The present invention relates to a perovskite film, a method for producing it, a light-emitting device and a solar cell.
Organic-inorganic halide perovskite solar cells (PSCs) are promising for next-generation clean energy because they can achieve high power conversion efficiencies (η) and be fabricated with simple and low-cost methods.1,2 Although a certified η of 22.1% has been achieved through state-of-the-art device engineering, the device stability is still not sufficient for widespread commercialization.3-5 Extrinsic factors such as moisture, oxygen, UV light, and temperature are known to limit the stability of perovskite materials and PSCs made from them,5,6-9 but intrinsic degradation mechanisms must still be further clarified to find new solutions for fabricating PSCs with excellent long-term stability.
Among the known intrinsic factors, carrier traps and defects that degrade the device performance and lifetime have already been observed in PSCs with methylammonium lead triiodide (CH3NH3PbI3) perovskite absorbers.10-12 Several possible origins of defects have been proposed based on different experimental techniques and theoretical simulations.13-15 Stevart et al. reported that the chemical equilibria among iodoplumbate species may play a role in the creation of charge recombination centers.14 By decreasing the concentration of the lead ion species used during perovskite film formation, the concentration of defect precursor could be reduced in solutions. In our work, we found that hole traps are easily generated after exposure of CH3NH3PbI3 perovskite films to the moisture in air, which accelerates the degradation of PSCs under continuous light irradiation.12 Through systematic experimental studies, we showed that Frenkel defects are detrimental to the stability of PSCs and that metallic lead is a possible intrinsic origin of carrier traps.15 By virtue of the weak reduction properties of a benzoquinone additive, we were able to suppress the formation of metallic lead and effectively extend the lifetime of the PSCs.
Another important consideration is that phase transitions exist in most perovskite materials. For example, the widely used CH3NH3PbI3 has two phase transitions: one is the phase transition between the octahedral structure and the tetragonal structure at around 161 K and the other is the phase transition between the tetragonal structure and the cubic structure at around 328 K.16 Based on the analysis of thermally stimulated current (TSC), the phase transition at around 161 K has been shown to induce the formation of carrier traps.11,12,15 Since this phase transition temperature is much lower than the operating temperature of PSCs in naturally occurring terrestrial environments, the influence of the low-temperature phase transition on device performance should be negligible. However, the high-temperature phase transition is at a temperature just slightly higher than room temperature.17 Therefore, how the high-temperature phase transition affects the device performance and stability must be understood to develop PSCs that can pass strict lifetime tests under high temperatures up to 85° C. for future practical applications.
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Although a power conversion efficiency of over 20% has been achieved in CH3NH3PbI3-based perovskite solar cells, low thermal stability associated with the presence of a phase transition between the tetragonal structure and the cubic structure near room temperature is a major issue that must be overcome for future practical applications. Here, the influence of the phase transition on the thermal stability of perovskite solar cells was investigated in detail by comparing five kinds of perovskite films with different compositions of halogen atoms, rubidium, and organic components. Thermally stimulated current measurements revealed that a large number of carrier traps are generated in solar cells with the perovskite CH3NH3PbI3 as a light absorber after operation at 85° C., which is higher than the phase transition temperature. These carrier traps are detrimental to the thermal stability. The perovskite alloys do not have this phase transition, resulting in effectively suppressed formation of carrier traps. By introducing rubidium ions into the perovskite, the device performance and thermal stability of the solar cells were further improved because of reduced non-radiative recombination and suppressed carrier trap formation, respectively, during frequent cycling of device temperature. Perovskite solar cells with improved thermal stability under standard thermal cycling test were realized.
The present application discloses the following inventions:
(1) A perovskite film having substantially-no phase transition within the temperature range of from 0° C. to 100° C.
(2) The perovskite film according to (1), wherein the phase transition is a change of crystal structure.
(3) The perovskite film according to (2), wherein the phase transition is a phase transition between a tetragonal structure and a cubic structure.
(4) The perovskite film according to (2), wherein the phase transition is a phase transition between an octahedral structure and a tetragonal structure.
(5) A perovskite film wherein formation of carrier traps is suppressed within the temperature range of from 0° C. to 100° C.
(6) The perovskite according to (5), wherein formation of carrier traps is suppressed within the temperature range of from 10° C. to 100° C.
(7) The perovskite according to (5) or (6), wherein formation of carrier traps is suppressed more than CH3NH3PbI3.
(8) The perovskite film according to any one of (1) to (7), comprising a perovskite compound represented by the following Formula (1),
A1nA21−nBX1mX23−m (1)
Wherein one of A1 and A2 represents methyl ammonium (CH3NH3+) and the other of A1 and A2 represents formamidinium (NH2CH2NH2+), B represents a divalent metal ion, one of X1 and X2 represents I−and the other of X1 and X2 represents Br−, n represents a number of 0 or more and less than 1, m represents a number of 0 or more and less than 3, and at least one of n and m is more than 0.
(9) The perovskite film according to (8), wherein both n and m are more than 0.
(10) The perovskite film according to (8) or (9), wherein A1 is formamidinium, A2 is methyl ammonium, n is 0.1 or more and 0.7 or less.
(11) The perovskite film according to any one of (8) to (10), wherein X1 is Br−, X2 is I−, m is 0.1 or more and 0.7 or less.
(12) The perovskite film according to any one of (8) to (11), wherein B is Pb2+.
(13) The perovskite film according to any one of (1) to (7), comprising a perovskite compound represented by the following General Formula (2),
MrA1tA21−(r+t)BX1mX23−m (2)
Wherein M represents Rb+, Cs or K, one of A1 and A2 represents methyl ammonium (CH3NH3+) and the other of A1 and A2 represents is formamidinium (NH2CH2NH2+), B represents a divalent metal ion, one of X1 and X2 represents I−and the other of X1 and X2 represents Br−, r represents a number of more than 0 and 0.1 or less, t represents a number of 0 or more and less than 0.9, m represents a number of 0 or more and less than 3, and at least one of t and m is more than 0.
(14) The perovskite film according to (13), wherein M is Rb+.
(15) The perovskite film according to (14), wherein both t and m are more than 0.
(16) The perovskite film according to (14) or (15) wherein A1 is formamidinium, A2 is methyl ammonium, and t is 0.1 or more and 0.7 or less.
(17) The perovskite film according to any one of (14) to (16), wherein, X1 is Br−, X2 is I−, and m is 0.1 or more and 0.7 or less.
(18) The perovskite film according to any one of (14) to (17), wherein, B is Pb2+.
(19) A perovskite film comprising a perovskite compound represented by the following General Formula (1′),
(NH2CH2NH2)n′(CH3NH3)1−n′PbBrm′I3−m′ (1′)
wherein n′ and m′ each independently represent 0 or a number of 0.1 or more and 0.7 or less, and at least one of n′ and m′ is 0.1 or more and 0.7 or less.
(20) The perovskite film according to (19), wherein both n′ and m′ are 0.1 or more and 0.7 or less.
(21) A perovskite film comprising a perovskite compound represented by the following General Formula (2′),
Rbr′(NH2CH2NH2)t′(CH3NH3)1−(r′+t′)PbBrm′I3−m′ (2′)
wherein r′ represents a number of 0.01 or more and 0.1 or less, t′ and m′ each independently represent 0 or a number of 0.1 or more and 0.7 or less, and at least one of n′ and m′ is 0.1 or more and 0.7 or less.
(22) The perovskite film according to (21), wherein both t′ and m′ are 0.1 or more and 0.7 or less.
(23) A method for producing a perovskite film, comprising:
observing phase transition of two or more perovskite films having different atomic compositions within a predetermined temperature range to detect tendency of contribution of atomic composition ratio to suppression of the phase transition,
determining a better atomic composition for a perovskite film based on the tendency, and
producing a perovskite film having the better atomic composition.
(24) A method for producing a perovskite film, comprising:
observing formation of carrier traps in two or more perovskite films having different atomic compositions within a predetermined temperature range to detect tendency of contribution of atomic composition ratio to suppression of the carrier trap formation,
determining a better atomic composition for a perovskite film based on the tendency, and
producing a perovskite film having the better atomic composition.
(25) A light-emitting device comprising the perovskite film according to any one of (1) to (22).
(26) A solar cell comprising the perovskite film according to any one of (1) to (22).
We first correlate the phase transition with device properties such as conversion efficiency, degradation behavior, and lifetime at 85° C. for four kinds of lead-based perovskite materials with different combinations of halogens [bromine (Br) and iodine (I)] and organic components [methylammonium (MA) and formamidinium (FA)]. The chemical formulas of the perovskites used in this study are MA0.6FA0.4PbI3, MAPbI2.6Br0.4, MA0.6FA0.4PbI2.8Br0.2, and MAPbI3. Among them, the perovskite alloys (MA0.6FA0.4PbI3, MAPbI2.6Br0.4, and MA0.6FA0.4PbI2.8Br0.2) do not exhibit a phase transition in the temperature range from room temperature to 200° C. while the pure perovskite MAPbI3 has a phase transition at 54.6° C. and 56.2° C. for the exothermic and endothermic processes, respectively, as measured by differential scanning calorimetry. Furthermore, PSCs utilizing the pure perovskite and perovskite alloys as the light absorber demonstrated different degradation behavior under continuous light irradiation at 85° C.18 Among the PSCs tested in this study, the MA0.6FA0.4PbI2.8Br0.2-based PSCs achieved the best thermal stability due to reduced carrier trap formation as confirmed by TSC analysis. We further fabricated Rb0.05MA0.55FA0.4PbI2.8Br0.2 films for PSCs by incorporating rubidium iodide into the precursor solution used for the perovskite film fabrication. The inclusion of rubidium led to an open-circuit voltage of 1.21 V, which is the result of the lowest loss-of-voltage among all planar PSCs, and an improvement of both the conversion efficiency and device thermal stability in Rb0.05MA0.55FA0.4PbI2.8Br0.2-based PSCs.
Since perovskite alloys have mainly been used in mesoporous solar cells with the perovskite alloy infiltrating a semiconductor scaffold,19-21 we first screened several types of perovskite materials, MA0.6FA0.4PbI3, MAPbI2.6Br0.4, MA0.6FA0.4PbI2.8Br0.2, and MAPbI3, to find the optimal components for high-performance planar devices. The spin-coated perovskite alloy films fabricated here have absorption characteristics similar to what has been previously reported:19,20 introduction of FA or Br into MAPbI3 to yield MA0.6FA0.4PbI3 and MAPbI2.6Br0.4 causes the absorption onset to shift to the red or blue, respectively, as shown in
The X-ray diffraction (XRD) patterns of our perovskite films shown in
To understand the thermal properties of the perovskite alloy compounds, thermogravimetric analysis (TGA) and differential scanning calorimetry (DSC) were performed on MA0.6FA0.4PbI3, MAPbI2.6Br0.4, MA0.6FA0.4PbI2.8Br0.2, and MAPbI3 powders prepared by drying the precursor solutions used for the device fabrication at 100° C. for 30 min in a nitrogen-filled glove box. The TGA results in
Solar cells were fabricated by spin coating the perovskite alloys and MAPbI3 layers from precursor solutions, as detailed in the Methods section, on top of glass substrates coated with a layer of indium tin oxide (ITO) and a layer of poly(3,4-ethylenedioxythiophene)polystyrene sulfonate (PEDOT:PSS). To obtain uniform, flat perovskite films and similar device performance for unbiased comparison of the different compositions, we individually optimized spin-coating conditions for each perovskite film. While the PEDOT:PSS layer was fabricated in air, all of the perovskite layers were fabricated in a nitrogen-filled glove box to avoid any degradation in air. After deposition of C60 (30 nm), bathocuproine (BCP, 10 nm), and gold on the perovskite layers, all of the PSCs were encapsulated in the glove box with a glass cap and UV sealant before being removed for evaluation in ambient air.
The CH3NH3PbI3-based PSC exhibited JSC=20.93 mA cm−2, VOC=1.02 V, FF=0.72, and η=15.35% when measured under a forward bias scan. An enhanced JSC of 21.31 mA cm−2 for the MA0.6FA0.4PbI3-based PSC is attributed to a broader external quantum efficiency (EQE) spectrum as shown in
To discuss the influence of the perovskite composition on the stability without effects from UV-induced perovskite degradation complicating the results, white light-emitting diodes (WLEDs) were used as the light source. We firstly screened the high-temperature stability of the four kinds of PSCs under continuous light irradiation of 500 h at 85° C. Two regimes with different degradation speeds are observed in
SEM surface images (
In TSC profiles measured for PSCs degraded by 500 h of illumination at 85° C. (
The TSC profile of MAPbI3 PSC was more complex. Two TSC peaks were observed at 161 K and 201 K, indicating the formation of two kinds of carrier traps with corresponding trap depths of 0.32 eV and 0.41 eV, respectively. The presence of carrier traps related to the low-temperature phase transition is consistent with previous reports.11,12 However, no detectable signals were observed in this temperature range in the degraded PSCs based on perovskite alloys (see
Similar TSC curves were observed in the degraded MAPbI2.6Br0.4 device, which had a degradation behavior similar to that of the MAPbI3 PSC as shown in
Based on these results and recent reports,21 we introduced rubidium (Rb) ions into the mixed perovskite to form Rb0.05MA0.55FA0.4PbI2.8Br0.2. The suitable ionic radius of Rb (152 pm) should maintain an appropriate Goldschmidt tolerance factor between 0.8 and 1.0, which can be calculated by t=rA+rX/[2(rB+rX)]1/2, where r represents the ionic radii of the corresponding ions of ABX3, and lead to a three-dimensional perovskite.28 The low-angle XRD peaks for perovskite films with and without Rb ion occur at 13.8° and 14.0°, respectively, revealing that Rb is indeed incorporated into the crystal lattice (see
Using the same inverted PSC architecture with Rb-doped perovskite as the absorber, a champion η of 18.11% was achieved with a JSC of 21.23 mA cm−2, a VOC of 1.21 V and a FF of 0.70, as shown in
According to the earlier discussion of device stability, a reduction of carrier traps will contribute to improving the device stability. To further confirm the thermal stability of the new Rb-perovskite alloy and the influence of the phase transition, we perform thermal cycling tests using standard ISOS-T-1 thermal cycling.17
As the devices continued to operate at 85° C., efficiency only slightly reduced under continuous heating and light irradiation in the case of the Rb-perovskite-alloy-based device. On the contrary, the performance of the MAPbI3-based device quickly decreased because of a reduction in JSC, which is similar to the previous results. When the temperature returned to 25° C., the device performance of Rb-perovskite slightly increased, owing to a recovery of the VOC, and then reduced at a slow rate that continued to decrease after further cycles. However, the efficiency of the MAPbI3 PSC did not recover as much because of a significant drop in FF despite a recovery of VOC.
The degradation is further seen in the second high-temperature operation region, during which the JSC, FF, and η continuously and greatly decrease. The reduction of FF means the morphology and interface became worse. As a comparison, Rb-perovskite-based device still showed similar behavior as during the first cycle and with only a small amount of degradation. In the later three cycles, the Rb-perovskite-based device became more stable with smaller variations in FF and almost no change in the other two parameters. After all five cycles, its n remained at 87% of its initial. In contrast, η of the MAPbI3 PSC maintained only 18% of its initial η.
To further understand the relationship between phase transition and device degradation, we selected two perovskites based devices for EIS measurements,28,29 fresh and aged for 500 h MAPbI3 and MA0.6FA0.4PbI2.8Br0.2 devices, respectively. EIS was performed at 25° C., 55° C. and 70° C. during heating and again at the same temperatures during cooling down. A waiting time of 10 min was inserted prior to each measurement to ensure thermal equilibrium. It is noteworthy that we also measured current density-voltage curves before and after each EIS. The parameters FF, η, JSC, and VOC did not show any distinct trend during these tests, and device performance was not affected by the EIS measurements. The obtained spectra were fitted to a simple process-oriented equivalent circuit model (ECM) as shown in
The Ohmic resistances, R0, for all samples lie between 5.04 and 5.73 Ωcm2 after the temperature treatment (
Another noticeable feature in this series is the reduction of R2 of the fresh MAPbI3 device during the first heating, from 28 Ωcm2 at 25° C. to 9 Ωcm2 at 70° C., indicating a serious change in MAPbI3 device whereas R2 for the MA0.6FA0.4PbI2.8Br0.2 device is almost unaffected by the first heat treatment. However, all fresh samples show an increase in R2 after cooling down, which is attributed to the state before device recovery, as will be discussed below. R2 has been attributed to the interfaces or a coupled electronic-ionic impedance, where the distribution of ions strongly influences charge carrier recombination, which in turn would be expected to happen predominantly at the interfaces. Still, we think the following observations are unlikely to be caused by a morphology change: (i) the 68.6% drop in R2 for the fresh MAPbI3 device at 70° C., and (ii) the increase of R2 for MAPbI3 by almost two orders of magnitude after ageing without affecting R0 or C1. Rather, we see these results as a further indication that the phase transformation during heat treatment of the MAPbI3 device introduces additional carrier traps and that these are the main reason for the reduced thermal stability of this material.
It is obvious from the impedance analysis of fresh and aged devices that MAPbI3 shows a distinct degradation upon temperature cycling already for one thermal cycle as well as for the device after the 500 h aging test, whereas the MA0.6FA0.4PbI2.8Br0.2 device is robust against heat treatments up to 70° C. for all tests discussed in this section. All model parameters and the residuals for the fits are provided in
We studied the degradation behavior of five different perovskite-based solar cells. Large carrier trap densities were observed in the TSC curve of MAPbI3-based PSCs aged under high operating temperatures. These carrier traps are detrimental to long-term stability. Perovskite alloys with mixed both cations and anions could effectively avoid the formation of phase-transition-induced carrier traps because of a lack of a similar intrinsic phase transition. By virtue of introduction of rubidium ions, device performance of perovskite-alloy-based solar cells were further improved owing to reduced defects and non-radiative recombination. Finally, perovskite solar cells with improved thermal stability were realized, with η dropping only 13% after five thermal cycles under continuous light irradiation of 1,000 h. We believe that the present findings offer insight to help obtain efficient and stable organic-inorganic hybrid perovskite solar cells for future applications.
Glass substrates coated with prepatterned ITO layers with a thickness of ˜150 nm (ATSUGI MICRO) and sheet resistance of 12 Ω/sq. were cleaned sequentially by ultrasonicating in a detergent solution, pure water, acetone, and isopropanol for 10 min each and then subjected to UV/ozone treatment for 15 min. A thin layer (˜50 nm) of PEDOT:PSS (Clevios, A14083) was prepared by spin coating at 3000 rpm for 45 s on top of ITO in air using a poly(tetrafluoroethylene) syringe filter with a 0.45 μm pore diameter, followed by baking the PEDOT:PSS layer at 160° C. for 10 min. The perovskite layer was prepared in a nitrogen-filled glove box (H2O and O2 concentrations <0.1 ppm) using a one-step method in the following way. A mixture of PbI2 (98%; TCI) and CH3NH3I (1:1 by mol) for CH3NH3PbI3 and mixtures with certain ratio of PbI2, PbBr2 (98%; TCI), CH3NH3I (TCI), HC(NH2)2I (TCI), and RbI ((Aldrich, 99.999% trace metals basis)) for perovskite alloys were dissolved in mixtures of γ-butyrolactone (GBL) and DMF (4:6 vol/vol; GBL, ≥99%; DMF, 99.8%; TCI) at 1.2 M and stirred at 60° C. for 12 h. The mixtures were then spin-coated on the PEDOT:PSS layer at 4000 rpm for 30 s. During spin coating, 0.3 mL of toluene was dropped onto the perovskite precursor layer. The precursor layer was baked on a hotplate at 60° C. for 15 min, followed by 100° C. for 30 min. The thickness of the perovskite layer was measured to be around 300 nm using a Dektak profilometer (DektakXT, Bruker). Finally, 30 nm C60, 10 nm BCP, and 100 nm Au layers were thermally deposited on top of the CH3NH3PbI3 layer under a high vacuum (10−4 Pa) through a contact shadow mask. After unloading the PSCs directly into a glove box attached to the evaporation system, the PSCs were encapsulated using a glass lid and UV-cured sealant. Current density-voltage and external quantum efficiency measurements were performed on the PSCs using a computer-controlled Keithley 2400 source unit and an external quantum efficiency measurement system (WXS-155S-10: Wacom Denso) under simulated AM 1.5 G solar illumination from a Xe lamp-based solar simulator (SRO-25 GD, Bunkokeiki). The active area of the PSC was defined to be 16 mm2 by the overlap of the patterned ITO and Au electrodes. The lamp power was carefully calibrated at 100 mW cm−2 (1 sun) using a crystalline Si reference cell with an amorphous Si optical filter (Bunkokeiki), which was certificated by the National Institute of Advanced Industrial Science and Technology of Japan. The photovoltaic performance of our devices was not confirmed from independent certification laboratories.
For characterization of degraded perovskites, such as XRD and SEM, we use scotch tape to peel off the top metal electrode after carefully removing the encapsulation glass.
Stimulated solar light (AM 1.5 G) from WLEDs was continuously illuminated onto the PSCs at open-circuit conditions with the devices held at 25° C. or 85° C. by a temperature controller. Time-dependent VOC, JSC, FF, and η were measured automatically using a lifetime measurement system (System Engineers). For thermal cycling tests, the device temperature was changed by hand approximately every hundred hours.
The PSC was placed in a TSC measurement chamber (Rigaku TSC-FETT EL2000), and the ITO anode and Au cathode layers were connected to gold leads. The chamber was then evacuated using a rotary mechanical pump and filled with helium, which acted as a heat transfer medium. These evacuation and filling procedures were repeated three times to completely replace the atmosphere in the chamber with helium. The device was cooled to −183° C. (90 K) using liquid nitrogen. The PSC was biased at 1 mA cm−2 for 2 min at liquid nitrogen temperatures to fill carrier traps with injected carriers from the electrodes. The device temperature was then increased up to 110° C. (383 K) at a heating rate of 5 K min−1. The carriers released from the traps during the heating process were measured as current to draw the TSC curves. The background current curve was measured without trap filling at the liquid nitrogen temperature. The trap depth (ET) can be calculated using equation 1.
ET=kBTm1n(Tm4/β) (1)
where kB is Bolzmann's constant (8.617×10−5 eV K−1), Tm is the temperature of the TSC peak, and β is the heating rate (5 K min−1).
The trap density (Nt) is given by equation 2.
Nt=Q/qAL (2)
where Q is the area under the TSC peak, which is equal to the number of charges (in this case, holes) emitted from the sample during the heating process, q is the electronic charge, A is the active device area, and L is the layer thickness.
Ultraviolet-visible-near infrared absorption spectra of the perovskite films were measured using a Perkin-Elmer Lambda 950-PKA spectrophotometer in air with a relative humidity of 25%. An ITO-coated glass substrate was used as a reference.
The XRD characteristics were evaluated with an X-ray diffraction system using a 2 θ/θ technique [λ=1.54 Å (CuKα)] (Rigaku, RINT-2500). Diffraction peaks coming from ITO, PEDOT:PSS, and C60 were undetectable.
The J-V-L-EQE characteristics of the PSCs were measured using an absolute EQE measurement system (C9920-12, Hamamatsu Photonics) connected with a computer-controlled source meter (2400, Keithley) and multichannel analyzer (PMA-12, Hamamatsu Photonics). EL spectra were automatically recorded using the same system at each measurement point.
Number | Date | Country | Kind |
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2017-096690 | May 2017 | JP | national |
Filing Document | Filing Date | Country | Kind |
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PCT/JP2018/019420 | 5/15/2018 | WO | 00 |