CN203172117U - Automatic prepressing and aligning system - Google Patents

Automatic prepressing and aligning system Download PDF

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Publication number
CN203172117U
CN203172117U CN 201320035466 CN201320035466U CN203172117U CN 203172117 U CN203172117 U CN 203172117U CN 201320035466 CN201320035466 CN 201320035466 CN 201320035466 U CN201320035466 U CN 201320035466U CN 203172117 U CN203172117 U CN 203172117U
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CN
China
Prior art keywords
automatic
servo
prepressing
alignment
fpc
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Expired - Lifetime
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CN 201320035466
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Chinese (zh)
Inventor
施忠清
郭付伟
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.)
Fair Shenzhen Silver Science And Technology Ltd
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Fair Shenzhen Silver Science And Technology Ltd
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Priority to CN 201320035466 priority Critical patent/CN203172117U/en
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Abstract

The utility model provides an automatic prepressing and aligning system. The automatic prepressing and aligning system comprises a machine frame, and further comprises a machine body, a support, a servo conveying system, a three-shaft aligning system, a servo lifting system, a prepressing system, an FPC (flexible printed circuit) placing platform and a glass placing platform, wherein the machine body is connected with the machine frame and is positioned above the machine frame; the support is placed on the bottom surface of the machine body; the three-shaft aligning system is connected with the servo conveying system and is positioned above the servo conveying system; both the FPC placing platform and the glass placing platform are positioned above the three-shaft aligning system; and both the prepressing system and the servo lifting system are positioned behind the three-shaft aligning system. Compared with the prior art, the automatic prepressing and aligning system has the advantages as follows: automatic alignment and automatic prepressing in the whole process are achieved; alignment precision and working efficiency are improved; and the qualification rate and the productivity are greatly improved.

Description

A kind of automatic precompressed alignment system
Technical field
The utility model relates to a kind of OGS(one chip contact panel) automatic contraposition preformer, refer in particular to the pre-pressing system of automatic contraposition that adopts on this equipment.
Background technology
Present common OGS(one chip contact panel) pre-pressing process adopts the manual contraposition mode of manufacture of manually-operated, has following problem: 1, manually-operated fully, and the batch jobs fatiguability, the contraposition difficulty is big, and the mode of production is more backward; 2, the contraposition of OGS product requires height, and the manual contraposition efficient of printing opacity screen glass is low especially at being difficult for, and easily makes mistakes, and can't satisfy production requirement; 3, OGS manually presses to each explained hereafter bottleneck in advance.
The utility model content
In view of the foregoing, the purpose of this utility model is to provide a kind of automatic precompressed alignment system for glass and FPC, replaces artificial contraposition and precompressed, and it is bad to reduce the glass scuffing, has improved operating efficiency.
For achieving the above object, solution of the present utility model is:
A kind of automatic precompressed alignment system, comprise frame, also comprise fuselage, support, servo feed system, three alignment systems, servo jacking system, pre-pressing system, FPC placement platform and glass placement platforms, described fuselage is connected with frame and is positioned at the frame top, and support is positioned on the bottom surface of fuselage; Three alignment systems are connected with servo feed system and are positioned at servo feed system top; FPC placement platform and glass placement platform all are positioned at three alignment system tops; Pre-pressing system and servo jacking system all are positioned at the rear of three alignment systems.
Also further comprise installing plate, described installing plate is located on the bottom surface of fuselage, and servo feed system is fixedly arranged on this installing plate.
On fuselage, also be provided with the CCD camera system.
The utility model beneficial effect: FPC and glass are placed in corresponding FPC placement platform and the glass placement platform; By the feeding servo-drive system with FPC deliver to pre-pressing system under, i.e. position a, the adsorbent equipment on the pre-pressing system picks up FPC; The feeding servo-drive system is delivered to glass b place, position again, gather the contraposition information of FPC and glass afterwards respectively with high-accuracy CCD camera system, and send image information to vision system, three automatic contrapositions of alignment system of control after the vision system analysis, by the feeding servo-drive system glass is delivered to c(precompressed position, position at last) carry out precompressed, whole process is compared with prior art, automatic contraposition, the precompressed automatically of whole process have been realized, improve aligning accuracy and operating efficiency, promoted yield and production capacity greatly.
Description of drawings
Fig. 1 looks schematic diagram for master of the present utility model;
Fig. 2 looks schematic diagram for a left side of the present utility model;
Fig. 3 is schematic perspective view of the present utility model;
Fig. 4 is precompressed alignment system schematic diagram of the present utility model.
The specific embodiment
In order to make those skilled in the art person understand this New Scheme better, below in conjunction with drawings and embodiments to this novel being described in further detail.
Shown in Fig. 1-4, a kind of automatic precompressed alignment system comprises frame 1, also comprises fuselage 2, support 3, servo feed system 4, three alignment systems 5, servo jacking system 6, pre-pressing system 7, FPC placement platform 8 and glass placement platforms 9.
Also further comprise installing plate 10, described installing plate 10 is located on the bottom surface of fuselage 2, and servo feed system 4 is fixedly arranged on this installing plate 10.
Described fuselage 2 is connected with frame 1 and is positioned at frame 1 top, and support 3 is positioned on the bottom surface of fuselage 2; Three alignment systems 5 are connected with servo feed system 4 and are positioned at servo feed system 4 tops; FPC placement platform 8 and glass placement platform 9 all are positioned at three alignment system 5 tops; Pre-pressing system 7 and servo jacking system 6 all are positioned at the rear of three alignment systems 5.
Also comprise the CCD camera system of being located on the fuselage 2.
The utility model workflow: 1, glass and FPC are placed on corresponding FPC respectively and place flat
In platform 8 and the glass placement platform 9; 2, the vacuum absorption device that starts pre-pressing system 7 is fixed product; 3, servo feed system 4 is delivered to the CCD camera system a place, position of taking pictures automatically with glass and FPC, as shown in Figure 4; 4,8 times general who has surrendered FPC of servo jacking system pick up; 5, servo feed system 4 withdraws from glass is delivered to the CCD camera system b place, position of taking pictures, as shown in Figure 4; 6, vision CCD system carries out image acquisition and processing at position a and position b place to FPC and glass respectively; 7, alignment system calculates U/V/ θ skew, drives three alignment systems and compensates the rectification contraposition; 8, finish the location after, pre-pressing system 7 presses together FPC and glass.
Though described the utility model creation by embodiment, those of ordinary skills know, the utility model has many distortion and variation and does not break away from spirit of the present utility model, wishes that appended claim comprises these distortion and variation and do not break away from spirit of the present utility model.

Claims (3)

1. automatic precompressed alignment system, comprise frame, it is characterized in that, also comprise fuselage, support, servo feed system, three alignment systems, servo jacking system, pre-pressing system, FPC placement platform and glass placement platforms, described fuselage is connected with frame and is positioned at the frame top, and support is positioned on the bottom surface of fuselage; Three alignment systems are connected with servo feed system and are positioned at servo feed system top; FPC placement platform and glass placement platform all are positioned at three alignment system tops; Pre-pressing system and servo jacking system all are positioned at the rear of three alignment systems.
2. a kind of automatic precompressed alignment system as claimed in claim 1 is characterized in that, comprises further that also installing plate, described installing plate be located on the bottom surface of fuselage, and servo feed system is fixedly arranged on this installing plate.
3. a kind of automatic precompressed alignment system as claimed in claim 1 is characterized in that, also is provided with the CCD camera system on fuselage.
CN 201320035466 2013-01-23 2013-01-23 Automatic prepressing and aligning system Expired - Lifetime CN203172117U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201320035466 CN203172117U (en) 2013-01-23 2013-01-23 Automatic prepressing and aligning system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201320035466 CN203172117U (en) 2013-01-23 2013-01-23 Automatic prepressing and aligning system

Publications (1)

Publication Number Publication Date
CN203172117U true CN203172117U (en) 2013-09-04

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201320035466 Expired - Lifetime CN203172117U (en) 2013-01-23 2013-01-23 Automatic prepressing and aligning system

Country Status (1)

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CN (1) CN203172117U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103640311A (en) * 2013-11-15 2014-03-19 南京沃联科技有限公司 Vacuum-adsorption semi-automatic three-shaft assembled press-fitting machine
CN105334449A (en) * 2015-11-16 2016-02-17 珠海市博杰电子有限公司 High-precision automatic alignment ICT (In Circuit Tester)
CN105911958A (en) * 2016-05-27 2016-08-31 惠州旭鑫精密自动化设备有限公司 Screen connector ultra-precision intelligent alignment system

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103640311A (en) * 2013-11-15 2014-03-19 南京沃联科技有限公司 Vacuum-adsorption semi-automatic three-shaft assembled press-fitting machine
CN105334449A (en) * 2015-11-16 2016-02-17 珠海市博杰电子有限公司 High-precision automatic alignment ICT (In Circuit Tester)
CN105334449B (en) * 2015-11-16 2019-03-01 珠海博杰电子股份有限公司 A kind of High Precision Automatic contraposition ICT test machine
CN105911958A (en) * 2016-05-27 2016-08-31 惠州旭鑫精密自动化设备有限公司 Screen connector ultra-precision intelligent alignment system

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Granted publication date: 20130904