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
Authority
CN
China
Prior art keywords
interior trimming
trimming panel
plug
trim panel
connecting structure
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
Other languages
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

The utility model provides a plug-in type interior trimming panel connecting structure, and relates to airplane interior trimming. The problem that an existing interior trimming panel connecting and fixing structure is relatively complex is solved. According to the technical scheme, the plug-in type interior trimming panel connecting structure comprises a first interior trimming panel and a second interior trimming panel, a concave clamping groove is arranged in the external surface of the first interior trimming panel in a bonding mode, a convex embedded piece is arranged on the external surface of the second interior trimming panel in a bonding mode, screw holes are formed in the concave clamping groove, the convex embedded piece is inserted between the first interior trimming panel and the concave clamping groove, and the convex embedded piece covers the screw holes in the concave clamping groove from the internal surface of the convex embedded piece. The plug-in type interior trimming panel connecting structure is simple in structure, convenient and fast to mount, capable of covering a fastening piece and meanwhile improving the stability and the firmness of interior trimming connection, and suitable for various airplanes.

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 (1)

* 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

Cited By (1)

* 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

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GR01 Patent grant
CX01 Expiry of patent term
CX01 Expiry of patent term

Granted publication date: 20130807