CN205210336U - Adopt aviation light guide plate mosaic structure of different in nature material - Google Patents
Adopt aviation light guide plate mosaic structure of different in nature material Download PDFInfo
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- CN205210336U CN205210336U CN201520985738.8U CN201520985738U CN205210336U CN 205210336 U CN205210336 U CN 205210336U CN 201520985738 U CN201520985738 U CN 201520985738U CN 205210336 U CN205210336 U CN 205210336U
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Abstract
The utility model discloses an adopt aviation light guide plate mosaic structure of different in nature material includes, and the panel is formed with holding mold insert hole on it, the top periphery in holding mold insert hole is formed with panel slant incision, the mold insert, its holding in the holding mold insert is downthehole, the material of mold insert with the material of panel is different, the top periphery of mold insert is formed with mold insert slant incision, mold insert slant incision with panel slant incision is relatively in order to constitute the concave groove space of holding, fill to glue, its holding in in the concave groove space of holding, again, the top surface of filling layer the top surface of mold insert reaches the mutual parallel and level of top surface three of panel, and, lacquer layer, its cover in the top surface of panel the top surface of mold insert reaches fill the top surface of gluing. The utility model has the advantages of: mold insert edge lacquer layer is difficult for receiving high low temperature affected and splits.
Description
Technical field
The utility model relates to aviation light guide plate, in particular, and a kind of aviation light guide plate mosaic texture adopting unlike material.
Background technology
At present, because each indication information in aviation light guide plate needs illumination separately, structurally generally inlay part by pressure and carry out every light process.In prior art, the mosaic texture of light guide plate as shown in Figure 1, comprise panel 1, mold insert 2 and enamelled coating 3, panel 1 and mold insert 2 are unlike material, usual panel 1 is metal material, mold insert 2 is printing opacity nonmetallic materials, and enamelled coating 3 primarily of priming paint, composition such as resistance lac varnish, protective paint etc., and the enamelled coating 3 of mold insert 2 correspondence etches corresponding printing opacity indication information.Because mold insert 2 adopts printing opacity nonmetallic materials, its thermal expansivity is much bigger compared with panel 1 metal material used, more easily deformation is there is in high/low temperature situation, and cause the enamelled coating fracture of mold insert edge, Fig. 2 is that mold insert causes enamelled coating cut-out schematic diagram in high-temperature expansion situation, Fig. 3 is that mold insert causes enamelled coating and breaks schematic diagram in low-temperature shrink situation, and high/low temperature ringing can aggravate the generation of enamelled coating crack conditions in Fig. 2 and Fig. 3.In light guide plate, enamelled coating fracture in mold insert edge not only affects product appearance, also can cause light leakage phenomena, affect usability, therefore urgently to be resolved hurrily.
Utility model content
The purpose of this utility model is the problem solving mold insert edge enamelled coating easy fracture in existing light guide plate embedding technique, provides a kind of aviation light guide plate mosaic texture of novel employing unlike material.
In order to realize this purpose, the technical solution of the utility model is as follows: a kind of aviation light guide plate mosaic texture adopting unlike material, includes,
Panel, it is formed with accommodating mold insert hole, and the top perimeter in described accommodating mold insert hole is formed with panel slant cutting edge;
Mold insert, it is placed in described accommodating mold insert hole, the material of described mold insert and the material of described panel different, the top perimeter of described mold insert is formed with mold insert slant cutting edge, and described mold insert slant cutting edge is relative to described panel slant cutting edge to form containing groove space;
Fill glue, it is placed in described containing groove space, and again, the end face three of the end face of described packed layer, the end face of described mold insert and described panel is mutually concordant; And,
Enamelled coating, it is covered in the end face of the end face of described panel, the end face of described mold insert and described filling glue.
As a kind of preferred version adopting the aviation light guide plate mosaic texture of unlike material, the inner face of tangent plane from described accommodating mold insert hole of described panel slant cutting edge outwards begins and extends upwardly to the end face of described panel, and the tangent plane of described mold insert slant cutting edge inwardly begins from the lateral surface of described mold insert and extends upwardly to the end face of described mold insert.
As a kind of preferred version adopting the aviation light guide plate mosaic texture of unlike material, the cross sectional shape system triangle in described containing groove space or arc.
As a kind of preferred version adopting the aviation light guide plate mosaic texture of unlike material, the material line aluminium alloy of described panel, the material system polysulfones of described mold insert or aerial organic glass.
As a kind of preferred version adopting the aviation light guide plate mosaic texture of unlike material, the silica gel of described filling glue system energy cementation metal material and nonmetallic materials.
Compared with prior art, advantage of the present utility model is at least: mold insert edge enamelled coating is not subject to high/low temperature impact and ruptures.
Accompanying drawing explanation
Fig. 1 is the structural representation of prior art.
Fig. 2 is A place enamelled coating fracture schematic diagram in the case of a high temperature in Fig. 1.
Fig. 3 is A place enamelled coating fracture schematic diagram at low temperatures in Fig. 1.
Fig. 4 is the structural representation of the utility model one embodiment.
Fig. 5 is B place enamelled coating view in the case of a high temperature in Fig. 4.
Fig. 6 is B place enamelled coating view at low temperatures in Fig. 4.
Embodiment
By reference to the accompanying drawings the utility model is described in further detail below by concrete embodiment.
Refer to Fig. 4, shown in figure is a kind of aviation light guide plate mosaic texture adopting unlike material, forms primarily of panel 1, mold insert 2, enamelled coating 3 and filling glue 4.
Described panel 1 is formed with accommodating mold insert hole.The top perimeter in described accommodating mold insert hole is formed with panel slant cutting edge, and the inner face of tangent plane from described accommodating mold insert hole of described panel slant cutting edge outwards begins and extend upwardly to the end face of described panel.
Described mold insert 2 is placed in described accommodating mold insert hole.Described mold insert 2 adopts interference fit with described accommodating mold insert hole.The material of described mold insert 2 and the material of described panel 1 different, in the present embodiment, the material line aluminium alloy of described panel 1, the material system polysulfones of described mold insert 2 or aerial organic glass.The top perimeter of described mold insert 2 is formed with mold insert slant cutting edge, and the tangent plane of described mold insert slant cutting edge inwardly begins from the lateral surface of described mold insert and extends upwardly to the end face of described mold insert.Described mold insert slant cutting edge is relative to described panel slant cutting edge to form containing groove space.The cross sectional shape in described containing groove space can be triangle, also can be arc.
Described filling glue 4 is placed in described containing groove space.In the present embodiment, described filling glue 4 is the silica gel of energy cementation metal material and nonmetallic materials.Again, the end face three of the end face of described packed layer, the end face of described mold insert and described panel is mutually concordant.
Described enamelled coating 3 is covered in the end face of the end face of described panel 1, the end face of described mold insert 2 and described filling glue 4.
Referring to shown in Fig. 5 and 6, figure is the enamelled coating view of marginal position B in high/low temperature situation of described mold insert 2.In Figure 5, described mold insert 2 is in high-temperature expansion situation, though there is crimp with described panel 1 at faying face 21 place, but due to the buffer action of described filling glue 4, make the enamelled coating 3 above described filling glue 4 that the change of approximate convex occur along with the surface configuration of described filling glue 4, avoid described enamelled coating 3 and be in sharply dissengaged positions.In figure 6, described mold insert 2 is in low-temperature shrink situation, though produce separation trend with described panel 1 at faying face 21 place, but due to the inhibition of described filling glue 4, make the enamelled coating 3 above described filling glue 4 that the change of approximate arcs of recesses occur along with the surface configuration of described filling glue 4, avoid described enamelled coating 3 and be in sharply drawing crack state.Be not difficult to find out thus, said structure is relative to existing embedding technique, and in identical high/low temperature situation, the mold insert edge enamelled coating of light guide plate not easily phenomenon of rupture occurs.
Below only have expressed embodiment of the present utility model, it describes comparatively concrete and detailed, but therefore can not be interpreted as the restriction to utility model patent scope.It should be pointed out that for the person of ordinary skill of the art, without departing from the concept of the premise utility, can also make some distortion and improvement, these all belong to protection domain of the present utility model.Therefore, the protection domain of the utility model patent should be as the criterion with claims.
Claims (5)
1. adopt an aviation light guide plate mosaic texture for unlike material, it is characterized in that, include,
Panel, it is formed with accommodating mold insert hole, and the top perimeter in described accommodating mold insert hole is formed with panel slant cutting edge;
Mold insert, it is placed in described accommodating mold insert hole, the material of described mold insert and the material of described panel different, the top perimeter of described mold insert is formed with mold insert slant cutting edge, and described mold insert slant cutting edge is relative to described panel slant cutting edge to form containing groove space;
Fill glue, it is placed in described containing groove space, and again, the end face three of the end face of described packed layer, the end face of described mold insert and described panel is mutually concordant; And,
Enamelled coating, it is covered in the end face of the end face of described panel, the end face of described mold insert and described filling glue.
2. a kind of aviation light guide plate mosaic texture adopting unlike material according to claim 1, it is characterized in that, the inner face of tangent plane from described accommodating mold insert hole of described panel slant cutting edge outwards begins and extends upwardly to the end face of described panel, and the tangent plane of described mold insert slant cutting edge inwardly begins from the lateral surface of described mold insert and extends upwardly to the end face of described mold insert.
3. a kind of aviation light guide plate mosaic texture adopting unlike material according to claim 2, is characterized in that: the cross sectional shape system triangle in described containing groove space or arc.
4. a kind of aviation light guide plate mosaic texture adopting unlike material as claimed in any of claims 1 to 3, is characterized in that, the material line aluminium alloy of described panel, the material system polysulfones of described mold insert or aerial organic glass.
5. a kind of aviation light guide plate mosaic texture adopting unlike material as claimed in any of claims 1 to 3, is characterized in that: the silica gel of described filling glue system energy cementation metal material and nonmetallic materials.
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN105353456A (en) * | 2015-12-02 | 2016-02-24 | 上海航空电器有限公司 | Aerial light guide plate mosaic structure adopting unlike materials |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN105353456A (en) * | 2015-12-02 | 2016-02-24 | 上海航空电器有限公司 | Aerial light guide plate mosaic structure adopting unlike materials |
CN105353456B (en) * | 2015-12-02 | 2024-04-12 | 上海航空电器有限公司 | Aviation light guide plate mosaic structure adopting different materials |
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