CN113788832B - chrysene -base aza-bis [6] helicene compound and application thereof in hole transport material and solar cell - Google Patents
chrysene -base aza-bis [6] helicene compound and application thereof in hole transport material and solar cell Download PDFInfo
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Abstract
The invention discloses aAzabicyclo [6] radical]The spiroalkene compound and the application thereof as a hole transport material in a solar cell. The experimental result shows that the invention is adopted to prepareAzabicyclo [6] radical]The energy conversion efficiency of the perovskite solar cell device prepared by taking the spiroalkene compound as the hole transport layer can reach 18.5-21.5%. Meanwhile, the stability of the device is good.
Description
Technical Field
Background
Organic-inorganic hybrid Perovskite Solar Cells (PSCs) are rapidly developed due to the advantages of low processing cost, high energy conversion efficiency (PCE) and the like, and the PCE of the Solar Cells exceeds 25% nowadays, and is expected to realize commercialization. However, the stability of the PSC device is one of important factors that restrict commercialization thereof. In the PSCs, a Hole Transport Material (HTM) avoids direct contact between a perovskite layer and a battery anode in the process of hole extraction and transmission, reduces the recombination of electron holes, improves the surface morphology of the perovskite layer, and is a key component of a PSCs device. The HTM with excellent performance should have the following properties (1) HOMO and LUMO energy levels matched with the perovskite layer; (2) high hole mobility and conductivity; (3) low cost of raw materials, simple synthesis and preparation, and stable physicochemical properties under the conditions of high temperature, high light, high humidity and the like. Research shows that the HTM with high glass transition temperature is beneficial to improving the thermal stability of the device.
In the prior art, the most widely used organic hole transport material in perovskite solar cells is mainly 2,2',7,7' -tetrakis [ N, N-bis (4-methoxyphenyl) amino ] -9,9' -spirobifluorene (Spiro-OMeTAD). However, the Spiro-OMeTAD has a complex chemical structure, a long synthesis route and high price, and the hole mobility of the material is low, so that the perovskite solar cell has low energy conversion efficiency. P-type doping with lithium bis (trifluoromethylsulfonyl imide) (LiTFSI), t-butylpyridine (t-BP), etc. is usually required to improve the mobility of the hole , but such doping can lead to unstable performance of the battery device and expensive material cost.
The spiroalkene is a polycyclic aromatic hydrocarbon compound formed by condensing and combining a plurality of aromatic ring ortho-positions, has a unique spiral pi extension structure, is easy to generate more intermolecular contacts due to molecular accumulation, is favorable for improving charge mobility, improves the solubility of molecules and is favorable for solution processing of devices; the invention is based onOf moleculesTwo Bay regions (Bay region) extend the pi system through two molecular amino groupsFusion to give azabicyclo [6] in the same bay]The spiroalkene molecule is terminated by an electron Donor (Donor) to obtain a D-pi-D type hole transport material. The invention providesAzabicyclo [6] radical]The migration rate of the spiroalkene hole transport material is proved by experimental results that the material prepared by the inventionAzabicyclo [6] radical]The energy conversion efficiency of the perovskite solar cell prepared by taking the spiroalkene compound as the hole transport layer can reach as high asMeanwhile, the glass transition temperature of the materials is high, and the thermal stability of the prepared perovskite solar cell device is good.
Reference documents:
1.Green,M.A.;Ho-Baillie,A.;Snaith,H.J.,The Emergence of Perovskite Solar Cells[J].Nature Photonics 2014,8(7),506-514.
2.National Renewable Energy Laboratory.(NREL)Best Research-Cell Efficiencies,https://www.nrel.gov/pv/assets/pdfs/best-research-cell-efficiencies.20200104.pdf.
3.Li,D.;Zhang,D.;Lim,K.-S.;Hu,Y.;Rong,Y.;Mei,A.;Park,N.-G.;Han,H.,A Review on Scaling Up Perovskite Solar Cells[J].Advanced Functional Materials 2020,31,2008621.
4.Sheibani,E.;Yang,L.;Zhang,J.,Recent Advances in Organic Hole Transporting Materials for Perovskite Solar Cells[J].Solar RRL 2020,4,2000461.
5.Hawash,Z.;Ono,L.K.;Qi Y.B.Recent Advances in Spiro-MeOTAD Hole Transport Material and Its Applications in Organic–Inorganic Halide Perovskite Solar Cells[J].Adv.Mater.Interfaces 2018,5,1700623.
6.Asghara,M.I.;Zhang J.;Wang H.;Lund P.D.,Device Stability of Perovskite Solar Cells–A Review[J].Renewable&Sustainable Energy Reviews 2017,77,131-146.
7.Shen,Y.,Chen,C.F.Helicenes:Synthesis and Applications[J].Chem.Rev.2012,112,1463-1535.
disclosure of Invention
The invention aims to overcome the defects of the prior art and discloses a method for preparing a novel anti-counterfeiting paperAzabicyclo [6] radical]A spiro-based hole transport material and its use in solar cells.
In order to achieve the purpose, the invention specifically adopts the following technical scheme:
in a first aspect, the present invention provides a methodAzabicyclo [6] radical]The spiroalkene compound DA6-HTM has a structural formula shown in a formula I:
wherein:
r is selected from H, C1-C16 alkyl or Cl-C16 alkoxy; d is selected from diamine groups:
r' is selected from H, C1-C16 alkyl or Cl-C16 alkoxy.
Preferably, the DA6-HTM is in the form of DA6-BMCA-C6, DA6-BMCA-C8, DA6-BDBA or DA6-BDNA, and the structural formulas are shown as formulas II to V respectively:
in a second aspect, the present invention provides a method as defined in any one of the above aspects of the first aspectAzabicyclo [6] radical]Use of spiroalkene compounds as hole transport materials.
In a third aspect, the present invention provides a perovskite solar cell, wherein the hole transport layer material of the solar cell is as defined in any one of the above first aspectsAzabicyclo [6] radical]A spiroalkene compound.
Preferably, the electrode sequentially comprises a substrate, a transparent oxide electrode, an electron transport layer, a photoactive layer, a hole transport layer and a metal electrode from top to bottom.
Further, the electron transport layer material is titanium dioxide.
Further, the photoactive layer material is perovskite.
Prepared by the inventionAzabicyclo [6] radical]The energy conversion efficiency of the perovskite solar cell prepared by taking the spiroalkene compound as the hole transport layer can reach 18.5% -21.5%, wherein the energy conversion efficiency of DA6-BMCA is 19.4%. Meanwhile, the glass transition temperature of the materials is high, and the thermal stability of the prepared perovskite solar cell device is good. Accordingly, the inventionAzabicyclo [6] radical]The spiroalkene compound is used as a hole transport material of the perovskite solar cell to promote charge transport and improve the energy of the solar cellQuantity conversion efficiency and stability.
Drawings
FIG. 1 is a schematic view of a structure of a PSC device in which a hole transport layer is made of a materialAzabicyclo [6] radical]The spiroalkene compound has electronic transmission layer of titania and optical active layer of perovskite.
FIG. 2 is a J-V curve of a PSCs device based on DA 6-BMCA-C6.
FIG. 3 is a PCE change curve of an aging process of a perovskite solar cell device with a hole transport layer based on DA6-BMCA-C6 under a dark condition of 60 ℃ for 21 days.
FIG. 4 comparison of stability of perovskite solar cell devices based on BA7-BMCA-C6 and DA6-BMCA-C6 (room temperature, AM 1.5G, 100mW cm) -2 )。
Detailed Description
The invention will be further elucidated and described with reference to the drawings and specific embodiments.
According to the inventionAzabicyclo [6] radical]The structural formula of the spiroalkene hole transport material is as follows:
wherein:
r is selected from H, C1-C16 alkyl or Cl-C16 alkoxy;
d is selected from diamine groups, and specifically comprises:
r' is selected from H, C1-C16 alkyl or Cl-C16 alkoxy.
According to the inventionAzabicyclo [6] radical]The spiroalkene compound is used as a hole transport material of the perovskite solar cell to promote charge transport, and the energy conversion efficiency and stability of the solar cell are improved.
To the prepared compound of formula IAzabicyclo [6] radical]The cavity mobility of the spiroalkene compound DA6-HTM is measured, and the distribution range of the cavity mobility is as follows: 4.36X 10 -5 ~8.25×10 -4 cm 2 V -1 。
The following examples will aid in the understanding of the present invention, but the scope of protection of the present invention is not limited to the contents of the following examples:
example 1 Synthesis of DA6-BMCA
in the above synthetic route, the synthetic method of the compounds 1-6 is as follows:
mixing the raw materials(2.0g, 228.3g/mol, 8.8mmol) was added to a 150mL stoppered tube containing 70mL of chloroform, and liquid bromine (1.4mL, 3.1g/mL, 4.2g, 159.8g/mol, 26.3mmol) was dissolved in 10mL of chlorineAdding into a sealed tube, slowly heating to 80 ℃ for reacting for 16h, cooling to room temperature after the reaction is completed, and adding 50mL of Na 2 S 2 O 3 The reaction was quenched with aqueous solution (0.1mol/L, 150mL) and dibromo was further treated with 100mL of poor solvent methanolAll precipitate was filtered under reduced pressure, the filtrate was again treated with aqueous sodium hydroxide solution to give a crude filter cake, and toluene was recrystallized to give 3.1g of a white solid (compound 1) in a yield of 90.4%. The structural characterization data for the synthesized compound 1 is as follows:
1 H NMR(500MHz,THF-d 8 )δ9.19–9.18(s,2H),8.93–8.92(d,J=8.0Hz,2H),8.43–8.42(d,J=7.6Hz,2H),7.84–7.76(m,4H). 13 C NMR(126MHz,THF-d 8 )δ130.70,130.67,128.34,128.31,127.95,127.89,127.65,125.36,123.75,122.95ppm.
synthesis of Compound 2:
compound 1(2.0g, 386.1g/mol, 5.2mmol) and 1-chloro-2-aminonaphthalene (2.8g, 177.6g/mol, 15.6mmol), Pd (OAc) 2 (34.9mg, 224.5g/mol, 15.5% mmol), DPEPhOS (251.0mg, 538.6g/mol, 0.5mmol), NaO (t-Bu) (2.5g, 96.0g/mol, 25.9mmol) were added to a 200mL single neck round bottom flask, 100mL toluene was added as solvent, heated under argon atmosphere at 120 ℃ under reflux for 16h, after completion of the reaction cooled to room temperature, the catalyst and base were filtered off with celite, the filtrate was concentrated and recrystallized with THF to give 2.4g of a white solid (Compound 2) in 79.6% yield. The structural characterization data for the synthesized compound 2 is as follows:
1 H NMR(500MHz,THF-d 8 )δ8.79–8.78(d,J=8.4Hz,2H),8.76–8.75(s,2H),8.27–8.26(d,J=8.3Hz,2H),8.18–8.17(d,J=8.5Hz,2H),7.75–7.72(m,4H),7.68–7.65(dd,J=8.4,6.8Hz,2H),7.60–7.54(m,6H),7.32–7.31(dd,J=8.0,6.5Hz,2H),7.09–7.08(d,J=8.9Hz,2H). 13 C NMR(126MHz,THF-d 8 )δ142.55,137.95,133.51,133.01,131.04,131.03,130.62,129.53,128.94,128.72,128.36,128.35,127.95,125.19,125.07,124.52,123.72,119.10,117.43.HR-MS(ESI)m/z calcd.For(C 38 H 24 Cl 2 N 2 ):578.1317.Found:578.1301.FT-IR:2956,2922,2852,1626,1597,1504,1474,1434,1351,1321,1293,1252,1025,988,863,811.
synthesis of Compound 3(DA6H)
Mixing compound 2(2.0g, 579.5g/mol, 3.5mmol), Pd (OAc) 2 (78.6mg,224.5g/mol,0.4mmol)、K 2 CO 3 (2.9g, 138.0g/mol, 20.7mmol) and P (t-Bu) 3 ·HBF 4 (200.0mg, 290.0g/mol, 0.7mmol) is added into a 300mL single-neck round-bottom flask, 200mL ultra-dry N, N-dimethylacetamide (DMAc) is taken as a reaction solvent, the mixture is stirred and reacted for 24 hours under the protection of argon and the heating condition of 130 ℃, after the reaction is completed, the reaction solution is extracted by DCM (30mL multiplied by 3), and the organic phase is extracted by anhydrous Na 2 SO 4 After drying, filtration and rotary evaporation gave the crude product which was purified by column separation over alumina eluting with THF and toluene (2: 1 by volume) to give 472.1mg of a yellow solid (compound 3) in 27.0% yield. The structural characterization data for the synthesized compound 3 is as follows:
1 H NMR(500MHz,THF-d 8 )δ11.99–11.98(s,2H),8.55–8.54(d,J=8.0Hz,2H),8.42–8.41(d,J=8.3Hz,2H),7.97-7.96(d,J=7.9Hz,2H),7.89–7.88(dd,J=12.7,8.7Hz,2H),7.83–7.82(d,J=8.4Hz,2H),7.62–7.59(m,2H),7.32–7.29(m,2H),7.25–7.22(m,2H),7.11–7.10(dd,J=11.7,4.5Hz,2H). 13 C NMR(126MHz,THF-d 8 )δ134.85,131.36,128.66,128.00,127.45,127.14,126.26,125.65,123.94,123.73,122.24,122.12,121.98,120.42,119.49,118.64,116.92,111.84,111.17ppm.HR-MS(ESI)m/z calcd.For(C 38 H 22 N 2 ):506.1783.Found:506.1778.FT-IR:2957,2924,2853,1667,1531,1454,1397,1262,1023,897,804,756,717,669.
synthesis of Compound 4(DA 6-C6):
dissolving compound 3(472.1mg, 506.6g/mol, 0.9mmol) in ultra-dry DMF and 50mL of ultra-dry THF (volume ratio 1:1), slowly adding NaH (446.4mg, 24g/mol, 18.6mmol), stirring under argon for 10min, adding iodohexane (789.0mg, 212.1g/mol, 3.7mmol), stirring at room temperature for 3h, slowly adding water (300mL) after the reaction is completed, quenching the reaction, adding DCM (50 mL. times.3), extracting, and using anhydrous Na as organic phase 2 SO 4 Drying, filtering, rotary evaporating to obtain crude product, separating with silica gel column, and eluting with toluene and petroleum ether (1:8) to obtain 503.8mg of yellow powder (compound 4) with yield of 98.0%. The structural characterization data for the synthesized compound 4 is as follows:
1 H NMR(500MHz,THF-d 8 )δ8.64–8.63(d,J=8.3Hz,2H),8.40–8.39(d,J=8.5,2H),8.02–8.01(d,J=9.0Hz,2H),7.97–7.95(dd,J=11.9,5.0Hz,4H),7.83–7.81(d,J=8.5Hz,2H),7.60–7.59(dd,J=8.3,6.8,2H),7.30–7.29(dd,J=7.9,6.7,2H),7.21–7.20(dd,J=8.2,6.8,2H),7.06–7.05(dd,J=8.4,6.8,2H),5.23–5.17(m,2H),5.07–5.00(m,2H),2.48–2.32(m,4H),1.79–1.76(m,4H),1.60–1.53(m,4H),1.50–1.43(m,4H),0.98–(t,J=7.3Hz,6H). 13 C NMR(126MHz,THF-d 8 )δ136.02,130.85,128.79,128.67,127.99,126.64,126.25,125.28,124.08,123.64,122.71,122.22,122.20,120.67,120.23,119.37,115.99,112.28,109.31,44.12,29.75,28.79,24.77,20.78,11.57ppm.HR-MS(MALDI-TOF)m/z calcd.For(C 50 H 46 N 2 ):674.3661.Found:674.3657.FT-IR:2925,2852,1616,1524,1442,1398,1288,1217,1023,798,750,715,629.
synthesis of Compound 5(DA6-C6-2 Br):
add Compound 4 to a 100mL single neck round bottom flask(503.8mg, 551.7g/mol, 0.9mmol), DCM50mL was added and dissolved completely, NBS (321.0mg, 178.0g/mol, 1.8mmol) was added and stirred at room temperature for 1h, and Na was added after completion of the reaction 2 S 2 O 3 The reaction was quenched with aqueous solution (0.1mol/L, 50mL), the reaction was extracted with DCM (20 mL. times.3), and the organic phase was washed with anhydrous Na 2 SO 4 Drying, filtering, rotary evaporating to obtain crude product, separating with silica gel column, and eluting with toluene and petroleum ether (volume ratio of 1:8) to obtain yellow solid (compound 5)562.5mg, with yield of 90.0%. The structural characterization data for the synthesized compound 5 is as follows:
1 H NMR(500MHz,CDCl 3 )δ8.44–8.43(dd,J=8.3,5.0Hz,4H),8.31–8.29(d,J=8.4Hz,2H),8.18–8.16(s,2H),7.85–7.83(d,J=8.4Hz,2H),7.56–7.54(dd,J=7.6Hz,2H),7.45–7.42(dd,J=7.6Hz,2H),7.24–7.20(m,2H),7.15–7.12(dd,J=7.7Hz,2H),5.02–4.96(m,2H),4.81–4.75(m,2H),2.41–2.25(m,4H),1.72–1.86(m,4H),1.55–1.50(m,4H),1.47–1.42(m,4H),0.98–0.96(t,J=7.2Hz,6H). 13 C NMR(126MHz,CDCl 3 )δ137.65,133.57,131.09,130.94,129.39,127.95,127.77,126.39,125.69,125.15,125.03,124.53,122.55,121.42,120.39,118.35,115.82,114.30,46.89,31.96,31.06,27.18,23.11,14.48.HR-MS(MALDI-TOF)m/z calcd.For(C 50 H 44 Br 2 N 2 ):830.1871.Found:830.122.FT-IR:2926,2852,1714,1499,1469,1424,1335,948,858,698.
synthesis of Compound 6(DA 6-BMCA-C6):
compound 5(500.0mg, 832.7g/mol, 0.6mmol), starting intermediate BMCA (675.9mg, 375.5g/mol, 1.8mmol), Pd 2 (dba) 3 (55.0mg,916.0g/mol,0.06mmol)、P(t-Bu) 3 ·HBF 4 (34.8mg, 290.0g/mol, 0.1mmol) and NaO (t-Bu) (288.0mg, 96.0g/mol, 3.0mmol) were added to a 200mL single neck round bottom flask, 100mL of toluene was added, and the reaction was refluxed at 120 ℃ under argon overnight. Cooling to the temperature after the reaction is completedThe catalyst and base were filtered through celite at room temperature, the filtrate was concentrated by rotary evaporation and then separated through a silica gel column, eluting with THF-petroleum ether (1: 3 by volume) to give 597.6mg of a yellow solid (compound 6) in 70% yield. The structural characterization data for synthesized compound 6 is as follows:
1 H NMR(500MHz,THF-d 8 )δ8.59–8.54(m,4H),8.43–8.41(m,2H),7.99–7.96(m,4H),7.95–7.93(m,2H),7.89–7.86(m,6H),7.55–7.53(m,2H),7.42–7.38(m,12H),7.35–7.33(m,4H),7.25–7.23(m,2H),7.11–7.08(m,2H),7.04–6.98(m,6H),5.03–4.97(m,2H),4.87–4.80(m,2H),3.86(s,12H),2.21–2.17(m,4H),1.47–1.41(m,4H),1.24–1.21(m,4H),1.14–1.09(m,J=7.4Hz,4H),0.70–0.68(t,J=7.3Hz,6H).13C NMR(125MHz,THF-d 8 )δ145.42,144.31,142.48,139.22,137.95,133.77,131.37,131.24,130.81,128.26,128.19,126.30,126.23,126.04,125.32,125.01,124.80,124.36,123.55,123.35,123.30,122.73,121.98,120.98,118.92,116.84,115.14,115.10,112.53,109.70,108.98,46.52,32.13,31.30,30.47,28.97,27.27,14.03.HR-MS(MALDI-TOF)m/z calcd.For(C 102 H 84 N 8 ):1420.6819.Found:1420.8735.
the hole migration rate of the prepared DA6-BMCA-C6 is measured, and the hole migration rate is as follows: 8.25X 10 - 4 cm 2 V -1 . DA6-BMCA-C6 has a Tg of 233 ℃ as measured by Differential Scanning Calorimetry (DSC) over anotherAza [7 ] yl]194 ℃ of spiroalkene compound BA 7-BMCA-C6.
example 2 Synthesis of DA 6-BMCA-C8:
DA6-BMCA-C8 was synthesized by the procedure of example 1 using Compound 3 as a starting material. The synthetic route is as follows:
the structural characterization data for compound DA6-BMCA-C8 are as follows:
1 H NMR(500MHz,THF-d 8 )δ8.59–8.55(m,4H),8.43–8.40(m,2H),7.99–7.96(m,4H),7.95–7.92(m,2H),7.89–7.86(m,6H),7.55–7.53(m,2H),7.42–7.38(m,12H),7.35–7.33(m,4H),7.25–7.23(m,2H),7.11–7.08(m,2H),7.04–6.97(m,6H),5.03–4.97(m,1H),4.87–4.80(m,1H),3.86–3.83(s,12H),3.53-3.50(m,4H),2.21–2.16(m,4H),1.47–1.41(m,4H),1.24–1.21(m,4H),1.14–1.09(m,J=7.4Hz,4H),0.85-0.83(t,J=7.0Hz,6H),0.68-0.66(t,J=7.0Hz,6H).13C NMR(125MHz,THF-d 8 )δ145.43,144.32,142.49,139.23,137.96,133.76,131.38,131.24,130.81,128.26,128.18,126.32,126.24,126.06,125.32,125.02,124.82,124.38,123.56,123.37,123.31,122.73,121.98,120.98,118.92,116.84,115.14,115.10,112.53,109.70,108.98,46.53,32.15,31.31,30.48,29.86,28.96,27.29,14.06.HR-MS(MALDI-TOF)m/z calcd.For(C 106 H 92 N 8 ):1477.9488.Found:1477.9525.
the hole migration rate of the prepared DA6-BMCA-C8 is measured, and the hole migration rate is as follows: 6.23X 10 - 4 cm 2 V -1 . The Tg of DA6-BMCA-C8 was 225 ℃ as determined by Differential Scanning Calorimetry (DSC).
Example 3 synthesis of DA 6-BDBA:
DA6-BDBA was synthesized by referring to the procedure in example 1 using compound 5 as a starting material. The reaction equation is as follows:
the structural characterization data for the synthesized compound DA6-BDBA is as follows:
1 H NMR(500MHz,THF-d 8 )δ8.79–8.64(m,4H),7.93–7.95(m,2H),7.89–7.86(m,6H),7.42–7.38(m,16H),7.36–7.28(m,4H),7.11(dd,10,5Hz,2H),5.03–4.97(m,2H),4.87–4.80(m,2H),3.83(s,12H),2.22–2.17(m,4H),1.46–1.41(m,4H),1.24–1.20(m,4H),1.13–1.09(m,J=7.4Hz,4H),0.70–0.68(t,J=7.3Hz,6H). 13 C NMR(125MHz,THF-d 8 )δ145.43,144.32,142.48,139.22,137.96,133.78,131.37,130.81,128.26,126.30,126.05,125.33,124.80,123.55,123.30,122.73,121.98,120.99,118.92,116.84,115.10,55.85,46.52,32.13,31.31,28.97,27.27,14.02.HR-MS(MALDI-TOF)m/z calcd.For(C 78 H 72 N 4 O 4 ):1129.4508.Found:1129.4585.
the hole mobility of the prepared DA6-BDBA was measured, and the hole mobility was as follows: 6.25X 10 -5 cm 2 V -1 . The Tg of DA6-BDBA was 195 ℃ as determined by Differential Scanning Calorimetry (DSC).
Example 4 synthesis of DA 6-BDNA:
DA6-BDNA was synthesized by following the procedure of example 1 using Compound 5 as a starting material. The reaction equation is as follows:
the structural characterization data of compound DA6-BDNA is as follows:
1 H NMR(500MHz,THF-d 8 )δ8.70–8.64(m,4H),8.43–8.41(m,2H),7.95–7.93(m,2H),7.89–7.85(m,6H),7.55–7.51(m,2H),7.42–7.38(m,12H),7.35–7.33(m,4H),7.25–7.23(m,2H),7.11–7.09(m,2H),7.04–6.98(m,6H),5.03–4.97(m,2H),4.87–4.80(m,2H),3.82(s,12H),2.22–2.17(m,4H),1.46–1.41(m,4H),1.25–1.22(m,4H),1.13–1.09(m,J=7.4Hz,4H),0.70(t,J=7.3Hz,6H). 13 C NMR(125MHz,THF-d 8 )δ145.43,144.32,142.47,139.21,137.96,133.76,131.36,131.25,130.80,128.25,126.31,126.05,125.33,124.81,123.54,123.31,122.72,121.99,120.97,118.93,116.85,115.15,115.11,55.83,46.53,32.12,31.31,30.48,28.98,27.27,14.02.HR-MS(MALDI-TOF)m/z calcd.For(C 94 H 80 N 4 O 4 ):1329.6900.Found:1329.6987.
the hole mobility of the prepared DA6-BDNA is measured, and the hole mobility is as follows: 1.23X 10 -4 cm 2 V -1 . The Tg of DA6-BDNA was 203 ℃ as determined by Differential Scanning Calorimetry (DSC).
Example 5 preparation of solar cell device:
the FTO glass was cleaned in turn with detergent, deionized water, acetone, ethanol and isopropanol in an ultrasonic instrument for 10 minutes each time. Dissolving 0.6mL of diisopropyl di (acetylacetonate) titanate and 0.4mL of acetylacetone in 9mL of absolute ethanol to prepare a precursor solution, and depositing the prepared precursor solution on FTO by a spray pyrolysis method at 450 ℃ by taking oxygen as a carrier gas to form dense TiO with the thickness of 30nm 2 And (3) a layer. Adding commercial TiO 2 The paste (30NR-D) and absolute ethyl alcohol were diluted at a mass ratio of 1:6, and then at 2000rpm s -1 Spin coating for 10s at a rotating speed to make the mesoporous TiO 2 Depositing on a substrate to form 200 nm-thick mesoporous TiO 2 And (3) a layer. Drying at 80 deg.C for 10min, and drying the TiO 2 The film was thermally annealed at 450 ℃ for 30min under a dry air flow to remove organic components, and then subjected to ultraviolet-ozone treatment for 30 min. Dissolving 1.30M PbI2, 1.19M FAI, 0.14M PbBr in mixed solution of DMSO/DMF (volume ratio of 1:4) 2 And 0.14M MABr and 0.07M CsI (FAPbI) 3 )0.875(MAPbBr 3 )0.075(CsPbI 3 )0.05(PbI 2 )0.03 perovskite precursor solution, followed by the preparation of a perovskite layer in a glove under a flow of dry air with a relative humidity of less than 2%, in two successive steps at 200rpm s -1 Spin at 10s and 2000rpm s -1 The perovskite precursor solution is deposited on the electron transport layer by spin coating for 30s at the rotating speed. 150 μ L of chlorobenzene was dropped on the rotating light-absorbing layer 15s before the end of the procedure, and then the perovskite layer was thermally annealed at 120 ℃ for 1h to complete the preparation of the perovskite layer.
The preparation of the hole-transporting layer was also carried out in a glove box with a flow of dry air at a relative humidity of less than 2%, the above examples being carried out separatelySynthesizedAzabicyclo [6] radical]The spiroalkene compound is used as a hole transport material, the hole transport material is doped with 0.5 equivalent of HTFSI (bis (trifluoromethylsulfonyl) amide) and 3.3 equivalents of t-BP (tert-butylpyridine) to prepare a 30mM chlorobenzene solution, and then the mixture is subjected to s-stirring at 4000rpm -1 Spin coating at a rotation speed of 20s, depositing the film on the annealed perovskite film, and finally performing vacuum evaporation of a layer of gold with a thickness of 120nm to obtain the final productAzabicyclo [6] radical]The perovskite solar cell device with the hole transport layer made of the spiroalkene compound is manufactured, and the structure of the perovskite solar cell device is shown in figure 1.
In this example, 4 kinds of the compounds synthesized in examples 1 to 4 were usedRadical aza bis [6]]And preparing a hole transport layer by using spiroalkene compounds DA6-BMCA-C6, DA6-BMCA-C8, DA6-BDBA or DA6-BDNA to obtain four types of solar cell devices. The photovoltaic performance test is carried out on four types of perovskite solar cell devices, and the results are as follows:
TABLE 1 differs byAzabicyclo [6] radical]Photovoltaic performance parameters of perovskite solar cell device with hole transport layer made of spiroalkene compound
In which fig. 2 exemplarily shows the J-V curve of a perovskite solar cell device based on a hole transport layer prepared from DA 6-BMCA-C6.
Example 6 stability testing:
the stability test results are shown in FIG. 3, and the PCE retention rate of the DA 6-BMCA-based PSCs after aging at 60 ℃ for 21 days in the dark is 77%.
After being stored for 30 days under the conditions of dry air atmosphere and room temperature, the perovskite solar cell device based on DA6-BMCA-C6 as a hole transport layer and another perovskite solar cell deviceAza [7 ] yl]Stability test (room temperature, AM 1.5G, 100mW cm) is carried out on the perovskite solar cell device with the spiroalkene compound BA7-BMCA-C6 as the hole transport layer -2 ). The perovskite solar cell device based on BA7-BMCA-C6 and serving as a hole transport layer is the same as the perovskite solar cell device based on DA6-BMCA-C6 and serving as a hole transport layer in example 2 except that the hole transport layer is BA 7-BMCA-C6. The stability test results are shown in fig. 4, and the PCE retention rates of the two solar cell devices are 93.1% and 81.3%, respectively. The perovskite solar cell device based on DA6-BMCA-C6 is proved to have better stability compared with the perovskite solar cell device based on BA 7-BMCA-C6.
The above-described embodiments are merely preferred embodiments of the present invention, which should not be construed as limiting the invention. Various changes and modifications may be made by one of ordinary skill in the pertinent art without departing from the spirit and scope of the present invention. Therefore, the technical scheme obtained by adopting the mode of equivalent replacement or equivalent transformation is within the protection scope of the invention.
Claims (7)
3. Use of the chrysene -based azabicyclo [6] spiroalkene compounds of claim 1 or claim 2 as hole transport materials.
4. A perovskite solar cell, wherein a hole transport layer material of the solar cell is the chrysene -based azabicyclo [6] spiroalkene-based compound according to claim 1 or 2.
5. The perovskite solar cell according to claim 4, which consists of a substrate, a transparent oxide electrode, an electron transport layer, a photoactive layer, a hole transport layer and a metal electrode in this order from top to bottom.
6. The perovskite solar cell of claim 5, wherein the electron transport layer material is titanium dioxide.
7. The perovskite solar cell of claim 5, wherein the photoactive layer material is a perovskite.
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