Rear face element for a solar module
11004992 · 2021-05-11
Assignee
Inventors
Cpc classification
H01L31/0475
ELECTRICITY
Y02E10/44
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
F24S25/20
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02E10/50
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
F24S25/63
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
H02S30/00
ELECTRICITY
F21S9/037
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F24S25/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F24S25/67
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F24S2020/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F21S9/035
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F24S25/40
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
H01L31/0475
ELECTRICITY
Abstract
The invention relates to a rear face element for a solar module, said element being made of a material sheet that is shaped, in particular embossed and/or stamped. Some sections of the material sheet are arranged on a first plane, and some sections are arranged on at least one second plane parallel to the first plane. The material sheet forms spacer elements in a transition region between the first and the second plane in order to space the first plane from the second plane, and at least one first material sheet section extends from a first lateral edge to an opposing second lateral edge of the material sheet continuously, in particular in a linear manner. The invention also relates to a solar module and to a method for producing a solar module.
Claims
1. A rear face element of a solar module formed from one single material sheet that is shaped, cut into in some sections, thus forming material sections, wherein some material sections of the material sheet are arranged in a first plane and some sections are arranged in at least one second plane parallel to the first plane, and wherein the material sheet forms spacing elements in a transitional region from the first plane to the second plane in order to keep the first plane at a spacing distance from the second plane, and wherein at least one first material sheet section extends continuously, from a first lateral edge to an opposite second lateral edge of the material sheet in the first plane, wherein n first material sheet sections, where n=1, 2, 3, 4, 5, 6, 7, 8, 9 or more, extend from a first side edge to an opposite second side edge of the material sheet in the first plane and/or m second material sheet sections, where m=1, 2, 3, 4, 5, 6, 7, 8, 9 or more, extend from a third side edge of the material sheet to an opposite fourth side edge in the first plane, wherein the first and second material sheet sections extend at angles to one another, and wherein the at least one first material sheet section, the second material sheet sections, the spacing elements, and material sheet sections in the second plane have a shape with openings in the rear face element.
2. The rear face element as claimed in claim 1, characterized in that the n first material sheet sections extend continuously, from a first side edge to an opposite second side edge of the material sheet, in the first plane and/or the m second material sheet sections extend continuously from a third side edge of the material sheet to an opposite forth side edge in the first plane.
3. The rear face element as claimed in claim 1, characterized in that the second plane p, where p=1, 2, 3, 4, 5, 6, 7, 8, 9 or more, comprises sheet-like elements which are arranged at a spacing distance from one another, and are arranged in each case between the n first material sheet sections and/or m second material sheet sections of the first plane.
4. The rear face element as claimed in claim 3, characterized in that each of the sheet-like elements of the second plane is connected to the first and/or second material sheet sections of the first plane by four spacing elements, the spacing elements being part of the material sheet.
5. The rear face element as claimed in claim 3, characterized in that the rear face element has q cells, where q=1, 2, 3, 4, 5, 6, 7, 8, 9 or more, wherein each of the q cells is formed from two first material sheet sections, two second material sheet sections in the first plane and a sheet-like element in the second plane.
6. The rear face element as claimed in claim 1, characterized in that the material sheet consists of and/or comprises metal, high-grade steel, steel sheet, iron sheet, copper, brass, aluminum, plastic, injection-molded plastic and/or partially encapsulated metal, and has a thickness in a range from 0.2 mm to 4 mm.
7. The rear face element as claimed in claim 1, characterized in that the rear face element has at least one clearance in the first plane and/or in the second plane, in order to receive a connection socket for electrical contact of a solar cell and/or a solar cell matrix and/or to allow electrical contact of a solar cell and/or a solar cell matrix wherein the region is exposed in the clearance of the cross-connectors of a solar cell and/or a solar cell matrix.
8. The rear face element as claimed in claim 1, characterized in that the material sheet comprises reinforcing elements arranged in a connecting region of the rear face element of the solar module to a substructure.
9. The rear face element as claimed in claim 3, characterized in that at least one sheet-like element of the second plane is shaped in such a way that a third plane is formed and/or has a shaped, or embossed, surface structure.
10. The rear face element as claimed in claim 1, characterized in that retaining eyelets, clamps, cable guides and/or cable ducts for the electrical contacting of the solar module are comprised and/or the rear face element has clearances in the edge region in order to allow secure transport of electrical contact elements, and to simplify/ensure fastening thereof after fitting of the solar module.
11. The rear face element as claimed in claim 1, characterized in that all the edges of the rear face elements have the shape of a flange.
12. The rear face element as claimed in claim 1, characterized in that all the edges of the rear face element comprise clearances and/or formations that can be brought into or are in operative connection with comparable clearances and/or formations of a further rear face element, the clearances and/or formations being designed and set up for aligning two rear face elements with one another.
13. The rear face element as claimed in claim 1, characterized in that all the edges of the rear face element have fastening devices and/or clearances.
14. The rear face element as claimed in claim 1, characterized in that the rear face element consists of a shaped material sheet.
Description
(1) Further features and advantages of the invention emerge from the following description, in which exemplary embodiments of the invention are explained by way of example on the basis of schematic drawings, without thereby restricting the invention. In the drawings:
(2)
(3)
(4)
(5)
(6) In
(7) In this case, the first first material sheet section 11 has a first side end 15 and the second first material sheet section 11′ has a second side end (not shown), opposite from the first side end 15. The first second material sheet section 13 has a third side end, arranged at right angles to the first and second side ends 15, and the second second material sheet section 13′ has a fourth side end 17′, opposite from the third side end 17. It goes without saying that this configuration should only be understood as given by way of example. The side ends 17, 17′ may alternatively also be curved, and so the spacing elements 9 are not rectangularly formed. The pointed corners of the first and second planes 5, 7 may of course also be formed as rounded.
(8) By shaping, a first cutout of the material sheet 3, beginning with the second second material sheet section 13′, extends at a first distance 21 parallel to the first first material sheet section 11 up to a first spacing distance 19 from the first second material sheet section 13 and a second cutout of the material sheet 3, beginning with the second second material sheet section 13′, extends at a second distance 21′, greater than the first distance 21, parallel to the first first material sheet section 11 up to a second spacing distance 19′, greater than the first spacing distance 19, from the first second material sheet section 13.
(9) There are corresponding cutouts turned in each case by 90°, in order to keep the second plane 7 at a spacing distance from the first plane 5 and in order to transmit the forces acting on the second plane 7 to the first plane 5.
(10) It can be seen well in
(11) It goes without saying that here, too, the number of cells 23 should only be understood as given by way of example and they can be formed in any desired number, symmetrically or asymmetrically. All nine cutouts have in
(12)
(13)
(14) In this case, the configurational variant of the rear face element 1″ according to the invention differs by a third plane 27, which is arranged between the first plane 5 and the second plane 7. As already stated above, the geometry and the number of the planes formed by the material sheet 3 can be adapted to the specific application, in order to stabilize and fasten the laminar structure 29 comprising the solar cells.
(15) The features of the invention that are disclosed in the foregoing description, the claims and the drawings may be essential both individually and in any desired combination for implementing the invention in various embodiments.