CN204087250U - Aeronautical maintenance bar code block - Google Patents
Aeronautical maintenance bar code block Download PDFInfo
- Publication number
- CN204087250U CN204087250U CN201420538529.4U CN201420538529U CN204087250U CN 204087250 U CN204087250 U CN 204087250U CN 201420538529 U CN201420538529 U CN 201420538529U CN 204087250 U CN204087250 U CN 204087250U
- Authority
- CN
- China
- Prior art keywords
- upper shell
- bar code
- lower house
- fore
- code block
- 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
Abstract
The utility model belongs to a kind of scanister, simple in particular to a kind of structure, non-damageable aeronautical maintenance bar code block, comprise block, block is made up of upper shell and lower house, it is characterized in that: described upper shell and the upper and lower surface of lower house are all in square, position near four limits on the lower surface of upper shell is provided with projection, position near four limits on the upper surface of lower house is provided with groove, the outer wall of upper shell and lower house is two-layer, be respectively the vacuum layer of outer field anticorrosive coat and internal layer, the center of lower house upper surface is provided with four fore-sets, induction chip is provided with above fore-set, upper shell lower surface center is also provided with four fore-sets, the utility model structure is simple, practical, solve bar code to be easily torn when aviation apparatus keeps in repair, the problem of corrosion, make maintenance process more smooth, also work efficiency is greatly improved.
Description
Technical field
The utility model belongs to a kind of scanister, particularly a kind of structure simple, non-damageable aeronautical maintenance bar code block.
Background technology
At present, bar code on traditional aviation machine mostly is paper material, paper material is also easily torn, and causes the problem that cannot scan, in addition, when keeping in repair aviation apparatus, aviation apparatus can be in different environment, sour environment and alkaline environment, and in maintenance process, the bar code of papery is easily corroded, have impact on carrying out smoothly of maintenance procedures, directly cause work efficiency greatly to reduce.
Summary of the invention
The purpose of this utility model is to overcome the deficiencies in the prior art, and provides a kind of structure simple, non-damageable aeronautical maintenance bar code block.
The purpose of this utility model is achieved in that a kind of aeronautical maintenance bar code block, comprise block, block is made up of upper shell and lower house, it is characterized in that: described upper shell and the upper and lower surface of lower house are all in square, position near four limits on the lower surface of upper shell is provided with projection, position near four limits on the upper surface of lower house is provided with groove, the outer wall of upper shell and lower house is two-layer, be respectively the vacuum layer of outer field anticorrosive coat and internal layer, the center of lower house upper surface is provided with four fore-sets, induction chip is provided with above fore-set, upper shell lower surface center is also provided with four fore-sets.
The line of four fore-sets of described upper shell is square, and on lower house, the line of four fore-sets is also square.
Two diagonal angles in described block corner are respectively arranged with two through holes.
Described fore-set is right cylinder, and its disc is provided with block rubber.
The length of described fore-set is identical with the equal degree of depth of upper shell and lower house.
The upper surface of described upper shell is provided with bar code line.
Described anticorrosive coat scribbles anticorrosive paint.
The beneficial effects of the utility model: the utility model structure is simple, practical, solve the problem that bar code is easily torn when aviation apparatus keeps in repair, corrodes, make maintenance process more smooth, also greatly improve work efficiency.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the structural representation of lower house.
Fig. 3 is the cut-open view of block outer wall.
Fig. 4 is the schematic diagram that projection and groove combine.
Embodiment
Below in conjunction with accompanying drawing, the utility model is described further.
Embodiment 1
As shown in Fig. 1 figure, a kind of aeronautical maintenance bar code block, comprise block, block is made up of upper shell 1 and lower house 2, the upper and lower surface of upper shell 1 and lower house 2 is all in square, position near four limits on the lower surface of upper shell 1 is provided with projection 3, position near four limits on the upper surface of lower house 2 is provided with groove 4, upper shell 1 is two-layer with the outer wall of lower house 2, be respectively the vacuum layer 9 of outer field anticorrosive coat 8 and internal layer, the center of lower house 2 upper surface is provided with four fore-sets 5, induction chip 6 is provided with above fore-set 5, upper shell 1 lower surface center is also provided with four fore-sets 5.
The line of four fore-sets 5 of described upper shell 1 is square, and on lower house 2, the line of four fore-sets 5 is also square.
Two diagonal angles in described block corner are respectively arranged with two through holes 7.
Described fore-set 5 is right cylinder, and its disc is provided with block rubber.
All the degree of depth is identical with lower house 2 for length and the upper shell 1 of described fore-set 5.
The upper surface of described upper shell 1 is provided with bar code line 10.
Described anticorrosive coat 8 scribbles anticorrosive paint.
The projection of upper shell and the groove of lower house are worked in coordination, upper shell and lower house is made to form block, the special construction of projection and groove can make upper shell and lower house combine tightr, induction chip in block holds out against by eight fore-sets, block rubber makes induction chip fixing more firm, not easily slide, cord can be passed in through-holes, block is facilitated to go out from aviation apparatus pull-up, convenient scanning, anticorrosive coat prevents block not to be corroded, and vacuum layer effectively reduces the weight of block, during scanning, scanner is aimed at bar code line.
The beneficial effects of the utility model: the utility model structure is simple, practical, solve the problem that bar code is easily torn when aviation apparatus keeps in repair, corrodes, make maintenance process more smooth, also greatly improve work efficiency.
Claims (7)
1. an aeronautical maintenance bar code block, comprise block, block is made up of upper shell and lower house, it is characterized in that: described upper shell and the upper and lower surface of lower house are all in square, position near four limits on the lower surface of upper shell is provided with projection, position near four limits on the upper surface of lower house is provided with groove, the outer wall of upper shell and lower house is two-layer, be respectively the vacuum layer of outer field anticorrosive coat and internal layer, the center of lower house upper surface is provided with four fore-sets, induction chip is provided with above fore-set, upper shell lower surface center is also provided with four fore-sets.
2. aeronautical maintenance bar code block according to claim 1, is characterized in that: the line of four fore-sets of described upper shell is square, and on lower house, the line of four fore-sets is also square.
3. aeronautical maintenance bar code block according to claim 1, is characterized in that: two diagonal angles in described block corner are respectively arranged with two through holes.
4. aeronautical maintenance bar code block according to claim 1, is characterized in that: described fore-set is right cylinder, and its disc is provided with block rubber.
5. aeronautical maintenance bar code block according to claim 1, is characterized in that: the length of described fore-set is identical with the equal degree of depth of upper shell and lower house.
6. aeronautical maintenance bar code block according to claim 1, is characterized in that: the upper surface of described upper shell is provided with bar code line.
7. aeronautical maintenance bar code block according to claim 1, is characterized in that: described anticorrosive coat scribbles anticorrosive paint.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420538529.4U CN204087250U (en) | 2014-09-19 | 2014-09-19 | Aeronautical maintenance bar code block |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420538529.4U CN204087250U (en) | 2014-09-19 | 2014-09-19 | Aeronautical maintenance bar code block |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204087250U true CN204087250U (en) | 2015-01-07 |
Family
ID=52179933
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420538529.4U Expired - Fee Related CN204087250U (en) | 2014-09-19 | 2014-09-19 | Aeronautical maintenance bar code block |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204087250U (en) |
-
2014
- 2014-09-19 CN CN201420538529.4U patent/CN204087250U/en not_active Expired - Fee Related
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150107 Termination date: 20200919 |