CN103963976A - Aircraft interior trim part connecting structure - Google Patents
Aircraft interior trim part connecting structure Download PDFInfo
- Publication number
- CN103963976A CN103963976A CN201310039767.0A CN201310039767A CN103963976A CN 103963976 A CN103963976 A CN 103963976A CN 201310039767 A CN201310039767 A CN 201310039767A CN 103963976 A CN103963976 A CN 103963976A
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- CN
- China
- Prior art keywords
- aircraft interior
- button block
- spherical
- fraising
- interior trim
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Abstract
The invention provides an aircraft interior trim part connecting structure, relates to aircraft interior trim parts, and solves the problems of a large number of mounting processes and poorer decoration effect in the prior art. The aircraft interior trim part connecting structure is characterized in that a movable connecting fastener seat (3) with a mounting support plate (2) is reversely fixed to a structural member (5); a connecting fastener (4) with a spherical hinge type bulge (42) is fixed to an interior trim part (1); when the spherical hinge type bulge (42) of the connecting fastener (4) penetrates through the structural member (5), the mounting support plate (2) and the through hole (32) of the connecting fastener seat (3) enter the spherical hinge hole (31) of the connecting fastener seat (3), the interior trim part (1) can be reliably connected with the structural member (5). The connecting structure is simple, convenient to operate and good in decoration effect, can be used for quickly dismounting the aircraft interior trim parts, and has a higher practical value.
Description
Technical field
The present invention relates to aircraft interior trim, relate in particular to a kind of connection structure of aircraft interior trimming parts.
Background technology
Traditional aircraft interior trimming parts adopts fastener to be connected with framing member, and usually uses interior trim cutting to hide fastener, and installation process is many and decorative effect is poor, cannot reach the object of fast assembling-disassembling.
Utility model content
The object of the invention is: a kind of connection structure of aircraft interior trimming parts is provided, can effectively improves decorative effect, and can make interior trimming parts fast assembling-disassembling, connect reliably, technique is simple, with low cost.
Technical scheme of the present invention is: a kind of connection structure of aircraft interior trimming parts, comprising: supporting plate is installed, is connected Button Block, ball-and-socket hinge style connection fastener, framing member,
The one side that supporting plate is installed has the "T"-shaped groove that inserts and can move about for connecting Button Block, and another side is plane, is connected with framing member by splicing or riveting method;
Connect Button Block and there is "T"-shaped structure, an end face of its "T"-shaped structure can insert in the "T"-shaped groove that supporting plate is installed, have through hole and spherical fraising perpendicular to the centre of "T"-shaped end face, the diameter of spherical fraising is greater than the diameter of through hole, and the cross-sectional plane of spherical fraising is circular;
Ball-and-socket hinge style connection fastener has T-shape structure, and an end face of its "T"-shaped structure is plane, is connected with aircraft interior trimming parts by splicing or riveting method; There is deformable ball-and-socket hinge style projection perpendicular to the other end of this end face, comprise the stylolitic part that is positioned at bottom and the head that is positioned at top, the maximum gauge of head is greater than the external diameter of stylolitic part, and excessive by sphere between the two, centre at head is axially provided with groove along it, and the ball pivot projection of connection fastener can coordinate with the spherical fraising that is connected Button Block;
The ball-and-socket hinge style projection of connection fastener enters in the spherical fraising that connects Button Block aircraft interior trimming parts is connected with framing member through the through hole of framing member, installation supporting plate and connection Button Block.
The invention has the beneficial effects as follows: overcome that the installation process of fastener method of attachment of traditional aircraft interior trimming parts is many and effect is poor, interior trimming parts cannot fast assembling-disassembling problem, a kind of aircraft method for connecting inner trimming part of novelty is provided, can effectively improve decorative effect, and can make interior trimming parts fast assembling-disassembling, connect reliably, technique is simple, with low cost.
Brief description of the drawings
Fig. 1 is aircraft interior trimming parts connection diagram of the present invention.
Fig. 2 is that aircraft interior trimming parts of the present invention connects cutaway view.
Fig. 3 is that the present invention installs supporting plate schematic diagram.
Fig. 4 is that the present invention connects Button Block schematic diagram.
Fig. 5 is connection fastener schematic diagram of the present invention.
Detailed description of the invention
Below in conjunction with accompanying drawing, the present invention is described in further detail:
The connection structure of aircraft interior trimming parts provided by the invention, as shown in Fig. 1,2,3,4,5, comprising: supporting plate 2 is installed, connected Button Block 3, ball-and-socket hinge style connection fastener 4, framing member 5,
The one side that supporting plate 2 is installed has the "T"-shaped groove 21 that inserts and can move about for connecting Button Block 3, and another side is plane, is connected with framing member 5 by splicing or riveting method;
Connect Button Block 3 and there is "T"-shaped structure, an end face of its "T"-shaped structure can insert in the "T"-shaped groove 21 that supporting plate 2 is installed, there is through hole 32 and spherical fraising 31 perpendicular to the centre of "T"-shaped end face, the diameter of spherical fraising 31 is greater than the diameter of through hole 32, and the cross-sectional plane of spherical fraising 31 is circular;
Ball-and-socket hinge style connection fastener 4 has T-shape structure, and an end face of its "T"-shaped structure is plane, is connected with aircraft interior trimming parts 1 by splicing or riveting method; There is deformable ball-and-socket hinge style projection 42 perpendicular to the other end of this end face, comprise the stylolitic part 41 that is positioned at bottom and the head 42 that is positioned at top, the maximum gauge of head 42 is greater than the external diameter of stylolitic part 41, and excessive by sphere between the two, centre at head 42 is axially provided with groove 43 along it, and the ball pivot projection 42 of connection fastener 4 can coordinate with the spherical fraising 31 that is connected Button Block 3.
The ball-and-socket hinge style projection 42 of connection fastener 4 enters and connects that the spherical fraising 31 of Button Block 3 is interior to be connected aircraft interior trimming parts 1 with framing member 5 through framing member 5, the through hole 32 supporting plate 2 being installed and being connected Button Block 3.
When installation, first, offer Long Circle through hole on framing member 5, its minimum diameter is identical with through hole 22 diameters that supporting plate 2 is installed, to oppositely be fixed on framing member 5 with the connection Button Block 3 moving about of supporting plate 2 is installed, and make to install the through hole 22 of supporting plate 2 and overlap with the through hole of framing member 5 is central; Secondly, the connection fastener with ball-and-socket hinge style projection 42 4 is fixed on aircraft interior trimming parts 1; Finally, press connection fastener 4 places on aircraft interior trimming parts 1, the ball-and-socket hinge style projection 42 of connection fastener 4 is entered in the spherical fraising 31 that connects Button Block 3 through the through hole 32 of framing member 5, installation supporting plate 2 and connection Button Block 3, can realize being connected between aircraft interior trimming parts 1 and framing member 5.
Claims (1)
1. a connection structure for aircraft interior trimming parts, is characterized in that, comprising: supporting plate (2) is installed, is connected Button Block (3), ball-and-socket hinge style connection fastener (4), framing member (5),
The one side that supporting plate (2) is installed has the "T"-shaped groove (21) that inserts and can move about for connecting Button Block (3), and another side is plane, is connected with framing member (5) by splicing or riveting method;
Connect Button Block (3) and there is "T"-shaped structure, an end face of its "T"-shaped structure can insert in the "T"-shaped groove (21) that supporting plate (2) is installed, there is through hole (32) and spherical fraising (31) perpendicular to the centre of "T"-shaped end face, the diameter of spherical fraising (31) is greater than the diameter of through hole (32), and the cross-sectional plane of spherical fraising (31) is circular;
Ball-and-socket hinge style connection fastener (4) has T-shape structure, and an end face of its "T"-shaped structure is plane, is connected with aircraft interior trimming parts (1) by splicing or riveting method; There is deformable ball-and-socket hinge style projection (42) perpendicular to the other end of this end face, comprise the stylolitic part (41) that is positioned at bottom and the head (42) that is positioned at top, the maximum gauge of head (42) is greater than the external diameter of stylolitic part (41), and excessive by sphere between the two, centre at head (42) is axially provided with groove (43) along it, and the ball pivot projection (42) of connection fastener (4) can coordinate with the spherical fraising (31) that is connected Button Block (3);
The ball-and-socket hinge style projection (42) of connection fastener (4) enters in the spherical fraising (31) that connects Button Block (3) aircraft interior trimming parts (1) is connected with framing member (5) through the through hole (32) of framing member (5), installation supporting plate (2) and connection Button Block (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310039767.0A CN103963976A (en) | 2013-02-01 | 2013-02-01 | Aircraft interior trim part connecting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310039767.0A CN103963976A (en) | 2013-02-01 | 2013-02-01 | Aircraft interior trim part connecting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103963976A true CN103963976A (en) | 2014-08-06 |
Family
ID=51234082
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310039767.0A Pending CN103963976A (en) | 2013-02-01 | 2013-02-01 | Aircraft interior trim part connecting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103963976A (en) |
Cited By (1)
| 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 |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10025359C1 (en) * | 2000-05-23 | 2001-10-25 | Draexlmaier Lisa Gmbh | Decorative connection part, especially for vehicle interior, has decorative part elements with bowl-shaped openings and pin-shaped projections, which are fused into openings to form undercuts |
| WO2005099848A2 (en) * | 2004-04-16 | 2005-10-27 | Niko Fric | Device and method for coupling decorative balloons |
| US20090059610A1 (en) * | 2007-08-31 | 2009-03-05 | Marshall Joseph A | Starry Sky Lighting Panels |
| CN201342996Y (en) * | 2008-12-23 | 2009-11-11 | 比亚迪股份有限公司 | Installation device for automotive interior trim parts |
| CN201712788U (en) * | 2010-06-13 | 2011-01-19 | 昌河飞机工业（集团）有限责任公司 | Internal decoration framework component of helicopter |
| US20110084164A1 (en) * | 2009-10-09 | 2011-04-14 | Mag Aerospace Industries, Inc. D/B/A Monogram Systems, Inc. | Panel inserts for aircraft and other vessels |
-
2013
- 2013-02-01 CN CN201310039767.0A patent/CN103963976A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE10025359C1 (en) * | 2000-05-23 | 2001-10-25 | Draexlmaier Lisa Gmbh | Decorative connection part, especially for vehicle interior, has decorative part elements with bowl-shaped openings and pin-shaped projections, which are fused into openings to form undercuts |
| WO2005099848A2 (en) * | 2004-04-16 | 2005-10-27 | Niko Fric | Device and method for coupling decorative balloons |
| US20090059610A1 (en) * | 2007-08-31 | 2009-03-05 | Marshall Joseph A | Starry Sky Lighting Panels |
| CN201342996Y (en) * | 2008-12-23 | 2009-11-11 | 比亚迪股份有限公司 | Installation device for automotive interior trim parts |
| US20110084164A1 (en) * | 2009-10-09 | 2011-04-14 | Mag Aerospace Industries, Inc. D/B/A Monogram Systems, Inc. | Panel inserts for aircraft and other vessels |
| CN201712788U (en) * | 2010-06-13 | 2011-01-19 | 昌河飞机工业（集团）有限责任公司 | Internal decoration framework component of helicopter |
Cited By (1)
| 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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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140806 |