阅读说明：本技术 一种飞机系统标牌整体式粘接板 (Integrated bonding plate for airplane system label ) 是由 张耀 祁旭亮 王林 万艳松 毛聪聪 罗欣 周博 谭启政 高双 于 2021-07-26 设计创作，主要内容包括：本发明公开了一种飞机系统标牌整体式粘接板,属于粘贴标志领域。包括离型纸、转贴膜和零件标牌层,零件标牌层包括至少一个零件标牌,零件标牌层设置在离型纸与转贴膜之间且矩阵排列,零件标牌的其中一面设有粘胶层。本发明将飞机上可使用的多个零件标牌以矩阵式排列在离型纸上,粘贴时可进行整体粘贴,一次多贴,提高了粘贴的效率,零件标牌的贴标更加稳定,化零为整,以离型纸作为载体进行存管,便于管理。(The invention discloses an integrated bonding plate for a label of an aircraft system, and belongs to the field of bonding marks. Including from type paper, change pad pasting and part sign layer, the part sign layer includes at least one part sign, and the part sign layer sets up from type paper and changes between the pad pasting and the matrix arrangement, and one of them one side of part sign is equipped with the viscose layer. According to the invention, a plurality of part labels which can be used on the airplane are arranged on the release paper in a matrix manner, and can be integrally pasted and pasted for a plurality of times in one time, so that the pasting efficiency is improved, the labeling of the part labels is more stable and is changed into a whole, and the release paper is used as a carrier for storing and managing, so that the management is convenient.)

1. An integrated bonding board of aircraft system sign, its characterized in that: comprises that

Release paper as carrier;

the transfer film comprises a waterproof surface and an adhesive surface, and the adhesive surface is adhered to the release paper;

the part label layer comprises at least one part label, the part label is arranged between the release paper and the transfer film and arranged in a matrix manner, and an adhesive layer is arranged on one surface of the part label;

the adhesive layer and the airplane are provided with a first peeling strength, the part label and the rotary adhesive film are provided with a second peeling strength, and the first peeling strength is greater than the second peeling strength.

2. The integrated aircraft system sign bonding sheet of claim 1, wherein: the part label comprises a label front surface and a label back surface, and the adhesive layer is arranged on the label back surface; the part label is adhered to the surface of the release paper through the adhesive layer, and the front surface of the label is adhered to the adhering surface of the transfer film.

3. The integrated aircraft system sign bonding sheet of claim 1, wherein: and one surface of the part label in contact with the adhesive layer is a frosted surface.

4. The integrated aircraft system sign bonding sheet of claim 1, wherein: the label back of the part label and the release paper have a third peel strength, the adhesive surface of the transfer film and the release paper have a fourth peel strength, the adhesive surface of the transfer film and the airplane have a fifth peel strength, and the third peel strength is smaller than the second peel strength.

5. The integrated aircraft system sign bonding sheet of claim 1, wherein: the rotary adhesive film is provided with easy-to-tear lines parallel to the edges of the rotary adhesive film.

6. An aircraft system sign integral bonding sheet according to claim 5, wherein: the easy-to-tear line is arranged between two adjacent columns of the part labels.

7. The integrated aircraft system sign bonding sheet of claim 6, wherein: the using method comprises the following steps:

(1) taking out the release paper with the transfer adhesive film and the part label, separating the transfer adhesive film from the release paper, and forming a bonding whole body by the transfer adhesive film and the part label;

(2) adhering the adhesive surface of the transfer film to the surface of the airplane, and adhering the adhesive layer of the part label to the surface of the airplane; the rotary adhesive film is torn, and the rotary adhesive film is separated from the part label, so that the integrated quick label pasting of the airplane is realized.

8. The integrated aircraft system sign bonding sheet of claim 7, wherein: in the step (1), the transfer film is separated from the release paper in one or more rows according to the easy-to-tear line.

Technical Field

The invention relates to a sticking mark stuck on the surface of an object, in particular to an integrated sticking board for a label of an aircraft system.

Background

Aiming at the airplane system label, all the system labels on the airplane body need to be adhered to corresponding required positions to serve as indication marks for connection of an airplane upper ring control system, a fuel system, an electromechanical finished product and a cable, and the indication marks serve as auxiliary references in subsequent maintenance. Currently, the number of fuselage tags is about 1500, and each tag is managed and installed as a single part during shipping, storage, and distribution.

The existing bonding method is mainly to bond and assemble the single label parts to the machine body one by one. However, the number of labels is large, and the types of labels are various, so that the storage and the installation are difficult, and the installation workload is large.

Disclosure of Invention

In order to solve the problems, the invention provides an integrated type sticking board for the tags of the airplane system, which arranges a plurality of tags on a rubber plate in a matrix form, integrates the tags, stores the tags in a pipe by taking the rubber plate as a carrier, can stick the tags on the same plane to the corresponding parts of a machine body at one time by using the rubber plate, is convenient to store and manage, and improves the efficiency and the accuracy of tag sticking.

In order to achieve the purpose, the invention is realized by the following technical scheme:

an integrated bonding board for aircraft system labels, comprising

Release paper as carrier;

the transfer film comprises a waterproof surface and an adhesive surface, and the adhesive surface is adhered to the release paper;

the part label layer comprises at least one part label, the part label is arranged between the release paper and the transfer film and arranged in a matrix manner, and an adhesive layer is arranged on one surface of the part label;

the adhesive layer and the airplane are provided with a first peeling strength, the part label and the rotary adhesive film are provided with a second peeling strength, and the first peeling strength is greater than the second peeling strength.

Furthermore, the part label comprises a label front surface and a label back surface, and the adhesive layer is arranged on the label back surface; the part label is adhered to the surface of the release paper through the adhesive layer, and the front surface of the label is adhered to the adhering surface of the transfer film.

Furthermore, one surface of the part label in contact with the viscose layer is a frosted surface.

Furthermore, a third peel strength is provided between the back surface of the part label and the release paper, a fourth peel strength is provided between the adhesive surface of the transfer film and the release paper, a fifth peel strength is provided between the adhesive surface of the transfer film and the airplane, and the third peel strength is smaller than the second peel strength.

Furthermore, the rotary film is provided with easy-to-tear lines parallel to the edges of the rotary film.

Further, the easy-to-tear line is arranged between two adjacent columns of the part labels.

Further, the use method of the integrated adhesive plate for the aircraft system sign comprises the following steps:

(1) taking out the release paper with the transfer adhesive film and the part label, separating the transfer adhesive film from the release paper, and forming a bonding whole body by the transfer adhesive film and the part label;

(2) adhering the adhesive surface of the transfer film to the surface of the airplane, and adhering the adhesive layer of the part label to the surface of the airplane; the rotary adhesive film is torn, and the rotary adhesive film is separated from the part label, so that the integrated quick label pasting of the airplane is realized.

Further, in the step (1), the transfer film is separated from the release paper in one or more rows according to the easy-to-tear line.

The integrated bonding plate for the airplane system label has the advantages that:

(1) arrange usable a plurality of part signs on the aircraft with the matrix on from type paper, can carry out whole pasting when pasting, once paste more, improved the efficiency of pasting.

(2) The back of the label of the part label is provided with the frosted surface, the adhesive layer is attached to the frosted surface, so that the adhesive force between the adhesive layer and the surface of the airplane can be greatly improved, and the label of the part label is more stable.

(3) Be equipped with easily tearing the line on changeing the pad pasting, easily tear the setting for of line and can satisfy different aircraft surface structure's use, can will change the pad pasting and fall into different pasting intervals when the label pasting according to the actual mark condition, more convenient operation.

(4) A plurality of part labels which can be used on the airplane are arranged on release paper in a matrix form, and are changed into a whole, and the release paper is used as a carrier for storing tubes, so that the management is convenient.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

FIG. 1 is a schematic of the peel strength of the present invention;

FIG. 2 is a schematic view of an L-shaped peel-away structure of the present invention;

FIG. 3 is a schematic view of the U-shaped peel-off structure of the present invention;

FIG. 4 is a schematic view of the release paper of the present invention before it is peeled;

FIG. 5 is a schematic view of the release paper of the present invention when peeled;

FIG. 6 is a schematic structural view of a part tag of the present invention;

FIG. 7 is a schematic structural view of a transfer film of the present invention;

FIG. 8 is a schematic view of another embodiment of a transfer film of the present invention;

1, release paper, 2-turn adhesive film, 3 part label layers and 4 part labels;

201 an easy-tear line;

the front side of the 401 sign, the back side of the 402 sign, the frosted side of 403, and the adhesive layer 404.

Detailed Description

In order to make the technical solutions of the present invention better understood, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the specification of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Example 1

An integrated adhesive plate for airplane system labels, as shown in fig. 1 and 6, comprises release paper 1, transfer film 2 and part label layer 3. The part label layer 3 is arranged between the release paper 1 and the transfer film 2.

The release paper 1 is a carrier of the whole adhesive board and consists of a three-layer structure, namely a first layer of bottom paper; a second layer of laminating film; the third layer is an anti-adhesive substance, typically silicone oil.

The transfer film 2 comprises a waterproof surface and a bonding surface, and the bonding surface is bonded with the release paper 1. The waterproof surface is mainly the main body of the transfer film 2 and has certain strength, waterproofness, moisture resistance and high temperature resistance. The bonding surface is a PE micro-adhesive film, and the peel strength between the bonding surface and the release paper 1 is fourth peel strength F2.

The part label layer 3 comprises at least one part label 4, the part label is arranged between the release paper 1 and the transfer film 2 and is arranged in a matrix mode according to a certain distance, and an adhesive layer 404 is arranged on one side of the part label 4.

Specifically, the part label 4 comprises a label front side 401 and a label back side 402, wherein the label back side 402 is adhered to the surface of the release paper 1, and the label front side 401 is adhered to the adhering surface of the transfer film 2. Adhesive layer 404 is disposed on label back 402; the part label 4 is adhered to the surface of the release paper 1 through an adhesive layer 404, and the adhesive layer 404 is mainly used for adhering to a machine body.

The surface of the part label 4 in contact with the adhesive layer 404 is a frosted surface 403. After the frosting process, the adhesive is applied to the frosted surface 403, and the natural adhesive layer 404 also has a frosted structure. The frosted structure can greatly improve the bonding force between the part tag 4 and the airplane.

The adhesive plate is mainly related to the peeling strength under the classification of the adhesive strength in the using process, and the peeling strength is the maximum load born by the unit width when an adhesive piece is separated and is the unit N/m.

The third peel strength F1 is provided between the label back 402 of the part label 4 and the release paper 1, the fourth peel strength F2 is provided between the adhesive surface of the transfer film 2 and the release paper 1, the second peel strength F3 is provided between the part label 4 and the transfer film 2, the first peel strength F4 is provided between the adhesive layer 404 and the airplane, and the fifth peel strength F5 is provided between the adhesive surface of the transfer film 2 and the airplane.

The integral bonding plate has two states, namely a storage management state and a pasting state;

(1) storing the management state: the label comprises release paper 1, label part layer and transfer film 2. The state is mainly used for convenient management of the part label 4, and the part label 4 is changed into a whole, so that the problem that the part label 4 is difficult to find in the labeling process is solved.

When the label layer and the transfer film 2 are peeled off from the release paper 1, in order to adhere the part label layer 3 and the transfer film 2 together without being stuck by the release paper 1, it is necessary to ensure that the second peel strength F3 > the third peel strength F1 > 0, which is independent of the fourth peel strength F2.

(2) The pasting state: namely, after the release paper 1 is removed, only the part label layer 3 and the transfer film 2 are in a two-layer state. This state is mainly used for attaching the part label 4 to the surface of the airplane. At the moment, the rotary adhesive film 2 is used as a carrier of the part label 4, the rotary adhesive film 2 is square in a general state, has the functions of positioning and measuring scale, can effectively avoid the part label 4 from being inclined in the labeling process, reduces the labeling rework rate, and improves the labeling effect and quality.

When the part label 4 and the transfer film 2 are bonded to the airplane as a bonded unit and the transfer film 2 is peeled off from the body, the first peel strength F4 > the second peel strength F3 is required to be ensured so that the part label 4 is not stuck to the body by the transfer film 2, which is independent of the fifth peel strength F5.

The theoretical basic principle of the integral bonding plate is that the first peel strength F4 is greater than the second peel strength F3 is greater than the third peel strength F1 is greater than 0.

Example 2

An integrated bonding plate for a sign of an aircraft system is disclosed, as shown in fig. 7 and 8, on the basis of embodiment 1, an easy-to-tear line 201 is additionally arranged on a transfer film 2, and the easy-to-tear line 201 is arranged in two modes.

One of the easy-to-tear lines 201 is disposed between two adjacent rows of the part tags 4, and a row of the transfer films 2 with the part tags 4 is integrally torn off to form a new whole as a row of the part tags 4 and the transfer films 2. The setting of the easy-to-tear line 201 is convenient for taking, placing and pasting in the labeling process, and is convenient for pasting at a narrow position of the machine body.

The other type of the easy-to-tear lines 201 is arranged along the length and width of the transfer film 2 in a perpendicular intersecting manner, and the easy-to-tear lines 201 are arranged between two adjacent part tags 4. The mutual pulling force of the vertical intersected easy-to-tear lines 201 at the intersection is larger, and when the transfer film 2 is separated from the release paper 1, two adjacent transfer films 2 with the part labels 4 are not easy to separate. The arrangement of the easy-to-tear line 201 has no influence on the storage and management of the part label 4, but can effectively solve the sticking problem of the part label 4 at a smaller sticking position of the machine body.

Example 3

A method of using an integrated, aircraft system sign bonding sheet, the method comprising the steps of:

(1) taking out the release paper 1 with the transfer film 2 and the part label 4, separating the transfer film 2 from the release paper 1, and forming a bonding whole body by the transfer film 2 and the part label 4;

(2) the bonding surface of the transfer film 2 is bonded to the surface of the airplane, and the adhesive layer 404 of the part label 4 is bonded to the surface of the airplane; the rotary film 2 is torn, the rotary film 2 is separated from the part label 4, and the integrated quick labeling of the airplane is achieved.

The specific using steps are as follows:

checking whether the label parts in the integral bonding plate meet the requirements or not, and whether the label parts have foaming or not and are debonded or not;

secondly, taking out the whole bonding plate, and flatly paving the bonding plate on a neat and flat operating platform according to the positions of the release paper 1 above and the transfer film 2 below;

fixing one end of the integral bonding plate, and rolling the integral bonding plate along one direction by hand to remove redundant bubbles, as shown in figure 4;

and fourthly, opening one corner of the release paper 1, slightly tearing off the release paper 1 along the 45-degree direction, if the individual label is adhered on the release paper 1, slightly pressing the label from the back of the integral adhesive plate, continuing to move along the tearing direction, and paying attention to control the tearing angle, as shown in fig. 5.

The tearing angles are generally L-shaped peeling and U-shaped peeling. The peeling angle of the L-shaped peeling is less than or equal to 90 degrees, as shown in figure 2, and the peeling angle of the U-shaped peeling is more than 90 degrees and less than or equal to 180 degrees, as shown in figure 3. Keeping the tearing direction parallel to the rubber plate as much as possible, namely turning the rubber plate 180 degrees;

the part label 4 is stuck to the machine body singly, in a row, in multiple rows, integrally and the like according to the labeling requirement, the rotary sticking film 2 is peeled off from the part label 4 after the pressing is flat and firm, and the process is kept constant and slow;

finally, checking whether the sticking position of the label meets the requirement or not, and correspondingly adjusting the position which does not meet the requirement.

Reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment can be included in at least one embodiment of the invention. The appearances of the phrase in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. It is explicitly and implicitly understood by one skilled in the art that the embodiments described herein can be combined with other embodiments.

Finally, it should be noted that: the embodiment of the present invention is disclosed only as a preferred embodiment of the present invention, which is only used for illustrating the technical solutions of the present invention and not for limiting the same; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those skilled in the art; the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and the modifications or the substitutions do not make the essence of the corresponding technical solutions depart from the spirit and scope of the technical solutions of the embodiments of the present invention.