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

Anti-deformation aviation light guide plate inlaying structure and inlaying process thereof

A mosaic structure and light guide plate technology, which is applied in the aviation field, can solve the problems of affecting the service life, breakage of the light guide plate, and the thermal expansion of the light guide plate, so as to achieve a good service life and improve the effect of use

Pending Publication Date: 2022-05-24
SUZHOU JOYO METAL TECH CO LTD
View PDF0 Cites 0 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The existing light guide plate is susceptible to thermal expansion during use

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
  • Anti-deformation aviation light guide plate inlaying structure and inlaying process thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0032] An anti-deformation aviation light guide plate mosaic structure, such as figure 1 As shown, it includes: a supporting substrate 1, a accommodating bearing port 2 is opened on the supporting substrate 1, and an oblique opening 3 is provided at the bottom edge of the accommodating bearing port 2; an insert 4 movably installed in the accommodating bearing port 2, A filling space 5 is formed between the bearing port 2 and the insert 4 ; a filling connecting piece for sealing the filling space 5 .

[0033] The filling connector includes: a first filling member 6, a second filling member 7 disposed opposite to the first filling member 6;

[0034] The support base plate 1 is made of metal material, the inclined opening 3 is arranged at a 45° angle, and the top of the insert 4 is provided with an inclined opening 9 matching the inclined opening 3 . The oblique opening 3 reserves the space required for the insert 4 to be deformed by heat, so as to prevent the insert 4 from pres...

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 relates to an anti-deformation aviation light guide plate inlaying structure and an inlaying process thereof, and the structure comprises a supporting substrate which is provided with an accommodating bearing port, and the edge of the bottom of the accommodating bearing port is provided with an inclined port; the insert is movably mounted in the accommodating bearing opening, and a filling space is formed by the accommodating bearing opening and the insert; the filling connecting piece is used for sealing the filling space; and the sealing shaping plate enables the upper surface of the supporting base plate and the insert to be located on the same horizontal plane. During operation, the insert is firstly placed in the containing bearing opening, and connection between the insert and the supporting base plate is achieved through the filling effect of the first filling piece and the second filling piece; after the insert is heated and expanded, the bottom of the insert expands towards the direction of the inclined opening under the action of the inclined opening; meanwhile, under the action of the second filling piece, the insert expands towards the direction of the containing bearing opening, so that the insert cannot expand upwards, the sealing shaping plate cannot be broken, and the light guide plate cannot be damaged.

Description

technical field [0001] The invention relates to the field of aviation technology, in particular to an inlaid structure of an anti-deformation aviation light guide plate and an inlaid process thereof. Background technique [0002] At present, since each indication information on the aviation light guide plate needs to be illuminated separately, the light-shielding treatment is generally performed by pressing the insert in the structure. The existing light guide plate is susceptible to thermal expansion during use, which causes the light guide plate to break and affects the service life. SUMMARY OF THE INVENTION [0003] In order to solve the above technical problems, the present invention provides an anti-deformation aviation light guide plate mosaic structure and a mosaic process thereof, which have the advantages of good service life. [0004] For achieving the above object, technical scheme of the present invention is as follows: [0005] An anti-deformation aviation l...

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
IPC IPC(8): G02B6/00
CPCG02B6/0095G02B6/0016G02B6/0065G02B6/0081G02B6/0086G02B6/0093
Inventor 张瑞张剑
Owner SUZHOU JOYO METAL TECH CO LTD
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