cpc solar mini
TRANSCRIPT
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Investigation on a mini-CPC hybrid solar thermoelectric generator unit
Y.J. Dai a , *, H.M. Hu a , T.S. Ge a, R.Z. Wang a , Per Kjellsen a, b
a Institute of Refrigeration and Cryogenics, Research Center of Solar Power and Refrigeration, M.O.E, Shanghai Jiao Tong University, Shanghai, Chinab Norwegian University of Science and Technology, Trondheim, Norway
a r t i c l e i n f o
Article history:
Received 31 August 2015
Received in revised form
20 January 2016
Accepted 20 January 2016
Available online xxx
Keywords:
Solar hot water
Thermoelectric generator
Mini-CPC
Ef ciency
a b s t r a c t
A hybrid solar hot water and Bi2Te3-based thermoelectric generator (TEG) unit using a heat pipe evac-
uated tube collector with mini-compound parabolic concentrator (mini-CPC) is proposed. In this unit, theheat from the heat pipe evacuated tube solar collector is transferred to the hot side of TEG. Simulta-
neously, water cooling is used at the cold side to maintain the temperature difference. Electricity is
generated by TEG and the remaining heat is transferred to water at the same time. This paper in-
vestigates how to convert excess solar heat into electricity more effectively. A mathematical model
regarding this unit is developed and validated. It is found that the mini-CPC can signi cantly improve the
electrical ef ciency. The optimal thermal conductance of TEG is determined, which could make the best
use of excess solar heat. The excess solar heat can be effectively converted into electricity when ZT of
Bi2Te3 can be improved from 100 C to 200 C. Using TEG with ZT ¼ 1.0 and a geometrical concentrating
ratio at 0.92, electrical and thermal ef ciencies of this system are predicted to be 3.3% and 48.6% when
solar radiation and water temperature are 800 Wm2 and 20 C, respectively.© 2016 Published by Elsevier Ltd.
1. Introduction
Increasing pressure from environment and energy crisis attracts
the development of solar thermal technologies for industrial and
domestic applications. Operation data in the USA show that water
heating accounts for 20% of household energy use [1]. Flat plate
solar collector and evacuated glass tube solar collector are
commonly used for solar water heating system. In China, evacuated
glass tube collector is more popularly used due to the improved
thermal performance and low cost.
Most of the evacuated glass tube solar collectors are non-
concentrating, and the operation temperature is normally low.
Recently, low concentrating solar evacuated collector has been
developed to be both cheaper and more compact. Li et al. [2]investigated thermal performance of evacuated collectors with
3 and 6 CPC reectors. It is found that thermal ef ciencies (hths)are ashigh as51% and 54% byusing 3 CPC and 6 CPCwhen watertemperature (T w) is150
C.Pei etal. [3] compared the performancesof solar evacuated collectors with and without mini-CPC. It is found
that solar evacuated collector with mini-CPC has a higher thermal
ef ciency than that without mini-CPC at high water temperature.
Zambolin [4] investigated the thermal performances of at plate
and evacuated tube solar collectors with external CPC reectors.
The ef ciency curves in steady-state and quasi-dynamic methods
are obtained. Kossyvakis et al. [5] modeled the solar thermoelectric
generator using ANSYS workbench software. The computational
results reveal that the performance can be signicantly improved
by optical concentrated congurations.
The ef ciencies of evacuated glass tube collectors with and
without low concentrating CPC are normally above 50% and 60%,
respectively, even if the water temperature is up to 90 C. Thetemperature range meets the operational requirement of thermo-
electric generator (TEG). The combined technology of TEG and
evacuated glass tube solar collector has received increasing atten-
tion. Chen et al. [6,7] proposed the concept of thermal concentra-tion to obtain a large temperature drop across thermoelectric (TE)
legs in a very cost-effective way. The experimental results showed
that electrical ef ciency (he) is around 4.6% with solar radiation (G)
at 1000 Wm2 and cold-side temperature of 20 C. However,commercial TEG could not be employed in this system because the
thermal concentration of the commercial TEG is not more than 10
[8], while in that system the thermal concentration is around 200
[7]. McEnaney et al. [9] also extended the concept of thermal
concentration into concentrating solar TEG. The results showed
that he can be 10% when geometric optical concentration ratio is 45
using skutterudite and Bi2Te3 materials. Lesage et al. [10] have* Corresponding author.
E-mail address: [email protected] (Y.J. Dai).
Contents lists available at ScienceDirect
Renewable Energy
j o u r n a l h o m e p a g e : w w w . e l s e v i e r . co m / l o c a t e / r e n e n e
http://dx.doi.org/10.1016/j.renene.2016.01.060
0960-1481/©
2016 Published by Elsevier Ltd.
Renewable Energy 92 (2016) 83e94
mailto:[email protected]://www.sciencedirect.com/science/journal/09601481http://www.elsevier.com/locate/renenehttp://dx.doi.org/10.1016/j.renene.2016.01.060http://dx.doi.org/10.1016/j.renene.2016.01.060http://dx.doi.org/10.1016/j.renene.2016.01.060http://dx.doi.org/10.1016/j.renene.2016.01.060http://dx.doi.org/10.1016/j.renene.2016.01.060http://dx.doi.org/10.1016/j.renene.2016.01.060http://www.elsevier.com/locate/renenehttp://www.sciencedirect.com/science/journal/09601481http://crossmark.crossref.org/dialog/?doi=10.1016/j.renene.2016.01.060&domain=pdfmailto:[email protected]
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Fig. 2 show the specication and schematic of heat pipe evacuatedglass tube solar collector with mini-CPC. The prototype of SHTG is
mounted facing south and inclined at 30 from the horizon using asupport. The angle of inclination for SHTG is nearly identical with
latitude of Shanghai (latitude 31.14) in order to obtain largestannual solar gain [13]. According to the study of Mills [14], the
geometrical concentration ratio (C ) can be dened as:
C ¼ W CPC pDi
(1)
3. Mathematical model
3.1. Optical analysis
In order to evaluate the performance of SHTG, a three dimen-
sional ray tracing program Tracepro (Lambda Research Corporation,
Littleton, MA) is employed to determine angular acceptance of
mini-CPC reector. The transversal projection angle of the rays is
varied in steps of 10 from 70 to þ70. As shown in Fig. 3, it canbe noted that the longitudinal projection angle of the rays is
changed from þ60 to 0 to þ60 in the whole day. So the longi-tudinal projection angle of the rays is varied in the steps of 10 from0 to þ60 .
The angular acceptance at a given incident angle can be calcu-
lated by Ref. [2]:
haðqÞ ¼ hað0; 0ÞhaðqT ; 0Þhað0; 0Þ
hað0; qLÞhað0; 0Þ
(2)
Fig. 4 shows the variation of the angular acceptances at any
given incident angle. It is noted that there exists a drop at qT ¼ ±60 , because part of incident rays reected by reector cannot reachthe absorber. It is also found that averageha ismore than84% at any
given incident angle in the whole day. It indicates that ha can
remain at a very high value without tracking system.
3.2. Thermal performance modeling
One-dimensional analytical mathematical model of SHTG is
established. The following assumptions have been made without
losing signicant accuracy:
(1) Heat transfer is assumed to be steady state.
(2) Thermal resistance along the heat pipe is neglected.
(3) Thermal properties of selective coating are constant.
Fig. 1. A general view of SHTG.
Fig. 2. Construction of heat pipe collector with mini-CPC.
Table 1
The specication of heat pipe collector with mini-CPC.
ai εi ao ¼ εo to Do (mm) Di (mm) L tube (m) L cpc (m) Wcpc (mm)0.86 0.10 0.80 0.90 47 58 1.75 1.75 136
South North
East
West
θ
30o
SHTG
θT
Fig. 3. Position of SHTG.
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(4) The Thomson effect of TEG is neglected.
(5) Heat transfers of the air gap inside TEG module are
neglected.
Fig. 5 shows the thermal network of SHTG. The mini-CPC
reector concentrates solar energy onto the selective coating and
then the thermal energy (S ) is produced, which contains useful
energy (Q U ) and thermal loss (Q L). Q U is the thermal energy
absorbed on the hot side of TEG. Based on the energy balance for
the TEG, Q U converts into electrical energy (P ) by TEG and the
remaining Q U is absorbed by hot water. So Q U contains electrical
energy (P ) and thermal energy (Q th).
3.2.1. Thermal loss coef cient
It is found that Q U can be expressed as [15]:
Q U ¼ S Q L ¼ GCAihref hatoai Q L (1)where G is the solar irradiance, C is the concentration ratio, Ai is the
area of the inner glass tube and a i is the absorptance of the inner
glass tube. The thermal loss can be expressed as [16]:
Q L ¼ U L AiðT i T aÞ (2)
where U L, T i and T a are the thermal loss coef cient, the temperature
of the inner glass tube and the ambient temperature. Then, the
thermal loss coef cient can be expressed as [16]:
U L ¼ 1
Ai
1
hi;o Aiþ 1
ho;a þ ho;s Ao!1
(3)
where hi,o is the radiation heat transfer coef cient between the
inner tube and outer glass tube. ho,a is the convection heat transfer
coef cient between outer glass tube and ambient, and ho,s is the
radiation heat transfer coef cient between outer glass tube andsky.
Ao is the surface area of outer glass tube.
hi,o can be expressed as [16]:
hi;o ¼s
T 2
i þ T 2o
ðT i þ T oÞ
1εi
þ A i Ao
1εo
1 (4)
where T o is the temperature of outer glass tube. s is the Ste-
faneBoltzmann constant. εi and εo are the emittances of the
absorber tube and outer glass tube, respectively.ho,s can be expressed as [16]:
ho;s ¼ sεo
T 2o þ T 2sky
T 2o þ T 2sky
(5)
where T sky is the temperature of the sky, T sky ¼ 0.0522T1:5a .ho,a can be expressed as [16]:
ho;a ¼ 5:7 þ 3:8v (6)
where v is the wind speed.
As shown in Fig. 5, the energy balance of the outer glass tube can
be expressed as:
GCAihref haao þ hi;o AiðT i T oÞ ¼ Aoho;sT o T skyþ ho;aðT o T aÞ
(7)
where ao is the absorptance of the outer glass tube. T i is assumed to
be T h here, thus U L can be obtained from Eq. (3) to Eq. (7).
3.2.2. Useful ef ciency
As shown in Fig. 5, the useful energy contains the electric energy
and thermal energy. It can be expressed as:
Q U ¼ P þ Q th (8)As shown in Appendix B, the ef ciencyof useful energy, which is
de
ned as useful ef
ciency (hU ), can be expressed as:
Fig. 4. The optical results of mini-CPC: a) the illustration ray tracing program for the
mini-CPC and b) variations of ha (0, qL ) and ha (0, qT) with longitudinal projection angleand longitudinal projection angle.
Fig. 5. Thermal network of SHTG.
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hU ¼ Q U GCAi
¼ F 0href haaito
U LGC
ðT h T aÞ
(9)
It is noted that C is WCPC/pDi, namely, 1/p for non-concentrating
evacuated collector. F0 is the collector ef ciency factor in Eq. (9). Itcan be expressed as [16]:
F 0 ¼ 1=U LW
" 1
WFU Lþ Lb
k find finþ LtubeRhp
# (10)
where W is the circumferential distance of the inner tube, Lb is the
average length of the bond, Ltube is the length of the tube, F is the n
ef ciency of straight n and Rhp is the resistance from n tohotside
of TEG. W is about pDi/2. R hp is the thermal resistance of the heat
pipe. It is given in Appendix A. F can be expressed as [16]:
F ¼ tanh½mW =2mW =2
(11)
where m is expressed as:
m ¼ ffiffiffiffiffiffiffiffiffiffiffiffiffiffi
U Lk find fin
s (12)
where k n and d n are the thermal conductivity and the thickness of
the n. The details of the derivation of the heat transfer model for
this n-type heat pipe are given in Appendix B.
(1). Maximum electrical ef ciency of SHTG
The energy balance equation of the hot side of TEG can be
expressed as:
GCAihU ¼ nateIT h þ kte AteLte ðT h T c Þ 1
2I 2
rte
Lte
Ate
(13)
where n is the number of thermoelectric legs. Ate and Lte are the
cross area and the length of TE legs. ate, kte and rte are the Seebeck
coef cient, thermal conductivity and electrical resistivity of TE legs,
respectively. In the present study, the TE legs are composed by the
Bi2Te3-based TE material. The properties of the TE material are
temperature dependent. Properties of Bi2Te3 are tted in Fig. 6
based on the experimental data from Ferrotec Company [17]. And
it is found that the ZT of commercial TEG available is around 0.59 at
the room temperature, which is far less than that discussed in the
previous studies (ZT ¼ 1) [12].
ate ¼
0:004111T 2m þ 2:84T m 272:2
106
VK 1
(14)
rte ¼
8:735 105T 2m þ 0:1241T m 15:85
106 ðUmÞ(15)
kte ¼ 6:954 105T 2m 0:03767T m þ 6:491
WK 1m1
(16)
where T m is (T h þ T c )/2.The electrical power produced by TEG is [18]:
P ¼ nateðT h T c Þnrte
Lte Ate
þ RL R2L ¼ n
ateI ðT h T c Þ I 2rte Lte Ate
(17)
where RL is the electrical resistance of the external load.
Thus, the electrical ef ciency of SHTG is:
he ¼ P
GCAi(18)
According to the study of solar thermoelectric generator from
Chen [6,7], the optimal current (I opt ) or optimal load (RL,opt ), leading
to maximum electrical ef ciency of the system, are found to be:
I opt ¼ ateðT h T c Þ1 þ ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi1 þ ZT mp rte Lte Ate (19)
RL;opt ¼ ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
1 þ ZT mp
rteLte
Ate(20)
where Z ¼ a2te=ðkterteÞ. We substitute Eq. (19) to Eq. (13) and it isfound that:
280 320 360 400 440190
200
210
220
measured
fit of
ρ measured
fit of ρk measured
fit of k
T/K
S / V K - 1
ρ / Ω m
k / W m - 1 K - 1
12
15
18
21
1.2
1.6
2.0
2.4
2.8
280 320 360 400 4400.2
0.3
0.4
0.5
0.6
0.7
ZT measured
ZT= 2
T/(k ρ)
Z T
T/K
Fig. 6. Experimental data and
tted curve of properties of TE material.
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nkte AteLte ¼ K TEG ¼ GCAihU
,ðT h T c Þ24 ZT h
1 þ ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi1 þ ZT mp þ 1 1
2
Z ðT h T c Þ1 þ ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi1 þ ZT mp 2
35
(21)
where K TEG is the thermal conductance of TEG in SHTG. It is found
that K TEG is related to the structure parameters of lowconcentrating
solar evacuated collector such as Ai and C , and is also related to
operating parameters including G and T c . More importantly, some
manufactures (Marlow, Ferrotec and Kryotherm) have already
given the thermal conductance of TEG. So the suitable TEG can be
directly obtained based on K TEG.
So Eq. (13) can be expressed as:
GCAihU ¼ K TEGðT h T c Þ0@ ZT h
1 þ ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi1 þ ZT mp þ 1
12
Z ðT h T c Þ1 þ ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi1 þ ZT mp 2
1A (22)
Substituting Eqs. (17), (19) and (21) to Eq. (18), the maximum
electrical ef ciency of SHTG can be expressed as:
he ¼ hU ðT h T c Þ
ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi1 þ ZT m
p 1T h ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
1 þ ZT mp þ T c =T h
¼ hU hTEG (23)
where the electrical ef
ciency of SHTG is the useful ef
ciency (hU )
of SHTG multiplied by the maximum electrical ef ciency (hTEG) of
TEG. It can be noted that the maximum he can be obtained at theK TEG and I opt or RL,opt, respectively.
(2) Thermal ef ciency of SHTG.
The energy balance on the cold side of TEG can be expressed as
[18]:
T c T wRw
¼ n
ateIT c þ kte AteLte
ðT h T c Þ þ1
2I 2rte
Lte Ate
(24)
where T w and Rw are the temperature of water and the thermal
resistance between cold side and water, respectively. Rw is
approximated to be 0.026 KW1 in this system [19].
The current of TEG is xedto be I opt , so Eq. (24) can be expressedas:
T c T wRw
¼ GCAihU ð1 hTEGÞ (25)
Hence, the thermal ef ciency of SHTG is dened as:
hth ¼ T c T w
Rw
GCAi ¼ hU ð1 hTEGÞ (26)
Input structure parameters
and operation parameters
Calculate U L and ηu
Determine T o using Eq.(7)
Guess T i
Guess T c
Calculate ηe and ηth
Determine T c using
Eq.(26)
Find maximum ηe under
T i s
Determine corresponding
T o, ηth, K TEG
Input K TEG
Determine T c using Eq.(22)
Determine T h using Eq.(26)
Determine corresponding ηthand ηe
Variable KTEG Fixed KTEG
Guess T o
Fig. 7. Flowchart of SHTG model.
20 40 60 80 100
160
170
180
190
200
Tw /oC
T h / o C
G=solar constant
C=0.92
Fig. 8. Variations of Th with Tw.
0.2 0.4 0.6 0.8 1.0 1.2
1.0
1.5
2.0
2.5 η
η
η
∆T
C
η
& η
/ %
G=800Wm
T =45 C44
48
52
56
η
/ %
60
80
100
120
∆ T / C
Fig. 9. Variations of he, hTEG, hth and DT with C.
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3.3. Solution
The M language in MATLAB is adopted to establish the mathe-
matic model described above. The owchart of SHTG calculation is
shown in Fig. 7. There are two kinds of calculation processes. One isto obtain maximum electrical ef ciency based on variable K TEG, the
other is to investigate the performance under xed suitable K TEG at
different solar irradiations and water temperatures.
4. Results and discussion
As the two calculation processes discussed in Fig. 7, the calcu-
lation process based on variable K TEG is used to investigate limited
T h of TEG, and effect of concentration ratio (C), operating parame-
ters and ZT of TEG on the performance of SHTG under the
maximum electrical ef ciency condition of SHTG. The calculation
process based on xed KTEG is adopted to investigate performance
of SHTG under different xed KTEGs at different solar irradiations,
which would be discussed in section 4.3. The reference value of solar irradiance is assumed to be 800 Wm2 for common data inShanghai [20]. The experimental validation is discussed in section
4.6.
4.1. Theoretical limits of hot side temperature of TEG
There exists a temperature limit on the hot side of TEG to avoid
melting of the solders, which are used to connect the TE legs to the
electrical connector. Hence, it is important to predict the hot side
temperature of TEG of SHTG in extreme condition.
Fig. 8 shows variations of T h with T w in the extreme condition.
The solar irradiance is set to be solar constant (assumed to be
1368 Wm2) [16]. It can be seen that T h increases with the increase
10 20 30 40 50
0.60
0.65
0.70
T / C
K
/ W K
1.2
1.5
1.8
2.1
2.4
K
η
η
η
/ %
G=800Wm
C=0.92
52
53
54
55
56
57
58
η
/ %
Fig. 10. Variations of KTEG, he and hth with Tw.
0 200 400 600 800 1000
0.2
0.4
0.6
0.8
1.0
K
/ W K
K
η
η
G/Wm
0.5
1.0
1.5
η
/ %
30
35
40
45
50
55
η
/ %
T =45 C
C=0.92
Fig. 11. Variations of KTEG, he and hth with G.
Fig.12. Variations of he and hth with G with respect to different K TEGs: a) he and b) hth.
0 200 400 600 800 1000 1200
80
120
160
200
Th for practical ZT
Th for constant ZT
T h
/ o C
0.2
0.4
0.6
0.8KTEG for constant ZT
KTEG
for practical ZT
K T E G
/ W K - 1
G/Wm-2
Tw=45
oC
C=0.92
Fig. 13. Variations of Th and KTEG for practical ZT and constant ZT with G.
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of T w and the largest value of T h is 201 C when T w is 100 C. The
commercial TEGs of some manufactures (Ferrotec, Marlow) can be
operated steadily below 250 C, so SHTG can work steadily.
4.2. Effect of concentration ratio (C)
Fig. 9 shows the variations of he, hTEG, hth and DT with C when T wis45 C and G is setto be800 W/m2. C increases from 0.32, which isnon-concentrating system, to 1.12. The temperature of 45 C canmeet the needs of domestic hot water [11]. Firstly, it is noted that
hTEG increases from 1.8% to 2.5%. It agrees with the variation of DT
with respect to the commercial TEG. It indicates that hTEG increases
with the increase of C due tothe increase of DT . Secondly, it is found
that hth increases from 45.0% to 56.2%. It is because hU increases
with the increase of C based on Eq. (9). Finally, he increases from
0.8% to 1.4%. It is noted that he increases by more than 50%. It is
because both of hTEG and hU increase with the increase of C. It in-dicates that the low concentrating system can improve hesignicantly.
4.3. Effects of operating parameters (T w and G)
The operating parameters (T w and G) are variable in SHTG. Thus,
the thermal conductance of TEG (K TEG) is variable along the process.
As a result, it is important to investigate the effects of these oper-
ating parameters on K TEG.
Fig. 10 shows the variations of K TEG, he and hth as T w increases
from 10 C to 50 C. he drops from 2.2% to 1.3% and hth drops from57.4% to 53.8% in the process. It is noted thathe drops by nearly 50%,
while hth drops slightly. It indicatesa high electrical ef ciency in the
process of heating watercan be obtained without severely reducingthermal ef ciency. It is also noted that K TEG increases slightly from
0.60 W/K to 0.71 W/K in this process. Thus, the impact of T w on K TEGcan be neglected in the process.
Fig. 11 shows the variations of K TEG, he and hth with G. It is found
that both he and hth increase with the increase of G, because hU increases with increasing of G according to Eq. (9). It is also noted
that he increases more drastically than hth. K TEG increases from 0.15
WK1 to 0.85 WK1 when G increases from 100 Wm2 to1000 Wm2. It implies that K TEG changes dramatically with G.However, variable K TEG could not be employed in SHTG in practice.
Hence, the optimal value, K TEG, is selected based on the large solar
irradiance and low solar irradiance in the following.
Fig. 12 shows the effect of G on hth and he with respect to
different K TEG including variable K TEG, summer K TEG, winter K TEG and
0 200 400 600 800 1000
0.5
1.0
1.5
2.0
constant ZT
pratical ZT
η e / %
G/Wm-2
constant ZT
Tw=45
oC
C=0.92
30
40
50
60
η t h
/ %
Fig. 14. Variations of he and hth for constant ZT and practical ZT with G. 10 20 30 40 50
2
3
4
5 ZT=0.5
ZT=1.0
ZT=1.5
η e
/ %
Tw
/o
C
C=0.92
G=800Wm-2
a)
10 20 30 40 50
45.0
46.5
48.0
49.5
51.0 ZT=0.5 ZT=1.0
ZT=1.5
η t h
/ %
Tw /
oC
C=0.92
G=800Wm-2
b)
10 20 30 40 50155
160
165
170
175
180
ZT=0.5
ZT=1.0
ZT=1.5
T h
/ o C
Tw
/o
C
C=0.92
G=800Wm-2
c)
Fig. 15. Effect of ZT of TEG on performance of SHTG. a) Variations of he with T w, b)
Variations of hth with T w and c) Variations of T h with T w.
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nonTEG. Summer K TEG and winter K TEG are the K TEG based on high
solar irradiance (1000 Wm2) and poor solar irradiance(100 Wm2), respectively. Variable K TEG is adopted on the basis of avariable solar irradiance, which leads to the largest electrical ef -
ciency under different solar irradiances. NonTEG is just a solar
evacuated heater without TEG. It is noted that hths for variable K TEGand nonTEG increase along with G due to the increase of hU shown
in Eq. (9). hth for variable K TEG is 30%e40% lower than that for
nonTEG. However, hth for summer K TEG increases rstly and then
decreases as G further increases. So there exists a maximum value
(60%) around 300 Wm2
, which is caused by the variation of hU . Asshown in Eq. (9), when G is low, hU can be improved by G. When G is
high, the increase of hL and Th due to the increase of T i leads to the
decrease of hU . Moreover, h th for summer K TEG is close to that for
nonTEG when G is at 300e500 Wm2, while hth for summer K TEG isclose to that for variable K TEG when G is higher than 500 Wm
2.Meanwhile, he for both variable K TEG and summer K TEG increase
with G. However, he for summer K TEG is close to that for variable
K TEG. Furthermore, it is found that hth for winter K TEG decreases with
increasing of G due to small K TEG. Though he for winter K TEG is close
to the maximum he at lower G level, hth for winter K TEG is far lower
than that for nonTEG. It can be seen that the summer K TEG can be
used in SHTG to fully use excess solar heat without reducing
thermal ef ciency when solar radiation is low.
4.4. Effect of temperature dependent properties of TE material
Fig. 13 shows variations of T h and K TEG for practical ZT and
constant ZT (ZT ¼ 0.59) with G. It is noted that T h for constant ZT ishigher than that for practical ZT, especially at large G. When G is
1000 Wm2, T h is 159 C and 192 C for practical and constant ZT,respectively. The reason is that ZT of traditional Bi2Te3 decreases
with the increase of temperature. Further, K TEG for constant ZT is
lower than that for practical ZT, especially at large G. Low T h can be
kept in orderto increasehU when K TEG is high at practical ZT. Thus, it
is effective to increase ZT value at high temperature from 100 C to200 C for Bi2Te3 TE material.
Fig. 14 shows variations of he and hth for constant ZT and prac-
tical ZT with G. Similarly, he for constant ZT is higher than that forpractical ZT while hth for constant ZT is lower than that for practical
ZT, especially at high G. It indicates that TEG cannot effectively
convert solar heat into electricity due to performance degradation
of TE material at high temperature.
4.5. Effect of ZT of TEG
ZT of TEG is the most important parameter to improve the
performance of SHTG. Though practical ZT for traditional Bi2Te3 is
temperature dependent, constant ZT with respect to different
values is adopted to investigate its effect in a straightforward way.
Fig.15 shows the effect of ZTof TEG on the performance of SHTG
under G and C is 800 Wm2 and 0.92, respectively. Recently, ZT
values at 0.5, 1.0 and 1.5 refer to common, good and excellent TEGs,respectively. The TEG, whose ZT is 1.0, can be fabricated by nano-
composites Bi2Te3 TE material and it is available in some manu-
factures [21]. The TEG, of which ZT is 1.5, can be prepared at the
Fig. 16. The experimental test system of SHTG.
Table 2
Specication of the experimental apparatus.
Apparatus Specication Production site Parameter
TEG 9500/127/060 B China L W H (mm): 39.7 39.7 4.1Thermostatic TZL-1015D China Water temperature: 0e100 (oC)
Side rheostat BC1e25 W 10U China Accuracy:0.1U
Temperature sensor PT1000 Germany Accuracy: ±0.15 CPyranometer CM22, Kipp&Zonen Netherlands Accuracy: ±1%
Flowmeter LFS15 China Accuracy: ±2.5%
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laboratory level. As shown in Fig. 15 a), it is noted that he increases
distinctly with the increase of ZT, especially at the low ZT. For
example, hes are 2.0%, 3.3% and 4.3% when ZTs are 0.5, 1.0 and 1.5 at
T w ¼ 20 C, respectively. It implied that the low ZT (ZT ¼ 0.5) valueshould be increased. It suggests that some commercial TE material
should be improved by nanocrystallization and doping [21]. More
importantly, hth could not decrease obviously with the increase of
ZT. As shown in Fig. 15 b), hth is 46.0%, 45.0% and 44.3% when ZT is
0.5, 1.0 and 1.5 when T w ¼ 50 C Fig.15 c) shows the variations of T hwith T w under different ZTs. It can be seen that T h decreases with
the increase of ZT and all of T hs are below 200 C. So in SHTG, highperformance TEG can ensure that T h is lower than melting tem-
perature of solders.
4.6. Experimental validation
In order to validate the simulation analysis, experimental setup
is established as shown in Fig.16. Experiments areconducted to test
the electrical and thermal performance of SHTG. The TEG of SHTG is
9500/127/060B from the Ferrotec Company (Hangzhou, China) and
its thermal conductance is about 0.64 W/K, which is K TEG for this
SHTG at 700 Wm2e800 Wm2 of solar irradiance. The specica-tion, mount and inclination of SHTG are described in Section 2. In
this testing system, various inlet water temperatures have been
maintained by using a thermostatic waterbath (Poxiwar China) and
the water is circulated using brushless DC pumps. The slide rheo-
stat (0e10U, 0.1U) is employed as electrical load and connected
with the TEG. The side rheostat is xed at 3.2 Uwhich is around the
optimal value of load (R opt).
he and hth can be measured by:
he ¼ P
GACPC ¼
U 2Load
.RL
GACPC (27)
hth ¼ C pmwðT out T inÞ
GACPC (28)
where ACPC is the area of the CPC, U Load is the voltage of external
load, RL is the resistance of the load, C p is the specic heat of water,
mw is the mass ow rate of water, T in is the inlet water temperature
and T out is the outlet water temperature.
Physical measurement parameters include the water temper-
ature at inlet and outlet of SHTG, the ambient temperature, the
ow rate of water, the incident solar irradiance and electrical
power of SHTG. The temperature sensors (PT1000) were used tomeasure the water temperatures of the inlet and outlet, and
ambient temperature. A pyranometer (CM22, Kipp&Zonen) was
employed to measure the global irradiance on SHTG. The output
voltage was measured by Keithley 2700 directly. The data of
temperatures and solar irradiance were transmitted to a data
logger (Keithley 2700) and then to computer for analysis shown
in Fig. 16. The owmeter (Rotameter) was employed to measure
the water ow rate. The specication of the experimental appa-
ratus is shown in Table 2.
Fig.17 shows the variations of experimental data and simulation
data with T ws when G is around 750Wm2. From Fig. 17 a), the
uctuation of P is small under the variable G due to the thermal
capacity of SHTG. It implies that continuous electricity can be
produced. From Fig. 17 b), it can be seen that the results of themodel agree with that of the experiment. The largest relative errors
of he and hth are 4.5% and 6.0%, respectively. Further, he drops from
1.88% to 1.23% and hth drops from 56.7% to 47.1% when T w increases
from 20 C to 50 C. The he and hth are higher than that predicted byMiao et al. [12], because the mini-CPC and TEG with suitable K TEGare employed in the present study.
Generally, the cost of thermoelectric generator module using in
SHTG is about 4e5 $/piece. This data is from a Chinese largest
online shop (Alibaba) or Amazon. The cost is very low compared to
evacuated tube solar collectors ($830/m2) [22]. In AM1.5G and
Tw ¼ 25 C, he is about 1.9%. As for this SHTG, P is about 4.5 W forone TEG. It indicates that the increased cost is about 1 $/W. This
value is close to that for solar PV.
5. Conclusion
A SHTG using heat pipe evacuated glass tube collector with
mini-CPC has been presented in this study. The following conclu-
sions can be obtained:
(1) ha of mini-CPC is more than 80% from 70 to 70 withouttracking system and the mini-CPC reector can signicantly
improve he.
(2) The optimal KTEG should be determined by high solar irra-
diance and is almost independent on the temperature of the
0 1 2 3 4 5 6 7
700
800
T =30 C
T =20 C
T =50 C
T =40 C
G / W m - 2
t/min
2.4
2.6
2.8
3.0
3.2
3.4
P
/ W
P for T =30 C
P for T =20 C
P for Tw=40 CP for T
w=50
oC
a)
20 25 30 35 40 45 500.0
0.4
0.8
1.2
1.6
2.0
simulation
experiment
η e
/ %
Tw /
oC
45
50
55
60
65
η t h
/ %
b)
Fig. 17. Variations of experimental data and simulation data with T ws, a) experimental
data for P at different Gs, b) variations of he and hth.
Y.J. Dai et al. / Renewable Energy 92 (2016) 83e9492
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hot water. SHTG with optimal KTEG can effectively convert
the excess solar heat into electricity.
(3) The excess solar heat can be effectively utilized if ZT of Bi2Te3TE material at the temperature from 100 Ce200 C isimproved to a great extent.
(4) he and hth of SHTG are predicted to be 3.3% and 48.6% when C ,
ZT, G and T w are 0.92, 1.0, 800 Wm2 and 20 C, respectively.
Acknowledgments
This work is supported by the National Science and Technology
Support Project of China under the Contract No.2012BAA05B04.
Appendix A. Thermal resistance of heat pipe
R w,E R E R C R w,CR b R con
T b Th
R hp
Fig. 18. Thermal network of the heat pipe.
As shown in Fig. 18, thermal resistance of the heat pipe can be
expressed as [23]:
Rhp ¼ Rw;E þ RE þ RC þ Rw;C þ Rcon (29)
where R w,E and R w,C are the wall radial thermal resistances of
evaporation and condensation sections. R E and R C are evaporation
and condensation interfacial thermal resistances. R con is the contact
resistance between the heat pipe and hot side of TEG. R con is
assumed to be 0.02 W K1 [12]. The thermal resistance of the vaporow is negligible.
Rw;E ¼ln
Do;E
Di;E
2pLE kw(30)
RE ¼ 1
pDi;E hE LE (31)
RC ¼ 1
pDi;C hC LC (32)
Rw;C ¼ln
Do;C
Di;C
2pLC kw(33)
The evaporation and condensation heat transfer coef cients can
be expressed as [24,25]:
hE ¼ A"
r21 gh fg k3l
mlðT w:E T sat :E ÞLE
#0:25(34)
A ¼h
0:997 0:334ðcos qÞ0:108i" LE
Di;E
#½0:254ðcos qÞ0:385(35)
hC ¼ 0:943"r1 g cos qðr1 rvÞh fg k3l
mlðT sat :C T w:C ÞLC
#0:25(36)
where q
is the incline angle for the SHTG (30 in this study).
Appendix B. Derivation of heat transfer for n-type heat pipe
Fig. 19. The details of the unfolding n.
Based on Fig. 2, the details of the unfolding n are shown in
Fig. 19. The half of the unfolding n inside of the inner glass tube is
selected due to symmetry.
Fig. 20. Energy balance on the n element.3
As shown in Fig. 20, the element balance on the n element can
be expressed as:
S D x Ai
U LD xð
T
T aÞ þ k find
dT
dx
x
k finddT
dx
xþD x
Ltube
¼ 0 (37)The n is directly connected with the inner glass tube of the
evacuatetube. So the input thermal energy per unit of length due to
solar energy is SDx/Ai. The corresponding output thermal energy
per unit of length is UL Dx (TTa).
Ai ¼ WLtube (38)
W ¼ pDi (39)
Boundary conditions:
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dT
dx
x¼0
¼ 0 (40)
It is insulated when x ¼ 0 due to thermal symmetry.
T j x¼W =2 ¼ T b (41)
The useful energy collected by n can be expressed as:
Q U ¼ F ½S U L AiðT b T aÞ (42)
F ¼ tanh½mW =2mW =2
(43)
The useful energy is transferred to the hot side of TEG. There
exist two thermal resistances: one is the bond resistance, the other
is the thermal resistance of the heat pipe. The useful energy can be
expressed as:
Q U ¼ T b T hRb þ Rhp
(44)
Based on the Eq. (42) and Eq. (44), we can nd that:
Q U ¼ F 0½S U L AiðT h T aÞ (45)
F 0 ¼ 1=U LW
" 1
WFU Lþ Lb
k find þ LtubeRhp
# (46)
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