the installation shell inboard collects the data of a plurality of aviation plug inputs through first circuit board, then carries out unified transmission to the second circuit board through the winding displacement and carries out data processing, then connects other equipment through the RS485 interface. The utility model provides a problem of a plurality of aviation plugs in constrictive space be not convenient for install, very big improvement the efficiency and the convenience of installation, standardized the mode of connection, the practicality is strong.
Drawings
Fig. 1 is a schematic structural diagram of an information acquisition device of the present invention;
fig. 2 is a circuit diagram of the aviation plug data collection processing circuit on the first circuit board of the present invention;
fig. 3 is a circuit diagram of the connection pins of different types of aviation plugs of the present invention;
the mounting shell comprises a mounting shell 1, an RS485 interface 10, a fastening bolt 2, an aviation plug 3, a first circuit board 4, a flat cable 5, a second circuit board 6, a fixing hole 61 and a cover plate 7.
Detailed Description
The invention will be described in detail with reference to the following drawings and specific embodiments:
as shown in fig. 1-3, the utility model discloses a novel mounting structure of aviation plug includes the installation shell, a plurality of perforation have evenly been seted up at the interval on one side of installation shell, pass the perforation is equipped with aviation plug, aviation plug is in the fixed first circuit board that is equipped with in one side in the installation shell, first circuit board is connected with the second circuit board through the winding displacement, four angle departments of second circuit board are equipped with the fixed orifices, the second circuit board passes through the fixed orifices to be established on the bottom surface of installation shell, be equipped with the RS485 interface on the installation shell with set up the perforation adjacent one side, the RS485 interface with the second circuit board is connected, aviation plug is equipped with fastening bolt in the outside of installation shell.
In this embodiment, the mounting case is rotatably provided with a cover plate on the side opposite to the side provided with the through hole.
In this embodiment, the number of the RS485 interfaces is 2. The number of the through holes and the number of the aviation plugs are 11.
In this embodiment, the first circuit board is configured to collect pins of a plurality of aviation plugs on the first circuit board, and the second circuit board is configured to process data transmission of the plurality of aviation plugs.
Although the present invention has been described in detail with reference to the preferred embodiments, those skilled in the art will understand that the present invention can be modified or replaced with other embodiments without departing from the spirit and scope of the present invention, which should be construed as limited only by the appended claims. The technology, shape and construction parts which are not described in detail in the present invention are all known technology.
Claims (4)
1. The utility model provides a novel mounting structure of aviation plug which characterized in that: including installation shell (1), a plurality of perforation have evenly been seted up at the interval on one side of installation shell (1), pass the perforation is equipped with aviation plug (3), aviation plug (3) one side in installation shell (1) is fixed and is equipped with first circuit board (4), first circuit board (4) are connected with second circuit board (6) through the winding displacement, four angles departments of second circuit board (6) are equipped with fixed orifices (61), establish through fixed orifices (61) second circuit board (6) on the bottom surface of installation shell (1), aviation plug (3) are equipped with fastening bolt (2) in the outside of installation shell (1).
2. The novel aviation plug mounting structure of claim 1, wherein: the mounting shell (1) is rotatably provided with a cover plate (7) on the side opposite to the side provided with the through hole.
3. The novel aviation plug mounting structure of claim 1, wherein: the installation shell (1) is provided with an RS485 interface (10) on one side adjacent to the opened hole, the RS485 interface (10) is connected with the second circuit board (6), and the number of the RS485 interfaces (10) is 2.
4. The novel aviation plug mounting structure of claim 1, wherein: the number of the through holes and the number of the aviation plugs (3) are 11.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120627366.7U CN214481742U (en) | 2021-03-29 | 2021-03-29 | Novel mounting structure of aviation plug |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120627366.7U CN214481742U (en) | 2021-03-29 | 2021-03-29 | Novel mounting structure of aviation plug |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214481742U true CN214481742U (en) | 2021-10-22 |
Family
ID=78175436
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120627366.7U Active CN214481742U (en) | 2021-03-29 | 2021-03-29 | Novel mounting structure of aviation plug |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214481742U (en) |
-
2021
- 2021-03-29 CN CN202120627366.7U patent/CN214481742U/en active Active
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