PEROVSKITE SOLAR CELLS WITH FLATTENED GRAIN-BOUNDARY GROOVES AND METHOD FOR MANUFACTURING THE SAME
20240164120 ยท 2024-05-16
Inventors
Cpc classification
H10K30/40
ELECTRICITY
H10K85/50
ELECTRICITY
International classification
H10K30/40
ELECTRICITY
Abstract
A perovskite solar cell includes an electron-transport layer (ETL), a perovskite layer, and an HTL. The ETL is with an additive phase buried therein and disposed over a substrate with a bottom electrode. The perovskite layer is disposed above the ETL and is in contact with the ETL. The perovskite layer includes a plurality of grains which arranged on a top surface of the ETL along a direction, in which two of the adjacent grains have adjacent side surfaces to form a void there between over the top surface of the ETL. The top of the void defines a GBG side-angle with the direction, in which a mean GBG side-angle of the perovskite layer is in a range from 5 degrees to 30 degrees. A HTL is disposed over the perovskite layer and between a top electrode and the perovskite layer.
Claims
1. A perovskite solar cell, comprising: an electron-transport layer with an additive phase buried therein and disposed over a substrate with a bottom electrode; a perovskite layer disposed above the electron-transport layer and in contact with the electron-transport layer and comprising a plurality of grains which arranged on a top surface of the electron-transport layer along a direction, wherein two of the adjacent grains have adjacent side surfaces to form a void therebetween over the top surface of the electron-transport layer, and a top of the void defines a grain boundary groove (GBG) side-angle with the direction, wherein a mean GBG side-angle of the perovskite layer is in a range from 5 degrees to 30 degrees; and a hole-transporting layer disposed over the perovskite layer and between a top electrode and the perovskite layer.
2. The perovskite solar cell of claim 1, wherein the perovskite layer has absorbance with respect to 760 nm defined as A before a stability testing with 22? C. and 65% relative humidity in 250 hours, and the perovskite layer has the absorbance measured as B*A after the stability testing, where B is in a range between 0.8 and 1.
3. The perovskite solar cell of claim 1, wherein the perovskite layer has the mean GBG side-angle in a range from 5 degrees to 10 degrees after a photothermal fatigue test in 100 hours that the perovskite layer is under stimulated AM 1.5G continuous one-sun illumination and has a photothermally induced sample temperature of 50? C.
4. The perovskite solar cell of claim 1, wherein the perovskite layer has power conversion efficiency defined as PCE before a damp heat testing with 85? C. and 85% relative humidity, and the perovskite layer has the power conversion efficiency measured as C*PCE after the damp heat testing in 400 hours, where C is in a range between 0.9 and 1.
5. The perovskite solar cell of claim 1, wherein the perovskite layer is adhered with the electron-transport layer, and an average specific fracture energy between the perovskite layer and the electron-transport layer is measured to be in a range from 8500 kJ/m.sup.3 to 9000 kJ/m.sup.3.
6. A perovskite solar cell, comprising: an electron-transport layer with an additive phase buried therein and disposed over a substrate with a bottom electrode, wherein the additive phase is created by a modifier comprising iso-butylammonium chloride (i-BACl), organic or inorganic halide (AX.sub.n), or combinations thereof, where A is ethylammonium (EA.sup.+), guanidinium (GA.sup.+), n-propylammonium (PA.sup.+), n-butylammonium (n-BA.sup.+), cyclohexylammonium (CA.sup.+), formamidinium (FA.sup.+), methylammonium (MA.sup.+) or phenethylamine (PEA.sup.+), where X is I.sup.?, Cl.sup.?, Br.sup.?, or a pseudohalide anion which comprises thiocyanate (SCN.sup.?), carboxylate ion (COO.sup.?), or combinations thereof; a perovskite layer disposed above the electron-transport layer and in contact with the electron-transport layer and comprising a plurality of grains which arranged on a top surface of the electron-transport layer along a direction; and a hole-transporting layer disposed over the perovskite layer and between the perovskite layer and a top electrode.
7. The perovskite solar cell of claim 6, wherein the perovskite layer has absorbance with respect to 760 nm defined as A before a stability testing with 22? C. and 65% relative humidity in 250 hours, and the perovskite layer has the absorbance measured as B*A after the stability testing, where B is in a range between 0.8 and 1.
8. The perovskite solar cell of claim 6, wherein the perovskite layer has the mean GBG side-angle in a range from 5 degrees to 10 degrees after a photothermal fatigue test in 100 hours that the perovskite layer is under stimulated AM 1.5G continuous one-sun illumination and has a photothermally induced sample temperature of 50? C.
9. The perovskite solar cell of claim 6, wherein the perovskite layer has power conversion efficiency defined as PCE before a damp heat testing with 85? C. and 85% relative humidity, and the perovskite layer has the power conversion efficiency measured as C*PCE after the damp heat testing in 400 hours, where C is in a range between 0.9 and 1.
10. A method for manufacturing a perovskite solar cell, comprising: adding a modifier into a nanoparticle solution to acquire an electron-transport layer solution, wherein the modifier comprises iso-butylammonium chloride (i-BACl), organic or inorganic halide (AX.sub.n), or combinations thereof, where A is ethylammonium (EA.sup.+), guanidinium (GA.sup.+), n-propylammonium (PA.sup.+), n-butylammonium (n-BA.sup.+), cyclohexylammonium (CA.sup.+), formamidinium (FA.sup.+), methylammonium (MA.sup.+) or phenethylamine (PEA.sup.+), where X is I.sup.?, Cl.sup.?, Br.sup.?, or a pseudohalide anion which comprises thiocyanate (SCN.sup.?), carboxylate ion (COO.sup.?), or combinations thereof; spin coating the electron-transport layer solution on a substrate with a bottom electrode to form an electron-transport layer with an additive phase buried therein over the substrate; forming a perovskite layer above the electron-transport layer; and forming a hole-transporting layer over the perovskite layer.
11. The method of claim 10, wherein the nanoparticles solution is prepared as A ml and is modified by the modifier with 13 mg i-BACl, and a ratio of A to B is 0.2.
12. The method of claim 10, wherein the perovskite layer is formed with a thickness in a range from 250 nm to 600 nm.
13. The method of claim 10, further comprising annealing the electron-transport layer in an ambient air condition.
14. The method of claim 10, wherein the nanoparticles solution comprises SnO.sub.2, TiO.sub.2, ZnO, or combinations thereof.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Embodiments of the invention are described in more details hereinafter with reference to the drawings, in which:
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DETAILED DESCRIPTION
[0038] In the following description, apparatuses, systems, and/or methods for perovskite solar cells and the likes are set forth as preferred examples. It will be apparent to those skilled in the art that modifications, including additions and/or substitutions may be made without departing from the scope and spirit of the invention. Specific details may be omitted so as not to obscure the invention; however, the disclosure is written to enable one skilled in the art to practice the teachings herein without undue experimentation.
[0039]
[0040] The bottom electrode 104 is disposed on the substrate 102. For example, the bottom electrode 104 can be coated on the substrate 102. In one embodiment, the substrate 102 is a transparent glass, and the bottom electrode is made of at least one transparent and conductive material, such as indium tin oxide (ITO) or fluorine-doped tin oxide (FTO), and thus a combination of the substrate 102 and the bottom electrode 104 is called an ITO glass substrate or a FTO glass substrate. The ITO or FTO glass substrate is suitable for solar cells where transparency and electrical conductivity are required, which can serve as an illumination receiving side.
[0041]
[0042] The perovskite layer 120 is disposed above the ETL 110 and in contact with the ETL 110 and includes one or more films configured to absorb light and generate electrical power. In one embodiment, the perovskite layer 120 may include FA.sub.0.9Cs.sub.0.1PbI.sub.3 or FA.sub.0.9Cs.sub.0.1PbI.sub.3 or FA.sub.0.9Cs.sub.0.07MA.sub.0.03Pb(I.sub.0.92Br.sub.0.08).sub.3; In some embodiments, the perovskite layer 120 may include a perovskite material as any composition with a chemical structure of ABX.sub.3, where A is an organic or alkali cation, including but not limit to methylammonium (MA.sup.+), formamidinium (FA.sup.+), and cesium (Cs.sup.+); B is usually Pb.sup.2+ or Sn.sup.2+; X is P, Cl.sup.?, or Br.
[0043] As show in
[0044] Referring back to
[0045] By this configuration, the inclusion of the additive phase in the ETL 110 results in flattened GB grooves, achieving an opto-mechanically reliable ETL-perovskite heterointerface that is resistant to photothermal fatigue. The improved mechanical integrity of the ETL-perovskite heterointerface also facilitates charge transport and enhances chemical stability by promoting carrier injection and reducing moisture or solvent trapping, respectively.
[0046] Regarding the enhancement to the stability, the perovskite layer 120 can have stable optoelectronic properties/characters and stable solar cell performance with respect to time, such as stable absorbance, stable power conversion efficiency (PCE). In some embodiments, the perovskite layer 120 can have absorbance with respect to 760 nm defined as A before a stability testing with 22? C. and 65% relative humidity in 250 hours, and the same perovskite layer 120 has the absorbance measured as B*A after the stability testing, where B is in a range between 0.8 and 1. In some embodiments, the perovskite layer 120 has power conversion efficiency defined as PCE before a damp heat testing with 85? C. and 85% relative humidity, and the perovskite layer 120 has the power conversion efficiency measured as C*PCE after the damp heat testing in 400 hours, where C is in a range between 0.9 and 1. In some embodiments, the perovskite layer 120 has power conversion efficiency defined as PCE before a light soaking testing with one-sun-intensity light generated by white LEDs and with nitrogen flowing, and the perovskite layer 120 has the power conversion efficiency measured as D*PCE after 150 hours of the light soaking testing, where D is in a range between 0.9 and 1. In some embodiments, the perovskite layer 120 has a trap density in a range from 1.5*10.sup.14 cm.sup.?3 to 1.6*10.sup.14 cm.sup.?3.
[0047] Regarding the improved mechanical integrity, the perovskite layer 120 can have stable structural feature; for example, in some embodiments, the perovskite layer 120 still has the mean GBG side-angle in a range from 5 degrees to 10 degrees after a photothermal fatigue test in 100 hours that the perovskite layer 120 is under stimulated AM 1.5G continuous one-sun illumination and has a photothermally induced sample temperature of 50? C. Moreover, by the improved mechanical integrity, the perovskite layer 120 can have great structural strength with the ETL 110. In some embodiments, the perovskite layer 120 is adhered to the ETL 110, and the tensile strength between the perovskite layer 120 and the ETL 110 is in the range of 2.3 MPa to 2.5 MPa. In some embodiments, the perovskite layer 120 is adhered with the ETL 110, and an average specific fracture energy between the perovskite layer 120 and the ETL 110 is measured to be in a range from 8500 kJ/m.sup.3 to 9000 kJ/m.sup.3.
[0048] Further details of the testing and proof of these improvements are described as follows.
[0049]
[0050] Referring to
?.sub.GB/?.sub.HI=2 cos(?/2)=2 sin(?)
where ?.sub.GB is the GB energy, ?.sub.HI is the heterointerface energy, ? and ? is the dihedral and side angles of a GBG as illustrated in
[0051] Referring to
[0052] Referring to
[0053] Details of the testing and proof regarding mechanical properties and photothermal fatigue resistance are described as follows.
[0054]
[0055] The effect of GBG side-angle reduction on the (opto-) mechanical behavior of the buried perovskite-ETL heterointerface is examined. First, the interlayer delamination tests are performed to compare the intrinsic mechanical reliability of the perovskite-ETL heterointerfaces with and without the GBG engineering. Here the film sample specimens are made with a multi-layer structure of glass/ITO/SnO.sub.2(ETL)/FA.sub.0.9Cs.sub.0.1PbI.sub.3 perovskite/poly(methyl methacrylate) (PMMA)/epoxy/glass. As schematically illustrated in
[0056] Then, quantitative measurement is performed for the mechanical strength of the perovskite-ETL heterointerface by using a double-cantilever beam delamination technique later, which refers to the later experiment statements and is shown in
[0057]
[0058] Photothermal fatigue experiments are performed to compare the opto-mechanical reliability of the two perovskite-ETL heterointerfaces by placing the films (in the PSC device setting) under continuous one-sun-intensity illumination, coupled with a photothermally induced sample temperature of 50? C. As schematically illustrated in
[0059] To further confirm this, AFM is used to probe the GBGs of the bottom perovskite surface after 100 hours photothermal stress, as shown in
[0060] Details of the testing and proof regarding mechanical properties and photothermal fatigue resistance are described as follows.
[0061]
[0062] The chemical stability and optoelectronic properties of perovskite thin films with regular are further compared with those of the flattened GBGs. Regarding the chemical stability, accelerated aging test conditions (three-sun-intensity light generated using the white LEDs, couple with a sample temperature of 80? C.) are used to monitor the degradation kinetics of both film samples.
[0063] Flattened GBGs also lead to obvious improvement in the ambient stability of the films under the testing conditions of 22? C. and 65% RH, which can be attributed to retarded ingression into the film of moisture from the air, as shown in
where e is the elementary charge, L is the thickness of perovskite film, ? is the relative dielectric constant of the perovskite and ?.sub.0 is the vacuum permittivity. The trap density in the perovskite film after the GBG engineering is reduced to 1.54?10.sup.14 cm.sup.?3 as compared with 3.22?10.sup.14 cm.sup.?3 in the regular perovskite film, calculated based on the extracted parameters shown in Table I.
TABLE-US-00001 TABLE I The parameters for the SCLC measurement Samples N.sub.trap(cm.sup.?3) V.sub.TFL (V) Flattened GBG 1.54 ? 10.sup.14 0.125 Regular GBG 3.22 ? 10.sup.14 0.262
[0064] Time-resolved PL (TRPL) spectra of the delaminated flipped perovskite film samples for both cases are further acquired. As shown in
TABLE-US-00002 TABLE II Fitting parameters for the TRPL spectra of the perovskite films (bottom side; delaminated film from the ETL) using the bi-exponential functions, and two time-constants ?.sub.1 and ?.sub.2. Samples A.sub.1 ?.sub.1 (ns) A.sub.2 ?.sub.2 (ns) ? (ns). Flattened 0.36 471.72 0.49 112.30 383.70 GBG Regular 0.45 129.37 1.82 21.44 86.21 GBG
[0065] The average PL lifetime (?.sub.avg) for the film with flattened GBGs is 383.70 ns, significantly larger than that (86.21 ns) for the regular GBGs case, suggesting the suppression of non-radiative recombination. Then carrier-extracting properties of the perovskite-ETL heterointerfaces are compared with regular and flattened GBGs using TRPL, as shown in
TABLE-US-00003 TABLE III Fitting parameters for the TRPL spectra of the perovskite films (top side; on SnO.sub.2 ETL-coated ITO glass) with the bi-exponential functions and two time-constants ?.sub.1 and ?.sub.2. Samples A.sub.1 ?.sub.1 (ns) A.sub.2 ?.sub.2 (ns) ? (ns) Flattened 1000.00 3.11 6.87 11.64 3.33 GBG Regular 1.17 28.95 6.28 10.50 16.76 GBG
[0066] Steady-state PL spectra and PL mapping are also acquired, showing more effective PL quenching and uniform emission distribution in the film with flattened GBGs, as shown in
[0067] Details of the testing and proof regarding solar cell performance and stability are described as follows.
[0068]
[0069] The PSCs are fabricated to evaluate the effects of GBG engineering on device PCEs and stability.
TABLE-US-00004 TABLE IV Device parameters for PSCs with regular and flattened GBGs. Samples Flattened GBG Regular GBG PCE (%) 23.75 20.62 Voc (V) 1.21 1.14 Jsc (mA .Math. cm.sup.2) 24.55 23.13 FF 0.80 0.78 Stabilizing J at MPP (mA .Math. cm.sup.2) 22.82 21.40 Stabilizing PCE (%) 23.75% 20.62%
[0070] The PSCs with GBG engineering exhibit improved stabilities under various test conditions. The PCE evolution upon MPP tracking is monitored under one-sun-intensity illumination, as show in
[0071] The significant role of GBG geometry in optoelectronic properties, chemical stability and most critically photothermal fatigue resistance of buried perovskite-ETL, heterointerface is demonstrated as above. It can be found that a chemical modification of this heterointerface that increases the interfacial energy will result into a flattening of GBGs. This fundamental knowledge can be translated to the device practice, leading to highly efficient PSCs with superior operational, environmental, and opto-mechanical reliability. Furthermore, in the present disclosure, both p-i-n or n-i-p structured PSC devices may be applied. The novel structure with a perovskite layer of the present invention, can be extended to other devices beyond solar cells, including light-emitting devices, memristors, and photodetectors.
[0072]
[0073] At the step S202, a modifier is added into a nanoparticle solution for preparing and acquiring an ETL solution. In some embodiments, the modifier includes iso-butylammonium chloride (i-BACl), organic or inorganic halide (AX.sub.n), or combinations thereof, where A is ethylammonium (EA.sup.+), guanidinium (GA.sup.+), n-propylammonium (PA.sup.+), n-butylammonium (n-BA.sup.+), cyclohexylammonium (CA.sup.+), formamidinium (FA.sup.+), methylammonium (MA.sup.+) or phenethylamine (PEA.sup.+), where X is I.sup.?, Cl.sup.?, Br.sup.?, or a pseudohalide anion which comprises SCN.sup.?, COO.sup.?, or combinations thereof. In some embodiments, the nanoparticles solution may include SnO.sub.2, TiO.sub.2, ZnO, or combinations thereof. In one embodiment, the nanoparticle solution, such as SnO.sub.2, TiO.sub.2 or ZnO, can be diluted using distilled water or other alcohols: For example, dilution by 5 times. Then, the nanoparticles solution is prepared as A ml and is modified by the additive phase of B mg modifier, and a ration of A to B is 0.2. For example, for preparing the ETL solution, the acquired SnO.sub.2 nanoparticles can be diluted using distilled water by 5 times, and then, for pre-burying i-BACl into SnO.sub.2 ETLs, 1 mL SnO.sub.2 nanoparticles solution can be modified by the modifier of 5 mg i-BACl.
[0074] At the step S204, the ETL solution is spin coated on a substrate with a bottom electrode for formation of an ETL layer over the substrate. As afore-mentioned, the substrate may be an ITO or FTO glass. In one embodiment, at least one ITO glass substrate is washed with cleaning fluid, deionized water, ethanol, and isopropanol sequentially. In one embodiment, the ETL solution can be spin coated on the ITO glass substrate at 3000 rpm for 30 s and then be annealed in an ambient air condition, such as annealing at 180? C. for 30 min in the ambient air. Thereafter, the ETL-coated substrate is transferred into a nitrogen-filled glovebox which is with H.sub.2O<0.01 ppm and O.sub.2<0.01 ppm.
[0075] At the step S206, a perovskite layer is formed above the ETL. In one embodiment, the perovskite layer can be formed from a FA.sub.0.9Cs.sub.0.1PbI.sub.3 perovskite film or a FA.sub.0.9Cs.sub.0.07MA.sub.0.03Pb(I.sub.0.92Br.sub.0.08).sub.3 film. In one embodiment, for preparing the FA.sub.0.9Cs.sub.0.1PbI.sub.3 perovskite thin film with flattened GBGs, a perovskite precursor solution with 1 M molar concentration is first prepared by co-dissolving 154.8 mg FAI, 26.0 mg CsI and 461.1 mg PbI.sub.2 in 1 mL mixed solvent of DMF/DMSO (v/v, 7:3), in which additional 23.0 mg PbI.sub.2 is added into the perovskite precursor. Then, 50 ?L of this precursor is spread on the SnO.sub.2 ETL coated ITO substrate, followed by a 3-stage spin-coating process (500 rpm for 5 s, 1000 rpm for 10 s and 6000 rpm for 30 s). During the next stage, 400 ?L of toluene (TB) is dripped at the center of the spinning substrate. Then, the spun film is annealed at 170? C. for 5 min to form the final perovskite film. As such, the film is fabricated on the ETL coated ITO substrate with the additional phase pre-buried therein. In one embodiment, for preparing FA.sub.0.9Cs.sub.0.07MA.sub.0.03Pb(I.sub.0.92Br.sub.0.08).sub.3 perovskite thin films with flattened GBGs, a perovskite precursor solution with 1.35 M molar concentration is first prepared by co-dissolving 6.4 mg MAI, 13.5 mg FABr, 24.6 mg CsI, 39.6 mg PbBr.sub.2, 190.4 mg FAI, and 574 mg PbI.sub.2 in 1 mL mixed solvent of DMF/DMSO (v/v, 4:1), in which additional 17.2 mg PbI.sub.2 is added into the perovskite precursor. Then, 50 ?L of this precursor is spread on the ETL coated ITO substrate, followed by a 2-stage spin-coating process (5000 rpm for 10 s and then 4000 rpm for 30 s). During the second stage, 300 ?L of ethyl acetate (EA) is dripped at the center of the spinning substrate. Then, the spun film is annealed at 100? C. for 40 min to form the final perovskite film. The film is fabricated on the ETL coated ITO substrate with the additional phase pre-buried therein. In some embodiments, the perovskite layer is formed with a thickness in a range from 250 nm to 600 nm. In some embodiments, the perovskite layer can be formed with a thickness in a range from 270 nm to 330 nm for further controlling.
[0076] At the step S208, a HTL is formed over the perovskite layer. The HTL can be formed by spin coating a HTL solution over the perovskite layer. In one embodiment, for preparing the HTL solution, 72.3 mg Spiro-OMeTAD, 28.8 ?L 4-tert-butylpyridine, 17.5 ?L lithium bis (trifluoromethyl sulphonyl) imide acetonitrile solution (520 mg.Math.mL.sup.?1) are dissolved into 1 mL CB; subsequently, the HTL is deposited on top of the perovskite layer by spin-coating at 4000 rpm for 30 s.
[0077] At the step S210, a top electrode is formed over the HTL. In one embodiment, a 80-nm Au electrode is thermally evaporated on top of the HTL.
[0078] The experiment or test details are stated as follows.
[0079] Regarding materials characterization and property measurement, the surface geometry of GBGs is measured using an AFM platform (RTESP-300, Bruker, USA) using a 0.01-0.025 ohm-cm antimony (n-)doped Si tip in a non-contact tapping mode. The top-view and cross-sectional microstructures of the thin films are observed using a scanning electron microscope. XRD is performed using a high-resolution diffractometer with Cu K? radiation (?=1.5406 ?) in the ?-2? scan mode. UV-vis spectra are obtained using a home-built spectrophotometer system. TRPL and steady-state PL are measured using a 375-nm picosecond laser as the excitation. The PL signal is directed into a spectrograph and further collected by an electron-multiplying charge-coupled device for the steady-state PL and a streak camera for the TRPL. PL mapping is performed on an optical microscope with a filter (long pass after 726 nm) and a UV light source (250-450 nm). All PL mapping images are captured using a digital microscope camera. SCLC measurements are performed using a 2612 Source Meter) using a capacitor-like device structure of ITO/SnO.sub.2/perovskite/PCBM/Ag. All the measurements are performed under ambient conditions with a relative humidity below 40%.
[0080] Regarding mechanical behavior testing, for the perovskite film delamination tests, sample specimens with a multi-layer structure of glass/ITO/SnO.sub.2/perovskite/PMMA/epoxy/ITO/glass are applied. To prepare such specimens, a SnO.sub.2 ETL with and without pre-buried i-BACl are deposited on the ITO coated glasses. Then, the perovskite layer of a thickness of ?300 nm is deposited, followed by the spin-coating of a PMMA layer using its 10 wt % CB solution at 6000 rpm for 60 s. The purpose of the PMMA coating is to protect the perovskite from chemical degradation. Then, a thin layer of epoxy (2 ?m) is applied to glue a glass substrate onto the film structure. The epoxy is cured for 24 hours in the dry air condition (less than 20% RH) to finalize the specimen fabrication. The effective area of a typical sample specimen is 0.64 cm.sup.2. The normalized delaminated area is defined by the ratio of the delaminated film area being divided by the whole sample area.
[0081] For the stress-displacement curve measurements, a double-cantilever beam delamination technique is used on a tensile tester using a method reported in the literature. The structure of the specimens with an area of 15 mm*15 mm is glass/ITO/SnO.sub.2/perovskite/PMMA/epoxy/glass. The PMMA layer (10 wt % in CB) is spin-coated on the perovskite layer at 6000 rpm for 60 s, followed by generating a planar defect using 5 mm tape adhesion at the edge of the PMMA-perovskite-ETL multilayer. Finally, a thin layer of epoxy (2 ?m) is applied to glue a glass substrate (area: 15 mm*15 mm) onto the PMMA layer. The epoxy is cured for 24 hours in the dry air condition (less than 20% RH) to finalize the specimen fabrication. The stress-strain curve measurement procedure is as follows: firstly, the adhesion surface of the specimen and the aluminum alloy clevis are fully cleaned using alcohol. The upper and lower surfaces of the specimens are adhered to the lower and higher devises using epoxy glue, respectively. To enhance the adhesion, the specimens are pressed by a 100 N force for 30 seconds followed by 7-days epoxy cured. Following that, the specimen is mounted on the tensile testing instrument fixture. The experiment is manually pre-tension to 5 N slowly. The tensile rate of the machine is controlled by displacement of the devises. For a typical perovskite sample, the final rate is set to 0.01 mm/s according to the repeatability of the results after several comparison tests. The termination condition of the experiment is the detachment of the upper and lower glasses, or the load is reduced to below 1 N. For calculating traction stress (S) and specific fracture energy (W) calculation, the following methods are used: S=F/A, where F is the magnitude of load, A is the area of specimen; W=?.sub.0.sup.?.sup.
[0082] Regarding DFT calculation, the first-principles computations are performed based on DFT methods as implemented in the Vienna ab initio simulation package (VASP 5.4). An energy cutoff of 520 eV is employed. Structural geometry optimization is performed using Perdew-Burke-Ernzerhof exchange-correlation functional and with energy convergence and force convergence of 10.sup.?6 eV and 0.02 eV ?.sup.?1, respectively. Grimme's DFT-D3 correction is adopted to describe the long-range van der Waals interaction. A ?-centred (2*2*1) k-point mesh is used to sample the Brillouin zone. The ion cores are described by using the projector augmented wave (PAW) method. A 2*2 supercell of (001)-plane rutile SnO.sub.2 surfaces is used. The slab consists of five symmetric layers of SnO.sub.2 with BA and Cl ions absorbing on the surface, with a vacuum size of about 20 ?.
[0083] Regarding solar cell testing, the current density-voltage (J-V) characterization for PSCs is measured by a source meter under AM 1.5 G one-sun illumination (100 mW.Math.cm.sup.?2) generated by a solar simulator in the nitrogen-filled glovebox. The device area is 0.05 cm.sup.2 as defined with a shadow mask. The scans are performed in the voltage range of 0 to 1.3 V at the reverse direction (from V.sub.OC to J.sub.SC) with a step size of 0.02 V and a dwell time of 10 ms. Steady-state current/PCE outputs are measured at the voltages determined from the MPPs of the reverse-scan J-V curves. The external quantum efficiency (EQE) measurement is measured using a quantum efficiency measurement system. For light-soaking stability tests, unencapsulated PSCs are placed in a sealed quartz cell holder in N.sub.2-filled glovebox under a one-sun-intensity illumination generated using white LEDs. For operational stability tests, PSCs are biased at the maximum-power-point voltage using a potentiostat under one-sun-intensity white-LED illumination at around 50? C. For damp heat tests, encapsulated PSCs are placed in a climate chamber with a controlled humidity of 85% RH and temperature of 85? C.
[0084] The functional units and modules of the apparatuses, systems, and/or methods in accordance with the embodiments disclosed herein may be implemented using computing teaching aids, computer processors, or electronic circuitries including but not limited to application specific integrated circuits (ASIC), field programmable gate arrays (FPGA), microcontrollers, and other programmable logic teaching aids configured or programmed according to the teachings of the present disclosure. Computer instructions or software codes running in the computing teaching aids, computer processors, or programmable logic teaching aids can readily be prepared by practitioners skilled in the software or electronic art based on the teachings of the present disclosure.
[0085] All or portions of the methods in accordance with the embodiments may be executed in one or more computing teaching aids including server computers, personal computers, laptop computers, and mobile computing teaching aids such as smartphones and tablet computers.
[0086] The embodiments may include computer storage media, transient and non-transient memory teaching aids having computer instructions or software codes stored therein, which can be used to program or configure the computing teaching aids, computer processors, or electronic circuitries to perform any of the processes of the present invention. The storage media, transient and non-transient memory teaching aids can include, but are not limited to, floppy disks, optical discs, Blu-ray Disc, DVD, CD-ROMs, and magneto-optical disks, ROMs, RAMs, flash memory teaching aids, or any type of media or teaching aids suitable for storing instructions, codes, and/or data.
[0087] Each of the functional units and modules in accordance with various embodiments also may be implemented in distributed computing environments and/or Cloud computing environments, wherein the whole or portions of machine instructions are executed in distributed fashion by one or more processing teaching aids interconnected by a communication network, such as an intranet, Wide Area Network (WAN), Local Area Network (LAN), the Internet, and other forms of data transmission medium.
[0088] The foregoing description of the present invention has been provided for the purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise forms disclosed. Many modifications and variations will be apparent to the practitioner skilled in the art.
[0089] The embodiments were chosen and described in order to best explain the principles of the invention and its practical application, thereby enabling others skilled in the art to understand the invention for various embodiments and with various modifications that are suited to the particular use contemplated.