CN102769054A - High-firmness connecting structure for solar frame component - Google Patents

High-firmness connecting structure for solar frame component Download PDF

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Publication number
CN102769054A
CN102769054A CN2012102541864A CN201210254186A CN102769054A CN 102769054 A CN102769054 A CN 102769054A CN 2012102541864 A CN2012102541864 A CN 2012102541864A CN 201210254186 A CN201210254186 A CN 201210254186A CN 102769054 A CN102769054 A CN 102769054A
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CN
China
Prior art keywords
frame
minor
long margin
groove
raised line
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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
CN2012102541864A
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Chinese (zh)
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CN102769054B (en
Inventor
吴莉莉
徐业进
查超麟
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.)
Jiangsu Akcome Solar Science & Technology Co Ltd
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Jiangsu Akcome Solar Science & Technology Co Ltd
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Priority to CN201210254186.4A priority Critical patent/CN102769054B/en
Publication of CN102769054A publication Critical patent/CN102769054A/en
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Publication of CN102769054B publication Critical patent/CN102769054B/en
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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

Abstract

The invention relates to a high-firmness connecting structure for a solar frame component. The high-firmness connecting structure comprises a long frame (1), a short frame (2) and a corner (3), wherein an extension section (14) of a vertical section of the long frame (1) is inserted into a vertical abdominal cavity (32) of one corner wing of the corner (3); and an extension section (24) of a vertical section of the short frame (2) and an extension section (25) of a transverse section of the short frame are respectively inserted into a vertical abdominal cavity (32) and a transverse abdominal cavity (33) of the other corner wing of the corner (3). Because a long frame raised line and a short frame raised line are embedded into clamping grooves of the corner wings, so that the long frame, the short frame and the corner are firmly matched with one another, and the connecting structure for the solar frame component has the advantages of convenience in connection and high firmness.

Description

A kind of syndeton of firmness higher solar energy frame assembly
Technical field
The present invention relates to a kind of syndeton of solar energy frame assembly, relate in particular to a kind of syndeton of firmness higher solar energy frame assembly, belong to technical field of solar.
Background technology
Solar panel is the core in the solar power system, also is to be worth the highest part in the solar power system.Its effect is that the radianting capacity with the sun converts electric energy into, or is sent in the storage battery and stores, or promotes loaded work piece.Solar panel is installed in the solar energy frame assembly; Solar energy frame assembly comprises two long margin frames and two minor face frames of rectangular arrangement; Perhaps connect continuous through bolt is directly continuous between traditional long margin frame and the minor face frame through the angle intersymbol; The directly continuous firmness of bolt is relatively poor and connect comparatively complicacy, comparatively makes things convenient for firmness relatively poor though the angle intersymbol connects to link to each other to connect.
Summary of the invention
The objective of the invention is to overcome above-mentioned deficiency, the syndeton of the comparatively convenient and firmness higher solar energy frame assembly of a kind of connection is provided.
The objective of the invention is to realize like this:
A kind of syndeton of firmness higher solar energy frame assembly, it comprises long margin frame, minor face frame and angle sign indicating number;
The cross section of said long margin frame comprises a long margin frame C type draw-in groove; The below of said long margin frame C type draw-in groove is provided with the perpendicular section of long margin frame; The bottom of the perpendicular section of said long margin frame is connected with the long margin frame crosspiece; The perpendicular section of said long margin frame is extended with the perpendicular section of long margin frame extension along the length direction of long margin frame, and a side of the perpendicular section of said long margin frame extension is provided with the long margin frame raised line, and the protrusion direction of said long margin frame raised line is consistent with the opening direction of long margin frame C type draw-in groove;
The cross section of said minor face frame comprises a minor face frame C type draw-in groove; The below of said minor face frame C type draw-in groove is provided with the perpendicular section of minor face frame; The bottom of the perpendicular section of said minor face frame is connected with minor face frame crosspiece; The perpendicular section of said minor face frame and minor face frame crosspiece are extended with perpendicular section extension of minor face frame and minor face frame crosspiece extension along the length direction of minor face frame; One side of the perpendicular section of said minor face frame extension is provided with minor face frame raised line, and the protrusion direction of said minor face frame raised line is consistent with the opening direction of minor face frame C type draw-in groove;
Said angle sign indicating number comprises two angle sign indicating number wings; The cross section of the said angle sign indicating number wing comprises one to the angle of inner opening sign indicating number wing C type draw-in groove; The below of said angle sign indicating number wing C type draw-in groove is provided with vertical abdominal cavity; The bottom in said vertical abdominal cavity is provided with inside horizontal abdominal cavity, and the madial wall in said vertical abdominal cavity is provided with draw-in groove;
Insert in the vertical abdominal cavity of an angle of sign indicating number, the angle sign indicating number wing the perpendicular section of the long margin frame of said long margin frame extension; Insert respectively in the vertical abdominal cavity and horizontal abdominal cavity of another angle sign indicating number wing of angle sign indicating number the minor face frame of said minor face frame perpendicular section extension and minor face frame crosspiece extension, and the opening direction of said long margin frame C type draw-in groove and minor face frame C type draw-in groove is consistent with the opening direction of angle sign indicating number wing C type draw-in groove.
As a kind of preferred, the number of said draw-in groove is a plurality of, said draw-in groove transverse arrangement of turbo, and the number of said long margin frame raised line and minor face frame raised line is identical with the number of draw-in groove, said long margin frame raised line and minor face frame raised line transverse arrangement of turbo.
As a kind of preferred, the number of said draw-in groove is a plurality of, said draw-in groove transverse arrangement of turbo, and the number of said long margin frame raised line and minor face frame raised line is identical with the number of draw-in groove, and said long margin frame raised line and minor face frame raised line are vertically arranged.
Compared with prior art, the invention has the beneficial effects as follows:
The present invention is because in the vertical abdominal cavity of an angle sign indicating number wing of the perpendicular section of long margin frame extension insertion; Insert respectively in the vertical abdominal cavity and horizontal abdominal cavity of another angle sign indicating number wing minor face frame perpendicular section extension and minor face frame crosspiece extension; Long margin frame raised line and minor face frame raised line embed in the draw-in groove of the angle sign indicating number wing; Make long margin frame, minor face frame all cooperate firmly with the angle sign indicating number, the syndeton of this solar energy frame assembly has the comparatively convenient and firmness advantage of higher of connection.
Description of drawings
Fig. 1 is the structural representation of the syndeton of firmness higher solar energy frame assembly of the present invention.
Fig. 2 is the explosive view of Fig. 1.
Fig. 3 is the long margin frame stereogram of the syndeton of firmness higher solar energy frame assembly of the present invention.
Fig. 4 is the A place partial enlarged drawing of Fig. 3.
Fig. 5 is the long margin frame cross-sectional view of the syndeton of firmness higher solar energy frame assembly of the present invention.
Fig. 6 is the minor face frame stereogram of the syndeton of firmness higher solar energy frame assembly of the present invention.
Fig. 7 is the B place partial enlarged drawing of Fig. 6.
Fig. 8 is the minor face frame cross-sectional view of the syndeton of firmness higher solar energy frame assembly of the present invention.
Fig. 9 is the stereogram of the angle sign indicating number of the syndeton of firmness higher solar energy frame assembly of the present invention.
Figure 10 is the structural representation of the embodiment of the invention one.
Figure 11 is the structural representation of the embodiment of the invention two.
Wherein:
Long margin frame 1, long margin frame C type draw-in groove 11, perpendicular section 12 of long margin frame, long margin frame crosspiece 13, the perpendicular section of a long margin frame extension 14, long margin frame raised line 15
Minor face frame 2, minor face frame C type draw-in groove 21, perpendicular section 22 of minor face frame, minor face frame crosspiece 23, the perpendicular section of a minor face frame extension 24, minor face frame crosspiece extension 25, minor face frame raised line 26
Angle sign indicating number 3, angle sign indicating number wing C type draw-in groove 31, vertical abdominal cavity 32, horizontal abdominal cavity 33, draw-in groove 34.
Embodiment
Referring to Fig. 1 ~ Fig. 9, the syndeton of a kind of firmness higher solar energy frame assembly that the present invention relates to, it comprises long margin frame 1, minor face frame 2 and angle sign indicating number 3;
The cross section of said long margin frame 1 comprises a long margin frame C type draw-in groove 11; The below of said long margin frame C type draw-in groove 11 is provided with the perpendicular section 12 of long margin frame; The bottom of the perpendicular section 12 of said long margin frame is connected with long margin frame crosspiece 13; The perpendicular section of said long margin frame 12 length directions along long margin frame 1 are extended with the perpendicular section of long margin frame extension 14, and a side of the perpendicular section of said long margin frame extension 14 is provided with long margin frame raised line 15, and the protrusion direction of said long margin frame raised line 15 is consistent with the opening direction of long margin frame C type draw-in groove 11;
The cross section of said minor face frame 2 comprises a minor face frame C type draw-in groove 21; The below of said minor face frame C type draw-in groove 21 is provided with the perpendicular section 22 of minor face frame; The bottom of the perpendicular section 22 of said minor face frame is connected with minor face frame crosspiece 23; The perpendicular section 22 of said minor face frame is extended with minor face frame perpendicular section extension 24 and minor face frame crosspiece extension 25 with minor face frame crosspiece 23 length directions along minor face frame 2; One side of the perpendicular section of said minor face frame extension 24 is provided with minor face frame raised line 26, and the protrusion direction of said minor face frame raised line 26 is consistent with the opening direction of minor face frame C type draw-in groove 21;
Said angle sign indicating number 3 comprises two angle sign indicating number wings; The cross section of the said angle sign indicating number wing comprises one to the angle of inner opening sign indicating number wing C type draw-in groove 31; The below of said angle sign indicating number wing C type draw-in groove 31 is provided with vertical abdominal cavity 32; The bottom in said vertical abdominal cavity 32 is provided with inside horizontal abdominal cavity 33, and the madial wall in said vertical abdominal cavity 32 is provided with draw-in groove 34;
In the vertical abdominal cavity 32 of the perpendicular section of the long margin frame of said long margin frame 13 one angles of sign indicating number, 14 insertion angle, extension sign indicating number wing; Insert respectively in the vertical abdominal cavity 32 and horizontal abdominal cavity 33 of angle sign indicating number 3 another angle sign indicating number wings with minor face frame crosspiece extension 25 the perpendicular section of the minor face frame of said minor face frame 2 extension 24; The opening direction of said long margin frame C type draw-in groove 11 and minor face frame C type draw-in groove 21 is consistent with the opening direction of angle sign indicating number wing C type draw-in groove 31, and said long margin frame raised line 15 embeds in the draw-in groove 34 with minor face frame raised line 26.
Embodiment 1, shown in figure 10; Said long margin frame raised line 15 is provided with two with minor face frame raised line 26; Said two long margin frame raised lines 15 and minor face frame raised line 26 be transverse arrangement of turbo up and down all, and the position of said draw-in groove 34 is corresponding with the position of minor face frame raised line 26 with long margin frame raised line 15.
Embodiment 2, shown in figure 11; Said long margin frame raised line 15 is provided with two with minor face frame raised line 26; Said two long margin frame raised lines 15 all arrange that vertically the position of said draw-in groove 34 is corresponding with the position of minor face frame raised line 26 with long margin frame raised line 15 in front and back with minor face frame raised line 26.

Claims (3)

1. the syndeton of a firmness higher solar energy frame assembly, it comprises long margin frame (1), minor face frame (2) and angle sign indicating number (3);
The cross section that it is characterized in that said long margin frame (1) comprises a long margin frame C type draw-in groove (11); The below of said long margin frame C type draw-in groove (11) is provided with the perpendicular section of long margin frame (12); The bottom of the perpendicular section of said long margin frame (12) is connected with long margin frame crosspiece (13); The perpendicular section of said long margin frame (12) is extended with the perpendicular section of long margin frame extension (14) along the length direction of long margin frame (1); One side of said long margin frame perpendicular section extension (14) is provided with long margin frame raised line (15), and the protrusion direction of said long margin frame raised line (15) is consistent with the opening direction of long margin frame C type draw-in groove (11);
The cross section of said minor face frame (2) comprises a minor face frame C type draw-in groove (21); The below of said minor face frame C type draw-in groove (21) is provided with the perpendicular section of minor face frame (22); The bottom of the perpendicular section of said minor face frame (22) is connected with minor face frame crosspiece (23); Perpendicular section of said minor face frame (22) and minor face frame crosspiece (23) are extended with minor face frame perpendicular section extension (24) and minor face frame crosspiece extension (25) along the length direction of minor face frame (2); One side of said minor face frame perpendicular section extension (24) is provided with minor face frame raised line (26), and the protrusion direction of said minor face frame raised line (26) is consistent with the opening direction of minor face frame C type draw-in groove (21);
Said angle sign indicating number (3) comprises two angle sign indicating number wings; The cross section of the said angle sign indicating number wing comprises one to the angle of inner opening sign indicating number wing C type draw-in groove (31); The below of said angle sign indicating number wing C type draw-in groove (31) is provided with vertical abdominal cavity (32), and the bottom in said vertical abdominal cavity (32) is provided with inside horizontal abdominal cavity (33);
Insert in the vertical abdominal cavity (32) of (3) angle sign indicating number wings of angle sign indicating number the long margin frame of said long margin frame (1) perpendicular section extension (14); Insert respectively in the vertical abdominal cavity (32) and horizontal abdominal cavity (33) of another angle sign indicating number wing of angle sign indicating number (3) with minor face frame crosspiece extension (25) the minor face frame of said minor face frame (2) perpendicular section extension (24), and the opening direction of said long margin frame C type draw-in groove (11) and minor face frame C type draw-in groove (21) is consistent with the opening direction of angle sign indicating number wing C type draw-in groove (31).
2. the syndeton of a kind of firmness higher solar energy frame assembly according to claim 1; The number that it is characterized in that said draw-in groove (34) is a plurality of; Said draw-in groove (34) transverse arrangement of turbo; The number of said long margin frame raised line (15) and minor face frame raised line (26) is identical with the number of draw-in groove (34), said long margin frame raised line (15) and minor face frame raised line (26) transverse arrangement of turbo.
3. the syndeton of a kind of firmness higher solar energy frame assembly according to claim 1; The number that it is characterized in that said draw-in groove (34) is a plurality of; Said draw-in groove (34) transverse arrangement of turbo; The number of said long margin frame raised line (15) and minor face frame raised line (26) is identical with the number of draw-in groove (34), and said long margin frame raised line (15) is arranged with minor face frame raised line (26) is vertical.
CN201210254186.4A 2012-07-23 2012-07-23 The syndeton of the solar energy border component that a kind of firmness is higher Active CN102769054B (en)

Priority Applications (1)

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CN201210254186.4A CN102769054B (en) 2012-07-23 2012-07-23 The syndeton of the solar energy border component that a kind of firmness is higher

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201210254186.4A CN102769054B (en) 2012-07-23 2012-07-23 The syndeton of the solar energy border component that a kind of firmness is higher

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CN102769054B CN102769054B (en) 2015-07-29

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103423260A (en) * 2013-08-07 2013-12-04 刘学军 Corner connector with detachable frame strip
US20180212556A1 (en) * 2015-07-06 2018-07-26 Hanwha Q Cells Gmbh Solar module

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201289246Y (en) * 2008-10-10 2009-08-12 云南一通太阳能科技有限公司 Stealth card connection cornerite of flat-plate type solar heat collector frame
US20110155127A1 (en) * 2009-12-31 2011-06-30 Du Pont Apollo Limited Frame for solar module
TWM422013U (en) * 2011-06-30 2012-02-01 Win Win Prec Technology Co Ltd Improved assembly structure of frame for solar panel
CN202797015U (en) * 2012-07-23 2013-03-13 江苏爱康太阳能科技股份有限公司 High-firmness connection structure of solar frame assembly

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201289246Y (en) * 2008-10-10 2009-08-12 云南一通太阳能科技有限公司 Stealth card connection cornerite of flat-plate type solar heat collector frame
US20110155127A1 (en) * 2009-12-31 2011-06-30 Du Pont Apollo Limited Frame for solar module
TWM422013U (en) * 2011-06-30 2012-02-01 Win Win Prec Technology Co Ltd Improved assembly structure of frame for solar panel
CN202797015U (en) * 2012-07-23 2013-03-13 江苏爱康太阳能科技股份有限公司 High-firmness connection structure of solar frame assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103423260A (en) * 2013-08-07 2013-12-04 刘学军 Corner connector with detachable frame strip
US20180212556A1 (en) * 2015-07-06 2018-07-26 Hanwha Q Cells Gmbh Solar module

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Address after: 214421 Jiangsu city of Wuxi province Jiangyin Huashi Industrial Zone Red Miao Qin Feng Park Road No. 1015

Applicant after: Jiangsu Ai Kang Science and Technology Co., Ltd.

Address before: 214421 Jiangsu city of Wuxi province Jiangyin Huashi Industrial Zone Red Miao Qin Feng Park Road No. 1015

Applicant before: Jiangsu Akcome Solar Science & Technology Co., Ltd.

COR Change of bibliographic data

Free format text: CORRECT: APPLICANT; FROM: JIANGSU AKCOME SOLAR SCIENCE AND TECHNOLOGY CO., LTD. TO: JIANGSU AKCOME TECHNOLOGY CO., LTD.

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CP02 Change in the address of a patent holder

Address after: No. 101, Jintang West Road, Zhangjiagang Economic Development Zone, Suzhou, Jiangsu 215600

Patentee after: Jiangsu Ai Kang Science and Technology Co., Ltd.

Address before: 214421 Jiangsu city of Wuxi province Jiangyin Huashi Industrial Zone Red Miao Qin Feng Park Road No. 1015

Patentee before: Jiangsu Ai Kang Science and Technology Co., Ltd.