IP Library Granted Patent US 10,090,430
Granted Patent B2
US 10,090,430 · App. 15/359,326 · Granted Oct 2, 2018

System for manufacturing a shingled solar cell module

Inventors: Ratson Morad (Palo Alto, CA); Gilad Almogy (Palo Alto, CA); Itai Suez (Santa Cruz, CA); Jean Hummel (San Carlos, CA); Nathan Beckett (Oakland, CA); Yafu Lin (San Jose, CA); John Gannon (Oakland, CA); Michael J. Starkey (Santa Clara, CA); Robert Stuart (Arcata, CA); Tamir Lance (Los Gatos, CA); Dan Maydan (Los Altos Hills, CA)
Assignee: SunPower Corporation
H01L31/186H01L31/02008H01L31/0508Y02E10/50
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Quick Facts
Patent No.
US 10,090,430
App. No.
15/359,326
Granted
Oct 2, 2018
Kind
B2
Abstract

A high efficiency configuration for a solar cell module comprises solar cells conductively bonded to each other in a shingled manner to form super cells, which may be arranged to efficiently use the area of the solar module, reduce series resistance, and increase module efficiency. The front surface metallization patterns on the solar cells may be configured to enable single step stencil printing, which is facilitated by the overlapping configuration of the solar cells in the super cells. A solar photovoltaic system may comprise two or more such high voltage solar cell modules electrically connected in parallel with each other and to an inverter. Solar cell cleaving tools and solar cell cleaving methods apply a vacuum between bottom surfaces of a solar cell wafer and a curved supporting surface to flex the solar cell wafer against the curved supporting surface and thereby cleave the solar cell wafer along one or more previously prepared scribe lines to provide a plurality of solar cells. An advantage of these cleaving tools and cleaving methods is that they need not require physical contact with the upper surfaces of the solar cell wafer. Solar cells are manufactured with reduced carrier recombination losses at edges of the solar cell, e.g., without cleaved edges that promote carrier recombination. The solar cells may have narrow rectangular geometries and may be advantageously employed in shingled (overlapping) arrangements to form super cells.

Claims (42)

1. A system, comprising:

a scriber to form a plurality of scribe lines in a solar cell wafer;

a printer to apply an electrically conductive bonding material to the solar cell wafer; and

a belt to, after the electrically conductive bonding material is applied to the solar cell wafer, separate the solar cell wafer along the scribe lines to provide a plurality of physically separated solar cell strips.

2. The system according to claim 1 , wherein the belt is a perforated belt and a vacuum manifold applies a vacuum to a bottom surface of the solar cell wafer.

3. The system according to claim 1 , wherein the printer is a screen, ink jet, or mask printer.

4. The system according to claim 1 , wherein the scriber is a laser scriber.

5. A system, comprising:

means for scribing a solar cell wafer to form a plurality of scribe lines in the solar cell wafer;

means for applying an electrically conductive bonding material to the solar cell wafer; and

means for separating, after the applying the electrically conductive bonding material to the solar cell wafer, the solar cell wafer along the scribe lines to provide a plurality of physically separated solar cell strips.

6. The system of claim 1 , comprising a vacuum manifold, wherein:

the belt advances the solar cell wafer along a surface of the vacuum manifold;

the vacuum manifold applies a vacuum to a bottom surface of the solar cell wafer through perforations in the belt to pull the solar cell wafer against the surface of the vacuum manifold; and

as the belt advances the solar cell wafer along the surface of the vacuum manifold the solar cell wafer is flexed by the vacuum against a curved portion of the surface of the vacuum manifold to thereby cleave the solar cell wafer along one or more of the scribe lines.

7. The system of claim 6 , wherein the vacuum applied to the bottom surface of the solar cell wafer by the vacuum manifold varies along the direction in which the solar cell wafer is advanced and is strongest in a region of the surface of the vacuum manifold in which the solar cell wafer is cleaved.

8. The system of claim 6 , wherein the perforations in the belt are arranged so that leading and trailing edges of the solar cell wafer along the direction in which the solar cell wafer is advanced must overlie at least one perforation in the belt.

9. The system of claim 6 , wherein:

the surface of the vacuum manifold comprises a flat region, a transitional curved region adjoining the flat region and having a first curvature, and a cleave region adjoining the transitional curved region and having a second curvature tighter than the first curvature; and

the belt advances the solar cell wafer along the flat region, then into and through the transitional region, then into the cleave region where the solar cell wafer is cleaved along one or more of the scribe lines.

10. The system of claim 9 , wherein the vacuum manifold applies a stronger vacuum in the cleave region than in the flat region.

11. The system of claim 9 , wherein:

the surface of the vacuum manifold comprises a post-cleave region adjoining the cleave region and having a third curvature tighter than the second curvature;

the belt advances solar cell strips cleaved from the solar cell wafer from the cleave region into the post-cleave region; and

the third curvature is sufficiently tight to prevent cleaved edges of sequentially cleaved solar cell strips from touching as the cleaved solar cell strips are advanced by the belt.

12. The system of claim 11 , wherein the vacuum manifold applies a stronger vacuum in the cleave region than in the flat region and the post-cleave region.

13. The system of claim 6 , wherein the vacuum applied by the vacuum manifold causes an asymmetric stress distribution along a scribe line that promotes nucleation and propagation of a single cleaving crack along the scribe line.

14. A system comprising:

a vacuum manifold having a surface; and

a belt that advances a solar cell wafer along the surface of the vacuum manifold;

wherein the vacuum manifold applies a vacuum to a bottom surface of the solar cell wafer to flex the solar cell wafer against a curved portion of the surface of the vacuum manifold and thereby sequentially cleave the solar cell along a plurality of scribe lines in the solar cell wafer.

15. The system of claim 14 , wherein:

the surface of the vacuum manifold comprises a flat region, a transitional curved region adjoining the flat region and having a first curvature, and a cleave region adjoining the transitional curved region and having a second curvature tighter than the first curvature; and

the belt advances the solar cell wafer along the flat region, then into and through the transitional region, then into the cleave region where the solar cell wafer is cleaved along one or more of the scribe lines.

16. The system of claim 15 , wherein the vacuum manifold applies a stronger vacuum in the cleave region than in the flat region.

17. The system of claim 15 , wherein:

the surface of the vacuum manifold comprises a post-cleave region adjoining the cleave region and having a third curvature tighter than the second curvature;

the belt advances solar cell strips cleaved from the solar cell wafer from the cleave region into the post-cleave region; and

the third curvature is sufficiently tight to prevent cleaved edges of sequentially cleaved solar cell strips from touching as the cleaved solar cell strips are advanced by the belt.

18. The system of claim 14 , wherein the vacuum applied by the vacuum manifold causes an asymmetric stress distribution along a scribe line that promotes nucleation and propagation of a single cleaving crack along the scribe line.

19. The system of claim 14 , comprising a laser scriber that forms the plurality of scribe lines in the solar cell wafer.

20. The system of claim 14 , comprising a printer that applies an electrically conductive bonding material to the solar cell wafer before the solar cell wafer is cleaved.

Assignments (5)
SECURITY INTEREST Recorded Jun 27, 2024
From: MAXEON SOLAR PTE. LTD.
To: DB TRUSTEES (HONG KONG) LIMITED
Reel/Frame 067924/0062 →
SECOND LIEN SECURITY INTEREST AGREEMENT Recorded Jun 26, 2024
From: MAXEON SOLAR PTE. LTD
To: DB TRUSTEES (HONG KONG) LIMITED
Reel/Frame 071343/0553 →
SECURITY INTEREST Recorded Jun 5, 2024
From: MAXEON SOLAR PTE. LTD.
To: DB TRUSTEES (HONG KONG) LIMITED
Reel/Frame 067637/0598 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 24, 2023
From: SUNPOWER CORPORATION
To: MAXEON SOLAR PTE. LTD.
Reel/Frame 062490/0742 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 9, 2018
From: MORAD, RATSON; ALMOGY, GILAD; SUEZ, ITAI; HUMMEL, JEAN; BECKETT, NATHAN; LIN, YAFU; GANNON, JOHN; STARKEY, MICHAEL J.; STUART, ROBERT; LANCE, TAMIR; MAYDAN, DAN
To: SUNPOWER CORPORATION
Reel/Frame 046295/0074 →
Continuity (39)
Continuation PCTUS2015032472 · May 26, 2015
Continuation In Part 29506415 · Oct 15, 2014
Continuation In Part 29506755 · Oct 20, 2014
Continuation In Part 14530405 · Oct 31, 2014
Continuation In Part 14532293 · Nov 4, 2014
Continuation In Part 29508323 · Nov 5, 2014
Continuation In Part 14536486 · Nov 7, 2014
Continuation In Part 14539546 · Nov 12, 2014
Continuation In Part 14543580 · Nov 17, 2014
Continuation In Part 14548081 · Nov 19, 2014
Continuation In Part 29509586 · Nov 19, 2014
Continuation In Part 29509588 · Nov 19, 2014
Continuation In Part 14550676 · Nov 21, 2014
Continuation In Part 14552761 · Nov 25, 2014
Continuation In Part 14560577 · Dec 4, 2014
Continuation In Part 14566278 · Dec 10, 2014
Continuation In Part 14565820 · Dec 10, 2014
Continuation In Part 14572206 · Dec 16, 2014
Continuation In Part 14577593 · Dec 19, 2014
Continuation In Part 14586025 · Dec 30, 2014
Continuation In Part 14585917 · Dec 30, 2014
Continuation In Part 14594439 · Jan 12, 2015
Continuation In Part 14605695 · Jan 26, 2015
Continuation In Part 14674983 · Mar 31, 2015
Provisional Application 62003223 · May 27, 2014
Provisional Application 62035624 · Aug 11, 2014
Provisional Application 62036215 · Aug 12, 2014
Provisional Application 62042615 · Aug 27, 2014
Provisional Application 62048858 · Sep 11, 2014
Provisional Application 62064260 · Oct 15, 2014
Provisional Application 62064834 · Oct 16, 2014
Provisional Application 62081200 · Nov 18, 2014
Provisional Application 62082904 · Nov 21, 2014
Provisional Application 62103816 · Jan 15, 2015
Provisional Application 62111757 · Feb 4, 2015
Provisional Application 62113250 · Feb 6, 2015
Provisional Application 62134176 · Mar 17, 2015
Provisional Application 62150426 · Apr 21, 2015
Related Publication 20170077343A1 · Mar 16, 2017