CN202797017U - Buckle-type connection structure of solar frame assembly - Google Patents
Buckle-type connection structure of solar frame assembly Download PDFInfo
- Publication number
- CN202797017U CN202797017U CN2012203559451U CN201220355945U CN202797017U CN 202797017 U CN202797017 U CN 202797017U CN 2012203559451 U CN2012203559451 U CN 2012203559451U CN 201220355945 U CN201220355945 U CN 201220355945U CN 202797017 U CN202797017 U CN 202797017U
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- CN
- China
- Prior art keywords
- frame
- long margin
- buckle
- corner brace
- short frame
- 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.)
- Withdrawn - After Issue
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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
- 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
Abstract
The utility model relates to a buckle-type connection structure of a solar frame assembly. The buckle-type connection structure of the solar frame assembly comprises a long frame (1), a short frame (2) and a corner brace (3). A long-frame vertical-section extension section (14) of the long frame (1) is inserted into a vertical abdominal cavity (32) of one corner brace wing of the corner brace; and a short-frame vertical-section extension section (24) and a short-frame transverse-section extension section (25) of the short frame (2) are respectively inserted into a vertical abdominal cavity (32) and a transverse abdominal cavity (33) of the other corner brace wing of the corner brace. According to the buckle-type connection structure of the solar frame assembly of the utility model, long frame buckles and short frame buckles are buckled in buckling openings of the corner brace wings, as a result, the long frame and the short frame can be both matched with the corner brace, and therefore, the buckle-type connection structure of the solar frame assembly has the advantages of convenient and high-firmness connection.
Description
Technical field
The utility model relates to a kind of syndeton of solar energy border component, relates in particular to a kind of buckle-type syndeton of solar energy border component, belongs 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 is converted to electric energy, or is sent in the storage battery and stores, or promotes loaded work piece.Solar panel is installed in the solar energy border component, the solar energy border component comprises two long margin frames and two short frames of rectangular arrangement, directly link to each other by bolt between traditional long margin frame and the short frame or indirectly link to each other by corner brace, the bolt firmness that directly links to each other is relatively poor and connect comparatively complicatedly, and to connect comparatively convenient firmness relatively poor although corner brace links to each other indirectly.
Summary of the invention
The purpose of this utility model is to overcome above-mentioned deficiency, and the buckle-type syndeton of the comparatively convenient and solar energy border component that firmness is higher of a kind of connection is provided.
The purpose of this utility model is achieved in that
A kind of buckle-type syndeton of solar energy border component, it comprises long margin frame, short frame and corner brace;
The cross section of described long margin frame comprises a long margin frame C type draw-in groove, the below of described 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 described long margin frame is connected with the long margin frame crosspiece, the perpendicular section of described long margin frame is extended with the perpendicular section of long margin frame extension along the length direction of long margin frame, one side of the perpendicular section of described long margin frame extension is provided with the long margin frame buckle, described long margin frame buckle to stretch out direction consistent with the opening direction of long margin frame C type draw-in groove;
The cross section of described short frame comprises a short frame C type draw-in groove, the below of described short frame C type draw-in groove is provided with the perpendicular section of short frame, the bottom of the perpendicular section of described short frame is connected with the short frame crosspiece, the perpendicular section of described short frame and short frame crosspiece are extended with the perpendicular section extension of short frame and short frame crosspiece extension along the length direction of short frame, one side of the perpendicular section of described short frame extension is provided with the short frame buckle, the short frame buckle to stretch out direction consistent with the opening direction of short frame C type draw-in groove;
Described corner brace comprises two corner brace wings, the cross section of the described corner brace wing comprises one to the corner brace wing C type draw-in groove of inner opening, the below of described corner brace wing C type draw-in groove is provided with vertical abdominal cavity, the bottom in described vertical abdominal cavity is provided with inside horizontal abdominal cavity, and the madial wall in described vertical abdominal cavity is provided with bayonet socket;
Insert in the vertical abdominal cavity of a corner brace wing of corner brace the perpendicular section of the long margin frame of described long margin frame extension, insert respectively in the vertical abdominal cavity and horizontal abdominal cavity of another corner brace wing of corner brace the short frame of described short frame perpendicular section extension and short frame crosspiece extension, and the opening direction of described long margin frame C type draw-in groove and short frame C type draw-in groove is consistent with the opening direction of corner brace wing C type draw-in groove.
As a kind of preferred, described bayonet socket is provided with a plurality of, described a plurality of bayonet socket is arranged along the length direction of the corner brace wing, the number of described long margin frame buckle and short frame buckle is identical with the number of bayonet socket, described long margin frame buckle arranges that along the length of long margin frame described short frame buckle is arranged along the length of short frame.
Compared with prior art, the beneficial effects of the utility model are:
The utility model is because in the vertical abdominal cavity of a corner brace wing of the perpendicular section of long margin frame extension insertion, insert respectively in the vertical abdominal cavity and horizontal abdominal cavity of another corner brace wing short frame perpendicular section extension and short frame crosspiece extension, long margin frame buckle and short frame buckle snap in the bayonet socket of the corner brace wing, so that long margin frame, short frame all cooperate with corner brace firmly, the buckle-type syndeton of this solar energy border component has the comparatively convenient and higher advantage of firmness of connection.
Description of drawings
Fig. 1 is the structural representation of the buckle-type syndeton of the utility model solar energy border component.
Fig. 2 is the explosive view of Fig. 1.
Fig. 3 is the long margin frame stereogram of the buckle-type syndeton of the utility model solar energy border component.
Fig. 4 is the A place partial enlarged drawing of Fig. 3.
Fig. 5 is the long margin frame cross-sectional view of the buckle-type syndeton of the utility model solar energy border component.
Fig. 6 is the short frame stereogram of the buckle-type syndeton of the utility model solar energy border component.
Fig. 7 is the B place partial enlarged drawing of Fig. 6.
Fig. 8 is the short frame cross-sectional view of the buckle-type syndeton of the utility model solar energy border component.
Fig. 9 is the stereogram of corner brace of the buckle-type syndeton of the utility model solar energy border component.
Wherein:
Embodiment
Referring to Fig. 1 ~ Fig. 9, the buckle-type syndeton of a kind of solar energy border component that the utility model relates to, it comprises long margin frame 1, short frame 2 and corner brace 3;
The cross section of described long margin frame 1 comprises a long margin frame C type draw-in groove 11, the below of described 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 described long margin frame is connected with long margin frame crosspiece 13, the perpendicular section of described long margin frame 12 length directions along long margin frame 1 are extended with the perpendicular section of long margin frame extension 14, one side of the perpendicular section of described long margin frame extension 14 is provided with long margin frame buckle 15, described long margin frame buckle 15 to stretch out direction consistent with the opening direction of long margin frame C type draw-in groove 11;
The cross section of described short frame 2 comprises a short frame C type draw-in groove 21, the below of described short frame C type draw-in groove 21 is provided with the perpendicular section 22 of short frame, the bottom of the perpendicular section 22 of described short frame is connected with short frame crosspiece 23, the perpendicular section 22 of described short frame and short frame crosspiece 23 are extended with short frame perpendicular section extension 24 and short frame crosspiece extension 25 along the length direction of short frame 2, one side of the perpendicular section of described short frame extension 24 is provided with short frame buckle 26, described short frame buckle 26 to stretch out direction consistent with the opening direction of short frame C type draw-in groove 21;
Described corner brace 3 comprises two corner brace wings, the cross section of the described corner brace wing comprises one to the corner brace wing C type draw-in groove 31 of inner opening, the below of described corner brace wing C type draw-in groove 31 is provided with vertical abdominal cavity 32, the bottom in described vertical abdominal cavity 32 is provided with inside horizontal abdominal cavity 33, and the madial wall in described vertical abdominal cavity 32 is provided with bayonet socket 34;
Insert in the vertical abdominal cavity 32 of 3 one corner brace wings of corner brace the perpendicular section of the long margin frame of described long margin frame 1 extension 14, insert respectively in the vertical abdominal cavity 32 and horizontal abdominal cavity 33 of corner brace 3 another corner brace wings with short frame crosspiece extension 25 the perpendicular section of the short frame of described short frame 2 extension 24, the opening direction of described long margin frame C type draw-in groove 11 and short frame C type draw-in groove 21 is consistent with the opening direction of corner brace wing C type draw-in groove 31, and described long margin frame buckle 15 snaps in the bayonet socket 34 with short frame buckle 26.
As shown in Figure 1, described long margin frame buckle 15 is provided with two with short frame buckle 26, described two long margin frame buckles 15 are arranged along the length of long margin frame, described four short frame buckles 26 are arranged along the length of short frame, described bayonet socket 34 also is provided with two, and described bayonet socket 34 is arranged along the length direction of the corner brace wing.
Claims (2)
1. the buckle-type syndeton of a solar energy border component, it comprises long margin frame (1), short frame (2) and corner brace (3);
The cross section that it is characterized in that described long margin frame (1) comprises a long margin frame C type draw-in groove (11), the below of described 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 described long margin frame (12) is connected with long margin frame crosspiece (13), the perpendicular section of described 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 described long margin frame perpendicular section extension (14) is provided with long margin frame buckle (15), described long margin frame buckle (15) to stretch out direction consistent with the opening direction of long margin frame C type draw-in groove (11);
The cross section of described short frame (2) comprises a short frame C type draw-in groove (21), the below of described short frame C type draw-in groove (21) is provided with the perpendicular section of short frame (22), the bottom of the perpendicular section of described short frame (22) is connected with short frame crosspiece (23), the perpendicular section of described short frame (22) and short frame crosspiece (23) are extended with short frame perpendicular section extension (24) and short frame crosspiece extension (25) along the length direction of short frame (2), one side of described short frame perpendicular section extension (24) is provided with short frame buckle (26), described short frame buckle (26) to stretch out direction consistent with the opening direction of short frame C type draw-in groove (21);
Described corner brace (3) comprises two corner brace wings, the cross section of the described corner brace wing comprises one to the corner brace wing C type draw-in groove (31) of inner opening, the below of described corner brace wing C type draw-in groove (31) is provided with vertical abdominal cavity (32), and the bottom in described vertical abdominal cavity (32) is provided with inside horizontal abdominal cavity (33);
Insert in the vertical abdominal cavity (32) of (3) corner brace wings of corner brace the long margin frame of described long margin frame (1) perpendicular section extension (14), insert respectively in the vertical abdominal cavity (32) and horizontal abdominal cavity (33) of another corner brace wing of corner brace (3) with short frame crosspiece extension (25) short frame of described short frame (2) perpendicular section extension (24), the opening direction of described long margin frame C type draw-in groove (11) and short frame C type draw-in groove (21) is consistent with the opening direction of corner brace wing C type draw-in groove (31), and described long margin frame buckle (15) snaps in the bayonet socket (34) with short frame buckle (26).
2. the buckle-type syndeton of a kind of solar energy border component according to claim 1, it is characterized in that described bayonet socket (34) is provided with a plurality of, described a plurality of bayonet socket (34) is arranged along the length direction of the corner brace wing, the number of described long margin frame buckle (15) and short frame buckle (26) is identical with the number of bayonet socket (34), described long margin frame buckle (15) arranges that along the length of long margin frame described short frame buckle (26) is arranged along the length of short frame.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012203559451U CN202797017U (en) | 2012-07-23 | 2012-07-23 | Buckle-type connection structure of solar frame assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012203559451U CN202797017U (en) | 2012-07-23 | 2012-07-23 | Buckle-type connection structure of solar frame assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202797017U true CN202797017U (en) | 2013-03-13 |
Family
ID=47824218
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012203559451U Withdrawn - After Issue CN202797017U (en) | 2012-07-23 | 2012-07-23 | Buckle-type connection structure of solar frame assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202797017U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102769050A (en) * | 2012-07-23 | 2012-11-07 | 江苏爱康太阳能科技股份有限公司 | Fastened connecting structure for solar frame component |
| CN103825543A (en) * | 2014-01-28 | 2014-05-28 | 金发科技股份有限公司 | Solar cell frame |
| CN111343827A (en) * | 2020-03-19 | 2020-06-26 | 江苏利通电子股份有限公司 | Plastic-metal self-locking integrated back plate |
-
2012
- 2012-07-23 CN CN2012203559451U patent/CN202797017U/en not_active Withdrawn - After Issue
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102769050A (en) * | 2012-07-23 | 2012-11-07 | 江苏爱康太阳能科技股份有限公司 | Fastened connecting structure for solar frame component |
| CN102769050B (en) * | 2012-07-23 | 2015-08-12 | 江苏爱康科技股份有限公司 | The buckle-type syndeton of solar energy border component |
| CN103825543A (en) * | 2014-01-28 | 2014-05-28 | 金发科技股份有限公司 | Solar cell frame |
| CN111343827A (en) * | 2020-03-19 | 2020-06-26 | 江苏利通电子股份有限公司 | Plastic-metal self-locking integrated back plate |
| CN111343827B (en) * | 2020-03-19 | 2021-01-26 | 江苏利通电子股份有限公司 | Plastic-metal self-locking integrated back plate |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: JIANGSU AKCOME TECHNOLOGY CO., LTD. Free format text: FORMER NAME: JIANGSU AKCOME SOLAR SCIENCE AND TECHNOLOGY CO., LTD. |
|
| CP01 | Change in the name or title of a patent holder |
Address after: 214421 Jiangsu city of Wuxi province Jiangyin Huashi Industrial Zone Red Miao Qin Feng Park Road No. 1015 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 Akcome Solar Science & Technology Co., Ltd. |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20130313 Effective date of abandoning: 20150812 |
|
| RGAV | Abandon patent right to avoid regrant |