Solar panel

1. A method for manufacturing a solar module, the method comprising:

arranging silicon solar cells in line with sides of adjacent silicon solar cells overlapping in a shingled manner, each silicon solar cell comprising a front surface, an oppositely positioned rear surface, an n-p junction between the front and rear surfaces, and a rear surface metallization pattern;

conductively bonding, for pairs of adjacent silicon solar cells, the rear surface of one of the silicon solar cells to a front surface of the other silicon solar cell to electrically and mechanically connect the silicon solar cells in series to form a first super cell comprising a shingled string of solar cells;

conductively bonding a first conductive metal ribbon to the rear surface metallization pattern of a first end silicon solar cell located at a first end of the first super cell to provide an electrical output from the first super cell having a first polarity; and

conductively bonding a second conductive metal ribbon to the rear surface metallization pattern of a second end silicon solar cell located at a second end of the first super cell to provide an electrical output from the first super cell having a second polarity opposite from the first polarity,

where the rear surface metallization of the first and second end silicon solar cells are both disposed on then side of the n-p junction or the rear surface metallization of the first and second end silicon solar cells are both disposed on the p side of the n-p junction.

2. The method of claim 1 , wherein each of the plurality of silicon solar cells have identical front and rear surface metallization patterns.

3. The method of claim 1 , further comprising:

arranging a plurality of super cells including the first super cell side-by-side and physically parallel with each other;

electrically connecting a first intermediate silicon solar cell located at a position intermediate between the ends of the first super cell to a correspondingly positioned solar cell in each of the other super cells in the plurality by one or more conductive interconnects extending transversely to the plurality of super cells.

4. The method of claim 3 , wherein the one or more conductive interconnects extend transversely to the plurality of super cells electrically to segment each of the super cells into two or more groups of solar cells, and each group of solar cells is electrically in parallel with a corresponding bypass diode.

5. The method of claim 1 , wherein the method further comprises arranging the first super cell to span or substantially span the solar module from a first edge of the solar module to an oppositely positioned second edge of the solar module.

6. The method of claim 5 , wherein the method further comprises:

arranging the first end silicon solar cell adjacent to and spaced apart from the first edge of the solar module by a first distance;

arranging the second end silicon solar cell adjacent to and spaced apart from the second edge of the solar module by a second distance; and

the second distance is greater than the first distance such that the portion of the first super cell excluding the first end silicon solar cell is centered lengthwise along the solar module between the first edge and the second edge.

7. The method of claim 1 , wherein conductively bonding the second conductive metal ribbon to the rear surface metallization pattern of the second end silicon solar cell comprises conductively bonding the second conductive metal ribbon to a plurality of rear surface discrete contact pads of the rear surface metallization pattern of the second end silicon solar cell.

8. The method of claim 1 , wherein the method further comprises:

operating a first conveyor belt to advance the shingled string of solar cells across a gap between the first conveyor belt and a second collinearly arranged conveyor belt, the shingled string of solar cells thereby supported by the first conveyor belt and the second conveyor belt; and

making a laser cut through a solar cell positioned over the gap between the first conveyor belt and the second conveyor belt to separate the shingled string of solar cells.

9. The method of claim 8 , comprising making the laser cut in a direction transverse to the long axis of the first super cell in a solar cell that is located at an end of the first super cell and overlaps a front surface of its adjacent solar cell, the laser cut trimming off a portion of the solar cell and thereby narrowing the solar cell.

10. A method for manufacturing a solar module, the method comprising:

forming a plurality of super cells by arranging silicon solar cells in line with sides of adjacent silicon solar cells overlapping in a shingled manner, each silicon solar cell comprising a front, an oppositely positioned rear surface, an n-p junction between the front and rear surfaces, and a rear surface metallization pattern; and

conductively bonding, for pairs of adjacent silicon solar cells, the rear surface of one of the silicon solar cells to a front surface of the other silicon solar cell to electrically and mechanically connect the silicon solar cells in series;

arranging the plurality of super cells side-by-side and physically parallel with each other;

conductively bonding a first conductive metal ribbon to the rear surface metallization pattern of a first end silicon solar cell located at a first end of each of the plurality of super cells to provide an electrical output from each super cell having a first polarity; and

conductively bonding a second conductive metal ribbon to the rear surface metallization pattern of a second end silicon solar cell located at a second end of each of the plurality of super cells to provide an electrical output from each super cell having a second polarity opposite from the first polarity,

where the rear surface metallization of the first and second end silicon solar cells are both disposed on then side of the n-p junction or the rear surface metallization of the first and second end silicon solar cells are both disposed on the p side of the n-p junction.

11. The method of claim 10 , further comprising:

electrically connecting a plurality of first intermediate silicon solar cells located at a first intermediate position between the ends of each super cell via one or more conductive interconnects extending transversely to the plurality of super cells.

12. The method of claim 11 , further comprising:

electrically connecting a plurality of second intermediate silicon solar cells located at a second intermediate position between the ends of each super cell via one or more conductive interconnects extending transversely to the plurality of super cells.

13. The method of claim 11 , wherein the one or more conductive interconnects extend transversely to the plurality of super cells electrically to segment each of the super cells into two or more groups of solar cells.

14. The method of claim 13 , further comprising electrically connecting each group of solar cells in parallel with a corresponding bypass diode.

15. The method of claim 14 , further comprising electrically connecting each group of solar cells in parallel with a corresponding bypass diode in a junction box by one or more longitudinally extending conductors.

16. The method of claim 10 , wherein arranging the plurality of super cells side-by-side and physically parallel with each other comprises arranging the plurality of super cells front surface side down on a transparent front sheet in a physical configuration desired for the module such that the first and second conductive metal ribbons are arranged in the desired physical configuration on the rear surfaces of the super cells.

17. The method of claim 10 , wherein the method further comprises positioning an encapsulant layer between the plurality of super cells and a transparent front sheet.

18. The method of claim 10 , wherein the method further comprises centering the super cells lengthwise along the length of the solar module.