CN204300053U - A kind of spring clip type trim panel anchor fitting - Google Patents
A kind of spring clip type trim panel anchor fitting Download PDFInfo
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- CN204300053U CN204300053U CN201420697733.0U CN201420697733U CN204300053U CN 204300053 U CN204300053 U CN 204300053U CN 201420697733 U CN201420697733 U CN 201420697733U CN 204300053 U CN204300053 U CN 204300053U
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- connecting element
- trim panel
- spring steel
- common connecting
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Abstract
The utility model relates to a kind of design of installing fixed form for the trim board in aircraft cabin.A kind of spring clip type trim panel anchor fitting is provided, comprises: the common connecting element 1 of L plate shape and the spring steel connecting element 2 of L plate shape; One side medial surface of described common connecting element 1 and spring steel connecting element 2 while fit, it is little that common connecting element 1 another side and spring steel connecting element 2 another side form opening, the draw-in groove that inner space is large; Common connecting element 1 and spring steel connecting element 2 fit while be fixedly connected with aircaft configuration; Trim panel 3 one end is inserted in the draw-in groove that common connecting element 1 and spring steel connecting element 2 form.The utility model adopts spring clip draw-in groove mode to fix trim panel, solves a difficult problem for fast assembling-disassembling and assembly clearance.Structure is simple, is convenient to the airborne equipment after to trim panel and trim panel self is safeguarded, takes into account aesthetic property, practicality, greatly improve the maintainability of complete machine simultaneously while meeting system functional requirement.
Description
Technical field
The utility model relates to a kind of design of installing fixed form for the trim board in aircraft cabin.
Background technology
At present, the trim panel great majority of Domestic Aircraft adopt fixed type mounting means.This mode for be installed on the airborne equipment after trim panel maintenance, safeguard cause certain difficulty.Though some fast-spliced trim panel solves the quick despatch problem of trim panel, but due to slot width and trim panel thickness close, difficulty is inserted during installation, and owing to inevitably producing gap between the reason trim panel of making and installation precision and fixed slot, along with the increase of dismounting number of times, gap can be increasing, the trim panel be in slot can be produced in flight is long and rock and produce noise.
Utility model content
Utility model object
A kind of spring clip type trim panel anchor fitting is provided, to reach fast assembling-disassembling, fixed effect, and while meeting system functionality, take into account aesthetic property and practicality.
Technical scheme
A kind of spring clip type trim panel anchor fitting, comprising:
The common connecting element 1 of L plate shape and the spring steel connecting element 2 of L plate shape;
One side medial surface of described common connecting element 1 and spring steel connecting element 2 while fit, it is little that common connecting element 1 another side and spring steel connecting element 2 another side form opening, the draw-in groove that inner space is large; Common connecting element 1 and spring steel connecting element 2 fit while be fixedly connected with aircaft configuration; Trim panel 3 one end is inserted in the draw-in groove that common connecting element 1 and spring steel connecting element 2 form.
The draw-in groove opening part that common connecting element 1 and spring steel connecting element 2 are formed turns up 30 ° of angles.
Common connecting element 1 is provided with flange in both sides, draw-in groove position.
Spring steel connecting element 2 adopts the spring steel of 0.5mm to make.
The paint that common connecting element 1 is identical with trim panel 3 color with the spray of spring steel connecting element 2 surface.
Beneficial effect
The utility model adopts spring clip draw-in groove mode to fix trim panel, solves a difficult problem for fast assembling-disassembling and assembly clearance.Structure is simple, is convenient to the airborne equipment after to trim panel and trim panel self is safeguarded, takes into account aesthetic property, practicality, greatly improve the maintainability of complete machine simultaneously while meeting system functional requirement.
Accompanying drawing explanation
Fig. 1 is the schematic diagram such as geodesic structure such as axle such as grade of spring clip type trim panel anchor fitting.
Fig. 2 is spring clip type trim panel anchor fitting cross section structure schematic diagram.
Fig. 3 is spring clip type trim panel anchor fitting common connecting element 1 end detailed view.
Detailed description of the invention
A kind of spring clip type trim panel anchor fitting, as shown in Figure 1, comprising:
The common connecting element 1 of L plate shape and the spring steel connecting element 2 of L plate shape;
One side medial surface of described common connecting element 1 and spring steel connecting element 2 while fit, it is little that common connecting element 1 another side and spring steel connecting element 2 another side form opening, the draw-in groove that inner space is large; Common connecting element 1 and spring steel connecting element 2 fit while be fixedly connected with aircaft configuration; Trim panel 3 one end is inserted in the draw-in groove that common connecting element 1 and spring steel connecting element 2 form.This little inner space of anchor fitting draw-in groove opening is large, to ensure that trim panel is installed convenient, firm, does not rock, does not produce noise.
As shown in Figure 2, the draw-in groove opening part that common connecting element 1 and spring steel connecting element 2 are formed turns up 30 ° of angles, convenient installation trim panel 3.
As shown in Figure 3, common connecting element 1 is provided with flange in both sides, draw-in groove position, to ensure that trim panel is installed firmly, not slippage.
Spring steel connecting element 2 adopts the spring steel of 0.5mm to make, lightweight, good rigidity.
The paint that common connecting element 1 is identical with trim panel 3 color with the spray of spring steel connecting element 2 surface, to reach the effect of decoration.
Spring clip type trim panel anchor fitting is combined with spring steel connecting element 2 by common connecting element 1, and this anchor fitting is by screw and anatomical connectivity.Only trim panel need be put into anchor fitting draw-in groove during use, operation is simple and reliable.Solve a difficult problem for fast assembling-disassembling and assembly clearance.Be convenient to the airborne equipment after to trim panel and trim panel self is safeguarded, while meeting system functional requirement, take into account aesthetic property, practicality, greatly improve the maintainability of complete machine simultaneously.
Above-mentioned embodiment is only for illustrating technical conceive of the present utility model and feature; object is person skilled in the art can be understood content of the present utility model and be implemented; protection domain of the present utility model can not be limited with this; all equivalences done according to the utility model Spirit Essence change or modify, and all should be encompassed in protection domain of the present utility model.
Claims (5)
1. a spring clip type trim panel anchor fitting, is characterized in that, comprising:
The common connecting element (1) of L plate shape and the spring steel connecting element (2) of L plate shape;
One side medial surface of described common connecting element (1) and spring steel connecting element (2) while fit, it is little that common connecting element (1) another side and spring steel connecting element (2) another side form opening, the draw-in groove that inner space is large; Common connecting element (1) and spring steel connecting element (2) fit while be fixedly connected with aircaft configuration; Trim panel (3) one end is inserted in the draw-in groove that common connecting element (1) and spring steel connecting element (2) form.
2. a kind of spring clip type trim panel anchor fitting as claimed in claim 1, is characterized in that,
The draw-in groove opening part that common connecting element (1) and spring steel connecting element (2) are formed turns up 30 ° of angles.
3. a kind of spring clip type trim panel anchor fitting as claimed in claim 1, is characterized in that,
Common connecting element (1) is provided with flange in both sides, draw-in groove position.
4. a kind of spring clip type trim panel anchor fitting as claimed in claim 1, is characterized in that,
Spring steel connecting element (2) adopts the spring steel of 0.5mm to make.
5. a kind of spring clip type trim panel anchor fitting as claimed in claim 1, is characterized in that,
The paint that common connecting element (1) is identical with trim panel (3) color with the spray of spring steel connecting element (2) surface.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420697733.0U CN204300053U (en) | 2014-11-19 | 2014-11-19 | A kind of spring clip type trim panel anchor fitting |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201420697733.0U CN204300053U (en) | 2014-11-19 | 2014-11-19 | A kind of spring clip type trim panel anchor fitting |
Publications (1)
Publication Number | Publication Date |
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CN204300053U true CN204300053U (en) | 2015-04-29 |
Family
ID=53105596
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201420697733.0U Active CN204300053U (en) | 2014-11-19 | 2014-11-19 | A kind of spring clip type trim panel anchor fitting |
Country Status (1)
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CN (1) | CN204300053U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104843168A (en) * | 2015-05-05 | 2015-08-19 | 江苏逸帆航空科技有限公司 | Rapid-disassembly rapid-assembly structure for aircraft interior decoration |
-
2014
- 2014-11-19 CN CN201420697733.0U patent/CN204300053U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104843168A (en) * | 2015-05-05 | 2015-08-19 | 江苏逸帆航空科技有限公司 | Rapid-disassembly rapid-assembly structure for aircraft interior decoration |
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