CN210627669U - Label for marking surface defects of airplane - Google Patents
Label for marking surface defects of airplane Download PDFInfo
- Publication number
- CN210627669U CN210627669U CN201921830549.8U CN201921830549U CN210627669U CN 210627669 U CN210627669 U CN 210627669U CN 201921830549 U CN201921830549 U CN 201921830549U CN 210627669 U CN210627669 U CN 210627669U
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- label
- writing
- outer edge
- identifying
- varnish
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Abstract
The utility model discloses a label for marking aircraft outward appearance defect, it includes superficial layer, viscose layer and base stock, the superficial layer includes that circular surface can be used to write portion, annular connecting portion and annular outside portion, the middle hole site of outside portion is the varnish coverage area who is used for coating the varnish, write the portion in the middle of varnish coverage area, connecting portion set up between outside portion and write portion, all be equipped with the line of cut between write portion and connecting portion and between connecting portion and outside portion; the adhesive layer is arranged on the bottom surface of the surface layer; the adhesive layer is detachably adhered to the upper surface of the base paper. The utility model is suitable for a carry out the sign to aircraft surface defect.
Description
Technical Field
The utility model relates to a label for sign aircraft outward appearance defect.
Background
During the operation of the airplane, the appearance of the airplane can be greatly and slightly damaged, such as: pits and scratches, damage in some locations, must be repaired immediately, and damage in some locations, which has very little effect on the aerodynamic profile of the aircraft, allow the existence of such damage in the aircraft manufacturer without further maintenance.
At present, each aircraft manufacturer does not have a method for identifying and marking the damage, so when the exterior damage of the aircraft is checked, workers do not know whether the damage is evaluated or not and whether the damage is allowed by the aircraft manufacturer or not, the reevaluation is caused, resources are wasted, and flight delay is possibly caused.
The common tag cannot identify the appearance of the airplane because the airplane is in a severe environment in high altitude during the flight process, such as: low temperature of minus 60 ℃, strong wind and strong ultraviolet.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the technical problem that a label for marking aircraft appearance defect is provided, it is applicable to and carries out the sign to aircraft surface defect.
Solve above-mentioned technical problem, the utility model discloses a technical scheme as follows:
a label for identifying an aircraft appearance defect, comprising:
the writing part is positioned in the middle of the varnish covering area, the connecting part is arranged between the outer edge part and the writing part, and cutting lines are arranged between the writing part and the connecting part and between the connecting part and the outer edge part;
the adhesive layer is arranged on the bottom surface of the surface layer;
the adhesive layer is detachably adhered to the upper surface of the base paper.
Furthermore, a disconnection line which is cut off in the radial direction is arranged on the annular connecting part.
Further, a character mark or a pattern mark formed by printing ultraviolet-resistant ink is provided on the surface of the writing section.
Furthermore, a protective film which can be torn off is arranged on the upper surface of the surface layer.
Furthermore, a lug is arranged on the upper edge of the outer edge part.
Furthermore, the thickness of the label is 0.08-0.10 mm.
Compared with the prior art, the utility model discloses following beneficial effect has:
1. because the airplane is a special vehicle, the size of the label on the outer surface of the airplane needs to be limited (the diameter is less than or equal to 25.4 mm). The utility model discloses a varnish coverage area is injectd to the outside portion of superficial layer to make the diameter that finally forms at the apparent sign of aircraft can not exceed the regulation scope, finally form the width that covers at the peripheral varnish of writing portion in the apparent sign of aircraft through the shared region of connecting portion of superficial layer injects, thereby guarantee sufficient coverage area.
In use, when the surface layer is adhered to the exterior of the aircraft and the connecting part is torn off, varnish is coated on the surface of the writing part and the area between the writing part and the outer edge part, so that the label can adapt to the severe environment in high altitude.
2. The utility model discloses be equipped with the sign characters or the pattern that forms through ultraviolet resistance printing ink printing on the surface of writing portion to make the sign characters or the pattern of writing portion can ultraviolet resistance.
Drawings
Fig. 1 is a schematic front view of the present invention;
fig. 2 is an enlarged cross-sectional view in the direction a-a of fig. 1.
The reference numerals in the drawings mean:
1-a surface layer; 1.1-writing part; 1.2-linker moiety; 1.3-outer edge portion; 1.3.1-lugs; 2-character identification; 3-cutting line; 4-break line; 5-protective film; 6-an adhesive layer; 7-base paper.
Detailed Description
The present invention will be further described with reference to the following examples.
A label for identifying a defect in the appearance of an aircraft, as shown in figures 1 and 2, comprises a surface layer 1, an adhesive layer 6 and a backing paper 7.
The surface layer 1 comprises a writing part 1.1 with a circular surface and used for writing, an annular connecting part 1.2 and an annular outer part 1.3, a middle hole of the outer part 1.3 is a varnish covering area used for coating varnish, the writing part 1.1 is positioned in the middle of the varnish covering area, the connecting part 1.2 is arranged between the outer edge part 1.3 and the writing part 1.1, cutting lines 3 are arranged between the writing part 1.1 and the connecting part 1.2 and between the connecting part 1.2 and the outer edge part 1.3, and the writing part 1.1 and the connecting part 1.2 and the outer edge part 1.3 can be separated through the cutting lines 3.
The adhesive layer 6 is arranged on the bottom surface of the surface layer 1, and the adhesive layer 6 can be detachably adhered to the upper surface of the base paper 7, so that the surface layer 1 and the adhesive layer 6 can be torn off from the base paper 7 together.
In order to facilitate the tearing off of the connection 1.2, the annular connection 1.2 is provided with a radially severed break line 4.
In the embodiment, the character mark 2 formed by printing the ultraviolet-resistant ink is arranged on the surface of the writing part 1.1, so that the influence of ultraviolet rays on image-text information can be reduced under the condition of not increasing the thickness of a label, and the printing mode is silk-screen printing or printing.
In order to protect the surface of the label, a tear-off protective film 5 may be provided on the upper surface of the surface layer 1.
In order to facilitate the tearing off of the protective film 5 and the outer edge portion 1.3, a lug 1.3.1 may be provided on the upper edge of the outer edge portion 1.3.
The thickness of the label of the embodiment is 0.08-0.10 mm, the radius of the writing part 1.1 is 12.7mm, and the radius of the varnish covering area is 20.4mm, so that the influence of the label on the aerodynamic shape of an airplane can be greatly reduced. The outer edge 1.3 has a radius of 25.4 mm.
When the label is used, sundries are removed from the position to be marked on the outer surface of the airplane through alcohol, the pasting area is cleaned, the adhesive force of the label is affected if the pasting area is not cleaned completely, and the using effect of the label is reduced. After that, the base paper 7 of the label is torn off, the surface layer 1 is adhered on the cleaned adhering area through the adhesive layer 6, the adhering area is scraped off through a scraper blade during adhering so as to prevent the label from bubbling to influence the adhesive force and reduce the using effect of the label, after the adhering is finished, the protective film 5 is torn off, and then the mark content such as date can be written on the surface of the writing part 1.1 through a fine paint pen. After two minutes of writing, the connecting portion 1.2 is torn off and then the surface of the writing portion 1.1 and the area between the writing portion 1.1 and the outer edge portion 1.3 are coated with varnish, which should be completely covered and uniformly distributed, the number of coats being recommended not to exceed three times in order to avoid sagging of the varnish. Thereafter, the outer edge 1.3 is torn off, so that the covered area of varnish forms a circle. Waiting 3.5-4 hours the varnish will completely dry, whereupon a transparent varnish layer will form on the surface 1.1 of the writing part and in the area between the writing part 1.1 and the outer edge 1.2. The thickness of the final formed label is less than or equal to 0.4 mm.
In the use process, the pasting position of the label is close to the outer edge of the defect, and the specific position can be determined according to actual conditions. The sticking label needs to be matched with a scraper for use, and the sticking label is not required to be pressed by fingers.
The above embodiments of the present invention are not right the utility model discloses the limited protection scope, the utility model discloses an embodiment is not limited to this, all kinds of basis according to the above-mentioned of the utility model discloses an under the above-mentioned basic technical thought prerequisite of the utility model, right according to ordinary technical knowledge and the conventional means in this field the modification, replacement or the change of other multiple forms that above-mentioned structure made all should fall within the protection scope of the utility model.
Claims (6)
1. A label for identifying an aircraft appearance defect, comprising:
the writing tool comprises a surface layer, a writing part, an annular connecting part and an annular outer edge part, wherein the circular surface can be used for writing, the middle hole of the outer edge part is a varnish covering area for coating varnish, the writing part is positioned in the middle of the varnish covering area, the connecting part is arranged between the outer edge part and the writing part, and cutting lines are arranged between the writing part and the connecting part and between the connecting part and the outer edge part;
the adhesive layer is arranged on the bottom surface of the surface layer;
the adhesive layer is detachably attached to the upper surface of the base paper.
2. A label for identifying an aircraft appearance defect according to claim 1, wherein: and a disconnection line which is cut off in the radial direction is arranged on the annular connecting part.
3. A label for identifying an aircraft appearance defect according to claim 1, wherein: and character marks or pattern marks formed by printing ultraviolet-resistant ink are arranged on the surface of the writing part.
4. A label for identifying an aircraft appearance defect according to claim 1, wherein: and the upper surface of the surface layer is provided with a tearable protective film.
5. A label for identifying an aircraft appearance defect according to claim 4, wherein: and the upper edge of the outer edge part is provided with a lug.
6. A label for identifying an aircraft appearance defect according to claim 1, wherein: the thickness of the label is 0.08-0.10 mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921830549.8U CN210627669U (en) | 2019-10-23 | 2019-10-23 | Label for marking surface defects of airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921830549.8U CN210627669U (en) | 2019-10-23 | 2019-10-23 | Label for marking surface defects of airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210627669U true CN210627669U (en) | 2020-05-26 |
Family
ID=70761979
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921830549.8U Active CN210627669U (en) | 2019-10-23 | 2019-10-23 | Label for marking surface defects of airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210627669U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114484093A (en) * | 2021-12-31 | 2022-05-13 | 中国航空工业集团公司西安飞机设计研究所 | Identification structure and identification method for fluid pipeline of aircraft system |
-
2019
- 2019-10-23 CN CN201921830549.8U patent/CN210627669U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114484093A (en) * | 2021-12-31 | 2022-05-13 | 中国航空工业集团公司西安飞机设计研究所 | Identification structure and identification method for fluid pipeline of aircraft system |
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