CN102162487A - Universal joint structure of solar laminating machine - Google Patents
Universal joint structure of solar laminating machine Download PDFInfo
- Publication number
- CN102162487A CN102162487A CN2011100524408A CN201110052440A CN102162487A CN 102162487 A CN102162487 A CN 102162487A CN 2011100524408 A CN2011100524408 A CN 2011100524408A CN 201110052440 A CN201110052440 A CN 201110052440A CN 102162487 A CN102162487 A CN 102162487A
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- CN
- China
- Prior art keywords
- rotating shaft
- connected element
- laminating machine
- laminater
- universal joint
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
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- Photovoltaic Devices (AREA)
Abstract
The invention discloses a universal joint structure of a solar laminating machine. The structure comprises an input joint, an output joint and a connecting component, wherein the input joint and the output joint are articulated through a first rotary shaft; the output joint and the connecting component are rotationally connected through a second rotary shaft; and the shaft axis of the first rotary shaft and the shaft axis of the second rotary shaft are vertical. The universal joint structure provided by the invention has the advantages of simple structure, good operation flexibility, solves the defects of great volume of a connector, complex structure, poor flexibility when the universal joint structure is installed on the solar laminating machine, thus the occurrence of stuck of the box body, damage of the screw thread and the like during the open and close of the laminating machine is avoided, and the rise and fall of the box body on the laminating machine are more flexible and free.
Description
Technical field
The invention belongs to a kind of connector, relate in particular to a kind of universal joint that is used on the laminater.
Background technique
Be installed at present that the connector volume that is used to connect upper box and lower box on the solar energy layer press is big, complex structure, very flexible, in case deflection takes place in upper box in process of rising or falling, the restraining force of connector produces very big torsion at connecting plate, causes connecting plate to produce to damage, upper box is stuck or the connecting screw damage.Though disclose flexibility ratio universal joint preferably on the existing market, majority belongs to curved grooved type or Rzeppa type structure, is unsuitable for using on laminater.
Summary of the invention
Problem to be solved by this invention just provides a kind of solar energy layer press gimbal structure, has characteristics simple in structure, reasonable in design, that operating flexibility is good, the appearance of situation such as casing is stuck in the time of can effectively avoiding laminater folding case.
For solving the problems of the technologies described above, the present invention adopts following technological scheme: a kind of solar energy layer press gimbal structure, it is characterized in that: comprise input adapter, out splice going splice and connected element, input adapter and out splice going splice are hinged by first rotating shaft, and out splice going splice and connected element are rotationally connected by second rotating shaft; The shaft axis of the shaft axis of described first rotating shaft and second rotating shaft is mutual plumbness.
Further, described out splice going splice is provided with the axis hole equipped with second rotating shaft, one end, and described connected element is provided with the attachment hole equipped with the second rotating shaft the other end, and attachment hole is provided with the positioning screwn that tightens up second rotating shaft.Be convenient to dismounting, and can the time prevent that second rotating shaft from deviating from connected element in work.
Further, this universal joint is used for laminater, and described connected element is fixed on the upper box of laminater, and described input adapter connects the lift cylinder that is located at laminater lower box sidepiece.
Further, adopt Spielpassung between described second rotating shaft and the axis hole, leave mobile space between out splice going splice and the connected element.Be convenient to the laminater upper box and in lifting process, adjust position, the left and right sides.
Beneficial effect of the present invention: gimbal structure provided by the present invention is simple, and operating flexibility is good; It is installed on the solar energy layer press, solved that connector volume on the existing solar energy layer press is big, the shortcoming of complex structure, very flexible, thereby the appearance of situations such as casing is stuck when having avoided laminater opening and closing case, screw damage, the lifting of laminater upper box more flexibly, freely.
Description of drawings
The present invention is described further below in conjunction with accompanying drawing:
Fig. 1 is the structural representation of universal joint of the present invention:
Fig. 2 is the A-A sectional view of Fig. 1;
Fig. 3 is a scheme of installation of the present invention;
Fig. 4 is user mode figure one of the present invention;
Fig. 5 is user mode figure two of the present invention;
Embodiment
With reference to Fig. 1,2, the present invention is a kind of solar energy layer press gimbal structure, comprise input adapter 1, out splice going splice 2 and connected element 3, input adapter 1 is hinged by first rotating shaft 4 with out splice going splice 2, and out splice going splice 2 is rotationally connected by second rotating shaft 5 with connected element 3; The shaft axis of the shaft axis of first rotating shaft 4 and second rotating shaft 5 is mutual plumbness.Out splice going splice 2 is provided with the axis hole 21 equipped with second rotating shaft, 5 one ends, on connected element 3, be provided with the attachment hole 31 equipped with second rotating shaft, 5 the other ends, attachment hole 31 is provided with the positioning screwn 32 that tightens up second rotating shaft 5, be convenient to dismounting like this, and can the time prevent that second rotating shaft 5 from deviating from connected element 3 in work.
With reference to Fig. 3, this useful application is on laminater the time, connected element 3 is fixed on the upper box 6 of laminater, input adapter 1 is connected with the lift cylinder 8 that is located at laminater lower box 7 sidepieces, adopt Spielpassung between second rotating shaft 5 and the axis hole 21, leave mobile space 9 between out splice going splice 2 and the connected element 3, be convenient to laminater upper box 6 and in lifting process, adjust position, the left and right sides.Be illustrated as profile, during as installed, two universal joints respectively arranged on the two sides, front and back of laminater.
Claims (4)
1. solar energy layer press gimbal structure, it is characterized in that: comprise input adapter (1), out splice going splice (2) and connected element (3), input adapter (1) is hinged by first rotating shaft (4) with out splice going splice (2), and out splice going splice (2) is rotationally connected by second rotating shaft (5) with connected element (3); The shaft axis of the shaft axis of described first rotating shaft (4) and second rotating shaft (5) is mutual plumbness.
2. a kind of solar energy layer press gimbal structure according to claim 1, it is characterized in that: described out splice going splice (2) is provided with the axis hole (21) equipped with second rotating shaft (5) one ends, described connected element (3) is provided with the attachment hole (31) equipped with second rotating shaft (5) the other end, and attachment hole (31) is provided with the positioning screwn (32) that tightens up second rotating shaft (5).
3. a kind of solar energy layer press gimbal structure according to claim 2, it is characterized in that: this universal joint is used for laminater, described connected element (3) is fixed on the upper box (6) of laminater, and described input adapter (1) connects the lift cylinder (8) that is located at laminater lower box (7) sidepiece.
4. a kind of solar energy layer press gimbal structure according to claim 3 is characterized in that: adopt Spielpassung between described second rotating shaft (5) and the axis hole (21), leave mobile space (9) between out splice going splice (2) and the connected element (3).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011100524408A CN102162487A (en) | 2011-03-04 | 2011-03-04 | Universal joint structure of solar laminating machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011100524408A CN102162487A (en) | 2011-03-04 | 2011-03-04 | Universal joint structure of solar laminating machine |
Publications (1)
Publication Number | Publication Date |
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CN102162487A true CN102162487A (en) | 2011-08-24 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2011100524408A Pending CN102162487A (en) | 2011-03-04 | 2011-03-04 | Universal joint structure of solar laminating machine |
Country Status (1)
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CN (1) | CN102162487A (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6478500B1 (en) * | 2000-03-20 | 2002-11-12 | Ptm Equipment Inc. | Hyperextending joint |
US20040258460A1 (en) * | 2003-06-20 | 2004-12-23 | Taylor Steve B. | Coupler |
CN201240415Y (en) * | 2008-06-03 | 2009-05-20 | 福田雷沃国际重工股份有限公司 | Angle adjustable steering column |
CN201745231U (en) * | 2010-05-28 | 2011-02-16 | 常州佳讯光电系统工程有限公司 | Solar cell laminating machine |
CN201973080U (en) * | 2011-03-04 | 2011-09-14 | 浙江长兴亚金机械有限公司 | Universal joint structure for solar laminating machine |
-
2011
- 2011-03-04 CN CN2011100524408A patent/CN102162487A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6478500B1 (en) * | 2000-03-20 | 2002-11-12 | Ptm Equipment Inc. | Hyperextending joint |
US20040258460A1 (en) * | 2003-06-20 | 2004-12-23 | Taylor Steve B. | Coupler |
CN201240415Y (en) * | 2008-06-03 | 2009-05-20 | 福田雷沃国际重工股份有限公司 | Angle adjustable steering column |
CN201745231U (en) * | 2010-05-28 | 2011-02-16 | 常州佳讯光电系统工程有限公司 | Solar cell laminating machine |
CN201973080U (en) * | 2011-03-04 | 2011-09-14 | 浙江长兴亚金机械有限公司 | Universal joint structure for solar laminating machine |
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Application publication date: 20110824 |