Volume 42, Issue 11 pp. 2331-2339
Research Article
Open Access

Fixed-Bed Heat Storage – Mathematical Modeling Approaches

Stefan Rönsch

Corresponding Author

Stefan Rönsch

Ernst-Abbe-Hochschule Jena, Carl-Zeiss-Promenade 2, 07745 Jena, Germany

Deutsches Biomasseforschungszentrum, Torgauer Strasse 116, 04347 Leipzig, Germany

Correspondence: Stefan Rönsch ([email protected]), Ernst-Abbe-Hochschule Jena, Carl-Zeiss-Promenade 2, 07745 Jena, Germany.Search for more papers by this author
Bernhard Auer

Bernhard Auer

Ernst-Abbe-Hochschule Jena, Carl-Zeiss-Promenade 2, 07745 Jena, Germany

Search for more papers by this author
First published: 17 July 2019
Citations: 3

Abstract

While renewable heat makes up only 13 % of overall German heat consumption, the share of renewable electricity produced from wind, solar, water, and geothermal power already reached 36 % of overall electricity consumption in 2017. One measure to support the integration of renewable heat in the German energy system is the use of heat storage systems. Although water-based heat storage systems for temperatures up to 100 °C are state of the art, systems for temperatures up to several hundred degrees Celsius are still under investigation or in the demonstration phase. Therefore, this work focuses on the development of a simulation model for analyzing and engineering fixed-bed thermal storage systems that are filled with an inert bulk material such as stone fragments.

1 Introduction

The transition in the German energy system from fossil to renewable energy carriers has reached a remarkable state in 2018. The share of electricity production from wind, solar, water, and geothermal energy has increased continuously over the last years and makes up 36 % of overall German electricity consumption. In contrast, the share of heat from renewables only makes up 13 % of overall German heat consumption and actually decreased slightly by 0.3 % from 2016 to 2017 1.

To increase the share of renewable heat in the energy system, heat storage systems play a key role 2. Heat storage helps overcome the time delay between heat demand and heat supply in industry and households 3. An example is combined heat and power (CHP) supply in industrial processes by gas engines. Due to their load flexibility, these engines are predestined to adapt their load, i.e., their electricity production, to the prices at the electricity exchange (EEX). The engines increase their load during periods of high electricity prices and, therefore, save money for the production site. When electricity prices are low, the engines reduce their load and the plant owner buys electricity from the EEX. To ensure that heat consumers at the plant site do not suffer a heat deficit while the gas engines reduce their load, heat can be stored when the engines operate at high load.

Among the multitude of heat storage systems available on the market or in the focus of research and development 4-7, fixed-bed systems filled with stone fragments are an especially promising option. This type of heat storage system can store heat up to several hundred degrees Celsius at comparatively low investment costs 8.

However, due to the exceptionally dynamic operation conditions of such heat storage systems, their design and proper adaption to specific applications is often a sophisticated task for engineers.

Therefore, this work aims at presenting a time-dependent, 2D (rotationally symmetrical) simulation model able to design fixed-bed heat storage systems filled with inert bulk materials. To emphasize the feasibility of the model, the dynamic behavior of a fixed-bed heat storage is exemplarily analyzed.

2 Heat Storage Concept

The simulation model was set up for an exemplary tubular reactor filled with a fixed bed of stone fragments (Fig. 1). The reactor is insulated by mineral wool and connected to the periphery by flanges. Dimensions and characteristics of the fixed-bed heat storage are presented in Table 1.

Table 1. Dimensions of the heat storage reactor and bulk material.

Parameter

Value

Length of reactor interior lR [m]

2.40

Inner diameter of reactor interior dR [m]

0.45

Diameter of bulk material dBM [m]

0.005

Porosity of bulk material ΦBM [–]

0.38

Thickness of insulation dI [m]

0.05

Details are in the caption following the image
Scheme of the fixed-bed heat storage reactor.

Hot flue gas from a CHP unit serves as a heat carrier that transfers its heat to the bulk of stone fragments of the heat storage. The flue gas flowing through the bulk is characterized by the temperature, pressure, volume flow rate, and composition shown in Tab. 2.

Table 2. Flue gas characteristics.

Parameter

Value

Pressure [bar]

1.0

Temperature [°C]

393

Volume flow rate [m3 h−1 (STP)]

298.96

Carbon dioxide [vol %]

8.50

Nitrogen [vol %]

72.28

Oxygen [vol %]

10.37

Water steam [vol %]

8.85

To analyze the dynamic behavior of the heat storage, exemplarily the store-in and the holding phases were considered. The store-in phase lasts 1 h. During this phase, heat is transferred from the flue gas entering the heat storage with a temperature of 669 K to the cooler bulk with a starting temperature of 298 K. The holding phase comprises a time period of 24 h directly after the store-in phase, during which no further heat is supplied to the storage.

3 Modeling and Simulation

The simulation model was conducted with the software COMSOL Multiphysics. Key aspects of the model, i.e., differential equations, heat transfer equations, material properties, and basic settings in COMSOL Multiphysics, are described in the following.

3.1 Differential Equations

The simulation model of the heat storage comprises three phases:
  • A gaseous phase representing the fluid (hot flue gas) flowing through the heat storage. All symbols related to the fluid are indexed with F.

  • A solid phase representing the bulk material (stone fragments) inside the heat storage. All symbols related to the bulk material are indexed with BM.

  • A solid phase representing the outer steel wall and flanges of the heat storage. All symbols related to the wall are indexed with W.

Each of the three phases is described by a specific energy balance in the form of a partial differential equation (PDE) 9. The connections between these three energy balances are the heat transfer terms.

The insulation is not described by a separate differential equation. Its temperature is set equal to ambient temperature. However, properties of the insulation, such as its thermal conductivity and thickness, contribute to the thermal transfer coefficient characterizing the heat transfer through the insulation between steel wall and surroundings.

3.1.1 Differential Equation of the Gaseous Phase (Fluid)

The energy balance of the fluid (Eq. 1) describes the temperature TF of the hot flue gas streaming through the bulk of stone fragments. It is influenced by the radial thermal conductivity of the fluid, the convective heat transport of the fluid, the heat transfer to the bulk material, and the heat transfer to the wall. To define the thermal conduction for the fluid and the bulk material, the same thermal conductivity is used, namely, the effective radial thermal conductivity Λr (see Sect. 3.4).
urn:x-wiley:09307516:media:ceat201800540-math-0001(1)

The spatial coordinate in the direction of fluid flow is indexed with z. The radial spatial coordinate, i.e., that with an angle of 90° to the flow direction, is indexed with y. The fluid flow is modeled as a bulk flow. Hence, heat conduction in flow direction, such as radial convective heat and mass transport, are neglected, as recommended in 10.

3.1.2 Differential Equation of the Solid Phase (Bulk Material)

The energy balance of the bulk material (Eq. 2) describes the bulk material temperature TBM, which depends on the thermal conductivity in directions z and y. Furthermore, the temperature of the bulk material is influenced by the heat transfer between bulk and fluid.
urn:x-wiley:09307516:media:ceat201800540-math-0002(2)

3.1.3 Differential Equation of the Solid Phase (Wall and Flanges)

The energy balance of the steel wall and flanges (Eq. 3) describes the behavior of the wall temperature TW in dependence on time. Besides the heat conduction, the wall temperature is influenced by the heat transfer from the fluid to the wall, by the heat transfer from the wall to the surroundings (S) through the insulation, and by the heat transfer from the flanges (FL) as a part of the wall to the surroundings.
urn:x-wiley:09307516:media:ceat201800540-math-0003(3)

The geometry of the heat storage is meshed by the software COMSOL Multiphysics. For solving the set of PDEs, COMSOL uses the backward differentiation formula (BDF) method with variable time stepping.

3.2 Heat Transfer Equations

The PDEs of Eqs. 13 reveal the dependence of fluid, bulk material, and wall temperatures on four heat transfer terms: the heat transfer between fluid and bulk material (urn:x-wiley:09307516:media:ceat201800540-math-0004), the heat transfer between fluid and reactor wall (urn:x-wiley:09307516:media:ceat201800540-math-0005), the heat transition between reactor wall and surroundings (urn:x-wiley:09307516:media:ceat201800540-math-0006), and the heat transfer between flanges and surroundings (urn:x-wiley:09307516:media:ceat201800540-math-0007). These four heat transfer terms are schematically shown in Fig. 2. Their calculation is described in the following.

Details are in the caption following the image
Scheme of the fixed-bed heat storage reactor with heat flows.

3.2.1 Heat Transfer between Fluid and Bulk Material

The heat transfer from fluid to the bulk material is defined by the heat transfer coefficient αF-BM (Eq. 4). It depends on the Nusselt number Nu, the thermal conductivity λF of the fluid, and the characteristic length of the bulk material fragments inside the reactor. The characteristic length of the bulk material corresponds to the average diameter dBM of a single stone fragment. Additionally, the heat transfer coefficient αNC is added, which characterizes the heat transfer due to natural convection. It is especially important to describe the heat transfer from fluid to bulk material when there is no forced convection, e.g., during the holding phase, in which no flue gas is directed through the storage. Here αNC was set to a constant value of 2.5 W m−2K−1.
urn:x-wiley:09307516:media:ceat201800540-math-0008(4)

3.2.2 Heat Transfer between Fluid and Reactor Wall

This heat transfer is characterized by the heat transfer coefficient αF-W between fluid (F) and wall (W) (Eq. 5). Its calculation equals the calculation of the heat transfer coefficient αF-BM. According to 11, the characteristic length is the average diameter dBM of a single stone fragment as well. Similar to the heat transfer from fluid to bulk material, a transfer coefficient αNC for natural convection is also added. The only difference between Eqs. 4 and 5 is the way of calculating the Nusselt number.
urn:x-wiley:09307516:media:ceat201800540-math-0009(5)

3.2.3 Heat Transfer between Reactor Wall and Surroundings

The heat transfer between the reactor wall (W) and the surroundings (S) through the insulation (I) is characterized by the heat transition coefficient kW-S. It is calculated by using the thickness dI of the insulation, the thermal conductivity λI of the insulation, and the heat transfer coefficient αI-S between insulation and surroundings (Eq. 6). The heat transfer coefficient αI-S was set to a constant value of 2.5 W m−2K−1.
urn:x-wiley:09307516:media:ceat201800540-math-0010(6)

3.2.4 Heat Transfer between Flange and Surroundings

Finally, the heat transfer coefficient αFL-S between flange (FL) and surroundings (S) has to be considered to determine the heat transfer from the flanges to the surroundings (Eq. 7). It is calculated in dependence on the flange temperature TFL according to the ASHRAE Handbook 12.
urn:x-wiley:09307516:media:ceat201800540-math-0011(7)

3.2.5 Dimensionless Numbers of Heat Transfer

The dimensionless numbers of heat transfer, i.e., the Nusselt number Nu, the Reynolds number Re, and the Prandtl number Pr, are calculated by Eqs. 811, respectively.

Nusselt number for the heat transfer between fluid and wall 13:
urn:x-wiley:09307516:media:ceat201800540-math-0012(8)
Nusselt number for the heat transfer between fluid and bulk material 14:
urn:x-wiley:09307516:media:ceat201800540-math-0013(9)
Reynolds number:
urn:x-wiley:09307516:media:ceat201800540-math-0014(10)
Prandtl number:
urn:x-wiley:09307516:media:ceat201800540-math-0015(11)

With regard to the calculation of the Reynolds and Prandtl numbers, ηF is defined as the dynamic viscosity of the fluid.

3.3 Variables of State

The thermal variables of state of the fluid as pressure, temperature, and specific volume were calculated according to the ideal gas law. The pressure drop was determined with the Ergun equation (Eq. 12) as defined in 15 using the friction number λ, the density ρF, and the average plug flow velocity w0 of the fluid as well as geometric parameters of reactor and bulk material:
urn:x-wiley:09307516:media:ceat201800540-math-0016(12)

3.4 Material Properties

To find a reasonable agreement of calculation time and model precision, the material properties used in the simulation model rely on different degrees of detail. While several properties are set to constant values, the effective radial thermal conductivity is calculated in more detail in dependence on the properties of the fluid and bulk material.

3.4.1 Effective Radial Thermal Conductivity of Fluid and Bulk Material

The calculation of the effective radial thermal conductivity follows the guideline from 16 as it was already applied and proven in a previous work 17. Therefore, the correlated thermal conductivity kBM of the bulk material fragments is calculated first 18. It is equal to the ratio of the thermal conductivity of the bulk material fragments λBM and the thermal conductivity of the fluid λF.
urn:x-wiley:09307516:media:ceat201800540-math-0017(13)
Subsequently, the deformation parameter B is determined by using the porosity Φ of the bulk material 19.
urn:x-wiley:09307516:media:ceat201800540-math-0018(14)
Together with the correlated thermal conductivity, the deformation parameter is used to calculate the parameter N 20:
urn:x-wiley:09307516:media:ceat201800540-math-0019(15)
All three parameters lead to the formula of the correlated thermal conductivity of the unified cell core (UC) kUC 21:
urn:x-wiley:09307516:media:ceat201800540-math-0020(16)
Then, it is possible to determine the correlated thermal conductivity of the pseudo-homogeneous (PH) reactor interior kPH 22:
urn:x-wiley:09307516:media:ceat201800540-math-0021(17)
Subsequently, the thermal conductivity λPH of the pseudo-homogeneous reactor interior can be calculated 18:
urn:x-wiley:09307516:media:ceat201800540-math-0022(18)
For the calculation of the effective radial thermal conductivity Λr, the parameter Kr 23 has to be determined also. It is based on the diameter dBM of the bulk material fragments, the inner diameter dR of the reactor, and the parameter Kr,∞. According to 24 for spherical fragments, Kr,∞ is 7.
urn:x-wiley:09307516:media:ceat201800540-math-0023(19)
The molecular Péclet number Pe0 is the last parameter required for the calculation of the effective radial thermal conductivity Λr. It relies on the average plug flow gas velocity w0, the density ρF of the fluid, the specific heat capacity cp,F of the fluid, the bulk material particle diameter dBM, and the thermal conductivity λF 25. The average plug flow gas velocity can be calculated on the basis of the volume flow rate urn:x-wiley:09307516:media:ceat201800540-math-0024 of the fluid and the inner reactor radius rR. For the calculation of the gas volume flow, the volume flow at standard temperature and pressure (Tab. 2) as well as the respective variables of state have to be taken into account.
urn:x-wiley:09307516:media:ceat201800540-math-0025(20)
Finally, the effective radial thermal conductivity Λr can be calculated 26.
urn:x-wiley:09307516:media:ceat201800540-math-0026(21)

3.4.2 Material Properties of the Fluid

The viscosity ηF, the thermal conductivity λF, and the specific heat capacity cp,F of the fluid are calculated independently of temperature and pressure. They rely on the molar composition of the fluid and the respective values of each gas component at a temperature of 300 °C. The density is calculated according to the ideal gas law.

3.4.3 Material Properties of Reactor Wall, Catalyst, and Insulation

The material properties of reactor wall, catalyst, and insulation are taken into account as constant values (Tab. 3). The reactor wall was assumed to be made from steel 1.4571, the bulk material from chamotte, and the insulation from mineral wool.

Table 3. Material properties of reactor wall, bulk material, and insulation.

Parameter

Value

Source

Density of reactor wall ρW [kg m−3]

7980.0

27, Dea 8

Specific heat capacity of reactor wall cp,W [J kg−1K−1]

530.0

27, Dea 12

Thermal conductivity of reactor wall λW [W m−1K−1]

18.0

27, Dea 11

Density of bulk material ρBM [kg m−3]

2150.0

27, Deb 6

Specific heat capacity of bulk material cp,BM [J kg−1K−1]

956.0

27, Deb 5

Thermal conductivity of bulk material λBM [W m−1K−1]

1.05

27, Deb 3

Thermal conductivity of insulation λI [W m−1K−1]

0.05

27, Dec 2

3.5 Basic Settings in COMSOL Multiphysics

To implement the mathematical model equations described above in COMSOL Multiphysics, a COMSOL model consisting of four different physics modules was set up. These modules correspond to the three energy balances (Eqs. 13) of Sect. 3.1 plus one physics module that pays attention to the mass transport of the fluid:
  • Heat transfer in fluids: This physics module represents the energy balance of the fluid (hot flue gas) flowing through the heat storage. The variable of this module is the fluid temperature TF, the initial value of which is set to ambient temperature. Additionally, in this module a temperature of 666 K is defined at the edge where the fluid enters the reactor. Furthermore, an outflow such as a heat flux and a heat source were added to this module. The heat flux is defined by the product of the heat transfer coefficient αF-W and the temperature difference between TF and TW. The heat source is defined by the product of the heat transfer coefficient αF-BM, the specific surface area of the stone fragments [m2m−3], and the temperature difference between TF and TBM.

  • Heat transfer in solids: This physics module represents the energy balance of the bulk material (stone fragments) inside the heat storage. The variable of the module is the temperature of the bulk material TBM, the initial value of which as well equals ambient temperature. Besides, a heat source was added to this physics module. It describes the heat transfer from the fluid to the bulk and is defined in the same way as the heat source in physics module 1, however, with a negative sign.

  • Heat transfer in solids: This physics module represents the energy balance of the outer steel wall and flanges of the heat storage. The variable of this module is the wall temperature TW. Again, the initial value of this temperature is the ambient temperature. In contrast to the other physics modules, here three different heat fluxes are defined. One heat flux describes the heat transfer between wall and fluid. The respective equation corresponds to that for the heat flux mentioned in physics module 1, however, with a negative sign. The second heat flux represents the heat transfer from the flanges to the surroundings. It is calculated as the product of the heat transfer coefficient αFL-S and the temperature difference between TW and ambient temperature. The third heat flux characterizes the heat transfer from the wall through the insulation to the surroundings. The respective equation is the same as for the heat transfer from the flanges to the surroundings, except that it uses the heat transition coefficient kW-S instead of the heat transfer coefficient αFL-S.

  • Transport of diluted species: This physics module represents the mass transport of the fluid (hot flue gas) flowing through the heat storage. The variables of this module are the gas concentrations of carbon dioxide, nitrogen, oxygen, and water steam. Their initial values are set to zero. Additionally, an inflow and an outflow were added to this physics module. The inflow was marked at the edge where the fluid enters the heat storage. At this edge the concentrations were defined in accordance with the mole fraction and variables of state listed in Tab. 2.

4 Results and Discussion

In the following, the simulation results of the heat storage system are discussed. As defined in Sect. 2, Sects. 4.1 and 4.2 focus on the store-in and heat-up phases, respectively, in which flue gas with a temperature of 669 K starts flowing through the bulk of stone fragments with a starting temperature of 298 K. In Sect. 4.3, the holding phase is discussed. The holding phase comprises a time period of 24 h, i.e., 86 400 s, during which no further heat is supplied to the storage. It takes place directly after the store-in phase and accordingly starts with the temperature reached by the store-in phase.

4.1 Bulk Temperature Development of the Store-in Phase

The development of the bulk temperature over space, i.e., along the spatial coordinate z, is shown in Fig. 3. As the temperature changes with time, the figure contains seven curves representing simulated times of 1, 600, 1200, 1800, 2400, 3000, and 3600 s. The 1-s curve (solid line) shows a horizontal shape characterized by the starting temperature of the bulk (298 K), which means that the bulk still has taken up no heat from the hot flue gas. After 600 s, the temperature of parts of the bulk (0.3 m) has already increased to the flue gas inlet temperature of 669 K. This phenomenon continues with proceeding time. After 1800 s, half of the bulk, i.e., 1.2 m, has reached the flue gas temperature of 669 K, and after 3600 s, almost all of the bulk has reached this temperature.

Details are in the caption following the image
Bulk temperature over spatial coordinate z (store-in phase).

Fig. 4 shows the bulk temperature over a period of 3600 s for three locations in the heat storage system. As locations, the inlet (z = 0 m), the middle (z = 1.2 m), and the outlet (z = 2.4 m) of the heat storage were chosen. Fig. 4 confirms the conclusions from Fig. 3: the temperatures at these three locations in the bulk increase over time. Thereby, the bulk temperature at the inlet increases earlier than the middle and outlet temperatures. While the inlet temperature of the bulk after approximately 200 s already has reached the flue gas inlet temperature of 669 K, the middle of the reactor reaches this temperature after 1800 s. The outlet of the reactor shows this temperature after 3600 s.

Details are in the caption following the image
Bulk temperature over time (store-in phase).

4.2 Flue Gas Temperature Development of the Store-in Phase

Figs. 5 and 6 show the development of the flue gas temperature in the heat storage reactor. In Fig. 5, the flue gas temperature is plotted over the spatial coordinate z for seven different times. Fig. 6 plots the flue gas temperature over a time period of 3600 s for three different reactor locations. The diagrams show almost identical curve shapes, as seen for the bulk temperature. Bulk and flue gas temperature only have a marginal shift, which cannot be distinguished in these diagrams. Fig. 5 shows that the flue gas temperature decreases as the spatial coordinate z increases. For example, the flue gas flows 0.3 m through the bulk without temperature loss after 600 s. After 2400 s, the flue gas flows about 1.8 m through the bulk without any temperature loss.

Details are in the caption following the image
Fluid temperature over spatial coordinate z (store-in phase).
Details are in the caption following the image
Fluid temperature over time (store-in phase).

4.3 Bulk Temperature Development of the Holding Phase

Fig. 7 characterizes the holding phase directly after the store-in phase for a period of 24 h (86 400 s). The three curves show the bulk temperature over time at three different locations in the heat storage unit, i.e., z = 0, 1.2, and 2.4 m. The figure emphasizes the trend that the bulk temperature decreases most significantly at the reactor inlet with z = 0 m and least significantly in the middle with z = 1.2 m. After 86 400 s, the bulk temperature at the inlet is only 338 K. At the reactor outlet, the bulk temperature decreases to 421 K, and in the middle, the temperature decreases only to 506 K.

Details are in the caption following the image
Bulk temperature over time (holding phase).

The slower cooling velocity at the outlet in comparison to the inlet is directly linked to the radial temperatures reached after the store-in phase: at the reactor outlet, only in the middle with y = 0 m, the flue gas temperature of approximately 669 K is reached. Therefore, due to the smaller driving temperature difference between fluid and wall, the heat transfer to the reactor wall is smaller than that at the reactor inlet, where this temperature difference is larger.

4.4 Experimental Validation

To prove the reliability of the simulation model, an experimental validation was conducted. Therefore, the simulation model was adapted to the specific characteristics of a laboratory test facility (geometric dimensions of reactor and bulk material, variables of state, etc.). The laboratory test facility comprises a van, an electrical air preheater, and a cylindrical steel vessel filled with a bulk of basalt stones. Instead of flue gas from a CHP unit, preheated air served as a heat carrier flowing through the bulk and, thereby, heating up the basalt stones.

The basalt stones have an average diameter between 3 and 5 mm and their total mass in the vessel amounts to 16.9 kg. An inner vessel diameter of 266 mm and a bulk density of 1448 kg m−3 lead to an overall bed height of the bulk material of 210 mm. The vessel is insulated with mineral wool and equipped with two thermocouples located in the middle of the vessel at bed heights of 70 and 170 mm, respectively. The air is characterized by an inlet temperature of 423.15 K, atmospheric pressure, and a volume flow rate of 0.01806 m3s−1 (STP).

Even without a fitting of model parameters to experimental results, measurements and simulation reveal accordance below measurement accuracy. While the experiments for the thermocouple at a bed height of 70 mm result in a temperature of 390 K after a heating time of 300 s, the simulation led to a temperature of 391 K. After 600 s the experiments showed a temperature of 421 K and the simulation a temperature of 424 K. The thermocouple located at a bed height of 170 mm measured 314 K after 300 s, 383 K after 600 s, and 423 K after 1020 s. The simulation calculated values of 315, 384, and 423 K, respectively.

5 Conclusion

A time-dependent, 2D (rotationally symmetrical) simulation model was designed for the analysis of fixed-bed heat storage systems filled with an inert bed of a bulk material such as stone fragments. On the basis of this model, a first analysis of an exemplary cylindrical heat storage with length of 2.4 m and an inner diameter of 0.45 m was conducted. The heat storage was filled with stone fragments, and flue gas from a CHP unit serving as a heat carrier with a temperature of 669 K was directed through the bed of fragments.

The analysis led to the following findings:
  • The simulation model is able to qualitatively predict the dynamic behavior of the heat storage system with regard to the heat transfer phenomena in axial and radial directions. Fluid flow phenomena such as turbulence and streamlines are neglected, but indirectly included in the heat transfer calculations (Nusselt number, etc.).

  • The simulation of the store-in/heating phase, in which the hot flue gas is directed through the bulk of stone fragments, shows the typical development of bed and flue gas temperatures over the reactor length. Specifically, the bulk heats up and the flue gas cools down with time.

  • The bulk temperature increases to the flue gas inlet temperature with time. Thereby, a hot zone characterized by the flue gas inlet temperature moves through the bulk.

  • After approximately 1 h, the overall bulk has adapted to the flue gas inlet temperature and the store-in process is finished. At this point, the flue gas does not cool down any more by flowing through the heat storage.

  • With regard to the holding phase, the typical effect of a slower cooling towards ambient temperature in the middle of the reactor in comparison to the inlet and outlet was proven.

  • Regardless of correct results of the heat storage model from a qualitative point of view, quantitative results need to be proven and validated by additional experimental data in future.

Acknowledgements

Open access funding enabled and organized by Projekt DEAL.

The authors have declared no conflict of interest.

    Symbols used

  1. B [–]
  2. deformation parameter

  3. cp,BM [J kg−1K−1]
  4. specific heat capacity of the bulk material

  5. cp,F [J kg−1K−1]
  6. specific heat capacity of the fluid

  7. cp,W [J kg−1K−1]
  8. specific heat capacity of the reactor wall

  9. dBM [m]
  10. diameter of the bulk material fragments

  11. dI [m]
  12. thickness of the insulation

  13. dR [m]
  14. inner diameter of the reactor

  15. kBM [–]
  16. correlated thermal conductivity of the bulk material fragments

  17. kPH [–]
  18. correlated thermal conductivity of the pseudo-homogeneous reactor interior

  19. Kr [–]
  20. parameter

  21. Kr,∞ [–]
  22. parameter

  23. kUC [–]
  24. correlated thermal conductivity of the unified cell core

  25. kW-S [W m−2K−1]
  26. heat transition coefficient between reactor wall and surroundings

  27. lR [m]
  28. reactor length

  29. N [–]
  30. parameter

  31. Nu [–]
  32. Nusselt number

  33. ΔpF [Pa]
  34. pressure drop of the fluid

  35. Pe0 [–]
  36. molecular Peclet number

  37. Pr [–]
  38. Prandtl number

  39. urn:x-wiley:09307516:media:ceat201800540-math-0027 [J s−1]
  40. heat flow between fluid and bulk material

  41. urn:x-wiley:09307516:media:ceat201800540-math-0028 [J s−1]
  42. heat flow between flanges and surroundings

  43. urn:x-wiley:09307516:media:ceat201800540-math-0029 [J s−1]
  44. heat flow between fluid and reactor wall

  45. urn:x-wiley:09307516:media:ceat201800540-math-0030 [J s−1]
  46. heat flow between reactor wall and surroundings

  47. rR [m]
  48. inner radius of the reactor

  49. Re [–]
  50. Reynolds number

  51. t [s]
  52. time

  53. TBM [K]
  54. temperature of bulk material

  55. TF [K]
  56. temperature of the fluid

  57. TFL [K]
  58. temperature of the flanges

  59. TW [K]
  60. temperature of the reactor wall

  61. VBM [m3]
  62. volume of the bulk material (including free space filled with fluid)

  63. VF [m3]
  64. volume of the fluid

  65. urn:x-wiley:09307516:media:ceat201800540-math-0031 [m3s−1]
  66. volume flow rate of the fluid

  67. VW [m3]
  68. volume of the reactor wall

  69. w0 [m s−1]
  70. average plug flow velocity of the fluid

  71. wz [m s−1]
  72. fluid velocity in direction z

  73. y [m]
  74. y-coordinate (perpendicular to fluid flow direction)

  75. z [m]
  76. z-coordinate (in fluid flow direction)

  77. Greek letters

  78. αF-BM [W m−2K−1]
  79. heat transfer coefficient between fluid and bulk material

  80. αFL-S [W m−2K−1]
  81. heat transfer coefficient between flange and surroundings

  82. αF-W [W m−2K−1]
  83. heat transfer coefficient between fluid and reactor wall

  84. αNC [W m−2K−1]
  85. heat transfer coefficient of natural convection

  86. ηF [Pa s]
  87. dynamic viscosity fluid

  88. λ [–]
  89. friction number

  90. λBM [W m−1K−1]
  91. thermal conductivity bulk material

  92. λF [W m−1K−1]
  93. thermal conductivity fluid

  94. λI [W m−1K−1]
  95. thermal conductivity insulation

  96. λPH [W m−1K−1]
  97. thermal conductivity pseudo-homogeneous reactor interior

  98. Λr [W m−1K−1]
  99. effective radial thermal conductivity

  100. λW [W m−1K−1]
  101. thermal conductivity reactor wall

  102. ρBM [kg m−3]
  103. density bulk material (chamotte)

  104. ρF [kg m−3]
  105. density fluid

  106. ρW [kg m−3]
  107. density reactor wall

  108. Φ [–]
  109. porosity of the bulk material

  110. Abbreviations

  111. BDF
  112. backward differentiation formula

  113. BM
  114. bulk material

  115. CHP
  116. combined heat and power

  117. EEX
  118. electricity exchange

  119. F
  120. fluid

  121. FL
  122. flange

  123. I
  124. insulation

  125. PDE
  126. partial differential equation

  127. PH
  128. pseudo-homogeneous

  129. S
  130. surroundings

  131. UC
  132. unified cell core

  133. W
  134. wall

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