CN110112251A - A kind of welding of space solar battery module and positioning mold - Google Patents
A kind of welding of space solar battery module and positioning mold Download PDFInfo
- Publication number
- CN110112251A CN110112251A CN201910307853.2A CN201910307853A CN110112251A CN 110112251 A CN110112251 A CN 110112251A CN 201910307853 A CN201910307853 A CN 201910307853A CN 110112251 A CN110112251 A CN 110112251A
- Authority
- CN
- China
- Prior art keywords
- panel
- welding
- bottom plate
- battery module
- solar battery
- 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.)
- Granted
Links
- 238000003466 welding Methods 0.000 title claims abstract description 41
- 229920001971 elastomer Polymers 0.000 claims abstract description 11
- 208000020442 loss of weight Diseases 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims 2
- 229910045601 alloy Inorganic materials 0.000 claims 2
- 239000000463 material Substances 0.000 claims 1
- 238000000465 moulding Methods 0.000 claims 1
- 229910000838 Al alloy Inorganic materials 0.000 abstract 2
- 229910052751 metal Inorganic materials 0.000 abstract 2
- 239000002184 metal Substances 0.000 abstract 2
- 229910001220 stainless steel Inorganic materials 0.000 abstract 2
- 239000013013 elastic material Substances 0.000 abstract 1
- 238000000034 method Methods 0.000 description 6
- 239000000758 substrate Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 229920002379 silicone rubber Polymers 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L21/00—Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
- H01L21/67—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere
- H01L21/68—Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere for positioning, orientation or alignment
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/04—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof adapted as photovoltaic [PV] conversion devices
- H01L31/042—PV modules or arrays of single PV cells
- H01L31/048—Encapsulation of modules
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01L—SEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
- H01L31/00—Semiconductor devices sensitive to infrared radiation, light, electromagnetic radiation of shorter wavelength or corpuscular radiation and specially adapted either for the conversion of the energy of such radiation into electrical energy or for the control of electrical energy by such radiation; Processes or apparatus specially adapted for the manufacture or treatment thereof or of parts thereof; Details thereof
- H01L31/18—Processes or apparatus specially adapted for the manufacture or treatment of these devices or of parts thereof
- H01L31/1876—Particular processes or apparatus for batch treatment of the devices
- H01L31/188—Apparatus specially adapted for automatic interconnection of solar cells in a module
-
- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- General Physics & Mathematics (AREA)
- Condensed Matter Physics & Semiconductors (AREA)
- Computer Hardware Design (AREA)
- Physics & Mathematics (AREA)
- Power Engineering (AREA)
- Electromagnetism (AREA)
- Manufacturing & Machinery (AREA)
- Life Sciences & Earth Sciences (AREA)
- Sustainable Development (AREA)
- Sustainable Energy (AREA)
- Photovoltaic Devices (AREA)
Abstract
The present invention discloses welding and the positioning mold of a kind of space solar battery module, including panel, bottom plate, rubber pad are placed between panel and bottom plate, and panel, bottom plate, rubber pad are connected by screw to;Panel is unlikely to deform metal by hard such as aluminium alloy, stainless steels and is made, and has N item along the x axis continuously to lean on grid on the panel, mutually abutting has several apertures on the panel between grid;Bottom plate is unlikely to deform metal by hard such as aluminium alloy, stainless steels and is made, and has several hollow out positions on bottom plate;Rubber pad is made of elastic material, is placed among panel and bottom plate.The welding of space solar battery module proposed by the present invention and positioning mold, convenient welding, positioning accuracy is high, it can satisfy the requirement of engineering application, the position that the mold is capable of relative position and component connection sheet effectively to component each in solar battery module is accurately positioned, and can complete the welding of solar module and component connection sheet.
Description
Technical field
The present invention relates to space power system fields, and in particular to a kind of welding and positioning mould of space solar battery module
Tool.
Background technique
Space solar cell passes through silicon rubber and substrate sticking as unit of single go here and there, due to operating irreversibility, silicon rubber
The features such as glue waits curing time long, causes production efficiency low, need to improve to solar cell and substrate sticking process.
In view of the deficiencies of the prior art, can several solar modules and component connection sheet be welded and is positioned by module
Solar battery module is formed by welding in mold, forms the independent circuit module with electric current output, the sun electricity after completing
Pond module global transfer, whole cloth patch, is changed to integrate with module in a manner of the upper plate of modularity by traditional by solar cell
The mode of upper plate, the stickup with substrate is carried out as unit of solar battery module can greatly improve production efficiency, and increase patch
The reliability of piece.
Summary of the invention
The technical problems to be solved by the present invention are: providing a kind of mould for positioning and welding for space solar battery module
Tool, the position which is capable of relative position and component connection sheet effectively to component each in solar battery module carry out accurately fixed
Position, and the welding of solar module and component connection sheet can be completed.
In order to realize above-mentioned technical proposal, a kind of welding of space solar battery module of the invention and positioning mold,
Including panel, bottom plate, elastic cushion is placed between panel and bottom plate, and panel, bottom plate, elastic cushion are connected by screw to;
Source location set, welding of the source location set as the space solar battery module is arranged in the panel upper left corner
And the telltale mark point of positioning mold, the direction that mold is placed is judged by the source location set;
There is N item along the x axis continuously to lean on grid on panel, mutually abutting there are several apertures on the panel between grid;
There are several hollow out positions on bottom plate;
Hollow out through-hole is set above panel;
Component connection sheet set-down location is located above panel, arranges along the y axis, and component connection sheet set-down location and panel are whole
It is process;
U-typed slot position is above panel, and U-typed slot is by the welding of space solar battery module and positioning mold and welding
Equipment is fastenedly connected by screw;
Hollowed out area is located at the two sides up and down of bottom plate, and corresponding position engraves on the hollowed out area and panel on the upside of bottom plate
Empty region forms closed cavity, and loss of weight is played in the hollowed out area positioned at baseplate underside.
The advantages and positive effects of the present invention are:
1. installation is easy to operate, it is not necessarily to auxiliary tool.
2. solar battery module is easy to loading and unloading on this mold, handling short time consumption is short.
3. mold can directly with welding machine stage+module.
Detailed description of the invention
Fig. 1 is the welding of the space solar battery module of the embodiment of the present invention and the main view sectional view of positioning mold;
Fig. 2 is the welding of the space solar battery module of the embodiment of the present invention and the top view of positioning mold;
Fig. 3 is the welding of the space solar battery module of the embodiment of the present invention and the bottom view of positioning mold;
Fig. 4 is the welding of the space solar battery module of the embodiment of the present invention and the bottom plate use state of positioning mold
Figure.
Specific embodiment
Integrally positioned technical problem to be solved by the invention is to provide one kind for solar cell and component connection sheet and
The mold of welding, and realize engineer application.
For that can further appreciate that summary of the invention of the invention, feature and using effect, the following examples are hereby given, and cooperates
Detailed description are as follows for attached drawing:
A kind of welding of space solar battery module and positioning mold referring to FIG. 1 to FIG. 4, main view sectional view such as Fig. 1
It is shown, including panel 1, bottom plate 3, rubber pad 2 be placed between panel 1 and bottom plate 3, panel 1, bottom plate 3, rubber pad 2 pass through spiral shell
4 connection of nail, in which:
The panel 1 of rectangular configuration, top view is as shown in Figure 2;
Source location set 5 is located at 1 upper left corner of rectangular configuration panel, which is used as the space solar cell
The welding of module and the telltale mark point of positioning mold judge the direction that mold is placed by the source location set;
Hollow out through-hole 6 is located above rectangular configuration panel, and the diameter of hollow out through-hole 6 isThe hollow out
Through-hole 6 runs through panel 1, and the lower section of every solar cell has the hollow hole of same number, below every solar cell
The number of hollow hole is 4~20;
It is located above rectangular configuration panel by grid 7, should be linear along X-direction by grid 7, two should be able between grid 7
Solar cell is accommodated, has N item depending on grid 7, the quantity view paper of " N " along Y direction.It can be with 1 overall processing of panel by grid 7
It forms, can also individually process and then be combined with the assembly of panel 1, assembly precision need to meet design drawing requirement;
Component connection sheet set-down location 8 is located above rectangular configuration panel, arranges along the y axis, component connection sheet set-down location
It is formed with 1 overall processing of panel, also there is hollow out through-hole in component connection sheet set-down location, which runs through panel 1, hollow out through-hole
Diameter isAnd what hollow out through-hole avoided component connection sheet subtracts stress ring position;
U-typed slot 9 is located above rectangular configuration panel, and U-typed slot is by the welding and positioning of space solar battery module
Mold and welding equipment are fastenedly connected by screw.
Rubber pad 2, as shown in Figure 1;
Rubber pad 2 is placed between panel 1 and bottom plate 3, and several hollowed out areas and hollow hole, vacancy section are provided on rubber pad
The closed cavity that domain corresponding panel 1 and bottom plate 3 are formed, and being connect with gas-tpe fitting, hollow hole corresponding panel 1 and bottom plate 3
Attachment screw position, rubber pad 2 play sealing and buffer function.
Bottom plate 3, as shown in Figure 3 and Figure 4:
Hollowed out area 10 is located at the two sides up and down of bottom plate 3, the corresponding position on the hollowed out area of 3 upside of bottom plate and panel
Hollowed out area form closed cavity, loss of weight is played in the hollowed out area positioned at the downside of bottom plate 3;
Attachment screw 4 is located at the downside of bottom plate 3, so that panel 1, rubber pad 2, bottom plate 3 is formed rigidity by the connection of screw
Body.
The application method of this preferred embodiment includes the following steps:
A. the welding of the space solar battery module completed the process and positioning mold are located at face according to source location set
It is placed on welding equipment to operator upper left side, which is fastenedly connected using screw with welding equipment by U-typed slot;
B. will series connection complete solar cell series connection component by the back side upward in the way of, be placed on space along the x axis
With on the welding of solar battery module and positioning mold, solar cell series connection component take it is top keep left (along by grid) (along
Anchor point by component connection sheet) mode complete the positioning on mold;
C. component connection sheet is placed on component connection sheet placement region, contrast design drawing by the back side in the way of upward
Confirm it is errorless after, open admission air valve, complete fixation of the solar battery module on mold, be subjected to;
D. after the completion of welding, close admission air valve, by solar battery module from the welding of space solar battery module and
It is taken out on positioning mold.
Claims (8)
1. welding and the positioning mold of a kind of space solar battery module, which is characterized in that including panel, bottom plate, elastic cushion
It is placed between panel and bottom plate, panel, bottom plate, elastic cushion are connected by screw to;
The panel upper left corner is arranged source location set, and source location set is as the welding of the space solar battery module and fixed
The telltale mark point of position mould judges the direction that mold is placed by the source location set;
There is N item along the x axis continuously to lean on grid on panel, mutually abutting there are several apertures on the panel between grid;
There are several hollow out positions on bottom plate;
Hollow out through-hole is set above panel;
Component connection sheet set-down location is located above panel, arranges along the y axis, component connection sheet set-down location and panel overall processing
It forms;
U-typed slot position is above panel, and U-typed slot is by the welding of space solar battery module and positioning mold and welding equipment
It is fastenedly connected by screw;
Hollowed out area is located at the two sides up and down of bottom plate, and on the hollowed out area and panel on the upside of bottom plate the vacancy section of corresponding position
Domain forms closed cavity, and loss of weight is played in the hollowed out area positioned at baseplate underside.
2. welding and the positioning mold of a kind of space solar battery module as described in claim 1, which is characterized in that described
Panel is constituted using 2A12,1Cr18Ni9Ti hard alloy, has the N item along X-axis that grid and bottom plate is continuously leaned on to add using integrated molding
Work, or individually processed by grid, meet assembly precision requirement and bottom plate assembles.
3. welding and the positioning mold of a kind of space solar battery module as described in claim 1, which is characterized in that described
Panel uses rectangular configuration, and there are the region placed for component connection sheet in the two sides of panel, and have perforative aperture.
4. welding and the positioning mold of a kind of space solar battery module as described in claim 1, which is characterized in that described
There is the threaded hole for screw connection at the back side of panel.
5. welding and the positioning mold of a kind of space solar battery module as described in claim 1, which is characterized in that described
Bottom plate is constituted using 2A12,1Cr18Ni9Ti hard alloy, there is N number of hollowed out area along the y axis.
6. welding and the positioning mold of a kind of space solar battery module as described in claim 1, which is characterized in that described
Bottom plate has several screw thread mouths for screw connection.
7. welding and the positioning mold of a kind of space solar battery module as described in claim 1, which is characterized in that described
Elastic cushion is made of rubber material.
8. welding and the positioning mold of a kind of space solar battery module as described in claim 1, which is characterized in that described
There is hollow out through-hole in component connection sheet set-down location, which runs through panel, and the diameter of hollow out through-hole is
And what hollow out through-hole avoided component connection sheet subtracts stress ring position.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910307853.2A CN110112251B (en) | 2019-04-17 | 2019-04-17 | Welding and positioning die of solar cell module for space |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201910307853.2A CN110112251B (en) | 2019-04-17 | 2019-04-17 | Welding and positioning die of solar cell module for space |
Publications (2)
Publication Number | Publication Date |
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CN110112251A true CN110112251A (en) | 2019-08-09 |
CN110112251B CN110112251B (en) | 2021-01-12 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201910307853.2A Active CN110112251B (en) | 2019-04-17 | 2019-04-17 | Welding and positioning die of solar cell module for space |
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Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN202684408U (en) * | 2012-07-03 | 2013-01-23 | 湖南格润新能源有限公司 | Template for series welding of solar battery piece |
CN203242655U (en) * | 2013-03-29 | 2013-10-16 | 晶科能源有限公司 | Photovoltaic module laminated template |
CN204316884U (en) * | 2014-12-12 | 2015-05-06 | 天津电气科学研究院有限公司 | A kind of MOSFET weld mold |
CN205869655U (en) * | 2016-07-15 | 2017-01-11 | 苏州硕诺尔自动化设备有限公司 | Automatic welding position tool |
CN106328764A (en) * | 2016-08-30 | 2017-01-11 | 江阴鑫辉太阳能有限公司 | Semi-piece assembly stringing and laminating method |
CN208722909U (en) * | 2018-09-28 | 2019-04-09 | 英利能源(中国)有限公司 | The manual weld mold of battery strings |
-
2019
- 2019-04-17 CN CN201910307853.2A patent/CN110112251B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN202684408U (en) * | 2012-07-03 | 2013-01-23 | 湖南格润新能源有限公司 | Template for series welding of solar battery piece |
CN203242655U (en) * | 2013-03-29 | 2013-10-16 | 晶科能源有限公司 | Photovoltaic module laminated template |
CN204316884U (en) * | 2014-12-12 | 2015-05-06 | 天津电气科学研究院有限公司 | A kind of MOSFET weld mold |
CN205869655U (en) * | 2016-07-15 | 2017-01-11 | 苏州硕诺尔自动化设备有限公司 | Automatic welding position tool |
CN106328764A (en) * | 2016-08-30 | 2017-01-11 | 江阴鑫辉太阳能有限公司 | Semi-piece assembly stringing and laminating method |
CN208722909U (en) * | 2018-09-28 | 2019-04-09 | 英利能源(中国)有限公司 | The manual weld mold of battery strings |
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Publication number | Publication date |
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CN110112251B (en) | 2021-01-12 |
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