CN201918400U - Solar Thin Frame Module - Google Patents

Solar Thin Frame Module Download PDF

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Publication number
CN201918400U
CN201918400U CN2010206963541U CN201020696354U CN201918400U CN 201918400 U CN201918400 U CN 201918400U CN 2010206963541 U CN2010206963541 U CN 2010206963541U CN 201020696354 U CN201020696354 U CN 201020696354U CN 201918400 U CN201918400 U CN 201918400U
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CN
China
Prior art keywords
frame
component
strip
aluminum
edge strip
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.)
Expired - Fee Related
Application number
CN2010206963541U
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Chinese (zh)
Inventor
杨小双
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.)
Trina Solar Co Ltd
Original Assignee
Changzhou Trina Solar Energy Co Ltd
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Publication date
Application filed by Changzhou Trina Solar Energy Co Ltd filed Critical Changzhou Trina Solar Energy Co Ltd
Priority to CN2010206963541U priority Critical patent/CN201918400U/en
Application granted granted Critical
Publication of CN201918400U publication Critical patent/CN201918400U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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    • 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

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  • Photovoltaic Devices (AREA)

Abstract

The utility model relates to the technical field of photovoltaic component structures, in particular to a solar component with thin frames. The solar component with the thin frames comprises a longer frame in the component length direction and a shorter frame in the component width direction both made of aluminum, wherein upper edge strips, lower edge strips and bottom edge strips all for fixing the component are respectively arranged on the inner sides of the longer frame and the shorter frame; the upper edge strip and the lower edge strip form a groove for being connected with a battery laminated part in an embedded manner; a supporting strip for connecting the lower edge strip and the bottom edge strip is arranged between the lower edge strip and the bottom edge strip of the longer frame; a screw mounting hole is formed in a cavity on the inner side of the supporting strip; and opposite angles of the longer frame and the shorter frame are connected via screws. By adopting the design provided by the utility model, the original thickness of the component is thinned, the strength requirement on the aluminum frame is simultaneously guaranteed; the longer frame can bear larger pressure owing to a closed ring structure, and the aluminum profile can be conveniently processed and the aluminum material can be saved since the shorter frame adopts an open ring structure; and the opposite angles of the longer frame can be connected via the screws, so that the strength and the stability of the component are better.

Description

Solar energy featheredge frame assembly
Technical field
The utility model relates to the photovoltaic module structure technical field, particularly a kind of solar energy featheredge frame assembly.
Background technology
Solar energy be clean most, the energy of environmental protection, its energy is inexhaustible, the nexhaustible energy that clean energy resourcies such as water power, wind-powered electricity generation, nuclear power can't be compared, and solar energy also is the most possible optimal main alternative energy source of replacing traditional fossil energy in this century.In recent years, production of global solar photovoltaic module and application obtain development faster, expensive current solar energy popularization and application biggest obstacle and the key problem of remaining, especially the photovoltaic system of building with the crystal silicon assembly, cost of electricity-generating is 3-3.5 times of wind-powered electricity generation at present approximately, be thermoelectricity mark post valency 4-5 doubly, the expensive maximum bottleneck that becomes the solar energy popularization and application.Because the aluminium section bar price is also relatively more expensive, so reduce the use of aluminum, the production cost of saving the aluminium frame is a trend.
The utility model content
Technical problem to be solved in the utility model is: a kind of solar energy featheredge frame assembly is provided, when reducing seal ring thickness, can guarantees the requirement of strength of frame.
The technical scheme that its technical problem that solves the utility model adopts is: a kind of solar energy featheredge frame assembly, comprise the aluminum long margin frame of length component direction and the aluminum minor face frame of element width direction, long margin frame and minor face frame inboard have upper sid strip, the skirt rail that lower sid strip is fixing with being used for assembly, upper sid strip and lower sid strip constitute the scarfing slot of interlocking battery laminate, the support bar that connects lower sid strip and skirt rail is set between the lower sid strip of long margin frame and the skirt rail, the screw installing hole is set in the cavity of support bar inboard, and the place, diagonal angle of long margin frame and minor face frame adopts screw to be connected.Be the purpose of the thickness that reduces original assembly, but guarantee the requirement of strength of aluminium frame simultaneously again, satisfy the standard-required of IEC etc., bear wind and carry and test request such as snow load.The design long margin frame uses closed-loop structure, and long margin frame is generally the place that installs and fixes, and the pressure ratio of bearing is bigger, and closed-loop structure intensity is more eager to excel in whatever one does than open loop.The minor face frame uses open loop structure, makes things convenient for the processing of aluminium section bar like that, saves aluminum simultaneously.Use the diagonal angle screw to connect on long margin frame, the intensity of assembly and stability are relatively good like that.
The thickness of long margin frame and minor face frame is 39~42mm, is preferably 40mm.
The skirt rail of long margin frame is provided with leaking hole, location hole and ground hole.
The beneficial effects of the utility model are by the structure of design length frame, can reduce the thickness of aluminium frame when being implemented in proof strength, the use of minimizing aluminum, saving aluminium frame production cost.Reduce the thickness of aluminium frame, can also save assembly production and memory space, reduce the logistics freight, save the logistics cost of transportation.The design can not change original mounting means, and new product and old product can mix use, and be easy for installation.After the material of aluminium frame reduced, the weight of whole assembly also alleviated, the convenient installation.
Description of drawings
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is the structural representation of long margin frame of the present utility model.
Fig. 2 is the structural representation of minor face frame of the present utility model.
Fig. 3 is the structural representation at the assembly of the present utility model back side.
1. long margin frames among the figure, 2. minor face frame, 3. upper sid strip, 4. lower sid strip, 5. skirt rail, 6. battery laminate, 7. scarfing slot, 8. support bar, 9. screw installing hole, 10. leaking hole, 11. location holes, 12. ground holes.
Embodiment
As Fig. 1,2 and 3 described a kind of solar energy featheredge frame assemblies, the minor face frame 2 that comprises the aluminum of the long margin frame 1 of aluminum of length component direction and element width direction, long margin frame 1 and minor face frame 2 inboards have upper sid strip 3, the skirt rail 5 that lower sid strip 4 is fixing with being used for assembly, upper sid strip 3 and lower sid strip 4 constitute the scarfing slot 7 of interlocking battery laminate 6, the support bar 8 that connects lower sid strip 4 and skirt rail 5 is set between the lower sid strip 4 of long margin frame 1 and the skirt rail 5, screw installing hole 9 is set in the cavity of support bar 8 inboards, and the place, diagonal angle of long margin frame 1 and minor face frame 2 adopts screw to be connected.The thickness of long margin frame 1 and minor face frame 2 is 39~42mm, is preferably 40mm.
As shown in Figure 3, the skirt rail 2 of long margin frame 1 is provided with leaking hole 10, location hole 11 and ground hole 12.

Claims (4)

1.一种太阳能薄边框组件,包括组件长度方向的铝制的长边框(1)和组件宽度方向的铝制的短边框(2),其特征是:长边框(1)和短边框(2)内侧具有上边条(3)、下边条(4)和用于组件固定的底边条(5),上边条(3)和下边条(4)构成嵌接电池层压件(6)的嵌接槽(7),长边框(1)的下边条(4)和底边条(5)之间设置连接下边条(4)和底边条(5)的支撑条(8),在支撑条(8)内侧的空腔内设置螺丝安装孔(9),长边框(1)和短边框(2)的对角处采用螺丝连接。1. A solar thin frame assembly, comprising a long frame (1) made of aluminum in the component length direction and a short frame (2) made of aluminum in the width direction of the component, characterized in that: the long frame (1) and the short frame (2) ) has an upper side strip (3), a lower side strip (4) and a bottom side strip (5) for component fixing on the inner side, and the upper side strip (3) and the lower side strip (4) form the embedded part of the embedded battery laminate (6) Connect the groove (7), the support bar (8) that connects the lower bar (4) and the bottom bar (5) is set between the lower bar (4) and the bottom bar (5) of the long frame (1). (8) Screw mounting holes (9) are provided in the inner cavity, and the opposite corners of the long frame (1) and the short frame (2) are connected by screws. 2.根据权利要求1所述的太阳能薄边框组件,其特征是:所述的长边框(1)和短边框(2)的厚度为39~42mm。2. The solar thin frame module according to claim 1, characterized in that: the thickness of the long frame (1) and the short frame (2) is 39-42 mm. 3.根据权利要求2所述的太阳能薄边框组件,其特征是:所述的长边框(1)和短边框(2)的厚度为40mm。3. The solar thin frame assembly according to claim 2, characterized in that: the thickness of the long frame (1) and the short frame (2) is 40mm. 4.根据权利要求1所述的太阳能薄边框组件,其特征是:所述的长边框(1)的底边条(2)上设置有漏水孔(10)、定位孔(11)和接地孔(12)。4. The solar thin frame assembly according to claim 1, characterized in that: the bottom edge strip (2) of the long frame (1) is provided with leaking holes (10), positioning holes (11) and grounding holes (12).
CN2010206963541U 2010-12-31 2010-12-31 Solar Thin Frame Module Expired - Fee Related CN201918400U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2010206963541U CN201918400U (en) 2010-12-31 2010-12-31 Solar Thin Frame Module

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2010206963541U CN201918400U (en) 2010-12-31 2010-12-31 Solar Thin Frame Module

Publications (1)

Publication Number Publication Date
CN201918400U true CN201918400U (en) 2011-08-03

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Family Applications (1)

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CN2010206963541U Expired - Fee Related CN201918400U (en) 2010-12-31 2010-12-31 Solar Thin Frame Module

Country Status (1)

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CN (1) CN201918400U (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102610681A (en) * 2012-03-30 2012-07-25 江苏明昊新材料科技有限公司 Frame of solar photovoltaic module
EP2579327A3 (en) * 2011-10-07 2014-05-14 Hulk Energy Technology Co., Ltd. Frame structure for solar cell module
WO2014075569A1 (en) * 2012-11-15 2014-05-22 Sun Tao Photovoltaic assembly integration plate
CN107331642A (en) * 2017-07-18 2017-11-07 杭州萧山江海实业有限公司 A kind of automatic production line for producing solar components long margin frame
CN109724784A (en) * 2018-12-28 2019-05-07 广东大粤新能源科技股份有限公司 Method for testing tensile resistance of threads of photovoltaic panel mounting structure
CN118137954A (en) * 2024-04-15 2024-06-04 天合光能股份有限公司 Frame structure and photovoltaic system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2579327A3 (en) * 2011-10-07 2014-05-14 Hulk Energy Technology Co., Ltd. Frame structure for solar cell module
CN102610681A (en) * 2012-03-30 2012-07-25 江苏明昊新材料科技有限公司 Frame of solar photovoltaic module
CN102610681B (en) * 2012-03-30 2014-03-05 江苏明昊新材料科技有限公司 Frame of solar photovoltaic module
WO2014075569A1 (en) * 2012-11-15 2014-05-22 Sun Tao Photovoltaic assembly integration plate
CN107331642A (en) * 2017-07-18 2017-11-07 杭州萧山江海实业有限公司 A kind of automatic production line for producing solar components long margin frame
CN109724784A (en) * 2018-12-28 2019-05-07 广东大粤新能源科技股份有限公司 Method for testing tensile resistance of threads of photovoltaic panel mounting structure
CN118137954A (en) * 2024-04-15 2024-06-04 天合光能股份有限公司 Frame structure and photovoltaic system

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: Solar photovoltaic industry park Tianhe Road 213031 north of Jiangsu Province, Changzhou City, No. 2

Patentee after: TRINASOLAR Co.,Ltd.

Address before: Solar photovoltaic industry park Tianhe Road 213031 north of Jiangsu Province, Changzhou City, No. 2

Patentee before: trina solar Ltd.

CP03 Change of name, title or address
CP03 Change of name, title or address

Address after: Solar photovoltaic industry park Tianhe Road 213031 north of Jiangsu Province, Changzhou City, No. 2

Patentee after: trina solar Ltd.

Address before: 213031, No. 2, Tianhe Road, Xinbei Industrial Park, Jiangsu, Changzhou

Patentee before: CHANGZHOU TRINA SOLAR ENERGY Co.,Ltd.

CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110803

Termination date: 20181231