Method of forming a buffer layer in a solar cell, and a solar cell formed by the method
09825197 · 2017-11-21
Assignee
Inventors
Cpc classification
H01L31/0749
ELECTRICITY
Y02E10/541
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
H01L31/1828
ELECTRICITY
H01L21/02614
ELECTRICITY
H01L21/02485
ELECTRICITY
H01L21/02568
ELECTRICITY
Y02E10/543
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
H01L31/18
ELECTRICITY
H01L31/0749
ELECTRICITY
H01L31/0296
ELECTRICITY
Abstract
A method of fabricating a buffer layer of a photovoltaic device comprises: providing a substrate having a back contact layer disposed above the substrate and an absorber layer disposed above the back contact layer; depositing a metal layer on the absorber layer; and performing a thermal treatment on the deposited metal layer in an atmosphere comprising sulfur, selenium or oxygen, to form a buffer layer.
Claims
1. A method of fabricating a buffer layer of a photovoltaic device comprising: providing a substrate having a back contact layer disposed above the substrate and an absorber layer disposed above the back contact layer; depositing a metal layer comprising cadmium or Zn.sub.1-xMg.sub.x on the absorber layer; and performing a thermal annealing treatment on the deposited metal layer in an atmosphere comprising sulfur or oxygen gas to transform the deposited metal layer into a buffer layer.
2. The method of claim 1, wherein the metal layer comprises cadmium, and the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S.
3. The method of claim 1, wherein the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S.
4. The method of claim 1, wherein the metal layer comprises Zn.sub.1-xMg.sub.x, and the atmosphere comprises oxygen.
5. The method of claim 1, wherein the step of depositing a metal layer on the absorber layer includes depositing from 1 nm to 1000 nm of metal.
6. The method of claim 1, wherein the step of depositing a metal layer on the absorber layer includes depositing from 5 nm to 500 nm of metal.
7. The method of claim 6, wherein the buffer layer has a thickness in a range from 13 nm to 1300 nm.
8. The method of claim 1, wherein the atmosphere further comprises an inert gas.
9. The method of claim 1, wherein the thermal treatment is a rapid thermal anneal.
10. The method of claim 8, wherein the thermal treatment is a rapid thermal anneal performed at a temperature from 300° C. to 600° C.
11. A method of fabricating a photovoltaic device comprising: providing a substrate; forming a back contact layer above the substrate; forming a copper indium gallium diselenide (CIGS) absorber layer from a plurality of CIGS precursors above the back contact layer; sputtering a metal layer on the CIGS absorber layer, the metal layer being an additional indium layer separate from the CIGS precursors ; and performing a rapid thermal anneal on the deposited metal layer in an atmosphere comprising sulfur, to form a buffer layer; and forming a front contact layer above the buffer layer.
12. The method of claim 11, wherein the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S.
13. A method of fabricating a photovoltaic device comprising: providing a substrate; forming a back contact layer above the substrate; forming an absorber layer above the back contact layer; sputtering a metal layer on the absorber layer, the metal layer comprising cadmium; and performing a thermal annealing treatment on the deposited metal layer in an atmosphere comprising sulfur gas, to form a buffer layer; and forming a front contact layer above the buffer layer.
14. The method of claim 13, wherein the atmosphere further comprises an inert gas.
15. The method of claim 1, wherein the thermal treatment is a rapid thermal anneal.
16. The method of claim 11, wherein the step of sputtering a metal layer on the absorber layer includes sputtering from 5 nm to 500 nm of metal.
17. The method of claim 11, wherein the atmosphere further comprises an inert gas.
18. The method of claim 11, wherein the rapid thermal anneal is performed at a temperature from 300° C. to 600° C.
19. The method of claim 13, wherein the step of depositing a metal layer on the absorber layer includes depositing from 5 nm to 500 nm of metal.
20. The method of claim 15, wherein the rapid thermal anneal is performed at a temperature from 300° C. to 600° C.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
(13) This description of the exemplary embodiments is intended to be read in connection with the accompanying drawings, which are to be considered part of the entire written description. In the description, relative terms such as “lower,” “upper,” “horizontal,” “vertical,”, “above,” “below,” “up,” “down,” “top” and “bottom” as well as derivative thereof (e.g., “horizontally,” “downwardly,” “upwardly,” etc.) should be construed to refer to the orientation as then described or as shown in the drawing under discussion. These relative terms are for convenience of description and do not require that the device be constructed or operated in a particular orientation.
(14) A method is disclosed for forming an n type semiconductor for the buffer layer of a solar cell. This buffer layer is formed by pre-depositing a specific metal on an absorber layer above a substrate. Subsequently the substrate is placed in a furnace to perform sulfurization, selenization or oxidation. The p-n junction is formed by this annealing process. This method reduces or avoids damage of the p-n junction, because the junction is not established until after completing the metal deposition for the buffer layer. In addition, the subsequent annealing process can passivate defects (such as selenium vacancy).
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(16) At step 400 of
(17) At step 402 of
(18) At step 404 of
(19) Other embodiments form the absorber layer by a different technique that provides suitable uniformity of composition. For example the Cu, In, Ga and Se.sub.2 can be coevaporated and simultaneously delivered by chemical vapor deposition (CVD) followed by heating to a temperature in the range of 400° C. to 600° C. In other embodiments, the Cu, In and Ga are delivered first, and then the absorber layer is annealed in an Se atmosphere at a temperature in the range of 400° C. to 600° C.
(20) In other embodiments, the absorber comprises different materials, such as CulnSe.sub.2 (CIS), CuGaSe.sub.2 (CGS), Cu(In,Ga)Se.sub.2 (CIGS), Cu(In,Ga)(Se,S).sub.2 (CIGSS), CdTe and amorphous silicon. Other embodiments include still other absorber layer materials.
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(22) In some embodiments, the formation of buffer layer 130 is divided into a two-part process. At step 406 of
(23) At step 408 of
(24) In some embodiments, the thermal treatment is a rapid thermal anneal (RTA) process performed in an atmosphere comprising sulfur, selenium or oxygen at a temperature in the range of 400° C. to 600° C. The choice of the atmosphere composition and temperature depends on the composition and thickness of the metal layer 129.
(25) In some embodiments, the metal layer 129 comprises cadmium, and the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S. The resulting buffer layer 130 comprises CdS.
(26) In some embodiments, the metal layer 129 comprises zinc, and the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S. The resulting buffer layer 130 comprises ZnS.
(27) In some embodiments, the metal layer 129 comprises indium, and the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S. The resulting buffer layer 130 comprises In.sub.2S.sub.3.
(28) In some embodiments, the metal layer 129 comprises indium, and the atmosphere comprises at least one of the group consisting of selenium and H.sub.2Se. The resulting buffer layer 130 comprises In.sub.2Se.sub.3.
(29) In some embodiments, the metal layer 129 comprises Zn.sub.1-xMg.sub.x, and the atmosphere comprises oxygen. The resulting buffer layer 130 comprises Zn.sub.1-xMg.sub.xO.
(30) In some embodiments, the atmosphere during the RTA process comprises one of the group consisting of sulfur, selenium, H.sub.2S, H.sub.2Se, and O.sub.2; and the atmosphere further comprises an inert gas, such as nitrogen, argon, or other noble gas.
(31) The RTA process transforms the metal layer 129 into the buffer layer 130. The buffer layer 130 has a thickness in a range from 13 nm to 1300 nm. The final thickness depends in part on which annealing gas is used.
(32) Following the RTA process, the P2 scribe line is formed in the contact layer.
(33) At step 410 of
(34) At step 412 of
(35) The final photovoltaic device 10, as shown in
(36) The p-n junction 131 is not formed by the metal layer 129 deposition. Rather, the p-n junction 131 is formed when the metal layer 129 is converted to the n-type buffer layer 130 during the anneal. Thus, the p-n junction 131 is not susceptible to damage by the process used to deposit the metal layer 129. Thus, a fast, uniform process such as sputtering with a high cathode voltage can be used to deposit metal layer 129, without damaging the p-n junction. In some embodiments, the sputtered metal layer provides highly uniform metal thickness and composition. In other embodiments, the metal layer is deposited by another process such as chemical bath deposition or atomic layer deposition.
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(42) Thus, in some embodiments, solar cells processed using the two step process (steps 406 and 408 of
(43) In other embodiments, depending on the degree of sulfurization in the absorber formation process, the percentage P2 of the sulfur atomic percentage profile is approximately the same as the percentage P1, and may be slightly less than P1 in some cases.
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(49) The method and devices described herein can be incorporated in a variety of configurations.
(50) In some embodiments, a method of fabricating a buffer layer of a photovoltaic device comprises: providing a substrate having a back contact layer disposed above the substrate and an absorber layer disposed above the back contact layer; depositing a metal layer on the absorber layer; and performing a thermal treatment on the deposited metal layer in an atmosphere comprising sulfur, selenium or oxygen, to form a buffer layer.
(51) In some embodiments, the metal layer comprises one of the group consisting of cadmium, zinc, indium and Zn.sub.1-xMg.sub.x.
(52) In some embodiments, the metal layer comprises cadmium, and the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S.
(53) In some embodiments, the metal layer comprises zinc, and the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S.
(54) In some embodiments, the metal layer comprises indium, and the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S.
(55) In some embodiments, wherein the metal layer comprises indium, and the atmosphere comprises at least one of the group consisting of selenium and H.sub.2Se.
(56) In some embodiments, wherein the metal layer comprises Zn.sub.1-xMg.sub.x, and the atmosphere comprises oxygen.
(57) In some embodiments, the step of depositing a metal layer on the absorber layer includes depositing from 1 nm to 1000 nm of metal.
(58) In some embodiments, the step of depositing a metal layer on the absorber layer includes depositing from 5 nm to 500 nm of metal.
(59) In some embodiments, the buffer layer has a thickness in a range from 13 nm to 1300 nm.
(60) In some embodiments, the atmosphere further comprises an inert gas.
(61) In some embodiments, the thermal treatment is a rapid thermal anneal.
(62) In some embodiments, the rapid thermal anneal is performed at a temperature from 300° C. to 600° C.
(63) In some embodiments, a method of fabricating a photovoltaic device comprises: providing a substrate; forming a back contact layer above the substrate; forming an absorber layer above the back contact layer; sputtering a metal layer on the absorber layer, the metal layer comprising one of the group consisting of cadmium, zinc, indium and Zn.sub.1-xMg.sub.x; and performing a rapid thermal anneal on the deposited metal layer in an atmosphere comprising sulfur, selenium or oxygen, to form a buffer layer; and forming a front contact layer above the buffer layer.
(64) In some embodiments, the metal layer comprises one of the group consisting of cadmium, indium and zinc, and the atmosphere comprises at least one of the group consisting of sulfur and H.sub.2S.
(65) In some embodiments, the metal layer comprises indium, and the atmosphere comprises at least one of the group consisting of selenium and H.sub.2Se.
(66) In some embodiments, the metal layer comprises Zn.sub.1-xMg.sub.x, and the atmosphere comprises oxygen.
(67) In some embodiments, a photovoltaic device comprises: a substrate, a back contact layer above the substrate, an absorber layer on the back contact layer, a buffer layer on the absorber layer, wherein the absorber has an atomic percentage of an element from the group consisting of sulfur, oxygen and selenium that is greater at an interface between the absorber layer and the buffer layer than the atomic percentage of the element at an interface between the absorber layer and the back contact layer, and a front contact layer above the buffer layer.
(68) In some embodiments, the absorber layer comprises Cu(InGa)SeS or the absorber layer comprises Cu(InGa)Se, the buffer layer comprises one of the group consisting of CdS, ZnS In2S.sub.3, In.sub.2Se.sub.3, and Zn.sub.1-xMg.sub.xO, and the buffer layer has a thickness from 13 nm to about 1300 nm.
(69) In some embodiments, a profile of the atomic percentage of the element in the absorber layer proximate to the interface between the absorber layer and the buffer layer is a continuous curve, and, at the interface, the profile has a same atomic percentage of the element as contained by the buffer layer.
(70) Although the subject matter has been described in terms of exemplary embodiments, it is not limited thereto. Rather, the appended claims should be construed broadly, to include other variants and embodiments, which may be made by those skilled in the art.