Kaijun
Jiang,1 Qiang
Zhang,1 Yanqiang Kong,1 Chao Xu,1 Xing Ju1
and Xiaoze Du1, 2*
1 Key Laboratory of Condition Monitoring and Control
for Power Plant Equipment (North China Electric Power University), Ministry of
Education, Beijing 102206, China.
2 School of
Energy and Power Engineering, Lanzhou University of Technology, Lanzhou 730050,
China.
*
Email: [email protected] (X. Du)
Abstract
Concentrated
solar power (CSP) plant integrated with thermal energy storage system has the
potential to scale up to megawatt scale. A new concept using dense particle
suspension flow in up bubbling fluidized bed (UBFB) solar receiver for solar
energy capture is promising. The characterization of the dense particle
suspension was rarely investigated when operating conditions and tube structure
changed. In this paper, a 3D two-fluids model is established to investigate the
behaviour
of dense particles suspension in the UBFB receiver. The impacts of the
superficial gas velocity, tube diameter and wall temperature on the dense
particle suspension hydrodynamics and wall-to-bed heat transfer process are
comprehensively studied. The results show that the stirring action of bubbles due
to bubble wake drift is enhanced when the superficial gas velocity increased and the wall-to-bed heat transfer coefficient is
increased with the tube diameter under a certain range. Moreover,
the radiation heat transfer becomes significant when the wall temperature
exceeds 1000 K. The results obtained can provide a valuable reference for the
design and operation of the UBFB receiver in CSP plant.
Table of Contents
Keywords: Concentrated solar
power; Dense particle suspension; Solid particle solar receiver; Two-fluids
model; Heat transfer coefficient.
1.
Introduction
Nowadays, the main ways of renewable energy utilization
are wind power generation, nuclear power generation, biomass energy generation
and solar energy generation.[1] Among all the
renewable energy applications, solar energy with the merits of huge abundance,
availability, unlimitedness and wide distribution has attracted great attention.[2] Concentrated solar power (CSP) is a potential
electricity generation technology that concentrates solar irradiance reflected
by heliostats into the receiver where the heat transfer fluid (HTF) is heated.[3] The CSP plant with energy storage system can operate
steadily at night. The solar power tower is favored by many researchers since
its advantages of higher efficiency, lower operating costs
and potential of scale-up. Direct steam, air and
molten salts (NaNO3-KNO3) are mainly used as HTF
in solar power tower currently. However, direct steam as
HTF has some drawbacks such as the temperature at the exit is low (<525 ℃),
steam can not be directly used as the
heat storage medium and so on. Pressure air receiver suffers from low heat flux
and low heat transfer coefficient (HTC).[4] The biggest
problem with molten salts as HTF is chemical instability when the temperature
exceeds 565 ℃ and solidification when the temperature is lower than 220 ℃.[5] Recently, a novel concept using dense particle
suspension (DPS) as HTF is proposed by Flamant et
al. [6,7] It has
advantages of higher temperature, lower costs, higher HTC, and the solid
particle can be directly used to store heat. These characteristics give the
opportunity to scale-up the CSP plant.[8]
Many research teams proposed
different kinds of solid particle receivers. According to the methods that HTF
absorbs solar irradiance, solid particle receivers can be mainly divided into
two categories: direct absorption and indirect absorption.[9] Direct absorption solid particle
receivers are very appealing due to its high solar flux density (~1 MW/m2).
However, from the view of engineering operation, the solid mass flow rate is
difficult to control and the convection heat losses
may be enormous. Indirect absorption solid particle receivers obtain lower
radiative flux density compared with direct absorption system, but indirect
absorption solid particle receivers have the merits of better control of solid
mass flow rate and low particle losses during operation.[10] Flamant et
al. [6] proposed a novel concept of solid particle receiver which uses the dense
particle suspension (DPS) composed of fine solid particles (SiC,
dp = 64 μm)
flow in the metallic tubes, named up bubbling fluidized bed (UBFB) receiver.
The solid volume fraction in the riser is under the range of 30–40 % and the
HTF outlet temperature can exceed 750 ℃. Besides, the requirements for
particle materials are lower and no particle losses when solid flux circulated
in the UBFB receiver compared with free-falling particle receiver. Fig. 1 shows a general diagram of a next-generation
CSP plant using solid particles as HTF and heat storage medium.[10] The particles are heated up to a certain
temperature and then transported to a hot pot which in turn feeds a heat
exchanger where the thermal energy is transmitted to the working fluid. After
that, the hot working fluid is sent to the power block. Cold particles are
transported to a cold pot that feeds the receiver. Therefore, it has the
potential to drive the high-efficiency power cycles, such as supercritical
steam Rankine cycle or supercritical carbon dioxide Bretton cycle.[11]
Fig. 1 Schematic diagram of solar power
tower plant. Reproduced with the permission from Ref. [10]. [email protected].
The wall-to-bed HTC is a critical parameter in the design
of the UBFB receiver.[12,13] The wall-to-bed HTC is
determined by many factors, including the superficial gas velocities,
tube diameter, tube wall temperature. Various empirical correlations to predict
HTC have been proposed by many scholars. The commonly used models are Molodstof-Muzyka model and Goriz-Grace
model.[14,15] However, the result determined by Molodstof-Muzyka model is not precise, and Goriz-Grace model only predicts HTC precisely within a
narrow range of operating conditions. Besides, Zhang et al. [16] proposed a modified surface renewal model to
predict HTC in different operating conditions, but it needs to measure too many
parameters to compute. In a word, this empirical correlation models do not yield detailed information about DPS
dynamics and heat transfer process.
With the development of the computer, computational fluid
dynamics (CFD) is an effective way to obtain detailed information about DPS
dynamics and heat transfer mechanism. There are two general methods of
simulation for granular flow: the discrete element method (DEM) and the
two-fluids model (TFM).[17] The main difference between DEM and TFM
is the method to solve the solid phase. The DEM is an Euler-Lagrangian method which
tracks the behaviour of each particle. The TFM is
also called Euler-Euler method which treats solid phase as a continuum basing
the Kinetic theory for granular flow (KTGF) to enclose the conservation
equations. Although the tracking of every particle is more precise, the
computational cost may be very high and the number of
tracking particles is limited (<106). In this study, the number
of particles in the rising tube is more than 109. As a result, the
Euler-Euler model is more suitable in this study. Many scholars used TFM to
simulate gas-solid behaviour in the tubes, but most
of them focused on traditional gas-solid system and only hydrodynamics is
investigated. Wang et al. [18] used TFM to
study the minimum bubbling velocity of A-type particles. Hosseini et al.
[19] successfully
used TFM to study the influence of various drag models on bubbles formation and
break up. For the UBFB receiver, scarce simulations are carried out in the
field. Ansart et al.[20] established a single tube 3D model in NEPTUNE_CFD, but the heat
transfer process is not considered. Marti et al. [21] successfully established a 2D model in OpenFoam to investigate the DPS heat transfer mechanism
while the simplified 2D model cannot capture the details of the DPS in the
tube. Urrutia et al. [22] used TFM to
simulate the behaviour of the DPS in the tubes, but
the influence of operating parameters and the radiation heat transfer is not
further investigated.
As mentioned above, the effects of operating conditions
and the tube structure under high-temperature on the
UBFB receiver need to be further investigated. To our best of knowledge, no CFD
model has been established to study the influences of operating conditions and
structural parameters on the thermo-flow of the UBFB receiver. Moreover, most
of the studies focused on the hydrodynamics of DPS in the rising tube. Based on reviewing prior work, the main aims of this
paper are (1) establishing the TFM model to simulate the behaviour of the
particles in the rising tube under the transient condition and predict the
wall-to-bed HTC; (2) investigating the effects of superficial gas velocity,
tube diameter, and wall temperature on the behaviours of DPS and the
wall-to-bed HTC; (3) considering the contribution of the radiation heat
transfer. Therefore, the results in this paper can provide a useful reference
for the UBFB receiver design in the future and explain the behaviour of the DPS
under the high temperature.
2 Physical and numerical model
2.1 Mathematical model
In this research, a modified Euler-Euler model
integrating the KTGF for solid phase is used to simulate the behaviour of DPS in the UBFB receiver under a wide range of
operating conditions. The modifications include a model to calculate the
effective conductivities according to solid volume fraction and a model to
estimate the radiation heat transfer. All cases are performed on ANSYS Fluent
15.0.
2.1.1 Conservation equations
Euler-Euler model
contains the set of mass, momentum and energy
conservation equations for both phases, which are coupled by the pressure and
interphase exchange coefficients. For the sake of brevity, only the governing
equations of the solid phase are represented due to the governing equations of
the gas phase are similar. The mass conservation equation for the solid phase
without any mass transfer between two phases is determined by
+
= 0 (1)
The momentum conservation equation is given by
(2)
The energy conservation equation is given by
(3)
where Srad represents the radiation
heat transfer through the solid phase, hg,p is the interfacial HTC.
2.1.2 Closure equations
In the Euler-Euler model, a series of
constitutive equations is needed to balance the conservation equations for the
solution because the solid phase is treated as the continuous phase. In this
paper, for solid phase, the constitutive equations derive from KTGF. The KTGF
is a significant tool to describe the movement and fluid property of the solid
phase. First of all, it needs to set a fundamental
parameter that is the granular temperature (=
/3) which describes the variations in the velocity of the particles. Table 1 summarizes the relevant constitutive
equations. [13,18]
Table 1 Constitutive equations [13,18]
Constitutive
equations |
|
|
Solid kinetic
viscosity |
|
Collisional
viscosity |
|
Frictional
viscosity doesn’t need to consider because |
Solid bulk
viscosity |
|
|
|
|
|
Table 2 Drag model equations [19, 24]
Drag model
equations |
|
2.1.3 Define the effective diameter
Because particles are non-spherical
actually, it needs to define effective diameter dp,eff
that satisfied the Ergun equation.[23] The effective diameter dp,eff is refer to the mean Sauter diameter dp
according to the following equation:
(4)
whereis the shape factor of particles. In this case, SiC particle is used,
=0.77, n=2.53.
2.1.4
Modified drag force model
Gas-solid drag force is the main
force in granular flow, especially in vertical flow, which determines bubble behaviour, entrainment and
transport of solid particles. The corresponding model is the key to describe
two-phase movement in numerical simulation accurately. There are two types of
drag force models for gas-solid interaction: one is empirical or semi-empirical
models based on pressure drop, superficial gas velocity and bed expansion such
as Syamlal-O’Brien, Gidaspow.
Another one is derived from gas-solid interaction theory such as Koch-Hill. In
this paper, a modified Syamlal-O’Brien drag force
model is applied and relevant equations can be seen from Table 2.[19, 24]
2.1.5
Radiation Model
The radiation model needs to be
selected according to optical thickness. In this case, DPS is composed of small particles and optical thickness
is greater than 1. As a result, P-1 radiation model is suitable in this case.[25] P-1 radiation is based on the spherical-harmonics method. Radiation flux
qr is given by
(5)
where ,
is the scattering coefficient,
is the linear-anisotropic phase function,
is the incident radiation. The incidence radiation is calculated from
(6)
As mentioned above, the radiation source term is given by
(7)
2.1.6 Effective conductivity
The heat transfer process may be
underestimated if the gas and solid phase conductivity directly be used in the
simulation. The reason is that the DPS is composed of the gas phase and solid
phase. Besides, the wall-to-bed HTC is determined by two phases. Therefore, it
is necessary to modify the correlations of conductivity. Kuipers
et al. [26] proposed an
expression comprehensively consider the effects of the gas phase and solids
phase as follows.
(8)
(9)
(10)
where,
and
.
2.1.7 Interphase heat transfer
Assuming particles are sphere, the interphase HTC in Eq. (3) is
determined by (11)
The Nusselt
number for the gas-solid system is determined by Gunn correlation [27] as follows
(12)
where Res is Reynolds number of particles
in the solid phase, Pr is Prandtl
number of the gas phase determined by
(13)
Table 3 SiC and Air thermophysical properties [28-30]
SiC
physical properties |
|
Air physical properties |
|
2.2 Details of the simulations
2.2.1 Phases properties
The solid particles used in this study are SiC and fluidized gas is air,
detailed information about the particle properties can be
seen from Table 3.[28-30]
2.2.2
Boundary and initial conditions
1) Inlet and outlet boundary conditions
The
inlet is set as a velocity inlet condition. Both particles and air enter the
tube with the same temperature which is determined by experiments. The solid
phase enters the tube with an interstitial velocity and volume fraction
corresponding to the average values measured by the experiment. The velocity
difference between the gas and solid is slip velocity (Uslip).
Therefore, the gas phase velocity at the entrance is set as Ug=Us+Uslip. These
settings applied to the simulations except investigating the effect of
superficial gas velocity. The gas phase velocity at the entrance is set as 3Umf,
5Umf, 7Umf and 9Umf for
investigating the impacts of superficial gas velocity.
The outlet is set as
a pressure outlet and zero-gauge pressure is fixed at the outlet.
2) Tube wall conditions
The circumferential temperature of the
rising tube is convenient to measure compared with the heat flux. Besides,
the circumferential temperature of the rising tube can be view as uniform due
to the drastic heat conduction in metallic tubes.[31] As a result, in the
heated tube section, the wall temperature condition is applied. Based on
average experimental results, the wall temperature profile is assumed a
polynomial change temperature function T(z). The functional relationship
is changed with the operating condition. The reduction at the top of the tube is assumed heat
insulation.
The no-slip boundary
condition is assumed for the two phases at the walls. [32]
3) Initial conditions and other settings
At the simulation
beginning, a fixed bed with a porosity of 0.4 and a height of 0.25 is assumed.
The temperature of the initial bed is equal to the gas inlet temperature.
Due to the fluidized bed fluctuates, all
simulations performed under the transitory state. The SIMPLE algorithm is used
for the pressure-velocity coupling. The second-order upwind discretization
scheme is used for discretizing density, momentum and
energy conservation equations. Quick discretization scheme is applied to
discretize volume fraction.
2.3
Experimental model and calculate domain
In order to
understand the dynamics and heat transfer process of DPS in the UBFB receiver,
a single rising tube experimental setup was constructed by Flamant
et al.[6,7] This study was conducted on a solar furnace (1WM) in
France CNRS-Promes. On the premise of minimizing the amount of calculation and keeping the
results accurate, only the section of the tube, length = 0.5 m, exposed
to concentrated radiative flux is simulated. The detail information about the
rig and experimental results can refer to the references.[6,7,21]
Fig. 2 3D schematic of the tube with mesh and the schematic of
the upper zone used to determine hwb and cross-sectional view of the
tube with mesh.
2.4 Date process method
To avoid impacts of
the initial conditions and boundary, the upper section of the tube is used to
determine the wall-to-bed HTC, as
shown in Fig. 2. The time-averaged power transmitted to the solid phasewhen simulation reaches quasi-steady state is
determined by
(14)
whereis the time-averaged solid mass flow rate,
is solid specific heat capacity, Ts,m
is the average middle cross-sectional solid particle temperature, Ts,o is the average outlet solid particle
temperature.
The
wall-to-bed HTC is given by
(15)
where theis upper section tube internal area,
is logarithmic mean temperature difference given by
where Tw,m is the middle tube wall temperature, Tw,o is the outlet tube wall temperature.[22]
3
Results and discussion
3.1
Model validation
3.1.1
Mesh independency validation
In this study, a
hybrid mesh is applied, as shown in Fig. 2. The
boundary layer grid is applied in the near-wall region because the temperature
intensely changes in the region. As shown in Fig. 2,
a reduction is added at the top of the rising tube to improve the simulation
convergence.
Fig. 3 Outlet solid temperature and time-averaged
solid volume fraction as a function of the number of cells.
Ensuring that the numerical results are
independent with the grid size before the simulation is important. Grid
independence of the simulation results is tested for four different grid sizes
by comparing the solid phase temperature at the tube outlet and the average
solid volume fraction in the tube.
The solid particles temperature at the tube outlet and the average solid volume
fraction as a function of the number of cells is illustrated in Fig. 3. As the grid size reduced, the solid phase
temperature at the tube outlet is increased and the solid volume fraction is
decreased. The
temperature difference between the last two cases of grids is less than 0.5%
and the solid volume fraction difference between the last two sets of grids is
less than 1%. The simulation result is almost unchanged. Therefore, the authors conclude that 334196 cells are enough and
grid size with 334196 cells is used in the following analysis.
Table 4 Simulation conditions
and results compared with experiment results.
|
D (mm) |
|
|
|
|
|
|
|
T(z), 0<z<0.5m |
42.35 |
36 |
455.78 |
577.36 |
548.83 |
4.94 |
489.71 |
449.66 |
8.18 |
-414z2+302z+559 |
64.29 |
36 |
421.76 |
532.67 |
516.86 |
2.97 |
630.75 |
596.35 |
5.45 |
-501z2+290z+538 |
70.59 |
36 |
485.40 |
582.14 |
564.26 |
3.07 |
656.20 |
637.70 |
2.82 |
-229z2+165z+585 |
87.81 |
36 |
389.70 |
528.15 |
495.85 |
6.11 |
666.53 |
628.56 |
5.70 |
-442z2+334z+505 |
3.1.2
Simulation results compared with experiment results and basic analysis
The simulation is deemed as convergence when
the mean solid temperature at the tube exit and mean solid fraction reached
relative stability. The solid mass flow rate is negatively related to the
simulation time. It needs approximate 24 days to compute with lower solid mass
flow rate and it needs approximate 14 days to finish the job with higher solid
mass flow rate. In Table 4, the numerical
results of the time-averaged outlet solid particles temperature and the
wall-to-bed HTC with the experimental results are compared. The temperature of solid
particles is convenient to determine by thermocouples in the experiment, so the
temperature difference between simulation and experiment is the main
comparison. The temperature was
much overestimated with low solid mass flow rate. The reason may be that the
solid phase recirculation at low solid mass flow rate is overestimated. Fig. 4 displays the solid particles velocity vector
line at ms=42.35kg/h, t=60s. It can
see from the figure that solid move downward at the vicinity of the wall and
wall-slugging is observed. The downward solid flux moves to the center region
due to lower pressure at the bubble wake. The maximum relative error of the
outlet solid phase temperature between simulation and experiment is 6.50%,
which verifies that the numerical model can correctly simulate the DPS behaviour in the rising tube.
Fig. 4 Typical picture of solid particles velocity vector
line.
3.2
Basic analysis
Fig. 5 shows the XZ-plane
temperature contour of the solid phase in different operating conditions. As
shown in Fig. 5, the solid mass flow rate
significantly impacts the solid temperature profile and Ts,o. The result shows the rapid increase of the solid phase
temperature with height and the radial profile distribution. In the radial
direction, a thermal penetration thickness exists near the wall area where heat
is transferred mainly by convection and conduction. As a result, the heat
transfer between the wall and DPS is acutely and the
temperature gradient is high. Fig. 6 shows the
solid volume fraction contours at different time. The solid concentration in
the near-wall region and rising bubbles at the top of the tube are obvious. The
solid concentration in the near-wall region is beneficial for the wall-to-bed
heat transfer. The differences in solid volume fraction, tube wall temperature
profile and superficial gas velocity between different operating conditions are
the main reason for the phenomenon. The factors will be further investigated in
the following sections.
Fig. 5 XZ-plane solid phase temperature
contours in different solid mass flow rate (a: ms=42.35kg/h;
b: ms=64.29kg/h; c: ms=70.59kg/h;
d: ms=87.81kg/h, t=73s).
3.3
The effects of superficial gas velocity
The
parameter of superficial gas velocity significantly influences the DPS dynamics
and heat transfer process. In order to investigate the
effect of the superficial gas velocities (Ug=3Umf,
5Umf, 7Umf and 9Umf), a
constant set of wall temperature condition and inlet solid phase velocity is
used.
Fig. 7
presents the time-averaged wall-to-bed HTC and outlet
solid
phase temperature as a function of Ug. The value of HTC tends
to progressively increase to a maximum value and then gradually decrease when
the Ug increased. For the bubbling fluidized bed, the
stirring action of bubbles due to bubble wake drift is enhanced when the Ug
increased. As a result, the renewal frequency of fresh solid particle in the
near-wall region is improved and wall-to-bed HTC is enhanced. However, the
solid phase concentration is decreased and the fraction of time that the
heating surface is covered by gas phase increased, and this eventually
outweighs the renewal effect and leads to the decrease of the wall-to-bed HTC. Fig. 8 presents the contour of the solids
holdup for various Ug at 3.5s. The results show that the
number and frequency of bubbles are increased with the Ug.
Therefore, the stirred affection of gas bubbles is obviously increased with Ug
increased.
Fig. 6 XZ-plane solid volume fraction at
different time (ms=87.81kg/h,
t=68s).
Fig. 7 The wall-to-bed HTC and outlet solid
phase temperature as a function of Ug.
Fig. 8 Solid volume fraction contours for
different Ug at 3.5s.
Fig. 9 Solid
phase temperature contours for different Ug at 60s (XZ-plane).
Fig. 9
presents the different cases instantaneous solid phase temperature contours at
60s. The result shows that the value of superficial gas velocity significantly
affects the solid phase temperature profile by improving the stirring action of
bubbles and solid particles concentration distribution. It is found that the
increase of solid particles temperature in different working conditions is
different in the Z-axis direction, and the temperature of solid particles
swiftly increased when superficial gas velocity is 5Umf. Fig. 10 presents the distributions of time-averaged
solid particles temperature along X-axis direction and Y-axis direction. In order to avoid reflux influence, the value is got from
the height of 0.4m. The distributions of time-averaged solid particles
temperature along X-axis direction and Y-axis direction present similar
variation tendency that maximum temperature occurs in the vicinity of the wall
and decrease toward the center. As shown in Fig. 10,
the temperature of the solid phase quickly decreases in the vicinity of the
wall. The results indicate that the main heat transfer process of solid
particles is concentrated near the wall by convection and conduction and the
heat transfer between wall and DPS is acutely in the near-wall region. The
maximum temperature of particles occurs in the near-wall region. This is mainly
due to that the solid particles concentrated in the near-wall region and the
maximum temperature gradient also occurs in the near-wall region. Fig. 10 also presents the temperature gradient near
the wall is different in each case. The most intense heat transfer occurs when Ug=5Umf
and the poorest heat transfer occurs when Ug=3Umf.
As a result, the inference above manifests that there is the effective
circulation of solid particles between the wall and the center tube that
maintains the driving force supporting the heat transfer from the wall to DPS.
Besides, the heat transfer between the wall and DPS is weakened for lower Ug.
These results are consistent with previous inference.
Fig. 10 The
distributions of time-average solid phase temperature (a) along X-axis and (b)
Y-axis at Z=0.
3.4
The effects of tube diameter
The cost of investigating the influence of
tube diameter through the experiment is too high. Besides, the tube diameter
significantly impacts the DPS behaviour in the rising
tube. In order to scrutinize the influences of tube
diameter on the DPS dynamics and heat transfer process in the rising tube, four
different tube diameters (D=24mm, D=36mm, D=48mm and D=60mm)
is set with a constant boundary condition.
Fig. 11 shows time-averaged wall-to-bed HTC and outlet solid phase temperature
as a function of tube diameters. The result indicates
that the wall-to-bed HTC is increased with the tube diameter for a certain
range. The total amount of heat power transmitted to the solid phase is
increased due to an increasing solid mass flow rate, 39.05kg/h to 156.03kg/h,
when the riser diameter increased. Therefore, the wall-to-bed HTC is increased
with the tube diameter. However, the outlet solid phase temperature is
negatively correlated with the tube diameter. The main reason is that the total
solid heat capacity rate Cs=Cp,s∙is swiftly increased with the increase of solid mass flow rate and the
increase rate of Cs is significantly higher than the increase
rate of power transmitted to the solid phase.
The instantaneous temperature profile of solid phase
under different tube diameters is presented in Fig. 12. Moreover, these findings may provide references to control the DPS
temperature by changing the solid mass flow rate.
Fig. 11 Time-averaged the wall-to-bed HTC and outlet solid phase temperature as
the function of tube diameters.
It is evident that the speed of the solid phase
temperature rising is faster in the small tube diameter. It is mainly due to
that the total solid heat capacity is lower when the same temperature in small
tube diameter increases. Fig. 13 presents the instantaneous solids holdup
contours of various tube diameter at 65s (XZ-plane). For A-type particles, the
dynamic balance of bubble merging and splitting causes the size of bubbles
gradually increase when the bubble moves upward in the axial direction and then
reaches the maximum size. The slug flow may occur when the size of the bubble
equal to the tube diameter. Moreover, the emergence of slug-flow in the rising
tube may cause pressure fluctuation between parallel tubes and then reduce the
operation reliability of a CSP plant. In the case of small pipe diameter, there
will be slug flow, and there is a tendency to form bubbles. The main reason is
that the wall constraint effect is more powerful for small tube diameter and
the possibility of bubble formation is increased. These results are helpful to
find an optimum tube diameter where slug flow doesn’t
occur in the UBFB receiver.
Fig. 12 Solid phase temperature for different
tube diameter at 71s (XZ-plane).
Fig. 13 Instantaneous solid volume fraction contours
of different tube diameter at 65s (XZ-plane).
3.5 The effects of the tube wall
temperature
In
an actual CSP plant, the tube wall temperature varies during operation and
significantly impacts the DPS behaviour. Thus, the
DPS behaviour with different tube wall temperature is
studied in this section. Four cases with different tube wall temperatures (Tw=600, 800, 1000, 1200K) are
introduced and the other boundary conditions are consistent.
Fig. 14 The
time-averaged wall-to-bed HTC and outlet solid phase temperature as a function
of Tw.
Fig. 15 The time-averaged logarithmic mean
temperature difference and solid volume fraction in the tube as a function of
the tube wall temperature.
Fig. 14
shows the time-averaged wall-to-bed HTC and outlet solid phase temperature as a
function of Tw. The
results show that wall-to-bed HTC reaches a maximum and then decreases with the
increase of tube wall temperature. However, the outlet solid phase temperature
presents a positive correlation with the tube wall temperature. The reason for
the outlet solid phase temperature increase is obvious, but the decrease of HTC
needs to be further analyzed. To find out the explanation for the results, the
calculation method of the wall-to-bed HTC needs to be analyzed in detail. The
wall-to-bed HTC is calculated from Eq (15) and depends on the,
TLMTD and A. The internal
wall area is constant, so the
and
TLMTD are the influence
factors. The power transmitted to the solid phase is increased. However, the
logarithmic mean temperature is progressively increased
and the solid volume fraction is decreased due to gas expansion, as depicted in
Fig. 15. The effects of TLMTD outweigh the effects of
.
The solid particles have enough time to be heated up in lower and middle tube
wall temperature. However, particles do not have enough time to take full
advantage of the higher tube wall temperature. The results indicate that higher
particle residence time or higher particle heating rate is required to take
full advantage of the higher tube wall temperature.
Fig. 16 shows time-averaged
quasi radiative HTC determined by and its fraction as a function of the tube
wall temperature. The result shows that hr
is increased with tube wall temperature and radiation heat transfer is not a
crucial factor for low and middle temperature. Radiation heat transfer should
be taken into consideration when tube wall temperature is higher than 1000K.
Fig. 16 The time-averaged quasi radiative HTC
and its fraction as a function of tube wall temperature.
4
Conclusions and prospects
In this study, a 3D
numerical model is established to investigate the comprehensive DPS behaviour in different operating conditions, including the
effects of superficial gas velocity, tube diameter and tube wall temperature on
the DPS dynamics and heat transfer process. The feasibility and accuracy of the
proposed 3D model have been confirmed against experimental results. Salient
findings are summarized as follows:
(1) The modified Syamlal-O’Brien drag force model and defined
effective conductivity for gas and solid phase is the key to simulate the DPS behaviour in the rising tube accurately. The former
significantly influences the dynamics and the latter ensure simulation of the
heat transfer process correctly.
(2) The superficial gas velocity
affects the DPS behaviour through improving the
stirring action of bubbles and the renewal frequency of fresh solid particles
in the near-wall region. The wall-to-bed HTC reaches a maximum and then
decreases. The results indicate that there is an optimum superficial gas
velocity during operation. Furthermore, these findings give the opportunity to
control the DPS temperature by changing the superficial gas velocity.
(3) The wall-to-bed HTC increases
with the increase of tube diameter. However, the outlet solid phase temperature
is negatively correlated with tube diameter. It is mainly due to the
significant increase of the total solid heat capacity outweighs the increase of
solid mass flow rate. Besides, tube wall diameter significantly affects the
bubble size and the slug flow formation. An appropriate tube diameter for the
designation of UBFB receiver should be selected.
(4) The parameter study presents that the
increase of the tube wall temperature results in a decrease of the wall-to-bed
HTC. A strong decrease of the logarithmic mean temperature is the main reason
for the result. Moreover, the increased tube wall temperature leads to gas
expansion and decrease of the solid fraction in the tube. Lastly, the influence
of superficial gas velocity and tube diameter on radiant heat transfer is not
significant. Radiation heat transfer presents a positive relationship with the
tube wall temperature and DPS temperature. Radiation heat transfer should be taken into account when the tube wall temperature exceeds
1000K.
Although the paper research provided a 3D
model based on TFM to investigate the DPS behaviour
in the tube, there are still some aspects that need to be further studied.
Future works can focus on the aspects as follows. (1) Considering the influence
of the particle size distribution; (2) investigating the characterizations of
parallel rising tubes in the actual UBFB receiver; (3) considering further
reduce the computational cost by using 2.5D model, which attempts to impose flow symmetry in a cylindrical
column by adopting the wedge-shape computational domain and it allows the flow
to pass through the central axis by incorporating the 2D Cartesian flow
assumption in the central region at the same time.
Acknowledgments
This
work was financially supported by the National Natural Science Foundation of
China (Grant No.: 51676069 and 51821004).
Supporting Information
Not
applicable
Conflict of interest
There
are no conflicts to declare
Nomenclature
Latin characters |
|
Aint |
Heat transfer
area (m2) |
Ar |
Archimedes number |
CD |
Drag coefficient |
Cp |
Specific heat
capacity (J/kgK) |
D |
Tube diameter (m) |
dp |
Sauter mean
particle diameter (μm) |
e |
Percentage
relative error (%) |
er |
Restitution coefficient |
G |
Incident
radiation |
h |
Heat transfer
coefficient (W/m2 K) |
hs |
Solid specific
enthalpy (kJ/kg) |
hg,s |
Interphase HTC
(W/m2 K) |
kg,s |
The momentum exchange coefficient (W/mK) |
kg,o |
Conductivity of SiC (W/mK) |
ks,o |
Conductivity of
Air (W/mK) |
ks,eff |
Effective
conductivity of SiC (W/mK) |
kg,eff |
Effective
conductivity of Air (W/mK) |
m |
Mass flow rate
(kg/s) |
Nu |
Nusselt number |
p |
Pressure (Pa) |
Pr |
Prandtl number |
q |
Heat flux (W/m2) |
Q |
Power (W) |
Re |
Reynolds number |
S |
Source term |
T |
Temperature (K) |
t |
Time (s) |
U |
Velocity (m/s) |
z |
Tube height (m) |
Greek symbols |
|
α |
Volume fraction |
β |
Extinction
coefficient |
μ |
Dynamic viscosity (kg/ms) |
ρ |
Density (kg/m3) |
▽ |
Nabla operator |
ω |
Scattering albedo
|
|
Optical thickness |
σs |
Scattering
coefficient (m-1) |
σ |
Stefan-Botzmann constant (W/m2K4) |
|
Shaper factor of
particles |
|
Granular
temperature (m2/s2) |
Subscripts |
|
col |
Collisional |
eff |
Effective |
fr |
Frictional |
g |
Gas-phase |
i |
Inlet |
kin |
Kinetic |
m |
Meddle |
max |
Maximum |
o |
Outlet |
rad |
Radiation |
s |
Solid-phase |
w |
Wall |
Superscript |
|
exp |
Experiment |
sim |
Simulation |
Abbreviations |
|
CFD |
Computational
fluid dynamics |
CSP |
Concentrated
solar power |
DPS |
Dense particle
suspension |
DEM |
Discrete element
method |
HTF |
Heat transfer
fluid |
KFGF |
Kinetic theory
for granular flow |
TFM |
Two-fluids model |
UBFB |
Up bubbling
fluidized bed |
References
[1] Q. Zhang, Z.M. Wang, X.Z Du., G. Yu and H. Wu, Renew. Energ., 2019, 135, 866-876, doi: 10.1016/j.renene.2018.12.064.
[2] H. L. Zhang, J.
Baeyens, G. Caceres, J. Degreve and Y.Q. Lv, Pro.
Energ. Combus. Sci., 2016, 53, 1-40, doi: 10.1016/j.pecs.2015.10.003.
[3] C.K. Ho and B.D.
Iverson, Renew. Sustain Energ. Rev.,
2014, 29, 835-846, doi: 10.1016/j.rser.2013.08.099.
[4] H.L. Zhang, H.
Benoit, I. Perez-Lopèz, G. Flamant, T. W. Tan and J. Baeyens, Renew Energ., 2017, 111, 438-446, doi: 10.1016/j.renene.2017.03.101.
[5] H. L. Zhang, W.B.
Kong, T.W. Tan and J. Baeyens, Energ.,
2017, 139, 52-64, doi: 10.1016/j.energy.2017.07.129.
[6] G. Flamant, D.
Gauthier, H. Benoit, J. L. Sans, R. Garcia, B. Boissière, R. Ansart and M.
Hemati, Chem. Eng. Sci., 2013, 102,
567-576, doi: 10.1016/j.ces.2013.08.051.
[7] G. Flamant, D.
Gauthier, H. Benoit, J. L. Sans, B. Boissière, R. Ansart and M. Hemati, Energ. Proc., 2014, 49, 617-626, doi: 10.1016/j.egypro.2014.03.067.
[8] H.L. Zhang, S. Li,
W.B. Kong, G. Flamant and J. Baeyens, AIP. Conf.
Proc., 2019, 2126, 030067, doi: 10.1063/1.5117579.
[9] C. K. Ho, Appl. Ther. Eng., 2016, 109, 958-969, doi: 10.1016/j.applthermaleng.2016.04.103.
[10] K. J. Jiang, X. Z.
Du, Y. Q. Kong, C. Xu, X. Ju, Renew. Sustain.
Energ. Rev., 2019, 116, 109463, doi: 10.1016/j.rser.2019.109463.
[11] H. L. Zhang, H.
Benoit, D. Gauthier, J. Degrève, J. Baeyens, I. P. López, M. Hemati and G.
Flamant, Appl. Energ., 2016, 161,
206-224, doi: 10.1016/j.apenergy.2015.10.005.
[12] H. L. Zhang, J.
Baeyens, J. Degrève and G. Cacères, Renew. Sustain.
Energ. Rev., 2013, 22, 466-481. doi: 10.1016/j.rser.2013.01.032.
[13] A. Brems, G.
Cáceres, R. Dewil, J. Baeyens and F. Pitié, Energ., 2013, 50, 493-500, doi: 10.1016/j.energy.2012.10.037.
[14] J. R. Grace, Heat
transfer in high velocity fluidized beds. International Heat Transfer
Conference Digital Library: Begel House Inc, 1990.
[15] D. W. Muzyka, The use
of probabilistic multiphase flow equations in the study of the hydrodynamics
and heat transfer in gas-solids suspensions. Western University, Digitized Theses, 1985.
[16] H. L. Zhang, J.
Baeyens, J. Degrève, A. Brems and R. Dewil, Adv.
Powder. Technol., 2014, 25, 710-715, doi: 10.1016/j.apt.2013.10.018.
[17] M. S. Alagha and P. Szentannai, Int. J. Heat. Mass. Trans., 2020, 147,
118907, doi: 10.1016/j.ijheatmasstransfer.2019.118907.
[18] J. W. Wang, M. A.
Hoef and J.A.M. Kuipers, Chem. Eng. Sci.,
2010, 65, 3772-3785, doi: 10.1016/j.ces.2010.03.023.
[19] S. H. Hosseini, W.
Zhong, M. N. Esfahany, L. Pourjafar and S. J. Azizi, J. Fluids. Eng., 2010, 132, 041301, doi: 10.1115/1.4001140.
[20] R. Ansart, P.
García-Triñanes, B. Boissière, H. Benoit, J.P. Seville and O. Simonin, Powder. Technol., 2017, 307, 25-36, doi: 10.1016/j.powtec.2016.11.006.
[21] J. Marti, A.
Haselbacher and A. Steinfeld, Int. J. Heat. Mass.
Trans., 2015, 90, 1056-1070, doi: 10.1016/j.ijheatmasstransfer.2015.07.033.
[22] A. R. Urrutia, H.
Benoit, M. Zambon, D. Gauthier, G. Flamant and G. Mazza, Chem. Eng. Res. Des., 2016, 106, 141-154, doi: 10.1016/j.cherd.2015.12.008.
[23] D. Kunii and O.
Levenspiel, Fluidization engineering. Elsevier, 2013.
[24] M. Syamlal and T. J.
O’Brien, The derivation of a drag coefficient from velocity-voidage
correlation. Office of Fossil Energy, National Energy Technology Laboratory,
Morgantown, West Virginia, 1987.
[25] S. S. Sazhin, E.M.
Sazhina, O. Faltsi-Saravelou and P.Wild, Fuel,
1996, 75, 289-294. doi: 10.1016/0016-2361(95)00269-3.
[26] J. Kuipers, K.J.
Duin, F.P.H. Beckum and W.P.M. Swaaij, Chem. Eng.
Sci., 1992, 47, 1913-1924, doi: 10.1016/0009-2509(92)80309-Z.
[27] D.J. Gunn, Int. J. Heat. Mass. Trans., 1978, 21,
467-476, doi: 10.1016/0017-9310(78)90080-7.
[28] B. P. Singh and M.
Kaviany, Int. J. Heat. Mass. Trans.,
1991, 34, 2869-2882, doi: 10.1016/0017-9310(91)90247-C.
[29] J. Marti, M. Roesle
and A. Steinfeld, J. Heat. Trans., 2014, 136, 092701. doi: 10.1115/1.4027768.
[30] B.E. Poling, G.H.
Thomson, D.G. Friend, R.L. Rowley and W.V. Wilding, Perry's Chemical Engineers'
Handbook. McGraw-Hill Publishing, 2008.
[31] H. Benoit, I. P.
López, D. Gauthier, J. L. Sans and G. Flamant, Sol.
Energ., 2015, 118, 622-633. doi: 10.1016/j.solener.2015.06.007.
[32] P. Fede, G. Moula, A. Ingram, T. Dumas and O. Simonin,
Fluids Engineering Division Summer Meeting (ASME), 2009, 1833-1842. doi: 10.1115/FEDSM2009-78048.
Author information
Kaijun Jiang, male, 1995–,
PhD candidate. Research field: next-generation CSP technologies especially in
solid particle solar receiver; gas-solid two phases flow; CFD.
Xiaoze Du, male, 1970–,
PhD. Research field: enhancing heat transfer; CSP; energy storage materials and
energy storage technology; hydrogen energy and fuel cells.
Publisher’s
Note: Engineered Science Publisher remains neutral with
regard to jurisdictional claims in published maps and institutional affiliations.