Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Integral type bonding plate of aircraft system label

An aircraft system, integrated technology, applied in the directions of stamps, instruments, identification devices, etc., can solve the problems of difficult storage, large installation workload, cumbersome installation, etc., to improve efficiency, improve adhesion, and facilitate management.

Pending Publication Date: 2021-10-22
CHENGDU AIRCRAFT INDUSTRY GROUP
View PDF12 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, due to the large number and variety of signs, it is difficult to store them, the installation is cumbersome, and the installation workload is heavy

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Integral type bonding plate of aircraft system label
  • Integral type bonding plate of aircraft system label
  • Integral type bonding plate of aircraft system label

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0039] An aircraft system signage integral adhesive panel such as figure 1 and Figure 6 As shown, it includes release paper 1, transfer film 2, and component label layer 3. The component label layer 3 is arranged between the release paper 1 and the transfer film 2 .

[0040] The release paper 1 is the carrier of the entire bonding board. The release paper is composed of three layers, the first layer of backing paper; the second layer of coating; the third layer is an anti-adhesive substance, generally silicone oil.

[0041] The transfer film 2 includes a waterproof surface and an adhesive surface, and the adhesive surface is bonded to the release paper 1 . The waterproof surface is mainly the main body of the transfer film 2, which has certain strength, water resistance, moisture resistance and high temperature resistance. The adhesive surface is a PE micro-adhesive film, and the peeling strength with the release paper 1 is the fourth peeling strength F2.

[0042] The par...

Embodiment 2

[0054] An aircraft system signage integral adhesive panel such as Figure 7 and Figure 8As shown, on the basis of Embodiment 1, an easy-tear line 201 is added on the transfer film 2, and there are two ways to set the easy-tear line 201 .

[0055] One of the easy-to-tear lines 201 is set between two adjacent columns of part labels 4, and a row of transfer film 2 with part labels 4 is torn off from the whole to form a new whole as a row of part labels 4 and transfer film 2 . The setting of the easy-to-tear line 201 is convenient for handling and sticking during the labeling process, and is convenient for sticking at narrow positions of the body.

[0056] The other type of easy-tear line 201 is vertically intersecting along the length and width of the transfer film 2 , and the easy-tear line 201 is set between two adjacent component labels 4 . The vertically intersecting easy-tear lines 201 have a relatively large mutual pulling force at the intersection, and when the transfe...

Embodiment 3

[0058] A method for using an aircraft system signage integral adhesive plate, the method comprising the following steps:

[0059] (1) Take out the release paper 1 with the transfer film 2 and the parts label 4, separate the transfer film 2 from the release paper 1, and form the bonding whole with the transfer film 2 and the parts label 4;

[0060] (2) The bonding surface of the transfer film 2 is pasted on the aircraft surface, and now the adhesive layer 404 of the parts label 4 is also bonded to the aircraft surface; the transfer film 2 is torn off, and the transfer film 2 is separated from the parts label 4 to achieve Aircraft integrated fast labeling.

[0061] The specific usage steps are:

[0062] ① Check whether the signage parts in the integral bonding plate meet the requirements, and whether there is any blistering and debonding at the signage;

[0063] ②Take out the whole bonding board, and spread it on a clean and flat operating table according to the position where...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

PUM

No PUM Login to View More

Abstract

The invention discloses an integral type bonding plate of an aircraft system label, and belongs to the field of label bonding. The integral type bonding plate comprises release paper, a repasting film and a part label layer, the part label layer comprises at least one part label, the part label layer is arranged between the release paper and the repasting film and arranged in a matrix mode, and one face of the part label is provided with an adhesive layer. According to the invention, a plurality of part labels which can be used on an airplane are arranged on the release paper in a matrix manner, the labels can be integrally pasted during pasting, and multiple labels can be pasted at one time, so that the pasting efficiency is improved, the labeling of the part labels is more stable, parts are changed into a whole, the release paper is taken as a carrier for storage, and the management is convenient.

Description

technical field [0001] The invention relates to an adhesive sign pasted on the surface of an object, in particular to an integral type adhesive plate of an aircraft system sign. Background technique [0002] For aircraft system signs, all system signs on the fuselage need to be bonded to the corresponding required parts, as indicators for the environmental control system, fuel system, mechanical and electrical products and cable connections on the aircraft, and as auxiliary references in subsequent maintenance. At present, there are about 1,500 labels on the fuselage, and each label is managed and installed as a single part during transportation, storage, and distribution. [0003] The existing bonding method is mainly to bond and assemble individual signage parts one by one to the fuselage. However, due to the large number and variety of signs, it is difficult to store them, the installation is cumbersome, and the installation workload is heavy. Contents of the invention...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to View More

Application Information

Patent Timeline
no application Login to View More
Patent Type & Authority Applications(China)
IPC IPC(8): G09F3/02G09F3/10
CPCG09F3/02G09F3/10
Inventor 张耀祁旭亮王林万艳松毛聪聪罗欣周博谭启政高双
Owner CHENGDU AIRCRAFT INDUSTRY GROUP
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products

Browse by: Latest US Patents, China's latest patents, Technical Efficacy Thesaurus, Application Domain, Technology Topic, Popular Technical Reports.

© 2024 PatSnap. All rights reserved.Legal|Privacy policy|Modern Slavery Act Transparency Statement|Sitemap|About US| Contact US: help@patsnap.com