SOLAR PANEL AND RAIL WITH EDGE CONNECTORS

Abstract

Solar panels, which at least at edges of two opposite sides, have frames, for use in fixed tilt solar system as well as use in tracking solar system, are provided with coupling parts together with rails and have coupling parts cooperating with each other, substantially in the form of tongue and groove. The coupling parts have integrated mechanical locking elements, which prevent drifting or separating apart of a coupled solar panel and rail in a direction perpendicular to the solar panel surface and parallel to the solar panel surface. The coupled tongue and groove are balanced by a set of forces and integrated to support each other, and to support solar panel with combined mechanical strength, which provide opportunities to reduce materials usage, dimensions, packaging materials, shipping costs, and installation time, as well as limiting installer error.

Claims

1. A solar panel (1) containing glass (103, 104) and aluminum frame (6, 7), and rail (2) containing steel, said solar panel (1) having an upper surface (14) terminating at opposed upper side edges (4, 5), where are the frames (6, 7), an underside groove (58, 59) with upper surface parallel to the upper side surface (14), and side edges terminating at said frame (6, 7) by inserting in a groove at the upper side of the said frame (6, 7), or terminating at said frame (6, 7) by glued on to the upper side of the said frame; wherein the under side of frame (6, 7) provided with coupling parts (8, 9) integrally formed with said frame (6, 7); wherein the upper side of rail (2) provided with coupling parts (10, 11) integrally formed with said rail (2); said coupling parts (10, 11) configured to cooperate by coupling with cooperative coupling parts (8, 9) of said frame (6, 7) of solar panel (1) and rail (2), said coupling parts comprising a tongue (10, 11) and a groove (8, 9) configured to lock together coupled identical ones of said solar panel (1) and identical ones of said rail (2) in a direction perpendicular to the plane of the coupled panels when cooperative coupling parts of the solar panels and rails are engaged, said tongue (10, 11) and groove (8, 9) having respective upper and lower sides, and wherein the panel side edge provided with frame (6, 7) which with the groove has a locking element (12, 13) located outer edge and adjacent the upper side surface of the groove (8, 9), and terminating at a distal upper lip edge, and a lower lip extending distally behind said distal upper lip edge in the plane of the solar panel; said coupling parts including locking elements (12, 13) formed integrally in one piece with said frame (6, 7) core, said locking elements (12, 13) including cooperative contact surfaces arranged to be engaged when said tongue (10, 11) of said rail (2) are coupled together with their coupling parts cooperatively engaged to prevent substantial separation of coupled solar panel (1) and rail (2) at said edges in a direction perpendicular to the edges of the panel sides; said locking means comprising a locking element (12, 13) in the form of a downwardly extending protrusion located on the upper side of the groove (8, 9), said cooperative contact surfaces defined respectively by said locking element (12, 13), said upper surface of groove (8, 9), said lower surface of groove (8, 9), said other surface of groove (8, 9); wherein upon coupling in a plane determined by the upper side of tongue (10, 11) in contact with the upper side surface of groove (8, 9).

2. A coupling solar panel (1) and rail (2) according to claim 1, wherein the material of the frame (6, 7), including the locking elements (12, 13), is constituted of a metal material consisting of aluminum, steel, Bakelite, plastic or other structural materials formed into the shape by extrusion or roll forming.

3. A coupling solar panel (1) and rail (2) according to claim 1, wherein the locking surface defined by the upper side of said tongue (10, 11) extends downwardly from the upper side of the tongue (10, 11) at an inclination that extends inwardly and downwardly from a proximally outer location to a distally inner location.

4. A coupling solar panel (1) and rail (2) according to claim 1, wherein upper contact surface of groove is generally parallel to the plane of solar panel (1) surface (14), so that they will apply minimum lateral strain on the frame (6, 7) of the other side and any connections in between when cooperative coupling parts of said locking means are coupled together with said contact surfaces located contiguous with each other.

5. A coupling solar panel (1) and rail (2) according to claim 1, wherein the contact surface defined by said surfaces inside of said groove or above of said surface parallel to solar panel (1) surface from an under location of the said solar panel (1) with glass (103, 104) engagement by glue to the groove or by glue to the upper surface of rail (2).

6. A coupling solar panel (1) and rail (2) according to claim 1, wherein said tongue (10, 11) may be on frame (6, 7) side or on rail (2) side.

7. A coupling solar panel (1) and rail (2) according to claim 1, wherein said tongue (10, 11) has a guiding surface downwardly angle similar to the angle of coupling locking element (12, 13) of said groove (8, 9) and/or wherein said tongue (10, 11) has distance from outer side to edge of inner side less than distance from locking element (12, 13) to inner surface of groove (8, 9).

8. A coupling solar panel (1) and rail (2) according to claim 1, wherein said groove has a guiding surface on said outer side of locking element (12, 13) downwardly angle equal or similar to the angle of guiding surface of said coupling tongue (10, 11).

9. A coupling solar panel (1) and rail (2) according to claim 1 wherein the tongue (10, 11) and groove (8, 9) have a shape such that in coupled condition of tongue (10, 11) and groove (8, 9) of said solar panel (1) and rail (2) there are provided chambers defined by a space between a lower surface of the downwardly guiding surface of said tongue (10, 11) and an adjacent upper surface of the groove (8, 9), as well as by a space between a curvature of said tongue (10, 11) of a larger radius and lower inside corner of said groove (8, 9) with a smaller radius, said chambers being located on the tip side of said tongue (10, 11) and inner side of groove (8, 9).

10. A coupling solar panel (1) and rail (2) according to claim 1, wherein the coupling parts are dimensioned to provide a coupling free-from-play in all panel (1)/rail (2) separation and/or drifting directions in a plane extending perpendicular to the said side edges when frame (6, 7) of said panel (1) are coupled together with rail (2).

11. A coupling solar panel (1) and rail (2) according to claim 1, wherein coupled the tongue (10, 11) and groove (8, 9) are configured such that when said solar panel (1) is coupled together with said rail (2), upon exertion of a pressure on top or on has bottom of said coupled solar panel (1) and rail (2) react to the pressure to support the upper surface of groove (8, 9) when pressure from top, and react to press lower surface of groove (8, 9) when pressure from bottom, such as wind pressure.

12. A coupling solar panel (1) and rail (2) according to claim 1, wherein said locking tongue (10, 11) and groove are configured and dimensioned such that when frames (6, 7) of two sides of said solar panel (1) are coupled in the identical rail (2) with their opposite upper side edges on the same plane of solar panel (1) surface, said frames (6, 7) of opposite sides of solar panels (1) exert minimum tension force upon each other tending to isolate movement and/or vibration upon each other, particularly in lateral direction, wherein preferably at least one of the coupling parts comprises an elastically yieldable portion which, when said panel and said rail (2) are coupled, is at least partially deformed within its elastic yield range to produce said tension force.

13. A coupling solar panel (1) and rail (2) according to claim 1, wherein the coupling parts are configured such that frame (6, 7) of said solar panel (1) and said rail (2) can be selectively coupled: either by laterally sliding and snapping the cooperative coupling parts together or by turning one relative to the other with their cooperative coupling parts partially engaged, whereby additional ones of said solar panel (1) can be sequentially coupled to previously coupled rail (2), and additional ones of said rail (2) can be sequentially coupled to previously coupled solar panel, by laterally sliding each additional panel into a previously coupled rail (2), and laterally sliding each additional rail (2) into a previously coupled panel, or by relative turning motions of an additional one relative to the other; or by sliding along the solar panel (1) edge and engage the coupling parts together, whereby additional ones of said solar panel (1) can be sequentially coupled to previously coupled rail (2), and additional ones of said rail (2) can be sequentially coupled to previously coupled solar panel.

14. A coupling solar panel (1) and rail (2) according to claim 1, wherein an upper surface of the groove (8, 9) of said solar panel (1) is flat and is configured to define a guidance surface for guiding the coupling parts of the tongue (10, 11) of said rail (2) into engagement with each other when said one of said solar panel (1) is rotated relative to said rail (2) with their coupling parts partially engaged.

15. A coupling solar panel (1) and rail (2) according to claim 1, wherein the distal end of the lower lip of said tongue (10, 11) of said rail (2) is provided with a sloped ramp surface, said ramp surface configured such that when the groove of said panel is moved laterally towards the tongue (10, 11) of said rail (2) approximately in a plane including the panel and rail (2) to cause engagement of cooperative coupling parts of the panels, the protrusion of said groove is guided over the distal outer end of the lower lip by said ramp as the groove traverses said distal outer end of the lower lip. The said contact surfaces of said groove (8, 9) and tongue (10, 11) may have slop as ranging from 0 to 45 degrees.

16. A coupling solar panel (1) and rail (2) according to claim 1, wherein said tongue (10, 11) and groove are dimensioned and configured such that ones of said solar panel (1) and said rail (2) can be coupled together from a position where the cooperative coupling parts of the solar panel (1) and rail (2) are partially engaged by turning one relative to the other and vice versa, and with said turning movement centered at the lower corner of groove of said solar panels, and such that during the turning movement the tongue (10, 11) of said rail (2) can freely slide into the groove (8, 9) of the said solar panel (1).

17. A coupling solar panel (1) and rail (2) according to claim 1, wherein the locking elements (12, 13) have rounded edges.

18. A coupling solar panel (1) and rail (2) according to claim 1, wherein the coupling parts are configured so that the panel (1) can be coupled to rail (2) with their cooperative coupling parts engaged and locked against lateral and vertical separation without glue or bolt, whereby the panel (1) and rail (2) can be freely disassembled and recoupled.

19. A coupling solar panel (1) and rail (2) according to claim 1, wherein the said thin film solar cells grown on glass (103, 104) include thin film silicon solar cells, thin film TdCe solar cells, thin film GaAs solar cells.

20. A coupling solar panel (1) and rail (2) according to claim 19, wherein the said frame (6, 7) are attached to under surface of the glass (103, 104).

Description

BRIEF DESCRIPTION OF DRAWINGS

[0036] FIG. 1A represents a diagram of solar panels assembled for fixed tiled solar system, with rails and frames coupled according to this invention.

[0037] FIG. 1B represents a schematic diagram of solar panels assembled for single axle tracking solar system, with rails and frames coupled according to this invention.

[0038] FIG. 2 represents a schematic cross section of a solar panel, single glass, with frame according to this invention, glass inserts into groove.

[0039] FIG. 3 represents a schematic cross section of a solar panel, double glasses, with frame according to this invention, glasses insert into groove.

[0040] FIG. 4 represents a schematic cross section of a solar panel, single glass, with frame according to this invention, glass glued on frame.

[0041] FIG. 5 represents a schematic cross section of a solar panel, double glasses, with frame according to this invention, glasses glued on frame.

[0042] FIG. 6 represents a cross section of solar panel frames coupled with a rail by tongue and groove according to this invention.

[0043] FIG. 7 represents a cross section of solar panel frames coupled with a rail by tongue and groove according to this invention, by parallel move to engage.

[0044] FIG. 8 represents a cross section of solar panel frames coupled with a rail by tongue and groove according to this invention.

[0045] FIG. 9 represents a cross section of solar panel frames coupled with a rail by tongue and groove according to this invention, by parallel move to engage.

[0046] FIG. 10 represents a cross section of solar panel frames coupled with a rail by tongue and groove according to this invention, by turning to engage.

[0047] FIG. 11 represents a cross section of solar panel frames coupled with a rail by tongue and groove according to this invention.

[0048] FIG. 12 represents a cross section of solar panel frames coupled with a rail by tongue and groove according to this invention, by turning to engage.

[0049] FIG. 13 represents a cross section of a coupling rail according to this invention.

[0050] FIG. 14 represents a cross section of a coupling rail according to this invention.

[0051] FIG. 15 represents a cross section of a coupling rail according to this invention.

[0052] FIG. 16A represents a cross section of a solar panel frame according to this invention.

[0053] FIG. 16B represents a cross section of a solar panel frame according to this invention, for glass or glasses glued on frame.

[0054] FIG. 17 represents a cross section of a solar panel frame according to this invention.

[0055] FIG. 18 represents a cross section of a solar panel frame according to this invention.

[0056] FIG. 19 represents a cross section of a solar panel frame according to this invention.

[0057] FIG. 20A represents a cross section of a solar panel frame according to this invention.

[0058] FIG. 20B represents a cross section of a solar panel frame according to this invention.

[0059] FIG. 21A represents a cross section of a solar panel frame according to this invention.

[0060] FIG. 21B represents a cross section of a solar panel frame according to this invention.

[0061] FIG. 22A represents a cross section of a solar panel frame according to this invention.

[0062] FIG. 22B represents a cross section of a solar panel frame according to this invention.

[0063] FIG. 23 represents a cross section of a solar panel coupling rail according to this invention.

[0064] FIG. 24 represents a cross section of solar panel frames coupled with a rail according to this invention.

[0065] FIG. 25 represents a detail cross section of solar panel frames coupled with a rail according to this invention.

[0066] FIG. 26 represents a detail cross section of a solar panel frame couples with rail according to this invention, moving parallel to panel surface.

[0067] FIG. 27 represents a detail cross section of a solar panel frame couples by an angle to engage with the rail according to this invention.

DETAILED DESCRIPTION

[0068] The invention relates to a solar panel and rail system, which is composed of solar panel 1 and coupling rail 2, for example, such as a solar panel and rail as shown in FIG. 1A and FIG. 1B.

[0069] These solar panels 1 can be of various shape, for example, rectangular or square, or of any other shape. These rails 2 can be of various shape, for example, c-channel with inward bending edge, or of any other shape.

[0070] In the most preferred form of embodiment, the solar panels shall be manufactured in an elongated form, such as shown in FIGS. 1A and 1B, for example, with a length of 1 to 4 meters, and width of 0.5 to 2 meters. The thickness, however, can also vary, but is preferably 1.0 to 6.0 cm, and more particularly 2.5 cm.

[0071] In the most preferred form of embodiment, the rails shall be manufactured in an elongated c-channel form, such as shown in FIGS. 1A and 1B, for example, with a length of 0.4 to 12 meters. The height and width, however, can also vary, but is preferably 4.0 to 16.0 cm, and more particularly 10 cm for height, and is preferably 3.0 to 11.0 cm, and more particularly 7 cm for width.

[0072] Each solar panel 1 is, at least at the edges of two opposite sides 4-5, has frames 6-7, provided with coupling grooves 8-9, as shown in FIG. 2 and FIG. 3, which permit two adjacent identical solar panels 1 to be coupled to rail 2 with coupling tongues 10-11, as shown in FIG. 6. Glass and glasses may insert in grooves 58 and 59 of frame 6 and 7. Whereas, 101 and 102 represent the location of the solar cells, 103 and 104 represent solar panel glasses.

[0073] Each solar panel 1 is, also, at least at the edges of two opposite sides 4-5, has frames 6-7, provided with coupling grooves 8-9, as shown in FIG. 4, and FIG. 5, which permit two adjacent identical solar panels 1 to be coupled to rail 2 with coupling tongues 10-11, as shown in FIG. 6. Glass and glasses may be glued on surfaces 68 and 9″ of frame 6 and 7.

[0074] According to this invention, the coupling grooves 8-9, and coupling tongues 10-11, as represented in the FIG. 6, are provided with integrated mechanical locking parts or elements 12-13 which prevent the drifting or sliding apart of coupled solar panels 1 and rail 2 in a direction A perpendicular to the respective sides 4-5 and parallel to the solar panel surface 14 of the coupled solar panels 1; the coupling grooves 4-5 and the locking elements 12-13 are formed in one piece with the core 15 of the frame 6-7 of the solar panels 1; the coupling grooves 8-9 have such a shape that rails with coupling tongues 10-11 can be engaged into each other solely by snapping-together and/or turning after the coupling parts are partially engaged, whereby each subsequent solar panel 1 can be laterally inserted into the previous rail, and each rail can be inserted into previous solar panel; and the coupling grooves 8-9, and coupling tongues 10-11 preferably are interlocked free-of-play in all directions in a plane which is located perpendicular to the aforementioned edges.

[0075] In the case of solar panels 1 with an elongated shape, as represented in FIG. 2-3, the respective coupling parts 8-9, and 10-11 are located at the longitudinal sides 4-5.

[0076] The coupling parts 8-9 and 10-11 can be realized in various forms, although the basic forms thereof will always be formed by tongue 15 and groove 16.

[0077] In the form of embodiment of FIGS. 6-7, the related solar panel 1 frame 6 is provided with coupling grooves 16, and related rail is provided with coupling tongue 15 and groove 16 which allow solar panels 1 to be engaged by means of a parallel movement in moving direction B, to ensure that solar panel 1 which is coupled to the rail 2 can not move perpendicularly in the vertical direction with respect to solar panel surface 14, without the occurrence of any snap-together effect. This particular design allows effortless engagement by parallel move, but not by turning to engage.

[0078] In the form of embodiment of FIGS. 8-10, the related solar panel 1 frame 6 is provided with coupling grooves 16, and related rail is provided with coupling tongue 15 and locking element 12 which allow solar panels 1 to be engaged by means of a parallel movement in moving direction B, with the occurrence of snap-together effect. The tongue 15 is formed with curve 17 and groove 16 is formed with a slope 18, to ensure that solar panel 1 which is coupled to the rail 2 can not move perpendicularly in the vertical direction D with respect to solar panel surface 14, also to ensure that solar panel 1 which is coupled to the rail 2 can not move parallel in the direction A with respect to solar panel surface 14,

[0079] In order to enable solar panel 1 and rail 2 to be inserted into each other by means of a turning movement, the tongue 15 on rail 2 preferably circular and roll formed more than 180°. The bottom side of element 17 on tongue 15 sits on lower side 18 of groove 16. The slope of lower side 18 of groove 16 creates a force F1 on the bottom side 17 of tongue 15. The surface of locking element 12 creates a force F2 on upper side 19 of tongue 15. The upper side 20 of groove 16 creates a force F3 on tongue 15. Together with the two angles α of blocking element 12 and slope β of bottom side 18 of groove 16, we shall have a balance of forces including weight of solar panel W, and forces on the solar panel created by wind load Fw, as below:

F2*Cos(α)=F1*Sin(β)ensures no lateral movement of solar panel 1 relate to rail 2.½W+F51*Cos(β)=F52*Sin(α)+F53+½Fw

[0080] Since Fw is randomly affected by wind, it requires the other forces, F51, F52 and F53 applied on solar panel 1 change accordingly. Coupled tongue and groove design with locking element serve this purpose.

[0081] Distance L between further most tip of tongue to the inner surface of groove ranges from 0 mm to 8 mm, preferably 5 mm. This distance ensures tolerance allowance caused by installer errors or mismatch from other parts, such as width tolerance of solar panels.

[0082] FIG. 9 represents a cross section of solar panel frames coupled with a rail by tongue and groove according to this invention, by parallel move to engage. The slope on bottom side 18 of groove 16 provides an entry guide to tongue 15. Certain deformation on upper side 19 and bottom side 17 of tongue 15, as well as locking element 12 and bottom side 18 of groove 16, allow the entry of tongue 15 into groove 16. Once in position, the forces F51, F52, F53 as well as solar panel weight W and wind load Fw, balance.

[0083] FIG. 10 represents a cross section of solar panel frames coupled with a rail by tongue and groove according to this invention, by turning to engage. The opening 20 of groove 16 allows tongue 15 to insert in without any deformation, making it effortless to enter. However when turning downward to engage with the locking element 12 of groove 16, certain deformation occur allow engagement and lock-in. This design in particular is easier for turning to engage.

[0084] As represented in the FIGS. 11-12, the solar panels 1 according to the invention can, can turn to engage when the tip 21 of tongue 15 insert into opening 20 of groove 16. The turning angle γ can be adjusted by adjusting the tip 21 of tongue 15, locking element 12, as well as another locking element 22, added on groove 16, of the frame 2 of solar panel 1. The turning angle γ is intentionally designed relatively larger, preferably larger than 30 degrees, to ensure elimination of both lateral movement on direction A and vertical movement on direction D. On FIG. 11, the tongue 15 of rail 2 can engage with groove 16 of frame 6 by sliding along direction E. Adjustments and deviations are allowed on either the tongue 15 side of rail 2, or on the groove 16 side of frame 6. This particular design as represented in FIGS. 11-12, according to the invention, is particular for easier sliding to engage.

[0085] As represented in FIGS. 13-15, the tongue 15 of rail 2, according to this invention, tongue 15 can have more shapes that can be inserted into groove 16 and engage by lateral movement on direction B or 5B, by turning direction C as well as slide in direction E. The variation of the shapes of tongue 15 affects the easiness on which of the directions B or 5B, C and E. It also affects the production processes, such as roll forming of the tongue 15 from flat metal plate, such as steel plate.

[0086] As represented in FIGS. 16-19, the frames, according to this invention, may have various shapes as long as two primary features, groove 16 for engagement with tongue 15 of rail 2 and groove 23 for engagement with glass or glasses of solar panel 2, are available. The groove 23 engage with glass if the solar panel is a single glass solar panel, and engage with glasses if the solar panel is a double glass solar panel. The gap width 24 of groove 23 can be adjusted to accommodate the thickness of the glass or glasses, accordingly.

[0087] As represented in FIGS. 20-22, according to this invention, the tongue 25 is made on the frame 6, while the groove 26 is made on rail 2. The frame 6 has two primary features, namely the groove 24 to engage with glass or glasses, and the tongue 25, to engage with groove 26 on the rail 2.

[0088] With tongue 25 on the frame 6 side, the frame 6 may engage with rail 2 by moving in direction 5B, turning in direction C, or slide in direction E.

[0089] As represented in FIGS. 20B and 22B, according to this invention, the tongue 25 is made on the frame 6, while the groove 26 is made on rail 2. The frame 6 has two primary features, namely the surface 68 to engage with glass or glasses by glue, and the tongue 25, to engage with groove 26 on the rail 2.

[0090] With tongue 25 on the frame 6 side, the frame 6 may engage with rail 2 by moving in direction 5B, turning in direction C, or slide in direction E.

[0091] The particular thickness T may vary. The frame may be produced by extrusion of aluminum, plastic, composite or other materials. For particular thickness T may remain the same, thus the frame may be produced by roll forming of metal plate such as steel and aluminum plate.

[0092] The various forms of embodiments according to this invention, such as various designs of frames and rails, either the tongue on the rail side, or on the frame side, all have the features that, the frame engage with glass or glasses with a groove or surface gluing, and engage with the rail through tongue and groove, either the tongue on frame side or on the rail side. The engagement between frame and rail allow both frame and rail to form an integrated system. This integrated system remain balanced through the tongue and groove as well as the locking element that create the forces between frame and rail along the entire engaged or coupled length of frame and rail to not only support the frame with the solar panel weight W, but also balance the wind load Fw applied on the solar panel.

[0093] This integration along the entire coupled length between frame 6 and rail 2, is the primary embodiment of this invention. The integration by tongue and groove on the solar panel frame and the rail, with or without locking element, with tongue on the frame side or on the rail side, allows the strength of the frame 6 and rail 2 to form an integrated system to support the solar panel 1.

[0094] This integration, according to this invention, provides the opportunity to install or engage solar panel to rail with ease and less time consuming, by parallel push and pull, by turning as well as by sliding, and, more importantly, provides the opportunity to reduce the use of materials on frame and/or rail, and reduce the size of frame height H2, which determines the thickness of solar panel 1. The reduction of material use, for example on frame materials, may lead to significant reduction on frame materials usage, such as aluminum usage, as presently most solar panel frames are made of aluminum. The reduction of height of frame, may lead to reduction of the solar panel thickness, thus increase the number of solar panels in the package of same volume, and reducing the packaging and shipping cost.

[0095] As represented in FIG. 23-27 is the most preferred embodiment of this invention.

[0096] Hereby, the parts, which correspond to the previous forms of embodiments are indicated with corresponding references.

[0097] The rail 2 may be made preferably of roll forming of metal plate, in particular of steel plate, with thickness T1 preferably in the range of 0.3 mm to 3 mm, in particular 1 mm to 1.5 mm. The width W1 preferably in the range 2 cm to 20 cm, in particular 6 cm to 10 cm. The height H1 preferably in the range of 3 cm to 30 cm, in particular 6 cm to 12 cm. The radius R1 preferable in the range 1 mm to 4 mm, in particular 2.5 mm to 3.5 mm. Radius R2 may be similar to R1 but not necessary the same. The radius R1 and radius R2 are preferably larger than thickness T1 by a factor of 2 to 3. This factor of 2 to 3 is particular for roll forming production procedures.

[0098] The frame 6 may be made preferably of extrusion of metal materials, in particular of aluminum, with surface anodized. The height H2 of frame 6 preferable in the range 10 mm to 60 mm, in particular 20 mm to 25 mm for solar panel sizes comparable to existing sizes. The preferred height H2 range increases accordingly to the increase of solar panel size. The thickness T2 of frame 6 in general may vary slightly and preferably in the range of 0.5 mm to 2 mm, in particular 1 mm to 1.5 mm.

[0099] The height H3 of the locking element 12 preferably in the range 0.5 mm to 4 mm, in particular 2 mm. The smaller value of H3 allows easier engage by moving in direction B, as in FIG. 26, while the bigger value of H3 allows larger locking force F52 on the frame 6, and still can be easily engage by tuming in direction C, as in FIG. 27.

[0100] When frame 6 and rail 2 engaged, the forces of F52, F53, F54, F55 as well as the weight W of solar panel and the wind load Fw from wind, balance as below:

F54=F52*Cos(δ)

[0101] The balance of forces ensures no lateral movement in direction A between frame 6 and rail 2.

½W+F55=F52*Sin(δ)+F53+½Fw

[0102] The balance of forces ensures no vertical movement in direction D between frame 6 and rail 2. These forces also provide support to the weight W of solar panel, as well as balance the wind load Fw as it happens. Furthermore, these forces between frame 6 and rail 2, generate friction force Ff between frame 6 and rail 2. The friction force Ff represents a combination of friction forces generated by forces F52, F53, F54 and F55. It is an option, however, to later add a locking pin between the frame 6 and rail 2 to further ensure no unwanted sliding between frame 6 and rail 2, along the direction E. This most preferred case according to this invention may engage by inserting tongue 28 of rail 2 into groove 16 of frame 6 in the moving direction B, or in the turning direction C. This preferred case optimized the materials uses that are to use the same materials, in particular, steel for rail and aluminum for frame. This case also optimized the production procedures, in particular, produce rail by roll forming and produce frame by extrusion and anodizing. Furthermore, this preferred case according to this invention optimized installation procedures with both parallel moving to engage as well as turning to engage, creating the snap-n-lock effect, illuminating or reducing installer tolerance and error, thus increase installation efficiency and speed. This most preferred case provides coupling tongue and groove on the two opposite long edges, wherein not on the two opposite short edges. In this case, the frame on the two opposite short edges are similar on the upper section, but without coupling groove on the lower section.

[0103] The most desired benefits may be derived from this invention are the optimization of combined benefits, namely, reduction of materials usage, reduction of solar panel thickness thus of packaging and shipping cost, increase of installation speed, among other benefits.

[0104] An important characteristic herein consists in that the coupling tongue 28 and groove 16 are provided with locking elements 12, in engaged condition with the panels in a common plane, exert a tension force upon each other, as a result of which the engaged frame 6 and rail 2 are locked to each other in compression and with friction force. As represented, this is realized preferably by providing the coupling parts with an elastically yieldable or bendable materials, in this case the aluminum frame and steel rail, which, in engaged condition, is at least partially deformed and in this way creates tension forces which results in the engaged frame 6 of solar panels 1 being locked to rail 2.

[0105] Due to, on one hand, the contact forces F52-F55, and, on the other hand, the fact that these tension forces F52-F55 are created, friction forces are produced for sliding along direction E, as a result of which the solar panels 1 are locked to the rail in compression and friction. The friction forces can be configured by adjusting the dimension of coupling parts so that no locking pins or bolts are needed to prevent later drifting along rail edge. Preferably, the angle E of the guiding plane 30 of tongue 28 in range 5° to 45°, in particular 30°, and the contacting angle δ of surface 31 of locking element 12 in range 5° to 45°, in particular 30°. The optimized choices of values ε and δ relate to the elasticity of the frame 6 and rail 2 materials, the thickness T, the pushing force in direction B as well as the locking forces F52-F55 and the friction forces accordingly. Although the locking force F52-F55 preferably are delivered by the aforementioned frame 6 and rail 2, the invention does not exclude other forms of locking elements or structures whereby these forces are delivered by other compression contacts.

[0106] It is noted that the deformation of compression is relatively small, for example, several hundredths up to several tenths of a millimeter, and does not have an influence upon the glass attached to frame nor the rail that may be fixed on racking.

[0107] Due to the fact that the compression contacts may be not uniform along the solar panel edge, at the initial installation, this uneven distribution of compression may be cured afterwards due to the wind load force on solar panel as well as due to repeated heat cycles of weather, or due to tracking, such as on single axle tracking system. This leads to further stable and uniform locking engagement of frame and rail.

[0108] According to a variant of the invention, the tension force can also be supplied by means of an added pin or bolt to the integrated tongue and groove, as an option.

[0109] A further particular characteristic of the embodiment of FIG. 25-27, consist in that the solar panels 1 with frame 6 can be selectively engaged by means of a tuming movement in direction C, as represented in FIG. 27, preferably in such a manner that, during the engagement by means of the turning movement with the coupling parts partially engaged, maximum compression forces F52-F55 result in the coupling parts. The advantage of this consists in that the solar panels 1 can be engaged easily by means of a turning movement, without necessitating use of a tool therefore. It is also noted by the inventor that by turning, disengagement may be achieved without tool and that is the best case in the situation that the solar panel need to be replaced later, for instance, in later maintenance. Engagement and disengagement without tool or excessive force and deformation ensures that the solar panel intact during installation and repair processes.

[0110] According to the invention, such as in FIG. 2-5, although the locking forces on the frame at one side 4 may be also balanced by the locking forces on another side 5, it is not preferred nor recommended by inventor due to the consideration that strain forces on frame on one side 4 and another side 5, may affect the connections in between these two sides, which include the engagement of glass and frame. The engagement strength may or may not sustain the strain between these two sides 4 and 5.

[0111] According to the invention, in the case that the four sides 4-5, 54-55 as shown in FIGS. 1A and 18, are provided with coupling frame 6-7, as in FIGS. 2-5, these coupling parts can be formed in such a manner that in one direction a firmer engagement than in the other direction is effected. In the case of elongated solar panels 1, for example, such as represented in FIGS. 1A and 1B, the locking at the small sides 54-5 may be more pronounced or less pronounced than, or equal to, at the longitudinal sides 4-5. The layout of solar panels may affect the engagement on long side or short side.

[0112] These differences in engagement can be obtained by configuring the contact surface 30 of tongue 28 and contact surface of locking element 12 of groove 16, as in FIG. 25 with different angles δ and ε.

[0113] In the preferred form of the invention, the solar panels 1 comprise coupling tongue 28, as in FIG. 25, exhibiting one of the following or the combination of two or more of the following features: [0114] Curvature 32 is circular with radius R1, at the lower side of the tongue 28 and a curvature at the lower corner 33 of groove 16, which form a guidance when turning solar panels 1 into locking position with rail 2, with the advantage that the solar panels 1 can be engaged into each other easily during installation; [0115] Angles δ and ε are the same or similar, with the advantages that the locking elements can easily shift over each other during their turning engagement, or during disassembly of the solar panels 1 and that the locking elements will not be damaged, for example, permanent deformation of frame and/or rail, even if the solar panels are engaged and disassembled; [0116] Dust chambers 34, as in FIG. 25, between tongue and groove, of the engaged solar panels 1, and rail 2, with the advantage that inclusions which get between the solar panels 1 during the engagement do not exert an adverse influence upon good engagement; [0117] A ramp surface 35, as shown in FIGS. 25-26, formed at the outer side of the locking element 12, with the advantage that the surface 30 of tongue 28 shifts smoothly over each other and that both tongue 28 and groove 16 deform uniformly; [0118] Contact surfaces 36, as in FIG. 25, formed by the upper side of the groove 16, which, is flat and run parallel to the plane which is defined by the solar panels 1, as well as lower contact surface cooperating with each other, formed by surface 37 at lower side of groove 16, with the advantage that no mutual displacement in height between two engaged solar panels 1 is possible, even if the insertion depth of the tongue 28 into the groove 16 should vary due to various causes; in other words, no height differences may occur between the adjacent solar panels.

[0119] In the embodiment of FIGS. 23 to 27, all these characteristics are combined; it is, however, clear that, as becomes evident from FIGS. 6-22B, these features can also be provided separately or in a limited combination with one another.

[0120] As becomes evident from FIGS. 6-27, an important characteristic of the preferred embodiment of the invention consists in that the cooperative locking element, in other words, the portion providing for the snap-n-lock and engagement effect, are situated in that portion of the upper lip 12 of the groove on frame side, or situated in the portion of the lower lip of the groove on rail side, wise versa, which extends beyond the distal edge of the lip 12.

[0121] It is obvious that the coupling tongue and groove can be shaped by extrusion, and can be shaped by roll forming or even by means of milling process.

[0122] According to a particular characteristic of the invention, the frame 6 of solar panels 1 are treated with oxidation before assembled with glass, more particularly a surface treatment process, which preferably is chosen from the following series of processes: anodic oxide coating, coloration, coating, mechanical surface treatment, chemical film coating, bright anodic oxide coating (gloss treatment), enamel coating, plating and no treatment. In addition, new technologies have been developed including ion plating and sputtering. Among these aforementioned treatments, the preferred treatment is anodic oxide coating.

[0123] According to a particular characteristic of the invention, the rail 2 is treated with zinc coating, more particularly a surface treatment process, which preferably is chosen from the following series of processes: galvanizing, plating, burnishing, spray, paint, anodizing and mgni coating. Among these aforementioned treatments, the preferred treatment is galvanizing and/or megni coating. The surface treatment process may be before roll forming processes, or may be after roll forming processes.

[0124] These surface treatments also offers the advantage that, at least in the long life span of solar system in the out door environment, the aforementioned solar panel frame and rail remain protective from rust. For use of stainless steel materials, or other materials that with weather sustaining characteristics, surface treatment may be not necessary.

[0125] The present invention is in no way limited to the forms of embodiment described by way of examples and represented in the aforementioned figures, however, can such solar panel and rail be embodied in various forms and dimensions without departing from the scope of the invention.

[0126] For example, the various characteristics, which are described by means of the presented embodiments or presented examples, may be selectively combined with each other.

[0127] Furthermore, all embodiments of coupling elements described before can be applied at the longer side as well as at the shorter side of a solar panel, or only the longer side or only the shorter side has such coupling elements from this invention.

[0128] Again, as noted, the tongue may be on frame side or on rail side, with the groove on opposite side.

[0129] FIG. 1A represents a schematic diagram of solar panels assembled for fixed tiled solar system, with rails and frames coupled according to this invention

[0130] FIG. 1B represents a schematic diagram of solar panels assembled for single axle tracking solar system, with rails and frames coupled according to this invention

[0131] FIG. 2 represents schematic cross sections of a solar panel, single glass, with frame according to this invention, glass inserts into groove

[0132] FIG. 3 represents schematic cross sections of a solar panel, double glass, with frame according to this invention, glass inserts into groove

[0133] FIG. 4 represents schematic cross sections of a solar panel, single glass, with frame according to this invention, glass glued on frame

[0134] FIG. 5 represents schematic cross sections of a solar panel, double glass, with frame according to this invention, glass glued on frame

[0135] FIG. 6-15 represent cross sections of several rail design embodiments with tongue according to this invention

[0136] FIG. 6-19 represent cross section of several frame design embodiments with groove according to this invention. FIG. 16B represents cross section of frame with glass glued on. Other frames are similar relative to the change from cross section in FIG. 16 to FIG. 16B.

[0137] FIG. 20-22 represents cross section of an embodiment of frame design with tongue and rail design with groove. It further shows the uniform thickness of frame and rail.

[0138] FIG. 23-27 represent cross section of a most preferred embodiment of frame and rail with tongue and groove, as well as locking element, according to this invention. The solar panel and rail may engage, by slide along the edge of tongue and groove, by slide perpendicular to the edge of tongue and groove (FIG. 26), and by turning to snap-in (FIG. 27).

TABLE-US-00001 6, 7 - frames F52 - force on frame by tongue 12, 13 - locking element F3 - force on tongue by upper 15 - tongue side of frame groove 16 - groove F53 - force on frame by tongue 17 - curve on the tongue D - up down moving direction 18 - lower side of the groove A - Lateral movement direction 19 - upper side of the tongue perpendicular to rail 20 - upper side of the groove E - Lateral movement direction W - weight of solar panel perallel to rail Fw - wind force on solar panel α - direction of locking F1 - force on tongue by lower element surface side of frame groove β - direction of lower groove F51 - force on frame by tongue surface F2 - force on tongue by locking element of frame

Notations for FIG. 8 References Signs

[0139]

TABLE-US-00002 1 - solar panel Ff - friction force on frame 2 - rail F52 - force on frame locking 6 - frame element by tongue 12 - locking element F53 - force on frame upper side of 16 - groove groove by tongue 28 - tongue F54 - force on frame side wall of 30 - guiding plane of tongue groove by tongue 31 - surface of locking element F55 - force on frame lower side of 32 - curvature of tongue groove by tongue 33 - inner corner of groove D - up down moving direction 34 - dust chamber A - Lateral movement direction 35 - ramp surface perpendicular to rail 36 - contact surface E - Lateral movement direction 37 - surface of lower side of groove parallel to rail T1 - rail thickness δ - direction of locking element W - weight of solar panel surface Fw - wind force on solar panel ε - guiding surface angle

[0140] Notations for FIG. 23-27 references signs