CN204524708U - A kind of backlight laminating machine of automatic Composition - Google Patents
A kind of backlight laminating machine of automatic Composition Download PDFInfo
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- CN204524708U CN204524708U CN201520045406.1U CN201520045406U CN204524708U CN 204524708 U CN204524708 U CN 204524708U CN 201520045406 U CN201520045406 U CN 201520045406U CN 204524708 U CN204524708 U CN 204524708U
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- fuselage
- laminating machine
- backlight
- automatic composition
- utility
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Abstract
The utility model relates to mobile phone plane plate display backlight production field, particularly relates to a kind of backlight laminating machine of automatic Composition.The utility model provides a kind of backlight laminating machine of automatic Composition, comprise frame and fuselage, also comprise the diffusion sheet feeder be arranged on fuselage from bottom to top, lifting transplanting machine hand assembly, material loading locating platform, anti-dazzling screen feeder, XY θ contraposition stacked wafer moudle, CCD image alignment system, also comprise and be positioned at the described fuselage accurate pressure-keeping mechanism arranged below from bottom to top, structure is transplanted in discharging, described accurate pressure-keeping mechanism is connected with described material loading locating platform, described fuselage is also provided with main body supply assembly, be provided with weight above described main body supply assembly and control tension mechanism and material film peeling mechanism.The utility model structure comparatively simple and stable, dustless, and the destabilizing factor existed is few, high to aligning accuracy, speed can do small-medium size soon, also can do large area backlight product.
Description
Technical field
The utility model relates to mobile phone or flat backlight source assembling field, particularly relates to a kind of backlight laminating machine of automatic Composition.
Background technology
Backlight source material is folded in glue frame by conventional manual work or multigraph press one by one, and such low precision cannot meet the narrow frame requirement of large scale.Now design this orthoscopic backlight laminating machine.Can reduce manpower, be all dustfree environment operation, and speed is fast, and precision is high.Also high-precision requirement is met during main energy operation large scale.And obtain large-scale popularization.
Utility model content
The purpose of this utility model is the deficiency for existing disc type backlight laminating machine, there is provided a kind of backlight laminating machine of dynamic assembling, adopt XY theta stage to combine with CCD assembly and carry out automatic aligning lamination, structure is comparatively simple, and the destabilizing factor existed is few, aligning accuracy is high.
To achieve these goals, the technical solution adopted in the utility model is to provide a kind of backlight laminating machine of automatic Composition, comprise frame and fuselage, also comprise the diffusion sheet feeder be arranged on fuselage from bottom to top, lifting transplanting machine hand assembly, material loading locating platform, anti-dazzling screen feeder, XY θ contraposition stacked wafer moudle, CCD image alignment system, also comprise and be positioned at the described fuselage accurate pressure-keeping mechanism arranged below from bottom to top, structure is transplanted in discharging, described accurate pressure-keeping mechanism is connected with described material loading locating platform, described fuselage is also provided with main body supply assembly, be provided with weight above described main body supply assembly and control tension mechanism and material film peeling mechanism.
As further improvement of the utility model, be also provided with PLC above described main body supply assembly and be arranged at the touch-screen in PLC.
As further improvement of the utility model, described fuselage is also provided with carrying XZ axle linkage unit.
As further improvement of the utility model, described CCD image alignment system is at least four, and wherein two are arranged at above described XY θ contraposition stacked wafer moudle, and two other is arranged at above described carrying XZ axle linkage unit.
The beneficial effects of the utility model are: the utility model structure comparatively simple and stable, dustless, and the destabilizing factor existed is few, and aligning accuracy is high, and speed can do small-medium size soon, also can do large area backlight product.
Accompanying drawing explanation
Fig. 1 is the schematic perspective view of the utility model orthoscopic backlight laminating machine;
Fig. 2 is the view in the utility model orthoscopic backlight laminating machine side-looking direction;
Fig. 3 is the internal structure schematic diagram of the utility model orthoscopic backlight laminating machine.
Detailed description of the invention
To illustrate below in conjunction with accompanying drawing and detailed description of the invention further illustrates the utility model.
Numeral in figure: 1, diffusion sheet feeder; 2, transplanting machine hand assembly is elevated; 3, material loading locating platform; 4, anti-dazzling screen feeder; 5, XY θ contraposition stacked wafer moudle; 6, CCD image alignment system; 7, accurate pressure-keeping mechanism; 8, structure is transplanted in discharging; 9, main body supply assembly; 10, touch-screen; 11, PLC; 12, XZ axle linkage unit is carried.
As Fig. 1, Fig. 2, shown in Fig. 3, the utility model provides a kind of backlight laminating machine of automatic Composition, also comprise the diffusion sheet feeder 1 be arranged on fuselage from bottom to top, lifting transplanting machine hand assembly 2, material loading locating platform 3, anti-dazzling screen feeder 4, XY θ contraposition stacked wafer moudle 5, CCD image alignment system 6, also comprise and be positioned at the described fuselage accurate pressure-keeping mechanism 7 arranged below from bottom to top, structure 8 is transplanted in discharging, described accurate pressure-keeping mechanism 7 is connected with described material loading locating platform 3, described fuselage is also provided with main body supply assembly 9, be provided with weight above described main body supply assembly 9 and control tension mechanism and material film peeling mechanism.
As shown in Figure 1 and Figure 2, the touch-screen 10 being also provided with PLC 11 above described main body supply assembly 9 and being arranged in PLC 11.
As shown in Figure 3, described fuselage is also provided with carrying XZ axle linkage unit 12.
As shown in Figure 3, described CCD image alignment system 6 is at least four, and wherein two are arranged at above described XY θ contraposition stacked wafer moudle 5, and two other is arranged at above described carrying XZ axle linkage unit 12.
First capture product target by 2 groups of CCD assemblies, analyze side-play amount, then side-play amount is transferred to PLC, PLC controls to perform side-play amount to XY θ automatic aligning again and moves, and realizes contraposition; After contraposition completes, lamination;
Above content is in conjunction with concrete preferred embodiment further detailed description of the utility model, can not assert that concrete enforcement of the present utility model is confined to these explanations.For the utility model person of an ordinary skill in the technical field, without departing from the concept of the premise utility, some simple deduction or replace can also be made, all should be considered as belonging to protection domain of the present utility model.
Claims (4)
1. the backlight laminating machine of an automatic Composition, comprise frame and fuselage, it is characterized in that: also comprise the diffusion sheet feeder be arranged on fuselage from bottom to top, lifting transplanting machine hand assembly, material loading locating platform, anti-dazzling screen feeder, XY θ contraposition stacked wafer moudle, CCD image alignment system, also comprise and be positioned at the described fuselage accurate pressure-keeping mechanism arranged below from bottom to top, structure is transplanted in discharging, described accurate pressure-keeping mechanism is connected with described material loading locating platform, described fuselage is also provided with main body supply assembly, be provided with weight above described main body supply assembly and control tension mechanism and material film peeling mechanism.
2. the backlight laminating machine of automatic Composition according to claim 1, is characterized in that: be also provided with PLC above described main body supply assembly and be arranged at the touch-screen in PLC.
3. the backlight laminating machine of automatic Composition according to claim 1, is characterized in that: described fuselage is also provided with carrying XZ axle linkage unit.
4. the backlight laminating machine of automatic Composition according to claim 3, it is characterized in that: described CCD image alignment system is at least four, wherein two are arranged at above described XY θ contraposition stacked wafer moudle, and two other is arranged at above described carrying XZ axle linkage unit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520045406.1U CN204524708U (en) | 2015-01-22 | 2015-01-22 | A kind of backlight laminating machine of automatic Composition |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520045406.1U CN204524708U (en) | 2015-01-22 | 2015-01-22 | A kind of backlight laminating machine of automatic Composition |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204524708U true CN204524708U (en) | 2015-08-05 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520045406.1U Active CN204524708U (en) | 2015-01-22 | 2015-01-22 | A kind of backlight laminating machine of automatic Composition |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204524708U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105116614A (en) * | 2015-09-28 | 2015-12-02 | 京东方光科技有限公司 | Assembling jig and method for backlight module |
-
2015
- 2015-01-22 CN CN201520045406.1U patent/CN204524708U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105116614A (en) * | 2015-09-28 | 2015-12-02 | 京东方光科技有限公司 | Assembling jig and method for backlight module |
| CN105116614B (en) * | 2015-09-28 | 2018-01-05 | 京东方光科技有限公司 | The assembled fixture and assemble method of a kind of backlight module |
| US10139084B2 (en) | 2015-09-28 | 2018-11-27 | Boe Technology Group Co., Ltd. | Assembly fixture and assembly method for backlight module |
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| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |