scattering observed

advertisement
1
The role of light scattering in the performance
2
of fluorescent solar collectors
3
Nazila Soleimani,a Sebastian Knabe,b Gottfried H. Bauer,b Tom
4
Markvart,a Otto L. Muskensc
a
5
Materials Research Group, School of Engineering Sciences, University of Southampton,
6
Highfield, Southampton. SO17 1BJ
b
7
Institute of Physics, Carl von Ossietzky University of Oldenburg, D-26111 Oldenburg,
8
9
Germany
c
SEPnet and Department of Physics and Astronomy, University of Southampton, Highfield,
10
Southampton. SO17 1BJ
11
12
Nazila.Soleimani@soton.ac.uk; T.Markvart@soton.ac.uk; O.Muskens@soton.ac.uk
13
14
Abstract. A fluorescent solar collector (FSC) is an optoelectronic waveguide
15
device that can concentrate both diffuse and direct sunlight onto a solar cell.
16
The electrical output of the device depends strongly on the photon fluxes that
17
are absorbed, emitted and trapped inside the FSC plate; for this reason, it is
18
important to study the photon transport losses inside the collector. One of the
19
losses in FSC is investigated to be scattering which increases the probability
20
of the escape cone losses. The purpose of this work is to determine the
21
scattering contributions in FSC by using angle dependence of light internally
22
reflected in the FSC. The cause of the scattering in spin-coated PMMA on
23
top of the glass collector is identified to be roughness from the top surface
24
rather than bulk losses. This loss can be suppressed using an index-matching
25
planarization layer.
1
26
Keywords: Fluorescent solar collector; Solar energy; Scattering; Scattering
27
measurements.
28
29
1 Introduction
30
In a typical fluorescent solar collector (FSC), the luminescent light is trapped by total internal
31
reflection (TIR) and guided to the edge of the plate where it can be harvested by a solar cell.
32
One objective of the collector design is to reduce the size of the solar cell with respect to the
33
area which collects light. Unlike their geometric counterparts, fluorescent collectors can
34
accept light from a wide angle of incidence and are thus able to make use of the diffuse light.1
35
The photon flux at the edge of an idealized FSC is the product of the absorbed solar flux, the
36
fraction of the trapped luminescence, and the geometric ratio of the area of the face directly
37
exposed to sunlight Af divided by the area Ae of the edge that is covered by the solar cell. The
38
geometric gain Ggeom of the FSC is then given by:
39
G geom 
Af
(1)
Ae
40
Weber and Lambe (1976) initially suggested the concept of luminescence trapping for solar
41
concentrators, which they named the luminescent greenhouse collector2. In experimental FSC
42
devices, the emitted photon flux is less than ideal due to several loss processes, including
43
reabsorption and scattering.1,2,3,4,5
44
In this work, we investigate the effect of surface scattering in realistic FCS devices based on a
45
dye-doped PMMA layer on top of a glass slide. To characterize the photon transport inside the
46
collector we monitor the angular distribution of a collimated light beam which enters the
47
collector from the edge, after propagation and total internal reflection. We find that the
48
surface scattering process is described well by Fraunhofer diffraction at surface
49
inhomogeneities of a size of several m.
50
2
51
2 Theory
52
We calculate the effect of diffraction due to surface roughness on the FSC efficiency using the
53
model developed by Weber and Lamb.2 In their model, they included the guiding of light in
54
the FSC at angles larger than the critical angle for total-internal-reflection, c. Attenuation of
55
reflected light by reabsorption is taken into account through an effective absorption
56
coefficient e, while Fresnel reflection losses at the interface between the low-index FSC and
57
the high-index solar cell is included through Fresnel’s reflection coefficients for s- and p-
58
polarized light.
59
In addition, we include here losses caused by angular spread of the reflected light due to
60
surface roughness. The effect is included as a divergence of angles with a Gaussian profile of
61
1/e half-width . Around the critical angle, this additional spread in angles results in part of
62
the light to be lost within the escape cone. The angular distribution of light remaining after
63
one reflection from the rough surface can be approximated from the convolution of the unit
64
step function with the Gaussian diffraction function, resulting in the error function
65
P()=erfc[(c-)/]/2. Under the condition that the scattering is only a small correction on
66
the distribution function, the sequence of total internal reflections can be written as a
67
multiplication of a number of error functions where the number is given by the amount of
68
internal reflections from the rough surface. Inclusion of this effect in the Weber and Lambe
69
model results in a total collection efficiency Q C given by
QC  (2L)
1
L
 dy
0
70
 /2
 d
0
 /2


1
2
erfc ( c   ) /  
N R ( , )
sin d
c
 exp   e ( L  y ) / sin  sin    exp   e ( L  y ) / sin  sin  
2
 [2  rs ( ,  )  r p ( ,  ) ].
2
71
Here the number of total internal reflections from the rough surface is given by
72
 2L  y

N R ( ,  )  
cot  cot   ,
 2T

(2)
(3)
3
73
where we have introduced the FSC thickness T. The brackets indicate the floor function which
74
rounds NR to the largest previous integer.
75
Results were calculated for the collection efficiency of the FSC for a representative collector
76
with index nc=1.5 coupled into a semiconductor of index ns=3.35. We assumed a thickness
77
given by T=L/50, which is typical for a medium-scale FSC device with a geometric gain of
78
50. Different values of T will only change the total amount of scattering loss, not the
79
qualitative response. Figure 1a shows computed values obtained by numerical integration of
80
Eq. (2). The curve in absence of surface scattering (closed circles) corresponds to the Weber
81
and Lambe result.2 Introduction of a surface roughness characterized by a =1.5° divergence
82
results in a reduction of the efficiency by several percent (open circles). Also shown are the
83
total (triangles) and relative (diamonds) scattering losses, where the latter is normalized to the
84
collection efficiency for a smooth film (=0). The right-hand panel in Fig. 1 shows the
85
absolute and relative scattering losses as a function of for a value of eL=10-2, i.e. low
86
reabsorption. Above =1°, the scattering loss increases roughly linear with the diffraction
87
width . The loss percentage of 5% for 2.5° indicates the importance of surface
88
roughness optimization in experimental FSC. For comparison we have also shown the results
89
for T=L/5.2, which corresponds to the small-scale experimental configuration in this work. As
90
can be seen the scattering loss does not scale linearly with the system size, i.e. the number of
91
internal reflections, indicating that the majority of the loss is accumulated during the first few
92
reflections. This can be understood from the fact that the angular range around the critical
93
angle gets depleted of photons after the first few internal reflections and therefore the effect
94
saturates.
4
95
96
Figure 1. (Left) collection efficiency for the FSC as a function of eL calculated using the
97
modified Weber and Lambe model Eq. (2), for a perfectly smooth surface (, closed dots)
98
and a surface roughness characterized by ° and T=L/50 (open dots). (Triangles, blue)
99
Absolute scattering loss and (diamonds, red) relative scattering loss normalized to the result for
100
. (Right) (Triangles, blue) Absolute and (diamonds, red) relative scattering loss at eL =
101
10-2 as a function of the 1/e half width of the diffraction cone, for T=L/50 (symbols) and for
102
T=L/5.2 (dashed lines).
103
2 Method
104
2.1 Sample
105
The substrate used in this study was a BK7 glass slide with dimensions of 26×26×5 mm3.
106
Before depositing the layers the slides were thoroughly cleaned. A solution of 9% - 10%
107
PMMA dissolved in Chlorobenzene (Micro Chem) was spin-coated (Laurell EDC-650-
108
15TFM) at a speed of 4000 rpm for 1 minute. The thickness of the spin-coated layer was
109
measured by using a profilometer (Talysurf-120 L, Taylor Hobson Ltd.) and was found to be
110
24.85 μm. The surface morphology of the PMMA layer was characterized using Atomic
111
Force Microscopy. Figure 4 shows a representative AFM image revealing that the layer shows
112
a roughness of around 48 nm over a typical correlation length of several m. This roughness
113
may be associated with the relatively large thickness of PMMA required for fluorescent
114
conversion in a realistic FSC, resulting in height variations during the spin-coating process.
5
115
However, fluctuations may also be intrinsic to the polymer itself. Large scale heterogeneities
116
have been observed even in very pure PMMA, and its nature may be related to local
117
alignment of polymer chains and strain produced during the drying process.6
118
119
Figure. 2. Atomic Force Microscopy measurement of the PMMA layer,
120
showing height fluctuations of ~48 nm over a distance of several m.
121
122
2.2 Scattering setup
123
For the characterization of light scattering, the samples were illuminated with a laser beam
124
impinging from one side-edge of the glass. The sample was placed at the center of a circular
125
goniometer table illuminated with a laser. A silicon photodiode (SM05PD1A, Thorlabs) was
126
mounted at the edge of the table as shown in Fig. 3. The distance between the sample and the
127
detector was 27 cm. A pinhole with a diameter of 1 mm was placed in front of the silicon
128
photodiode which gives a solid angle for collection of 0.2°. A frequency of 185 Hz was
129
applied via a chopper to the beam and the current was detected by a photodiode connected via
130
a lock-in amplifier (SR810). The lock-in amplifier was used to decrease the noise of the
6
131
measurement by locking in to the chopper frequency and the average of two current
132
measurements, captured 1 second apart, was taken. The interface of this setup was
133
programmed in Labview (8.6) software. A sample holder was fixed to the center of the
134
goniometer table. The laser beam was aligned perpendicular to the surface of the sample, and
135
the photodiode could be rotated around the table for measuring the scattered intensities at
136
different angles. The scattered light intensity was measured between 0° and 180° with a
137
scattering angle increment of 0.5°.
138
139
Figure 3. Schematic of the experimental setup for the angle-dependent scattering
140
measurements.
141
2.3 Scattering measurement of FSC by angular dependence method
142
This section describes the method for measuring the scattering of PMMA spin coated on top
143
of the BK7 glass by illumination from one edge in different incident angles and detection
144
from another edge.
7
145
146
Figure 4. PMMA spin coated glass illuminate with laser light from one edge and the
147
scattered light was detected from another edge at different angles, θ1=15° and
148
N=14.21mm, M=11.79 mm. The error in this experiment was 0.8 mm which is the
149
width of the laser beam.
150
The distance of M (distance from detector inside of the glass) can be calculated by
sin 1
151
n
 2 for n2=1.5 and n1=1
sin  2
n1
152
tan 2 
D
2N
, N=26-M .
(4)
(5)
153
Values for N for different incident angle from one edge are shown in Table 1. If N <26 mm,
154
the probability that the light is totally internally reflected increases if 90-θ2 is more than the
155
critical angle.
156
157
Table 1. Distance from the incident beam inside of the glass for different incident angle, the
158
error in this calculation is 0.8 cm, given by the width of the laser beam.
Angle of
incidence
No. of TIRS
Distance M(cm)
0°
0
N.A.
15°
1
14.21
35°
2
6.04
45°
3
4.77
159
8
160
For incident angles less than 8.3° there is no reflection inside of the collector. For incident
161
angles between 8.3° to 24.6° there is one reflection inside of the collector, for the incident
162
angles between 24.6° to 40.5° there are two reflections inside the collector, and for the
163
incident angle of 45° there are three reflections inside the collector.
164
165
166
3 Results
167
Values of the intensity of scattered light measured over a range of angles are plotted in Fig. 5
168
for three different angles of incidence of 15º, 35º and 45º. To compare the results the
169
maximum intensity for all the measurement was defined as 0º. Clearly, the light cone
170
transmitted through the PMMA-coated FSC is considerably broadened compared to a bare
171
glass slide. As seen in Table 2, the angular width of the scattered intensity cone increases for
172
larger angles of incidence up to 45°. The width here is determined as the length over which
173
the intensity drops to 1/e of the maximum. The measurements at 15° and 35° show the same
174
width, which can be understood from the fact that the second internal reflection takes place at
175
the opposite glass surface without PMMA. As we will show below, the observed behavior is
176
consistent with diffraction of the laser beam caused by the roughness of the PMMA layer.
177
In a simple model, we include the diffraction by describing the reflected light as a collection
178
of diffraction-limited cones with an aperture given by the correlation length of the surface
179
roughness.
180
9
Intensity (norm.)
1.00
-5
Glass
15
35
45
Gaussian
0.50
-4
-3
-2
181
0.00
-1
0
1
Scattering angle ( )
2
3
4
5
182
Figure. 5. Angular dependence of normalized intensity for different incident
183
angles for 670 nm incident light. Lines: Gaussian fits.
184
Table 2. Beam width for different incident angles of incidence.
Angle of incidence
0° laser beam
1/e half-width of the scattered
beam (º)
0.6
15°
1.3
35°
1.4
45°
1.6
185
186
187
Thus, if we consider the PMMA surface as a collection of uncorrelated areas, the angular
188
distribution of the reflected intensity can be fitted to the Fraunhofer diffraction formula for the
189
circular aperture, given by7
190
I  I0
G 2 2 J 1 ( ka sin  )
ka sin 
2 r 2
2
(6)
191
where the G=πa2, a is the radius of the aperture, r is the distance from observation point to
192
shadow area, λ is the wavelength of the incident, J1 is the Bessel function of the first order and
193
k is the optical wavenumber.
10
194
Equation (6) gives us the intensity of the scattered light in different detection angles known as
195
the Airy pattern. We note that the use of a Gaussian angular spread in Eq. (1) is a good
196
approximation as the central lobe of the Airy pattern shows close agreement with a Gaussian
197
profile.7 Good agreement is obtained for a radius of the aperture of 11 µm for the data taken at
198
670 nm wavelength and at 15º angle of incidence, as shown in Fig. 7.
199
200
201
Figure 6. Scheme showing PMMA spin coated on top of the glass illuminate
202
with laser light from one edge in incident angle of 15° and the forward
203
scattered light detected at different angles. The roughness from spin coated
204
PMMA is assumed to produce an effective circular aperture when the laser is
205
reflected by the rough layer.
11
1.00
15°, 670 nm
Intensity (norm.)
Fraunhofer diffraction, 670 nm
-5
206
0.50
-4
-3
-2
0.00
-1
0
1
2
Scattering angle (degree)
3
4
5
207
Figure 7. Normalized angular dependence of I in 15° incident angles in
208
PMMA side for 670 nm. The solid line was fitted by using equation 4, circles
209
indicate the experimental results.
210
211
The validity of the diffraction model can be verified by changing the optical wavelength.
212
Figure 8 shows the scattered light intensity measured over a range of angles when we
213
illuminate the sample from one edge at 15 degree through the PMMA part at different
214
wavelengths of respectively 401 nm, 532 nm, 633 nm , and 670 nm. Clearly, the scattered
215
light cones show a decrease in width for decreasing wavelength.
216
The Fraunhofer diffraction for the circular aperture was calculated when the size of the
217
particle is fixed at 11 µm while the wavelength was decreased according to the used lasers.
218
We find good quantitative agreement with our experimental results in Fig. 8 (lines), showing
219
that the diffraction pattern gets more and more compressed into a narrow cone around the
220
forward direction for shorter wavelengths.
12
1.00
15°, 670 nm
Fraunhofer diffraction, 670 nm
15°, 633 nm
Intensity (norm.)
Fraunhofer diffraction, 633 nm
15°, 532 nm
Fraunhofer diffraction, 532 nm
0.50
15°, 401 nm
Fraunhofer diffraction, 401 nm
221
0.00
-1
0
1
Scattering angle (°)
222
Figure 8. Comparison of normalized scattering intensity at wavelengths of
223
670 nm, 633 nm, 532 nm, and 401 nm detected over a range of angles with
224
illumination from 15° incident angles through the PMMA part of the sample.
-5
-4
-3
-2
2
1.00
3
4
5
15 °, without optical gel
15 °, with optical gel
Intensity (norm.)
Gaussian
-5
225
0.50
-4
-3
-2
0.00
-1
0
1
2
Scattering angle (degree)
3
4
226
Figure 9. Comparison of intensity of scattered light at a wavelength of 670
227
nm detected over a range of angles with illumination from 15° incident
228
angles once when the PMMA top surface covered with the optical gel
229
(circles, blue) and without optical gel (diamonds, green).
5
13
230
To further investigate the cause of the scattering in spin coated PMMA on top of the BK7
231
glass, the top surface in PMMA (n=1.49) part was covered by optical gel with refractive index
232
of 1.4646(THORLABS). The surface tension of the gel produced a smooth film which
233
compensated the surface roughness of the PMMA layer. Subsequently, the irradiance of
234
scattered light as a function of angle was measured when illuminating the sample at a 15º
235
angle of incidence. The results are compared with a measurement taken on the same sample
236
before the gel was added. Results are shown in Fig. 9. As we can see, application of the
237
optical gel results a decrease of the angular width of the scattering cone. This effect
238
unambiguously shows that the cause of the scattering in spin coated PMMA on top of the
239
glass is the surface roughness. Compared to the surface scattering contribution, the bulk
240
scattering in this type of sample is negligibly small, i.e. of order 10-5 cm-1.6
241
It is relevant to consider whether diffraction effects play a role in the situation that the
242
illumination is provided by mutually incoherent fluorescent molecules. To assess this we have
243
to compare the divergence of a point source with the diffraction provided by the surface
244
roughness. For example, when a point source illuminates an area of 10 m at a distance of 1
245
mm from the source, this corresponds to a divergence angle of 10-2 radians or 0.5º, i.e. smaller
246
than the typical diffraction broadening in our samples. Therefore surface scattering losses are
247
relevant for incoherent fluorescence emission at propagation distances larger than several
248
hundred m, which is the case in FSC.
249
250
4 Conclusion
251
In summary, the contribution of light scattering in fluorescent solar collectors (FSC) based on
252
a spin-coated dye/polymer layer was investigated. Measurements of the transmission cones as
253
a function of total internal reflections (TIR) revealed that the predominant loss factor is
254
surface scattering at the top layer, caused by roughness of the spin-coated PMMA.
14
255
Good agreement is obtained when we consider the PMMA roughness as an coherent aperture
256
with a circular shadow therefore the angular distribution of the scattering intensity can be
257
fitted using far-field Fraunhofer diffraction. The width of the scattered beam increases when
258
the wavelength is increased from 401 nm to 670 nm, in good agreement with Fraunhofer
259
diffraction for a circular aperture at different wavelengths where the size of the aperture is
260
fixed to the value of 11 µm. This value is of the same order as the correlation length of the
261
height variations observed in AFM measurements. The value of the scattering was found to
262
decrease significantly when we cover the top surface with optical gel, which unambiguously
263
shows that surface scattering is the predominant loss factor in our FCS compared to bulk
264
scattering effects. Surface roughness is caused by to the large required thickness of the
265
PMMA-dye layer for the operation of the FSC. Our results indicate that the performance of
266
the FSC can be improved by using a subsequent planarization with a thin index-matching
267
layer of low roughness.
268
269
Acknowledgements The authors would like to thank L. Danos for help with the
270
experimental setup. This project was funded partly through UK SUPERGEN (Sustainable
271
Power Generation and Supply) PV21 Programme.
272
References
273
1. A. Goetzberger, W. Greubel, Solar energy conversion with fluorescent collectors, Appl.
274
Phys. 14,123–139 (1977).
275
2. W.H.Weber and J. Lambe. Luminescent greenhouse collector for solar radiation. Appl.
276
Optics, 15, 2299 (1976).
277
3. J.S. Batchelder, A.H. Zewail, and T. Cole. Luminescent solar concentrators. 1: Theory of
278
operation and techniques for performance evaluation. Appl Optics, 18, 3090 (1979).
15
279
4. J.S. Batchelder, A.H. Zewail, and T. Cole. Luminescent solar concentrators. 2:
280
Experimental and theoretical analysis of their possible efficiencies. Appl Optics, 20, 3733
281
(1981).
282
5. P. Kittidachachan, L. Danos, T.J.J. Meyer, N. Alderman, and T. Markvart. Photon
283
collection efficiency of fluorescent solar collectors. CHIMIA. 61, 780 (2007).
284
6. Y. Koike, N. Tanio, and Y. Ohtsuka, Light scattering and heterogeneities in low-loss
285
poly(methyl metacrylate) glasses, Macromolecules 22, 1367-1373 (1989).
286
7. E. Hecht, 4ed Optics, Addison Wesley, 2002, Chap. 10.
287
288
289
16
Download