STRINGS OF SOLAR CELLS HAVING LASER ASSISTED METALLIZATION CONDUCTIVE CONTACT STRUCTURES AND THEIR METHODS OF MANUFACTURE
Strings of solar cells having laser assisted metallization conductive contact structures, and their methods of manufacture, are described. For example, a solar cell string includes a first solar cell having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a first metal foil to the back side of the first solar cell. The solar cell string also includes a second solar cell having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a second metal foil to the back side of the second solar cell. The solar cell string also includes a conductive interconnect coupling the first and second solar cells, the conductive interconnect including a strain relief feature.
1 . A solar cell string, comprising:
a first solar cell having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a first metal foil to the back side of the first solar cell;
a second solar cell having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a second metal foil to the back side of the second solar cell; and
a conductive interconnect coupling the first and second solar cells, the conductive interconnect comprising a strain relief feature, wherein the strain relief feature comprises a conductive piece bonded to a portion of the first metal foil and to a portion of the second metal foil, and wherein the portion of the first metal foil is on the first solar cell, and the portion of the second metal foil is on the second solar cell.
2 . A solar cell string, comprising:
a first solar cell having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a first metal foil to the back side of the first solar cell, wherein the first metal foil has an overhang portion; and
a second solar cell having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a second metal foil to the back side of the second solar cell, wherein the second metal foil has an overhang portion, and wherein the overhang portion of the second metal foil is coupled to the overhang portion of the first metal foil by a thermocompression bond.
3 . The solar cell string of claim 2 , wherein the thermocompression bond is an aluminum-aluminum bond.
4 . A solar cell module, comprising:
a first solar cell string comprising a first plurality of solar cells, each of the first plurality of solar cells having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a metal foil to the back side of each of the first plurality of solar cells, wherein the metal foil of an end one of the first plurality of solar cells has an overhang portion folded over the back side of the end one of the first plurality of solar cells;
a second solar cell string comprising a second plurality of solar cells, each of the second plurality of solar cells having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a metal foil to the back side of each of the second plurality of solar cells, wherein the metal foil of an end one of the second plurality of solar cells has an overhang portion folded over the back side of the end one of the second plurality of solar cells;
a conductive jumper coupling the overhang portions of the metal foil of the end ones of the first and second pluralities of solar cells; and
a return ribbon coupled to the end one of the second plurality of solar cells, the return ribbon over the back side of each of the second plurality of solar cells.
5 . The solar cell module of claim 4 , further comprising:
a J-box on a portion of the return ribbon.
6 . A solar cell module, comprising:
a first solar cell string comprising a first plurality of solar cells, each of the first plurality of solar cells having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a metal foil to the back side of each of the first plurality of solar cells, wherein the metal foil has an overhang portion;
a first busbar coupling the overhang portions of the metal foil of each of the first plurality of solar cells;
a second solar cell string comprising a second plurality of solar cells, each of the second plurality of solar cells having a front side and a back side, and one or more laser assisted metallization conductive contact structures electrically connecting a metal foil to the back side of each of the second plurality of solar cells, wherein the metal foil has an overhang portion;
a second busbar coupling the overhang portions of the metal foil of each of the second plurality of solar cells; and
an end-busbar coupling the first and second busbars.
7 . The solar cell module of claim 6 , further comprising:
one or more side-to-side busbars coupling the first and second busbars.
8 . A method of fabricating a solar cell string, the method comprising:
electrically connecting a first metal foil to a back side of a first solar cell by forming one or more laser assisted metallization conductive contact structures on the first solar cell;
electrically connecting a second metal foil to a back side of a second solar cell by forming one or more laser assisted metallization conductive contact structures on the second solar cell;
coupling the first and second solar cells with a conductive interconnect; and
forming a strain relief feature in the conductive interconnect.
9 . The method of claim 8 , wherein coupling the first and second solar cells with the conductive interconnect comprises coupling an overhang portion of the first metal foil and an overhang portion of the second metal foil.
10 . The method of claim 9 , wherein forming the strain relief feature in the conductive interconnect comprises using a press or a roller.
11 . The method of claim 9 , further comprising:
smoothing the overhang portion of the first metal foil and the overhang portion of the second metal foil prior to forming the strain relief feature in the conductive interconnect.