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CN203111508U - Plug-in type interior trimming panel connecting structure - Google Patents

Plug-in type interior trimming panel connecting structure Download PDF

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Publication number
CN203111508U
CN203111508U CN 201320061541 CN201320061541U CN203111508U CN 203111508 U CN203111508 U CN 203111508U CN 201320061541 CN201320061541 CN 201320061541 CN 201320061541 U CN201320061541 U CN 201320061541U CN 203111508 U CN203111508 U CN 203111508U
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CN
China
Prior art keywords
trim panel
utility
model
interior
plug
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 - Lifetime
Application number
CN 201320061541
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Chinese (zh)
Inventor
谷煜
黄奕佳
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Xian Aircraft Design and Research Institute of AVIC
Original Assignee
Xian Aircraft Design and Research Institute of AVIC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Xian Aircraft Design and Research Institute of AVIC filed Critical Xian Aircraft Design and Research Institute of AVIC
Priority to CN 201320061541 priority Critical patent/CN203111508U/en
Application granted granted Critical
Publication of CN203111508U publication Critical patent/CN203111508U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

本实用新型提供一种插接式内饰板连接结构,涉及飞机内饰,解决现有内饰板连接固定结构相对复杂的问题。本实用新型的技术方案包括:第一内饰板、第二内饰板,所述第一内饰板外表面粘接凹形卡槽,第二内饰板外表面粘接凸型嵌合件,凹形卡槽上开有螺钉孔,凸型嵌合件插接在第一内饰板与凹形卡槽之间,从内表面遮盖住凹形卡槽上的螺钉孔。本实用新型结构简单、安装便捷,并可遮盖紧固件,同时增加内饰连接的稳定性和牢固性,适用于各种飞机。

Figure 201320061541

The utility model provides a plug-in interior panel connection structure, relates to aircraft interior decoration, and solves the problem that the existing interior panel connection and fixing structure is relatively complicated. The technical scheme of the utility model includes: a first interior trim panel, a second interior trim panel, the outer surface of the first interior trim panel is bonded with a concave groove, and the outer surface of the second interior trim panel is bonded with a convex fitting , screw holes are provided on the concave card slot, and the convex fitting is inserted between the first interior trim panel and the concave card slot, covering the screw holes on the concave card slot from the inner surface. The utility model has the advantages of simple structure and convenient installation, and can cover fasteners, meanwhile, the stability and firmness of the interior decoration connection can be increased, and the utility model is suitable for various aircrafts.

Figure 201320061541

Description

Plug-in type trim panel connection structure
Technical field
The utility model relates to the aircraft interior trim, relates in particular to a kind of plug-in type trim panel connection structure.
Background technology
At present, the connection mode of aircraft trim panel is mainly used screw and is decorated and transplant a cutting or decorate card article, to reach the effect that hides fastener.What this kind connection mode need design that special structure is used for upholstery border is connected and fixed the structure relative complex.
The utility model content
The purpose of this utility model is: a kind of plug-in type trim panel connection structure is provided, and structure is simple relatively, and hides fastener.
The technical solution of the utility model is: a kind of plug-in type trim panel connection structure, it is characterized in that, and comprising:
First trim panel, second trim panel,
The bonding spill draw-in groove of the described first trim panel outside face, chimeric of the bonding convex of the second trim panel outside face, have screw hole on the spill draw-in groove, chimeric of convex is plugged between first trim panel and the spill draw-in groove, covers in screw hole on the spill draw-in groove from inside face.
The beneficial effects of the utility model are: the utility model has designed a kind of socket connection structure for the aircraft interior trim, have simple in structure, advantage easily is installed, and can hide fastener, and reach the effect that beautifies, increase interior trim connection stability and fastness simultaneously.
Description of drawings
Fig. 1 is the utility model plug-in type trim panel connection structure scheme drawing.
Fig. 2 is the utility model plug-in type trim panel connection structure cutaway view.
The specific embodiment
Below in conjunction with accompanying drawing the utility model is described in further detail:
The utility model provides a kind of plug-in type trim panel connection structure, as shown in Figure 1 and Figure 2, comprising:
First trim panel 1, second trim panel 2,
The bonding spill draw-in groove 4 of described first trim panel, 1 outside face, chimeric 3 of the bonding convex of second trim panel, 2 outside faces, have screw hole 5 on the spill draw-in groove 4, chimeric 3 of convex is plugged between first trim panel 1 and the spill draw-in groove 4, covers in screw hole 5 on the spill draw-in groove 4 from inside face.Use flathead screw that trim panel 1 is connected with support during installation earlier, peg graft again and go up trim panel 2, to reach the effect that hides fastener, beautifying and decorating.
Above-mentioned embodiment only is explanation technical conceive of the present utility model and characteristics; purpose is to allow the personage that is familiar with this technology can understand content of the present utility model and is implemented; can not limit protection domain of the present utility model with this; all equivalences of doing according to the utility model spirit essence change or modify, and all should be encompassed in the protection domain of the present utility model.

Claims (1)

1. a plug-in type trim panel connection structure is characterized in that, comprising:
First trim panel (1), second trim panel (2),
The bonding spill draw-in groove of described first trim panel (1) outside face (4), chimeric of bonding convex of second trim panel (2) outside face (3), have screw hole (5) on the spill draw-in groove (4), convex chimeric (3) is plugged between first trim panel (1) and the spill draw-in groove (4), covers in screw hole (5) on the spill draw-in groove (4) from inside face.
CN 201320061541 2013-02-01 2013-02-01 Plug-in type interior trimming panel connecting structure Expired - Lifetime CN203111508U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201320061541 CN203111508U (en) 2013-02-01 2013-02-01 Plug-in type interior trimming panel connecting structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201320061541 CN203111508U (en) 2013-02-01 2013-02-01 Plug-in type interior trimming panel connecting structure

Publications (1)

Publication Number Publication Date
CN203111508U true CN203111508U (en) 2013-08-07

Family

ID=48891878

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201320061541 Expired - Lifetime CN203111508U (en) 2013-02-01 2013-02-01 Plug-in type interior trimming panel connecting structure

Country Status (1)

Country Link
CN (1) CN203111508U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105620753A (en) * 2014-10-28 2016-06-01 中国航空工业集团公司西安飞机设计研究所 Airplane interior trim fixing method
CN119042203A (en) * 2024-09-05 2024-11-29 中国商用飞机有限责任公司 Buckle for board connection

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105620753A (en) * 2014-10-28 2016-06-01 中国航空工业集团公司西安飞机设计研究所 Airplane interior trim fixing method
CN119042203A (en) * 2024-09-05 2024-11-29 中国商用飞机有限责任公司 Buckle for board connection
CN119042203B (en) * 2024-09-05 2025-10-03 中国商用飞机有限责任公司 Clips for board connection

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Legal Events

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C14 Grant of patent or utility model
GR01 Patent grant
CX01 Expiry of patent term

Granted publication date: 20130807

CX01 Expiry of patent term