CN219393868U - Quick installation component of aviation plug - Google Patents
Quick installation component of aviation plug Download PDFInfo
- Publication number
- CN219393868U CN219393868U CN202223296348.9U CN202223296348U CN219393868U CN 219393868 U CN219393868 U CN 219393868U CN 202223296348 U CN202223296348 U CN 202223296348U CN 219393868 U CN219393868 U CN 219393868U
- Authority
- CN
- China
- Prior art keywords
- aviation plug
- bolt
- sensor housing
- plug
- mounting
- 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.)
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Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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- Connection Of Plates (AREA)
Abstract
The utility model relates to a quick installation component of an aviation plug, which comprises a sensor shell, the aviation plug arranged on the sensor shell and a fixing bolt for connecting the aviation plug with the sensor shell, wherein bolt installation holes are formed in the sensor shell and the aviation plug, and a quick installation piece for quickly installing the aviation plug on the sensor shell is arranged on the sensor shell.
Description
Technical Field
The utility model belongs to the technical field of sensor shell installation, and relates to an aviation plug quick installation assembly.
Background
The current sensor is a kind of detecting device, which can sense the information of the detected current and convert the information sensed by detection into electric signals meeting the requirement of certain standard or other information output in the required form according to certain rules, so as to meet the requirements of information transmission, processing, storage, display, recording, control and the like.
Some of the current sensors are usually applied to marine transportation, in order to reduce marine delay, aviation plugs are usually required to be installed on a shell, bolts and nuts are required to be fixed for installing the aviation plugs, because the nuts are installed on the inner side of the shell, workers need to stretch hands into the shell and rotate the nuts to fix the bolts when installing the nuts, and because the inner space of the shell is smaller, the hands cannot stretch, so that the installation speed is low, the cost is long, and the efficiency is low.
Disclosure of Invention
The utility model aims to solve the problems in the prior art and provides an aviation plug quick installation component.
The aim of the utility model can be achieved by the following technical scheme: the utility model provides an aviation plug installs subassembly fast, includes the sensor housing, sets up aviation plug on the sensor housing and is used for connecting aviation plug and sensor housing's fixing bolt, sensor housing and aviation plug on all be provided with the bolt mounting hole, the sensor housing on be provided with install the quick installed part on the sensor housing fast with aviation plug, quick installed part including setting up at sensor housing inner chamber bottom mounting panel, the mounting panel on set up and be used for holding nut and avoid nut pivoted standing groove, one side of mounting panel be provided with the side that is used for pressing from both sides tight sensor housing, the position of standing groove and the bolt mounting hole setting in line on the aviation plug, after fixing bolt passes the bolt mounting hole, can accomplish the connection of fixing bolt and nut through rotating fixing bolt.
In the quick installation component of aviation plug, the through hole for the fixing bolt to pass through is also formed in the placing groove.
In the quick installation component of aviation plug, the mounting plate is provided with the accommodating hole.
In the quick installation component of aviation plug, the sensor shell is provided with the plug installation hole for installing the aviation plug.
In the quick installation component of the aviation plug, the side edge isIn a special formA clamping groove is formed between the side edge and the mounting plate, and the clamping groove is matched with the side edge thickness of the sensor shell.
Compared with the prior art, the mounting plate, the placing groove and the through hole are arranged, the nut is placed in the placing groove when an installer installs the mounting plate, then the mounting plate is clamped on the sensor shell, the inner wall of the sensor shell is attached to the mounting plate, the nut, the sensor shell and the bolt mounting block on the aviation plug are aligned, then the fixing bolt is placed in the inserting bolt mounting hole, the fixing bolt is rotated, and the fixing bolt is rotated into the nut, so that the installation of the aviation plug is realized.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
FIG. 2 is a schematic view of the quick mount construction of the present utility model;
FIG. 3 is an assembly view of an aerial plug and sensor housing of the present utility model.
In the figure, 1, a sensor housing; 2. aviation plug; 3. a fixing bolt; 4. a bolt mounting hole; 5. a quick mount; 51. a mounting plate; 52. a placement groove; 53. a side edge; 6. a through hole; 7. a receiving hole; 8. a plug mounting hole; 9. and (3) a nut.
Detailed Description
The following are specific embodiments of the present utility model and the technical solutions of the present utility model will be further described with reference to the accompanying drawings, but the present utility model is not limited to these embodiments.
Examples
As shown in fig. 1 to 3, an aviation plug quick installation assembly comprises a sensor housing 1, an aviation plug 2 arranged on the sensor housing 1, and a fixing bolt 3 for connecting the aviation plug 2 with the sensor housing 1, wherein bolt installation holes 4 are formed in the sensor housing 1 and the aviation plug 2.
The sensor housing 1 on be provided with install the quick installed part 5 on the sensor housing 1 with aviation plug 2 fast, quick installed part 5 including setting up at sensor housing 1 inner chamber bottom mounting panel 51, mounting panel 51 on set up and be used for holding nut 9 and avoid nut 9 pivoted standing groove 52, standing groove 52 sets to triangle-shaped, quadrangle or polygon and non-circular, can place the bolt and drive nut 9 and rotate when rotating, standing groove 52 can play spacing effect to nut 9, improves the installation of bolt and nut 9.
The placing groove 52 is also internally provided with a through hole 6 for the fixing bolt 3 to pass through.
One side of the mounting plate 51 is provided with a side 53 for clamping the sensor housing 1, the side 53 is in the form ofAnd a clamping groove is formed between the side edge 53 and the mounting plate 51, and the clamping groove is matched with the thickness of the side edge 53 of the sensor shell 1. The whole mounting piece can be clamped on the sensor housing 1 by the side edges 53, the falling of the mounting plate 51 can be avoided, and the mounting can be completed without the need of holding the mounting plate 51 by hands of a installer during the mounting.
The position of the placing groove 52 is in line with the bolt mounting hole 4 on the aviation plug 2, and after the fixing bolt 3 passes through the bolt mounting hole 4, the connection between the fixing bolt 3 and the nut 9 can be completed by rotating the fixing bolt 3.
The mounting plate 51 is provided with a receiving hole 7. One side of the accommodating hole 7 horizontally penetrates through the mounting plate 51, so that the aviation plug 2 is convenient to detach from the mounting plate 51 after being mounted.
The sensor housing 1 is provided with a plug mounting hole 8 for mounting the aviation plug 2.
According to the utility model, the mounting plate 51, the placing groove 52 and the through hole 6 are arranged, when an installer installs, the nut 9 is placed in the placing groove 52 firstly, then the mounting plate 51 is clamped on the sensor shell 1, the inner wall of the sensor shell 1 is attached to the mounting plate 51, the nut 9 and the sensor shell 1 are aligned with the bolt mounting blocks on the aviation socket, then the fixing bolt 3 is placed in the inserting bolt mounting hole 4, the fixing bolt 3 is rotated, and the fixing bolt 3 is rotated into the nut 9, so that the installation of the aviation socket is realized.
The specific embodiments described herein are offered by way of example only to illustrate the spirit of the utility model. Those skilled in the art may make various modifications or additions to the described embodiments or substitutions thereof without departing from the spirit of the utility model or exceeding the scope of the utility model as defined in the accompanying claims.
Claims (4)
1. The utility model provides an aviation plug installs subassembly fast, its characterized in that, including sensor housing (1), aviation plug (2) and be used for connecting aviation plug (2) and fixing bolt (3) of sensor housing (1) on sensor housing (1), sensor housing (1) all be provided with bolt mounting hole (4) with aviation plug (2) on, sensor housing (1) on be provided with install fast mounting piece (5) on sensor housing (1) with aviation plug (2) fast, fast mounting piece (5) including setting up at sensor housing (1) inner chamber bottom mounting plate (51), mounting plate (51) on set up and be used for holding nut (9) and avoid nut (9) pivoted standing groove (52), one side of mounting plate (51) be provided with side (53) that are used for pressing from both sides sensor housing (1), the position of standing groove (52) and bolt mounting hole (4) on aviation plug (2) set up in line, quick mounting piece (5) including setting up and pass bolt (3) after fixing hole (3) pass through bolt (3) and accomplish bolt (3) and bolt (3) rotation, can be fixed with bolt (3) rotation fixing bolt (3)And a clamping groove is formed between the side edge (53) and the mounting plate (51), and the clamping groove is matched with the thickness of the side edge (53) of the sensor shell (1).
2. An aircraft plug quick install assembly according to claim 1, wherein: the placing groove (52) is also internally provided with a through hole (6) through which the fixing bolt (3) can pass.
3. An aircraft plug quick install assembly according to claim 1, wherein: the mounting plate (51) is provided with a containing hole (7).
4. An aircraft plug quick install assembly according to claim 1, wherein: the sensor shell (1) is provided with a plug mounting hole (8) for mounting the aviation plug (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223296348.9U CN219393868U (en) | 2022-12-08 | 2022-12-08 | Quick installation component of aviation plug |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223296348.9U CN219393868U (en) | 2022-12-08 | 2022-12-08 | Quick installation component of aviation plug |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219393868U true CN219393868U (en) | 2023-07-21 |
Family
ID=87188250
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223296348.9U Active CN219393868U (en) | 2022-12-08 | 2022-12-08 | Quick installation component of aviation plug |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219393868U (en) |
-
2022
- 2022-12-08 CN CN202223296348.9U patent/CN219393868U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |