TWI481059B - Annealing device for a thin-film solar cell - Google Patents
Annealing device for a thin-film solar cell Download PDFInfo
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- TWI481059B TWI481059B TW101118442A TW101118442A TWI481059B TW I481059 B TWI481059 B TW I481059B TW 101118442 A TW101118442 A TW 101118442A TW 101118442 A TW101118442 A TW 101118442A TW I481059 B TWI481059 B TW I481059B
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- 239000010409 thin film Substances 0.000 title claims description 103
- 238000000137 annealing Methods 0.000 title claims description 100
- 238000012546 transfer Methods 0.000 claims description 63
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 claims description 14
- 238000010438 heat treatment Methods 0.000 claims description 13
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 claims description 8
- NFFIWVVINABMKP-UHFFFAOYSA-N methylidynetantalum Chemical compound [Ta]#C NFFIWVVINABMKP-UHFFFAOYSA-N 0.000 claims description 6
- 229910003468 tantalcarbide Inorganic materials 0.000 claims description 6
- 230000003247 decreasing effect Effects 0.000 claims description 4
- 239000010408 film Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 description 16
- 238000001816 cooling Methods 0.000 description 9
- 239000011521 glass Substances 0.000 description 8
- 239000000758 substrate Substances 0.000 description 7
- BUGBHKTXTAQXES-UHFFFAOYSA-N Selenium Chemical compound [Se] BUGBHKTXTAQXES-UHFFFAOYSA-N 0.000 description 6
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 6
- 238000000034 method Methods 0.000 description 6
- 229910052711 selenium Inorganic materials 0.000 description 6
- 239000011669 selenium Substances 0.000 description 6
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 5
- 238000010586 diagram Methods 0.000 description 5
- 229910002804 graphite Inorganic materials 0.000 description 5
- 239000010439 graphite Substances 0.000 description 5
- 238000006243 chemical reaction Methods 0.000 description 4
- 229910052738 indium Inorganic materials 0.000 description 4
- APFVFJFRJDLVQX-UHFFFAOYSA-N indium atom Chemical compound [In] APFVFJFRJDLVQX-UHFFFAOYSA-N 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- GYHNNYVSQQEPJS-UHFFFAOYSA-N Gallium Chemical compound [Ga] GYHNNYVSQQEPJS-UHFFFAOYSA-N 0.000 description 3
- 238000009825 accumulation Methods 0.000 description 3
- CDZGJSREWGPJMG-UHFFFAOYSA-N copper gallium Chemical compound [Cu].[Ga] CDZGJSREWGPJMG-UHFFFAOYSA-N 0.000 description 3
- 238000000635 electron micrograph Methods 0.000 description 3
- 230000000630 rising effect Effects 0.000 description 3
- 239000004065 semiconductor Substances 0.000 description 3
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 238000002474 experimental method Methods 0.000 description 2
- 229910052733 gallium Inorganic materials 0.000 description 2
- ZKEYULQFFYBZBG-UHFFFAOYSA-N lanthanum carbide Chemical compound [La].[C-]#[C] ZKEYULQFFYBZBG-UHFFFAOYSA-N 0.000 description 2
- 238000010792 warming Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- HVMJUDPAXRRVQO-UHFFFAOYSA-N copper indium Chemical compound [Cu].[In] HVMJUDPAXRRVQO-UHFFFAOYSA-N 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 150000003346 selenoethers Chemical class 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 239000011800 void material Substances 0.000 description 1
Classifications
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- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
-
- Y—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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P70/00—Climate change mitigation technologies in the production process for final industrial or consumer products
- Y02P70/50—Manufacturing or production processes characterised by the final manufactured product
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- Photovoltaic Devices (AREA)
Description
本發明係關於一種薄膜太陽能電池的退火裝置,尤其關於一種改善薄膜太陽能電池之受熱不均現象的退火裝置。The present invention relates to an annealing apparatus for a thin film solar cell, and more particularly to an annealing apparatus for improving uneven heating of a thin film solar cell.
薄膜太陽能電池中的CIGS(copper indium gallium (di)selenide)是屬於化合物半導體。CIGS屬於多晶薄膜的形式,它是由銅、銦、鎵以及硒所組成的一三五族化合物半導體材料。圖1A顯示CIGS薄膜太陽能電池製造過程之一步驟的示意圖。圖1B顯示CIGS薄膜太陽能電池製造過程之一步驟的示意圖。如圖1A所示,CIGS薄膜太陽能電池10包含一玻璃基板11。於玻璃基板11上依序沉積鉬金屬層12、銅鎵金屬層13、銦金屬層14及硒層15。如圖1B所示,對圖1A步驟的CIGS薄膜太陽能電池10,進行退火(annealing)處理,退火主要是指一種使材料曝露於高溫一段時間後,然後再慢慢冷卻的製程,退火處理後,銅鎵金屬層13、銦金屬層14及硒層15會形成一CIGSe層16。CIGS (copper indium gallium (di) selenide) in thin film solar cells belongs to compound semiconductors. CIGS is in the form of a polycrystalline film, which is a group of three or five compound semiconductor materials composed of copper, indium, gallium and selenium. Figure 1A shows a schematic diagram of one of the steps in the fabrication of a CIGS thin film solar cell. Figure 1B shows a schematic diagram of one of the steps in the fabrication of a CIGS thin film solar cell. As shown in FIG. 1A, the CIGS thin film solar cell 10 includes a glass substrate 11. A molybdenum metal layer 12, a copper gallium metal layer 13, an indium metal layer 14, and a selenium layer 15 are sequentially deposited on the glass substrate 11. As shown in FIG. 1B, the CIGS thin film solar cell 10 of the step of FIG. 1A is subjected to an annealing treatment, and the annealing mainly refers to a process of exposing the material to a high temperature for a period of time and then slowly cooling, after annealing, The copper gallium metal layer 13, the indium metal layer 14, and the selenium layer 15 form a CIGSe layer 16.
圖2A顯示一習知薄膜太陽能電池的退火裝置之外部結 構的示意圖。習知薄膜太陽能電池的退火裝置20,包含互相連通的5個退火室21~25、及2個冷卻室31~32。進行退火處理時,從退火裝置20的入口35將圖1A所示的CIGS薄膜太陽能電池10,送入至退火室21進行預熱,再藉由傳送裝置(未圖示)送至退火室22快速加熱至高溫狀態,例如500℃~600℃。於退火室23中使CIGS薄膜太陽能電池10保持在高溫狀態下一段時間。在退火室24中使CIGS薄膜太陽能電池10開始降溫,最後再使CIGS薄膜太陽能電池10於冷卻室31~32中緩慢降溫至低溫狀態後,從出口36送出。2A shows an external junction of an annealing device of a conventional thin film solar cell Schematic diagram of the structure. The annealing device 20 for a thin film solar cell includes five annealing chambers 21 to 25 and two cooling chambers 31 to 32 that communicate with each other. When the annealing treatment is performed, the CIGS thin film solar cell 10 shown in FIG. 1A is sent from the inlet 35 of the annealing device 20 to the annealing chamber 21 for preheating, and then sent to the annealing chamber 22 by a transfer device (not shown). Heat to a high temperature state, for example, 500 ° C ~ 600 ° C. The CIGS thin film solar cell 10 is maintained in a high temperature state for a while in the annealing chamber 23. The CIGS thin film solar cell 10 is started to be cooled in the annealing chamber 24, and finally, the CIGS thin film solar cell 10 is slowly cooled to a low temperature state in the cooling chambers 31 to 32, and then sent out from the outlet 36.
圖2B顯示一習知薄膜太陽能電池的退火裝置之各退火室之內部結構的示意圖。如圖2B所示,退火室21中設有一底板26。CIGS薄膜太陽能電池10靜置於底板26上。一加熱器50隔著一蓋板60對CIGS薄膜太陽能電池10進行加熱。2B is a schematic view showing the internal structure of each annealing chamber of an annealing device of a conventional thin film solar cell. As shown in FIG. 2B, a bottom plate 26 is provided in the annealing chamber 21. The CIGS thin film solar cell 10 is placed on the bottom plate 26. A heater 50 heats the CIGS thin film solar cell 10 via a cover plate 60.
圖3顯示一習知薄膜太陽能電池退火裝置之傳送裝置的示意圖。如圖3所示,習知薄膜太陽能電池退火裝置之傳送裝置40設於退火室21~25的底板26,用以傳送CIGS薄膜太陽能電池10(亦即其玻璃基板11)。習知薄膜太陽能電池退火裝置之傳送裝置40包含至少一滾輪41、至少一推動桿44及至少一抵靠桿43。滾輪41設置於各退火室21~25的底板26,較佳的情況是大部分設於底板26內,並露出一小部分,此部分突出於底板26,使CIGS薄膜太陽能電池10的 玻璃基板11其背面,不接觸於底板26,而能於滾輪41上移動。Figure 3 shows a schematic view of a conventional transfer device for a thin film solar cell annealing apparatus. As shown in FIG. 3, a conventional thin film solar cell annealing apparatus 40 is disposed in the bottom plate 26 of the annealing chambers 21 to 25 for transporting the CIGS thin film solar cell 10 (i.e., its glass substrate 11). The transfer device 40 of the conventional thin film solar cell annealing device comprises at least one roller 41, at least one push rod 44 and at least one abutment rod 43. The roller 41 is disposed on the bottom plate 26 of each of the annealing chambers 21-25. Preferably, most of the rollers 41 are disposed in the bottom plate 26, and a small portion is exposed. The portion protrudes from the bottom plate 26 to make the CIGS thin film solar cell 10 The back surface of the glass substrate 11 can be moved on the roller 41 without coming into contact with the bottom plate 26.
圖3習知例中,採用兩個為圓柱狀的推動桿44,分別位於底板26的右半部及左半部中,並且不突出於底板26。抵靠桿43設於推動桿44,推動桿44置於推動桿導槽45內。在傳送裝置40的靜止狀態(未圖示)下,抵靠桿43位於凹槽27內,且呈不突出於底板26的狀態。在傳送裝置40的傳送狀態下,如圖3所示,推動桿44逆時鐘旋轉一預定角度,例如90度,使抵靠桿43突出於底板26。推動桿44往下個退火室移動時,CIGS薄膜太陽能電池10的玻璃基板11會抵靠在抵靠桿43,並隨著推動桿44在滾輪41上移動。當推動桿44及玻璃基板11均移動到下個退火室後,推動桿44再順時鐘旋轉(未圖示),使抵靠桿43處於另一凹槽27內,再次回到不突出於底板26的狀態,推動桿44退回當前退火室後,即完成CIGS薄膜太陽能電池10在各退火室21~25間的傳送操作。In the conventional example of Fig. 3, two cylindrical push rods 44 are used, which are respectively located in the right and left halves of the bottom plate 26 and do not protrude from the bottom plate 26. The abutment rod 43 is provided to the push rod 44, and the push rod 44 is placed in the push rod guide groove 45. In the stationary state (not shown) of the conveyor 40, the abutment rod 43 is located in the recess 27 and is in a state of not protruding from the bottom plate 26. In the transport state of the transport device 40, as shown in FIG. 3, the push lever 44 is rotated counterclockwise by a predetermined angle, for example, 90 degrees, so that the abutment lever 43 protrudes from the bottom plate 26. As the push rod 44 moves toward the next annealing chamber, the glass substrate 11 of the CIGS thin film solar cell 10 will abut against the abutment rod 43 and move with the push rod 44 on the roller 41. When both the push rod 44 and the glass substrate 11 are moved to the next annealing chamber, the push rod 44 is rotated clockwise (not shown), so that the abutting rod 43 is in the other recess 27, and returns to the bottom plate without protruding. In the state of 26, after the push rod 44 is retracted to the current annealing chamber, the transfer operation of the CIGS thin film solar cell 10 between the annealing chambers 21 to 25 is completed.
然而,習知退火裝置20所形成的CIGS薄膜太陽能電池10a,會因受熱不均勻的現象,而降低了CIGS薄膜太陽能電池10a的品質及良率。因此習知退火裝置20還有進一步改善的空間。However, the CIGS thin film solar cell 10a formed by the conventional annealing device 20 reduces the quality and yield of the CIGS thin film solar cell 10a due to uneven heating. Therefore, the conventional annealing device 20 has room for further improvement.
本發明一實施例之目的在於提供一種的薄膜太陽能電池的退火裝置。An object of an embodiment of the present invention is to provide an annealing apparatus for a thin film solar cell.
依據本發明一實施例,提供一種薄膜太陽能電池退火裝置,用以對一包含有第VIA族元素之薄膜太陽能電池進行退火製程。薄膜太陽能電池退火裝置包含至少一退火室。每一退火室包含一底板、一加熱器及一傳送裝置。底板用以放置包含有第VIA族元素之薄膜太陽能電池。加熱器用以對包含有第VIA族元素之薄膜太陽能電池加熱。傳送裝置用以傳送包含有第VIA族元素之薄膜太陽能電池,且傳送裝置的熱傳量高於底板的熱傳量。According to an embodiment of the invention, a thin film solar cell annealing device is provided for performing an annealing process on a thin film solar cell comprising a Group VIA element. The thin film solar cell annealing apparatus includes at least one annealing chamber. Each annealing chamber includes a bottom plate, a heater, and a transfer device. The bottom plate is used to place a thin film solar cell containing a Group VIA element. The heater is used to heat a thin film solar cell containing a Group VIA element. The transfer device is configured to transport a thin film solar cell containing a Group VIA element, and the heat transfer amount of the transfer device is higher than the heat transfer amount of the bottom plate.
於一實施例中,傳送裝置包含多個滾輪,滾輪設於底板內,並自底板露出一第一部分,該第一部分突出於底板,且傳送裝置之該些滾輪的熱傳導係數高於多孔隙三氧化二鋁的熱傳導係數。In one embodiment, the conveying device comprises a plurality of rollers, the roller is disposed in the bottom plate, and a first portion is exposed from the bottom plate, the first portion protrudes from the bottom plate, and the rollers of the conveying device have a higher thermal conductivity than the porous three-phase oxidation The thermal conductivity of aluminum.
於一實施例中,傳送裝置的熱傳導係數實質上大於或等於約16.0 W/m0 k。於一實施例中,傳送裝置的材質為一碳化矽(SiC)。In one embodiment, the heat transfer coefficient of the conveyor is substantially greater than or equal to about 16.0 W/m 0 k. In one embodiment, the material of the transfer device is tantalum carbide (SiC).
於一實施例中,在加溫段的退火室中的該些滾輪的熱傳導係數大於在降溫段的退火室中的該些滾輪的熱傳導係數。In one embodiment, the heat transfer coefficients of the rollers in the annealing chamber of the warming section are greater than the heat transfer coefficients of the rollers in the annealing chamber of the cooling section.
於一實施例中,一退火室中的該些滾輪與該包含有第 VI A族元素之薄膜太陽能電池間的相對位置,相異於另一退火室中的該些滾輪與該包含有第VI A族元素之薄膜太陽能電池間的相對位置。In one embodiment, the rollers in an annealing chamber and the included The relative position between the thin film solar cells of the VI group A element is different from the relative position between the rollers in the other annealing chamber and the thin film solar cell containing the Group VI A element.
於一實施例中,傳送裝置更包含至少一推動桿及至少一抵靠桿。推動桿設於底板,用以沿包含有第VI A族元素之薄膜太陽能電池的一傳送路徑移動。抵靠桿設於推動桿上,其中推動桿用以轉動抵靠桿,使抵靠桿選擇性地位於包含有第VIA族元素之薄膜太陽能電池的傳送路徑內或其傳送路徑外。In an embodiment, the conveying device further comprises at least one push rod and at least one abutting rod. The push rod is disposed on the bottom plate for moving along a transport path of the thin film solar cell including the Group VIA element. The abutment rod is disposed on the push rod, wherein the push rod is used to rotate against the rod such that the abutment rod is selectively located within the transport path of the thin film solar cell containing the Group VIA element or outside the transport path.
於一實施例中,底板界定出至少一推動桿導槽,該至少一推動桿位於該至少一推動桿導槽內。In an embodiment, the bottom plate defines at least one push rod guide groove, and the at least one push rod is located in the at least one push rod guide groove.
依本發明一實施例,由於傳送裝置的熱傳量高於或等於底板的熱傳量,較佳的情況是傳送裝置之該些滾輪的熱傳導係數高於多孔隙三氧化二鋁的熱傳導係數,因此能夠改善依據習知技術所產生之半導體局產生空洞的現象。According to an embodiment of the present invention, since the heat transfer amount of the transfer device is higher than or equal to the heat transfer amount of the bottom plate, it is preferable that the heat transfer coefficient of the rollers of the transfer device is higher than the heat transfer coefficient of the porous alumina. Therefore, it is possible to improve the occurrence of voids in the semiconductor board generated by the conventional technique.
於一實施例中,該些滾輪的熱傳導係數實質上大於或等於約16.0 W/m0 k。較佳的情況該些滾輪的材質為一緻密的三氧化二鋁,且該緻密的三氧化二鋁的密度大於或等於3.4 G/cm3,其純度大於或等於85%。於一實施例中,傳送裝置的該些滾輪的材質為一碳化矽(SiC)。In one embodiment, the rollers have a heat transfer coefficient substantially greater than or equal to about 16.0 W/m 0 k. Preferably, the rollers are made of uniformly dense aluminum oxide, and the dense aluminum oxide has a density greater than or equal to 3.4 G/cm 3 and a purity greater than or equal to 85%. In one embodiment, the rollers of the conveyor are made of tantalum carbide (SiC).
於一實施例中,底板包含多個滾輪蓋板並界定多個滾輪 槽,該些滾輪槽用以容置該些滾輪,該些滾輪蓋板蓋住該些滾輪槽並露出該些滾輪,且該些滾輪蓋板的高度高於底板之表面的高度,但低於該些滾輪之頂點的高度,藉以提高熱傳量且不影響該薄膜太陽能電池的傳送。In an embodiment, the bottom plate includes a plurality of roller cover plates and defines a plurality of rollers a slot for receiving the rollers, the roller cover covers the roller slots and exposing the rollers, and the height of the roller covers is higher than the height of the surface of the bottom plate, but lower The height of the apex of the rollers is used to increase the heat transfer without affecting the transmission of the thin film solar cell.
於一實施例中,在加溫段的退火室中的該些滾輪的熱傳導係數大於在降溫段的退火室中的該些滾輪的熱傳導係數,因此能夠減少升溫段及降溫段之製程條件差異,所造成之受熱不均現象。於一實施例中,一退火室中的該些滾輪與該包含有第VIA族元素之薄膜太陽能電池間的相對位置,相異於另一退火室中的該些滾輪與該包含有第VIA族元素之薄膜太陽能電池間的相對位置,因此能夠減少內應力的累積。In an embodiment, the heat transfer coefficient of the rollers in the annealing chamber of the heating section is greater than the heat transfer coefficient of the rollers in the annealing chamber of the cooling section, thereby reducing the difference in process conditions between the heating section and the cooling section. The uneven heating caused. In one embodiment, the relative positions of the rollers in an annealing chamber and the thin film solar cell including the Group VIA element are different from the rollers in the other annealing chamber and the group VIA The relative position between the thin film solar cells of the elements can therefore reduce the accumulation of internal stress.
本發明的其他目的和優點可以從本發明所揭露的技術特徵中得到進一步的了解。為讓本發明之上述和其他目的、特徵和優點能更明顯易懂,下文特舉實施例並配合所附圖式,作詳細說明如下。Other objects and advantages of the present invention will become apparent from the technical features disclosed herein. The above and other objects, features, and advantages of the invention will be apparent from
圖4顯示本發明一實施例薄膜太陽能電池的退火裝置的示意圖。如圖4所示,薄膜太陽能電池退火裝置100用以對一CIGS薄膜太陽能電池10進行退火製程,其包含至少一退 火室110。每一退火室110包含一底板130、一加熱器150一蓋板160及一傳送裝置120。4 is a schematic view showing an annealing apparatus of a thin film solar cell according to an embodiment of the present invention. As shown in FIG. 4, the thin film solar cell annealing apparatus 100 is configured to perform an annealing process on a CIGS thin film solar cell 10, which includes at least one retreat. Fire room 110. Each annealing chamber 110 includes a bottom plate 130, a heater 150, a cover plate 160, and a transfer device 120.
底板130用以放置CIGS薄膜太陽能電池10及傳送裝置120。加熱器150隔著蓋板160用以對CIGS薄膜太陽能電池10加熱,傳送裝置120用以傳送CIGS薄膜太陽能電池10。於一實施例中,加熱器150可以置於底板130及蓋板160內。此外,傳送裝置120的熱傳量要高於或等於底板130的熱傳量。更具體而言,一般的情況是底板130的材質為石墨。於一實施例中傳送裝置120可以包含有滾輪121及推動桿(未圖示)。且傳送裝置120之該些滾輪121的熱傳導係數高於多孔隙三氧化二鋁的熱傳導係數。The bottom plate 130 is used to place the CIGS thin film solar cell 10 and the transfer device 120. The heater 150 is used to heat the CIGS thin film solar cell 10 via the cover plate 160, and the transfer device 120 is used to transport the CIGS thin film solar cell 10. In one embodiment, the heater 150 can be placed within the bottom plate 130 and the cover plate 160. Further, the heat transfer amount of the conveying device 120 is higher than or equal to the heat transfer amount of the bottom plate 130. More specifically, it is generally the case that the material of the bottom plate 130 is graphite. In one embodiment, the transport device 120 can include a roller 121 and a push rod (not shown). And the heat transfer coefficient of the rollers 121 of the conveying device 120 is higher than the heat transfer coefficient of the porous alumina.
圖5顯示使用習知退火裝置完成退火後之CIGS薄膜太陽能電池的示意圖。如圖5所示,使用習知退火裝置40完成退火後之CIGS薄膜太陽能電池10a,其上的斑點大致可區分為點狀斑點51及條狀斑點52。再次參照圖3,一般而言,退火室的底板26的材質為石墨,而滾輪41的材質不是採用石墨,滾輪41的材質為習知的氧化鋁,亦即多孔隙三氧化二鋁,在推動桿44的區域,底板26還需要形成推動桿導槽45,推動桿44與推動桿導槽45之間有空隙,該些因素皆會造成CIGS薄膜太陽能電池10a受熱不均的現象,因此CIGS薄膜太陽能電池10a之對應滾輪41的部分會形成點狀斑點 51,而對應推動桿44的部分會形成條狀斑點52。習知的氧化鋁是採用多孔隙三氧化二鋁,其密度為2.0~2.5G/cm3 ,其熱傳導係數為3.1 W/m0 k。Figure 5 shows a schematic of a CIGS thin film solar cell after annealing using a conventional annealing device. As shown in FIG. 5, the conventionally annealed device 40 is used to complete the annealed CIGS thin film solar cell 10a, and the spots thereon can be roughly divided into a dot spot 51 and a strip spot 52. Referring again to FIG. 3, in general, the bottom plate 26 of the annealing chamber is made of graphite, and the material of the roller 41 is not graphite. The material of the roller 41 is a conventional alumina, that is, porous alumina, which is pushed. In the region of the rod 44, the bottom plate 26 also needs to form the push rod guide groove 45, and there is a gap between the push rod 44 and the push rod guide groove 45. These factors cause the CIGS thin film solar cell 10a to be unevenly heated, so the CIGS film A portion of the corresponding roller 41 of the solar cell 10a forms a spotted spot 51, and a portion corresponding to the pusher bar 44 forms a strip-like spot 52. The conventional alumina is made of porous alumina with a density of 2.0 to 2.5 G/cm 3 and a heat transfer coefficient of 3.1 W/m 0 k.
相較於此,依據本發明一實施例中,傳送裝置120的熱傳量高於或等於底板130的熱傳量,較佳的情況是傳送裝置120的滾輪121的材質採用熱傳導係數高於多孔隙三氧化二鋁的熱傳導係數的材質,因此能夠改善CIGS薄膜太陽能電池10a的光電轉換效率。更具體而言,例如可以採用不鏽鋼其熱傳導係數為6 W/m0 k。In contrast, in one embodiment of the present invention, the heat transfer amount of the transfer device 120 is higher than or equal to the heat transfer amount of the bottom plate 130. Preferably, the material of the roller 121 of the transfer device 120 adopts a heat transfer coefficient higher than that. The material of the thermal conductivity of the pore aluminum oxide can improve the photoelectric conversion efficiency of the CIGS thin film solar cell 10a. More specifically, for example, stainless steel may be used which has a heat transfer coefficient of 6 W/m 0 k.
然而,依發明人實驗得知,較佳的情況是採用緻密的三氧化二鋁,該緻密的三氧化二鋁是指:具有密度大於或等於3.4 G/cm3 ,純度大於或等於85%的三氧化二鋁。關於緻密的三氧化二鋁的種類還可以參考如下表一。However, according to experiments by the inventors, it is preferred to use dense aluminum oxide, which means that the density is greater than or equal to 3.4 G/cm 3 and the purity is greater than or equal to 85%. Aluminum oxide. For the types of dense aluminum oxide, reference can be made to Table 1 below.
此外於一實施例中例如可以採用碳化矽(SiC),碳化矽的熱傳導係數為150 W/m0 k,該些材質的熱傳係數皆高於習知的氧化鋁的熱傳導係數3.1 W/m0 k,因此能夠改善CIGS薄膜太陽能電池10a的光電轉換效率。依據發明人實驗得知,在熱傳導係數20W/m0 k以上,能夠得到較佳的光電轉換效率。因此較佳的情況,使用具有密度大於或等於3.7 G/cm3 ,其純度大於或等於96%的緻密的三氧化二鋁。In addition, in one embodiment, for example, lanthanum carbide (SiC) can be used, and the heat transfer coefficient of the tantalum carbide is 150 W/m 0 k, and the heat transfer coefficients of the materials are higher than the heat transfer coefficient of the conventional alumina of 3.1 W/m. 0 k, therefore, the photoelectric conversion efficiency of the CIGS thin film solar cell 10a can be improved. According to experiments by the inventors, it is found that a better photoelectric conversion efficiency can be obtained with a heat transfer coefficient of 20 W/m 0 k or more. Therefore, it is preferred to use a dense aluminum oxide having a density of greater than or equal to 3.7 G/cm 3 and a purity of greater than or equal to 96%.
圖6A顯示依據習知退火裝置完成退火後之CIGS薄膜太陽能電池之斑點的電子顯微鏡(scanning electron microscope,SEM)圖。圖6B顯示依據本創作一實施例之退火裝置完成退火後之CIGS薄膜太陽能電池之斑點的電子顯微鏡圖。如圖6A所示,習知退火裝置40所製得的CIGS薄膜太陽能電池10a,其CIGSe層16形成有很多的空洞。經發明人研究得知,該些空洞會影響CIGS薄膜太陽能電池10a的光電轉換效率。Figure 6A shows a scanning electron microscope (SEM) image of a spot of a CIGS thin film solar cell after annealing according to a conventional annealing apparatus. 6B is an electron micrograph showing spots of a CIGS thin film solar cell after annealing in accordance with an annealing apparatus according to an embodiment of the present invention. As shown in FIG. 6A, the CIGS thin film solar cell 10a produced by the conventional annealing device 40 has a large number of voids formed in the CIGSe layer 16. According to research by the inventors, the voids affect the photoelectric conversion efficiency of the CIGS thin film solar cell 10a.
為了改善CIGSe層16形成空洞的現象,發明人嘗試改變傳送裝置120的滾輪121的材質,並使用各種可能的材料,如圖6B所示,當使用碳化矽作為傳送裝置120的滾輪121的材質時,於CIGSe層16中已有明顯改善空洞的現象。其原因在於多孔隙三氧化二鋁的熱傳導係數與石墨的熱傳導係數,兩者間差異較大,因此導致CIGS薄膜太陽能電池 10受熱不均的現象。尤其多孔隙三氧化二鋁的熱傳導係數約3.1 W/m0 k,熱導係數較低,因此傳送裝置120的滾輪121的溫度會較低,由於傳送裝置120的滾輪121會直接接觸CIGS薄膜太陽能電池10,因此在該接觸部分的CIGSe層16中會形成空洞。In order to improve the formation of voids in the CIGSe layer 16, the inventors attempted to change the material of the roller 121 of the transport device 120 and use various possible materials, as shown in FIG. 6B, when using tantalum carbide as the material of the roller 121 of the transport device 120. There has been a significant improvement in voids in the CIGSe layer 16. The reason is that the thermal conductivity of the porous aluminum oxide and the thermal conductivity of the graphite are largely different, which causes the CIGS thin film solar cell 10 to be unevenly heated. In particular, the porous aluminum oxide has a heat transfer coefficient of about 3.1 W/m 0 k, and the thermal conductivity is low, so the temperature of the roller 121 of the conveying device 120 is low, since the roller 121 of the conveying device 120 directly contacts the CIGS thin film solar energy. The battery 10 thus forms a void in the CIGSe layer 16 of the contact portion.
由實施結果得知,傳送裝置120的滾輪121應使用熱傳導係數高於多孔隙三氧化二鋁的材質,即可改善受熱不均的現象。最好傳送裝置120的滾輪121是使用熱傳導係數實質上大於或等於約16 W/m0 k的材質,例如碳化矽(SiC)、一石墨、或一緻密的三氧化二鋁其密度大於或等於3.4 G/cm3 其純度大於或等於85%。較佳的情況是採用具有密度大於或等於3.7 G/cm3 、純度大於或等於96%的緻密的三氧化二鋁。It is known from the implementation results that the roller 121 of the conveying device 120 should use a material having a higher thermal conductivity than the porous aluminum oxide to improve the uneven heating. Preferably, the roller 121 of the transfer device 120 is made of a material having a heat transfer coefficient substantially greater than or equal to about 16 W/m 0 k, such as tantalum carbide (SiC), a graphite, or a dense aluminum oxide having a density greater than or equal to 3.4 G/cm 3 has a purity greater than or equal to 85%. It is preferred to use a dense aluminum oxide having a density of greater than or equal to 3.7 G/cm 3 and a purity of greater than or equal to 96%.
應了解的是,本發明不限定傳送裝置120的滾輪121的種類,於一實施例中可以使用滾輪121及推動桿,於其他實施例中亦可以使用目前現有或未來發展之傳送裝置。It should be understood that the present invention is not limited to the type of roller 121 of the conveyor 120. In one embodiment, the roller 121 and the push rod may be used. In other embodiments, currently available or future developed conveyors may be used.
此外,退火製程是從升溫到降溫的製程,因此該些退火室110可以區分成升溫段及降溫段。因此較佳的情況是,升溫段之傳送裝置120的滾輪121的材質相較於降溫段之傳送裝置120的滾輪121的材質。且較佳的情況是,在加溫段的退火室110中的該些滾輪121的熱傳導係數大於在降溫段的退火室110中的該些滾輪121的熱傳導係數。In addition, the annealing process is a process from temperature rising to cooling, so the annealing chambers 110 can be divided into a heating section and a cooling section. Therefore, it is preferable that the material of the roller 121 of the conveying device 120 of the heating section is higher than the material of the roller 121 of the conveying device 120 of the temperature decreasing section. And preferably, the heat transfer coefficient of the rollers 121 in the annealing chamber 110 of the warming section is greater than the heat transfer coefficient of the rollers 121 in the annealing chamber 110 of the temperature decreasing section.
更具體而言,為了使CIGS薄膜太陽能電池10平均受熱,則必需使CIGS薄膜太陽能電池10的每個部分與外部環境能夠有均勻的熱交換。More specifically, in order to heat the CIGS thin film solar cell 10 on average, it is necessary to have uniform heat exchange between each portion of the CIGS thin film solar cell 10 and the external environment.
於一實施例中,最好是使升溫及降溫的熱傳量大致上相等。更具體而言,在升溫段的退火室110中,升溫的速率較快,且滾輪121需要儘可能地加熱到大致上等於退火室110室內的溫度,因此需要具有較佳的熱傳導係數。如此能夠減少升溫及降溫的熱傳量間的差距,而能夠使經過升溫段及降溫段後的CIGS薄膜太陽能電池10,較均勻地被加熱,減少熱所產生的內應力。In one embodiment, it is preferred that the heat transfer rates for the temperature rise and the temperature decrease are substantially equal. More specifically, in the annealing chamber 110 of the temperature rising section, the rate of temperature rise is faster, and the roller 121 needs to be heated as much as possible to be substantially equal to the temperature in the chamber of the annealing chamber 110, and therefore it is necessary to have a better heat transfer coefficient. In this way, the difference between the heat transfer amounts of the temperature rise and the temperature drop can be reduced, and the CIGS thin film solar cell 10 after passing through the temperature rising section and the temperature decreasing section can be uniformly heated to reduce the internal stress generated by the heat.
依據習知技術,各退火室21~25中滾輪41與CIGS薄膜太陽能電池10間的相對位置大致相同,亦即各退火室21~25中滾輪41會大致上接觸於CIGS薄膜太陽能電池10的相同部分。然而在經過多個退火室21~25後,長時間所累積的受熱不均現象,導致CIGS薄膜太陽能電池10的前述接觸部分與其他部分間,會具有較大之熱所造成的內應力,因此容易造成玻璃的彎曲甚至於破裂。因此,如圖4所示,依據本發明一實施例,可以讓一退火室110中的該些滾輪121與CIGS薄膜太陽能電池10間的相對位置,相異於另一退火室110中的該些滾輪121與CIGS薄膜太陽能電池10間的相對位置。如此能夠減少內應力累積的現象,可以減少多次受 熱不勻造成內應力累積所產生的問題及缺陷。According to the prior art, the relative positions of the rollers 41 and the CIGS thin film solar cells 10 in the annealing chambers 21 to 25 are substantially the same, that is, the rollers 41 in the annealing chambers 21 to 25 are substantially in contact with the same of the CIGS thin film solar cells 10. section. However, after a plurality of annealing chambers 21 to 25, the uneven heating phenomenon accumulated for a long period of time causes the internal contact between the contact portion and the other portions of the CIGS thin film solar cell 10 to have a large heat. It is easy to cause the glass to bend or even rupture. Therefore, as shown in FIG. 4, according to an embodiment of the invention, the relative positions between the rollers 121 and the CIGS thin film solar cells 10 in an annealing chamber 110 can be different from those in the other annealing chamber 110. The relative position between the roller 121 and the CIGS thin film solar cell 10. This can reduce the accumulation of internal stress and can reduce multiple times. Thermal unevenness causes problems and defects caused by accumulation of internal stress.
於一實施例中,加熱器150設於退火室110內隔著蓋板160對CIGS薄膜太陽能電池10加熱,且包含多個加熱管151。加熱管151為長條狀且具有一長軸沿一第二方向延伸,較佳的情況是第二方向大致垂直於CIGS薄膜太陽能電池10的傳送方向,亦即第一方向D1。此外,底板130界定出至少一推動桿導槽(參見圖3),推動桿位於推動桿導槽內。In one embodiment, the heater 150 is disposed in the annealing chamber 110 to heat the CIGS thin film solar cell 10 via the cover plate 160 and includes a plurality of heating tubes 151. The heating tube 151 is elongated and has a long axis extending in a second direction. Preferably, the second direction is substantially perpendicular to the conveying direction of the CIGS thin film solar cell 10, that is, the first direction D1. In addition, the bottom plate 130 defines at least one push rod guide (see FIG. 3), and the push rod is located within the push rod guide.
此外,本發明雖然以包含有硒元素的CIGS薄膜太陽能電池10為示例加以說明,但本發明不限定於此,硒為第VIA族元素,因此於本領域具有通常知識者亦能夠明白,本發明可以適用於包含有第VIA族元素的薄膜太陽能電池。Further, although the present invention is described by taking the CIGS thin film solar cell 10 containing selenium as an example, the present invention is not limited thereto, and selenium is a Group VIA element, and therefore, those skilled in the art can understand that the present invention can also be understood. It can be applied to a thin film solar cell containing a Group VIA element.
雖然本發明已以較佳實施例揭露如上,然其並非用以限定本發明,任何熟習此技藝者,在不脫離本發明之精神和範圍內,當可作些許之更動與潤飾,因此本發明之保護範圍當視後附之申請專利範圍所界定者為準。另外,本發明的任一實施例或申請專利範圍不須達成本發明所揭露之全部目的或優點或特點。此外,摘要部分和標題僅是用來輔助專利文件搜尋之用,並非用來限制本發明之權利範圍。While the present invention has been described in its preferred embodiments, the present invention is not intended to limit the invention, and the present invention may be modified and modified without departing from the spirit and scope of the invention. The scope of protection is subject to the definition of the scope of the patent application. In addition, any of the objects or advantages or features of the present invention are not required to be achieved by any embodiment or application of the invention. In addition, the abstract sections and headings are only used to assist in the search of patent documents and are not intended to limit the scope of the invention.
10‧‧‧CIGS薄膜太陽能電池10‧‧‧CIGS thin film solar cells
100‧‧‧薄膜太陽能電池退火裝置100‧‧‧Thin film solar cell annealing device
10a‧‧‧CIGS薄膜太陽能電池10a‧‧‧CIGS thin film solar cell
11‧‧‧玻璃基板11‧‧‧ glass substrate
110‧‧‧退火室110‧‧ anneal room
12‧‧‧鉬金屬層12‧‧‧Molybdenum metal layer
120‧‧‧傳送裝置120‧‧‧Transfer device
121‧‧‧滾輪121‧‧‧Roller
13‧‧‧銅鎵金屬層13‧‧‧copper gallium metal layer
130‧‧‧底板130‧‧‧floor
14‧‧‧銦金屬層14‧‧‧Indium metal layer
15‧‧‧硒層15‧‧‧Selenium
150‧‧‧加熱器150‧‧‧heater
151‧‧‧加熱管151‧‧‧heat pipe
16‧‧‧CIGSe層16‧‧‧CIGSe layer
160‧‧‧蓋板160‧‧‧ cover
20‧‧‧退火裝置20‧‧‧ Annealing device
21~25‧‧‧退火室21~25‧‧‧ Annealing Room
26‧‧‧底板26‧‧‧floor
27‧‧‧凹槽27‧‧‧ Groove
31~32‧‧‧冷卻室31~32‧‧‧ Cooling room
35‧‧‧入口35‧‧‧ entrance
36‧‧‧出口36‧‧‧Export
40‧‧‧傳送裝置40‧‧‧Transfer
41‧‧‧滾輪41‧‧‧Roller
42‧‧‧滾輪蓋板42‧‧‧Roller cover
43‧‧‧抵靠桿43‧‧‧Abutment rod
44‧‧‧推動桿44‧‧‧Pushing rod
45‧‧‧推動桿導槽45‧‧‧Pushing rod guide
50‧‧‧加熱器50‧‧‧heater
51‧‧‧點狀斑點51‧‧‧ spotted spots
52‧‧‧條狀斑點52‧‧‧ strip spots
60‧‧‧蓋板60‧‧‧ cover
圖1A顯示CIGS薄膜太陽能電池製造過程之一步驟的 示意圖。Figure 1A shows one step of the manufacturing process of a CIGS thin film solar cell schematic diagram.
圖1B顯示CIGS薄膜太陽能電池製造過程之一步驟的示意圖。Figure 1B shows a schematic diagram of one of the steps in the fabrication of a CIGS thin film solar cell.
圖2A顯示一習知薄膜太陽能電池的退火裝置之外部結構的示意圖。2A is a schematic view showing the external structure of an annealing device of a conventional thin film solar cell.
圖2B顯示一習知薄膜太陽能電池的退火裝置之各退火室之內部結構的示意圖。2B is a schematic view showing the internal structure of each annealing chamber of an annealing device of a conventional thin film solar cell.
圖3顯示一習知薄膜太陽能電池退火裝置之傳送裝置的示意圖。Figure 3 shows a schematic view of a conventional transfer device for a thin film solar cell annealing apparatus.
圖4顯示本發明一實施例薄膜太陽能電池的退火裝置的示意圖。4 is a schematic view showing an annealing apparatus of a thin film solar cell according to an embodiment of the present invention.
圖5顯示使用習知退火裝置完成退火後之CIGS薄膜太陽能電池的示意圖。Figure 5 shows a schematic of a CIGS thin film solar cell after annealing using a conventional annealing device.
圖6A顯示依據習知退火裝置完成退火後之CIGS薄膜太陽能電池之斑點的電子顯微鏡圖。Figure 6A shows an electron micrograph of a spot of a CIGS thin film solar cell after annealing is completed in accordance with a conventional annealing apparatus.
圖6B顯示依據本創作一實施例之退火裝置完成退火後之CIGS薄膜太陽能電池之斑點的電子顯微鏡圖。6B is an electron micrograph showing spots of a CIGS thin film solar cell after annealing in accordance with an annealing apparatus according to an embodiment of the present invention.
10‧‧‧CIGS薄膜太陽能電池10‧‧‧CIGS thin film solar cells
100‧‧‧薄膜太陽能電池退火裝置100‧‧‧Thin film solar cell annealing device
110‧‧‧退火室110‧‧ anneal room
120‧‧‧傳送裝置120‧‧‧Transfer device
121‧‧‧滾輪121‧‧‧Roller
130‧‧‧底板130‧‧‧floor
150‧‧‧加熱器150‧‧‧heater
160‧‧‧蓋板160‧‧‧ cover
Claims (10)
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| TW101118442A TWI481059B (en) | 2012-05-24 | 2012-05-24 | Annealing device for a thin-film solar cell |
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| TW101118442A TWI481059B (en) | 2012-05-24 | 2012-05-24 | Annealing device for a thin-film solar cell |
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| TWI481059B true TWI481059B (en) | 2015-04-11 |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TW201036191A (en) * | 2008-12-12 | 2010-10-01 | Solopower Inc | Reactor to form solar cell absorbers |
| JP2010247963A (en) * | 2009-04-16 | 2010-11-04 | Shinko Seiki Co Ltd | Substrate heating transfer device |
| TW201220426A (en) * | 2010-10-28 | 2012-05-16 | Hitachi Int Electric Inc | Substrate processing apparatus and method of manufacturing a semiconductor device |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| TW201036191A (en) * | 2008-12-12 | 2010-10-01 | Solopower Inc | Reactor to form solar cell absorbers |
| JP2010247963A (en) * | 2009-04-16 | 2010-11-04 | Shinko Seiki Co Ltd | Substrate heating transfer device |
| TW201220426A (en) * | 2010-10-28 | 2012-05-16 | Hitachi Int Electric Inc | Substrate processing apparatus and method of manufacturing a semiconductor device |
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