Tiled solar cell laser process
Abstract
In an example, the present invention provides a method of separating a photovoltaic strip from a solar cell. The method includes providing a solar cell, placing the front side of the solar cell on a platen such that the backside is facing a laser source, initiating a laser source to output a laser beam having a wavelength from 200 to 600 nanometers and a spot size of 18 to 30 microns, subjecting a portion of the backside to the laser beam at a power level ranging from about 20 Watts to about 35 Watts to cause an ablation to form a scribe region having a depth, width, and a length, the depth being from 40% to 60% of a thickness of the solar cell, the width being between 16 and 35 microns to create a plurality of scribe regions spatially disposed on the backside of the solar cell.
Claims
exact text as granted — not AI-modified1 . A method comprising:
providing a solar cell comprising either a single crystalline silicon material or a polycrystalline solar cell, the solar cell having a backside and a front side and a thickness, the backside having a metal material; placing the front side of the solar cell on a platen such that the backside is facing a laser source; initiating a laser source to output a laser beam; subjecting a portion of the backside to the laser beam to cause an ablation to form a scribe region having a depth, width, and a length, the depth being from 40% to 60% of the thickness of the solar cell, and the length being equivalent to a length of the solar cell; removing a vaporized material from a vicinity of the ablation; capturing the vaporized material using a vacuum; and applying stress to initiate a crack separating the solar cell into a first piece and a second piece.
2 . The method of claim 1 wherein removing the vaporized material comprises subjecting a fluid, using a laminar flow, within the vicinity of the ablation.
3 . The method of claim 1 wherein removing the vaporized material comprises delivering a jet of fluid to the vicinity of the ablation.
4 . The method of claim 1 wherein applying the stress comprise applying mechanical stress.
5 . The method of claim 1 wherein the first piece comprises a fracture plane.
6 . The method of claim 5 further comprising removing the solar cell from a laser system prior to the applying stress to initiate the crack.
7 . The method of claim 1 wherein the laser beam has a wavelength in an ultraviolet (UV) portion of the spectrum.
8 . The method of claim 1 wherein the laser source comprises an infrared (IR) laser.
9 . The method of claim 1 wherein the scribe region is shaped as a notch as viewed along an end of the scribe region.
10 . The method of claim 1 wherein the scribe region is V-shaped.
11 . The method of claim 1 wherein the scribe region is a straight line +/−10 microns.
12 . The method of claim 1 wherein the thickness is from 170 to 220 microns.
13 . The method of claim 1 wherein the length is 156 mm+/−2 mm.
14 . The method of claim 1 wherein the depth is between about 65 and 132 microns.
15 . The method of claim 1 wherein the width is from about 15% to 40% of the depth.
16 . The method of claim 1 wherein the width is from about 7% to 20% of the thickness.
17 . The method of claim 1 wherein subjecting the portion of the backside to the laser beam comprises applying the laser beam at a repetition rate of between about 100-300 kHz.
18 . The method of claim 5 wherein the strip has a width of about ⅙th a width of the solar cell.
19 . The method of claim 1 wherein subjecting the portion of the backside to the laser beam is performed at a height varying not more than +/−50 μm.
20 . The method of claim 19 wherein the width varies by 5 μm or less along the length.Cited by (0)
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