1 11 L10 Solar Cells-I ECE F. Jain Operating conditions and applications: Terrestrial applications Space application for satellites or space.

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1 11 L10 Solar Cells-I ECE F. Jain Operating conditions and applications: Terrestrial applications Space application for satellites or space station Electrical power output, conversion efficiency, Cost/Watt-peak Cells 25% Modules 25% Panel installation cost 50% 6.1. Introduction Losses and Conversion Efficiency……………………………….…………..…….……… Material selection in solar cells……………………………………………….…..…….… Concentrated Solar Photovoltaics (CSP) and Tandem Multi-junction Cells Solar Spectrum and Air Mass m……………………………………………………….……… Absorption of Photons in Semiconductors……………………………………………….…… Photovoltaic Effect……………………………………………………………………………… Qualitative explanation…………………………...………………………………………… V-I Equation: Equivalent Circuit Approach……………………………………...………… Open Circuit Voltage Voc, Maximum Power Point and Fill Factor (FF) ……………… Conversion Efficiency and Losses………………………………………...…………………… Series and Shunt resistances in the equivalent circuit……………………...……….……… Solar Cell Materials and Technologies: Generation I…………………….……...………..… Solved Examples (Example 2-4)…………..……………………………….……….………… Solar Cell Design…………………………………………………………………………...…… Solar Cell Design for Air Mass m=1………………………………………………..……… Solar Cell Design for AM 0 (outer space)……………………………………...………...… Bar Chart of Losses for AM0, m =

2 2 Solar cells-ii Emerging new cell structures: Next we describe cells which have emerged during last 10 years. These include: 1. Sanyo’s HIT (heterojunction with intrinsic thin film) cell and amorphous Si window and crystalline Si cell 2. CdTe-CdS First Solar Corp. Cell junction tandem cells 4. Multiple exciton generation (MEG) cells 5. Intermediate Band Cell 6. Organic and polymer cells 7. Quantum dot and quantum wire cells. 8. Dye sensitized cells

3 3 Sanyo’s HIT Solar Cell using n-amorphous Si on p- crystalline Si and on glass substrates Fig. 44 Sanyo’s Heterojunction with intrinsic thin film (HIT) cell. (a) cSi-aSi-TCO-Metal grid contact HIT n-aSiH/a-n+Si/p-type Si wafer. (b) Glass/TCO(bottom contact)/p-mcSi (30nm)/i-mcSi(1mm)/n-aSi (40nm)/ZnO/Ag/Al. TCO= Transparent conducting oxides serving as contact. tin oxide, indium tin oxide, ZnO. Y. Tsunomura et al., Twenty two percent efficiency HIT solar cell”, Solar Energy Materials and Solar Cells, 93, pp , The HIT cells are surface textured on both sides of the wafer to eliminate reflections.

4 4 CdTe thin film cells Rance et al, 14% efficient CdTe solar cells on ultra-thin glass substrates, Applied Physics Letter, 104, p , Glass is deposited with fluorine doped tin oxide (FTO) and tin oxide at 550C, R=20 Ohm/sq 2.CdS layer by chemical bath deposition (CBD) using cadmium acetate, thiourea, ammonium acetate, ammonium hydroxide in a water bath at 92C 3.Deposit 4 micron CdTe at 660C using closed space sublimation (CSS) with a source plate of CdTe held at 660C for 2min. 4.RF sputter thin film of Cu:doped ZnTe. Ion mill 100nm of top ZnTe. 5.DC sputter titanium Ti thin contact. 6.Light is incident from glass substrate side.

5 5 Multi-junction Tandem cells Design Improve efficiency by: 1. Ge to absorb hv>0.67eV, --reduce long wavelength loss. 2. Multiple energy gap absorbers --reduce excess energy loss

6 6 Excess energy loss: energy not utilized in electron-hole pair formation (Fig. 49)

7 7 Projected efficiencies Projected conversion efficiencies are for various 3rd generation cells: I. 66% Three-junction tandem cells 40-50% in some Multi-junction or Tandem Cells II 66% Quantum Dot solar cells using Multi-Exciton generation (MEG) III. Intermediate band (IB) devices. IV. Si nanowire solar cells.

8 8 Multiple excitons generation MEG: Alternate to harnessing excess energy loss Multiple exciton generation (MGE) phenomena and cells: Quantum Dot based solar cells When the photon energy h is greater than the bandgap, the electron and hole generated have excess energy (h -E g ) that is given up as phonons eventually heating up the lattice. That is, the energy of the hot carriers is lost. Excess energy can be recovered in following ways: (a)recover hot carriers before they thermalize (ref 2-4), and (b) hot carriers producing 2-4 electron hole pair via impact ionization or via multiple exciton generation. Multiple exciton generation (MEG, this is shown in QDs of PbSe, CdSe etc.) Impact Ionization 1 Photon creates 2 electron-hole pairs or exciton pairs. This is known as MEG. A new possible mechanism for MEG involves simultaneous creation of multiple excitons. No group has yet reported enhanced photo carriers in the external circuit. Quantum Yield ~ 300% when 3 excitons are formed.

9 9 One photon forms 3 excitons or 3 electron-hole pairs Fig. 51 Quantum yield is 300% if 3 excitons are formed

10 Intermediate band (IB) absorption to harness below gap photons Loss of below band gap and sub-band gap photons. Here an intermediate level is introduced by introducing a deep impurity level in the band gap. This is shown theoretically to be useful for single junction as well as tandem cells. Fig. 52 shows Intermediate band (due to impurity level or levels; supperlattice mini-bands, lone pair bands) in the middle of Conduction Band and Valence Band. Fig D Analog of mini-bands found in superlattices

11 Types of QDot based Cells 1. Photoelectrodes composed of QD arrays. QDs such as InP (3-5nm dia) used to sensitize a TiO 2 nanocrystalline film. 2.QDs dispersed in Organic/polymeric Semiconductors [i.e. in blend of electron and hole transporting polymers]. 3. Dye sensitized cells.

12 QD cells

13 QDot cells

14 QDs in Organic Photovoltiacs

15 Dye sensitized solar cells. Figure shows dye-sensitized solar cell 57 using hybrid nanomaterials.

16 Solar modules The flowchart of Fig. 10(a) shows how energy conversion (solar cells) and storage (e.g. ultra-capacitors ) devices are used to implement alternate energy systems for various applications. Here, the middle block shows the interface circuits (such as micro-inverters 27, solar tracking, and capacitor switching) depending on the application. Figure

17 Solar module cost Fig. 43. Module price as a function of power production. Fig. 45. Module cost /Wp in [Ref: A. Slaoui and R. Collins, p. 211, MRS Bull, March 07]The goal here is to obtain $1.82 to $1.2/Wp in 2010 and 2015, respectively.

18 Comparison of various technologies 18 REF: M. Green et al, Progress in Photovoltaics: Research and Applications, 20, pp , 2012

19 Summary 1. Thin film cells: CdTe-CdS or CIGS (First Solar), 2. Multi-junction cells: Concentrated solar 3. Poly-Si cells: 4. cSi-aSi-TCO-Metal grid contact HIT n-aSi:H /a-n+Si/p-type Si wafer. Sanyo’s (HIT) cell. 5. Organic cells 6. Dye sensitized cells 7. Emerging quantum dot / quantum wire cells.

20 Summary Excess energy loss is the primary cause in poor efficiency It is the photon energy not used in electron-hole pair generation which results in loss and reduction in current. Let us look at DEFG trapezoid segment of solar spectrum Number of photons per second N PH whose power is represented by trapezoid DFEG. N PH =Area of trapezoid /h av, h av =(energy at G +D)/2, The photon energy is = 1.24/0.95  m = 1.3 eV at Point G or EG The photon energy is = 1.24/1.1  m = 1.1 eV at Line FD. Average photon energy h av in trapezoid = ( )/2 = 1.2 eV. Excess energy per photon in DFEG = 1.2 – 1.1 = 0.1 eV. Number of photons/s N PH in the trapezoid DFEG = Shaded Area/1.2 eV. DFEG Shaded Area = Rectangle + Triangle = 600(1.1 – 0.95) + (EE’ × E’F)/2 = (850 – 600)/2 = = W/m 2 Excess Photon Energy Loss in DFEG = 0.1(108.75/1.2) = 9.06 W/m 2 Excess energy lost per sec = Fig. 37. Solar spectrum at air mass 0, p.446 E’ 850 W/m W/m  m

21 Sample Quiz Questions: 1.Finding open circuit voltage V oc if I sc and I s are given; finding output voltage V m or V mp resulting in the maximum power output; finding I m or I mp the current at maximum power to the load; computing fill factor FF. (Here, I sc or I L is the light generated short circuit current. I s is reverse saturation current and it depends on minority doping concentrations P no or N po, diffusion coefficients D p or D n, and diffusion lengths L p or L n.) 2. Finding excess energy losses in a solar cell with given energy gap E g. 3. Familiarity with currently pursued competing technologies: a.CdS-CdTe and CdS-CuInGaSe (CIGS) cells b.Poly-Si cells: polycrystalline Si wafers are cheaper than single crystalline. c.Amorphous Si on glass and amorphous Si/crystalline Si cells (HIT cells): improved conversion efficiency over poly-Si wafer cells. d.Multi-junction tandem cells: GaAs or Ge substrates for concentrated solar e.Organic solar cells and dye-sensitized photochemical cells. Total excess energy lost per sec in spectral range DEFG =

22 Sample Quiz Questions (Cont.): 4. Familiarity with quantum dot based solar cells a.Absorption is high in a quantum dot layer, so thinner QD films absorb higher power. The energy gap in QDs is size dependent. b.Multiple exciton generation (MEG) and intra-band (IB) cells. 5. Is the short circuit current I sc higher for lower energy gap semiconductors? True 6. Is the open circuit voltage V oc lower for lower energy gap semiconductors? True 7. How does multi-junction/tandem cells improve efficiency? Different cells absorb different spectral energy photons. This reduces over all Excess Energy not used in creating electron-hole pairs when photons are absorbed. 8. Why do CdTe cell panels cost less? Higher conversion efficiency is achieved as p- doped thin CdTe absorber layers have less defect density when grown on glass. 9. Effect of doping concentrations on V oc via I s (Use equations from Q.1). a.Will the V oc increase if doping concentrations increase? True b.Will the V oc increase if the temperature is reduced? True.