IP Library Granted Patent US 12,396,270
Granted Patent B2
US 12,396,270 · App. 17/759,085 · Granted Aug 19, 2025

Method of manufacturing a solar cell with integral cover glass, and cell obtained

Inventors: Erminio Greco (Milan, IT); Mariacristina Casale (Milan, IT); Roberta Campesato (Milan, IT)
Assignee: CESI—Centro Elettrotecnico Sperimentale Italiano Giacinto Motta S.p.A.
H10F19/807H10F77/311
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,396,270
App. No.
17/759,085
Granted
Aug 19, 2025
Kind
B2
Abstract

Method of manufacturing a solar cell, comprising: providing a solar cell ( 100 ) having an active surface ( 105 a ) intended, in use, to be exposed to sunlight; forming, in correspondence of said active surface, a protection against low-energy protons and other radiations harmful to the solar cell. Forming a protection comprises forming a layer of resin ( 110; 210 ) and forming by deposition of material on the resin layer a layer of protective material ( 115; 215 b ) on top of the resin layer.

Claims (28)

1. Method of fabrication of a semiconductor space solar cell for uses in the space or at high altitude in atmosphere, comprising:

providing a semiconductor solar cell having an active surface which, in use, is intended to be exposed to sunlight for performing photovoltaic conversion;

forming, in correspondence of said active surface, a protection against low-energy protons harmful to the solar cell,

characterized in that

said forming a protection comprises:

forming an adhesive layer of resin and

forming by means of deposition of material on the adhesive layer of resin a single layer of a non-conductive protective material, transparent in an electromagnetic radiation frequency range in which the solar cell is intended to perform the photovoltaic conversion, over the adhesive layer of resin, wherein said forming by means of deposition of material comprises a process or processes of physical vapour deposition—“PVD”,

wherein said single layer of a non-conductive protective material has a thickness greater than 2 μm.

2. Method according to claim 1 , wherein said adhesive layer of resin is formed directly on the active surface of the solar cell.

3. Method according to claim 1 , further comprising:

forming by means of deposition of material a further layer of protective material interposed between the adhesive layer of resin and the active surface of the solar cell.

4. Method according to claim 3 , wherein said forming by means of deposition of material a further layer of protective material interposed between the adhesive layer of resin and the active surface of the solar cell comprise a process or processes of physical vapour deposition—“PVD”.

5. Method according to claim 3 , wherein said further layer of protective material has a thickness greater than 2 μm.

6. Method according to claim 3 , wherein said further layer of protective material comprise or consist of layers of oxide.

7. Method according to claim 6 , wherein said further layer of protective material comprises or consists of one or more layers of SiO 2 and/or Al 2 O 3 and/or Ta 2 O 5 and/or Nb 2 O 5 and/or Y 2 O 3 and/or TiO 2 and/or Sc 2 O 3 and/or CeO 2 and/or HfO 2 and/or SnO 2 and/or LaTiO 3 and/or other materials transparent in the range of frequencies exploited by the solar cell for performing the photovoltaic conversion, comprising MgF 2 and/or CeF 3 and/or ZnS and/or Si 3 N 4 .

8. Method according to claim 4 , wherein said forming by means of deposition of material a further layer of protective material interposed between the adhesive layer of resin and the active surface of the solar cell comprise one among the processes of: thermal evaporation, electron beam, pulsed-laser deposition—“PLD”, sputtering.

9. Method according to claim 1 , wherein said single layer of protective material comprise or consist of layers of oxide.

10. Method according to claim 9 , wherein said layers of oxide comprise or consist of one or more layers of SiO 2 and/or Al 2 O 3 and/or Ta 2 O 5 and/or Nb 2 O 5 and/or Y 2 O 3 and/or TiO 2 and/or Sc 2 O 3 and/or CeO 2 and/or HfO 2 and/or SnO 2 and/or LaTiO 3 and/or other materials transparent in the range of frequencies exploited by the solar cell for performing the photovoltaic conversion, comprising MgF 2 and/or CeF 3 and/or ZnS and/or Si 3 N 4 .

11. Method according to claim 1 , wherein said phase of forming an adhesive layer of resin comprises a process of deposition.

12. Method according to claim 1 , further comprising:

forming alternated adhesive layers of resin and layers of protective material repeated more times over said single layer of a non-conductive protective material.

13. Method according to claim 12 , wherein said alternated adhesive layers of resin and layers of protective material comprise a topmost layer of protective material, the method further comprising:

forming anti-reflecting layers on the topmost layer of protective material.

14. Method according to claim 1 , further comprising:

forming anti-reflecting layers on the single layer of protective material.

15. Method according to claim 1 , wherein said semiconductor solar cell is a III-V solar cell in compounds of groups III and V of the periodic table of the elements.

16. Method according to claim 15 , wherein said semiconductor solar cell is a solar cell in one among: gallium arsenide (GaAs), Indium and Gallium phosphide (InGaP).

17. Method according to claim 1 , wherein said process or processes of physical vapour deposition—“PVD”—comprises one among: thermal evaporation, electron beam, pulsed-laser deposition—“PLD”, sputtering.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 2, 2023
From: GRECO, ERMINIO; CASALE, MARIACRISTINA; CAMPESATO, ROBERTA
To: CESI - CENTRO ELETTROTECNICO SPERIMENTALE ITALIANO GIACINTO MOTTA S.P.A.
Reel/Frame 064473/0107 →
Priority Claims (1)
IT 102020000001051 · Jan 21, 2020 · national
Continuity (1)
Related Publication 20230039806A1 · Feb 9, 2023
References Cited (16)
US 3780424A · Forestieri · 1973 [cited by examiner]
US 8974899B1 · Wilt · 2015 [cited by applicant]
US 20090075098A1 · Tsukahara · 2009 [cited by examiner]
US 20100078075A1 · Tsukahara · 2010 [cited by examiner]
US 20100297798A1 · Adriani · 2010 [cited by examiner]
US 20120090661A1 · Capps et al. · 2012 [cited by applicant]
US 20120228668A1 · Thoumazet · 2012 [cited by examiner]
US 20140007924A1 · Gray · 2014 [cited by applicant]
US 20190172955A1 · Kruse · 2019 [cited by examiner]
RU 2584184C1 · 2016 [cited by examiner]
Machine translation of RU2584184C1 (Year: 2016). [cited by examiner]
Hadi Shaima M. et al, “Stopping power and range of proton interaction with AL203, Zr02 and Si02”, AIP Conference Proceedings 2201, 020017 (2019); https://doi.org/10.1063/1.5148441, Published Online: Dec. 17, 2019. [cited by applicant]
Capali Veli et al., “Geant4 calculations for space radiation shielding material Al203”, EPJ Web of Conferences 100, 02002 (2015), 2015, DOI:10.1021/epjconf/201510002002. [cited by applicant]
D. Roth et al., “Electronic Stopping of Slow Protons in Oxides: Scaling Properties” Physical Review Letters, Oct. 20, 2017; PRL 119, 163401 (2017); DOI: 10.1103/PhysRevLett.119.163401. [cited by applicant]
Roberta Campesato et al., “Effective Coating for High Efficiency Triple Junction Solar Cells”, Published in 2019 European Space Power Conference (ESPC); Date of Conference: Sep. 30, 2019-Oct. 4, 2019; DOI: 10.1109/ESPC.… [cited by applicant]
Samuel F. Pellicori et al., “Development and testing of coatings for orbital space radiation environments”, Applied Optics, vol. 53, No. 4, Feb. 1, 2014; Published Jan. 23, 2014; Doc. ID 195444; XP-001587806. [cited by applicant]