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 PDF

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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
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CN
China
Prior art keywords
panel
welding
bottom plate
battery module
solar battery
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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
Application number
CN201910307853.2A
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Chinese (zh)
Other versions
CN110112251B (en
Inventor
王凯
王志彬
陈萌炯
苏宝法
沈静曼
周近凝
孟晓丽
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Shanghai Institute of Space Power Sources
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Shanghai Institute of Space Power Sources
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Priority to CN201910307853.2A priority Critical patent/CN110112251B/en
Publication of CN110112251A publication Critical patent/CN110112251A/en
Application granted granted Critical
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    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/67Apparatus 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
    • H01L21/68Apparatus 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
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00Semiconductor 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
    • H01L31/04Semiconductor 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
    • H01L31/042PV modules or arrays of single PV cells
    • H01L31/048Encapsulation of modules
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L31/00Semiconductor 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
    • H01L31/18Processes or apparatus specially adapted for the manufacture or treatment of these devices or of parts thereof
    • H01L31/1876Particular processes or apparatus for batch treatment of the devices
    • H01L31/188Apparatus specially adapted for automatic interconnection of solar cells in a module
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/50Photovoltaic [PV] energy
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02PCLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P70/00Climate change mitigation technologies in the production process for final industrial or consumer products
    • Y02P70/50Manufacturing or production processes characterised by the final manufactured product

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  • 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

A kind of welding of space solar battery module and positioning mold
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.
CN201910307853.2A 2019-04-17 2019-04-17 Welding and positioning die of solar cell module for space Active CN110112251B (en)

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

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CN110112251A true CN110112251A (en) 2019-08-09
CN110112251B CN110112251B (en) 2021-01-12

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Citations (6)

* Cited by examiner, † Cited by third party
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

Patent Citations (6)

* Cited by examiner, † Cited by third party
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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