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Forschungszentrum Karlsruhein der Helmholtz-Gemeinschaft
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Gan and Kamlah, IMF II, Forschungszentrum Karlsruhe. CBBI-14, Petten, September 2006 1
Thermo-Mechanical Modelling of Ceramic Breeder Pebble Beds
and its Application in HELICA Mock-up
Yixiang Gan, Marc Kamlah
Institut für Materialforschung II, Forschungszentrum Karlsruhe
Forschungszentrum Karlsruhein der Helmholtz-Gemeinschaft
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Outline
Material model• Constitutive modelling• Identification of material parameters• Implementation and validation
Application in HELICA mock-up
Pebble-wall interaction• Thermal contact conductance• Friction
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Overview and cross-section of Li4
SiO4
(Reimann et al. 2006)
Material Modelling
Bulk material: Lithium-based ceramics (i.e. Li4
SiO4
)Microstructure: Spherical particlesSize:
d ~ 0.2mm-0.4mmProduction:
melt-spraying (Schott AG, Mainz)
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• Basic experimental results: Oedometric test
J. Reimann, L. Boccaccini, M. Enoeda, A. Y. Ying, Fusion Engineering and Design 61-62 (2002) 319-33
•
Pebble size (mm) is small compared to bed dimensions.•
Thermomechanical behaviour of ceramic breeder pebble beds can be described by the continuum-
mechanical approaches.
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• Nonlinear Elastic Law
• Drucker-Prager-Cap Theory (yielding and hardening)
• Creep Law based on the Drucker-Prager-Cap Model
• Volumetric Strain Dependent Conductivity
• Thermo-Mechanical Interaction (thermal expansion)
• Material Model for Pebble Beds
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Nonlinear Elastic Law (Coube, IWM Freiburg, 1998)
02/22 ])
21(3
31[ EpqAE s
e +−++
= νν
q
pContour Plot of Young’s Modulus at q-p
space
where,
ijij
ii
ssq
p
2331
=
−= σ is the equivalent pressure stress
is the Mises
pressure stress
Implemented in ABAQUS with USDFLD (user defined field).
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Drucker-Prager-Cap yield surface
pap( )βtanapdR +
bp
d
β
( )βα tanapd +
q
βtanapd +
shear failure, Fs
transition surface, Ft
cap, Fc
Drucker-Prager-Cap Theory
)tan1(,
)tan()()(
0tan22
β
β
β
RRdppwhere
pdRRqppF
dpqF
ba
aac
s
+−
=
+−+−=
=−−=
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Creep Mechanisms (strain-hardening)
Consolidation Creep:
If :No volumetric creep
p
q
ac ppp −=In ABAQUS:
Modification: ppc =for directly using the experimental data
]1)1[()/exp(1
1 1
0
10 −
Δ+−
+=Δ ++ mmn
c tttpTBA
mε
0111
011
])())/exp(1
1[( crmm
crmn
c tpTBAm
εεε −+Δ−+
=Δ +++(Buehler, 2002)
Implemented in ABAQUS with CREEP (user defined creep law).
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• From Experiments to Modelling
Nonlinear Elastic LawAe
, s, E0
, v
Drucker-Prager Cap ModelR, β, pb
, d
Cap CreepA, B, m, n
Oedometric test
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2σ
1σq
p
Deformation Mechanism in Oedometric Testing
Plasticity and Hardening (1)
⎪⎩
⎪⎨
⎧
=∂∂=
= 0|
0
311
σσσc
c
GF
2...),,( σβ Rdfpb = (*)
Yielding Criterion
Plastic Flow Law
pldε
pldε
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Reimann‘s Fit:LL CCLLL TCCC 54 1
1*
321 ])([ −+= εσUU CCUUU TCCC 54 1
1*
321 ])([ −+= εσ
plel εεε +=*
elεε =*
( , , )L Upl i ig C Cε σ= (**)
Eqn.(*) and Eqn.(**) plUi
Lib CCTRdp εβ ~...),,,,,(~
Implemented in ABAQUS with USDFLD (user defined field).
Plasticity and Hardening (2)
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plUi
Lib CCTRdp εβ ~...),,,,,(~
•
Using the experimental data by the method of trail and fail, with every set of material parameters.
The Advantages of the Improvement:
PresentBefore Modification
•
Introduce the temperature to the yielding and hardening laws.
Thermoplasticity
•
Directly using the empirical curve fittings, Reimann fit for experiments. Flexibilities in material parameters.
•
The yielding surface and hardening law based on Drucker-
Prager Cap theory, in stresses space.
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Validation
0.0 0.5 1.0 1.5 2.0 2.5 3.0 3.5 4.0 4.50
1
2
3
4
5
6
Com
pres
sive
Stre
ss (M
Pa)
Strain (%)
FEM at 500C Exp. at 500C FEM at 5500C Exp. at 5500C FEM at 7500C Exp. at 7500C FEM at 7500C Exp. at 7500C
HELICA Material Calibration: Lithium Orthosilicate
0 2000 4000 60000
1
2
3
4
5
Cre
ep S
train
(%)
Time (min)
T(0C) Stress(MPa) F.E.M. Exp. 840 4.1 850 2.1 765 2.1 700 2.1
Oedometric compression:T = 50~850 oC
Creep experiments
Experimental data for Li4SiO4 used in HELICA mock-up, from Reimann et al. 2006
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Mechanical interaction:Normal contact force, averaged as surface pressureFriction, μ=0.02/0.05
Thermal interaction:Thermal contact conductance (TCC) model
Contact area
Pebble
Pebble-Wall Interaction
Multiple spot contact conductance, hot-spots distributed randomly along the contact plane.(N contact pairs in the total area S; radius of pebble r)
QhT A
=Δ
2
SsNr
=
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b (>>a)
a
1 1 1, ,k E ν
2 2 2, ,k E ν
Solid spot contact conductance Hertzian
solution for contact problem
s gh h h= +
2
22 /( )sakh Nak S
sr= =
1 2
1 2
2k kkk k
=+
(Madhusudana, 1995,Chan and Tien, 1973)
1/31 23 ( )[ ]4
P K K ra π +=
1 ;2 2(1 )
i ii i
i i
EK GGν
π ν−
= =+
2P psr=
1/3 1/31 22 /3
2 [3 ( ) / 4] gkh K K p h
s rπ= + +
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T91 Steel(Fokkens, 2005)
Inconel 718(Fokkens, 2005)
Li4SiO4 (bulk)(Futamura, 2005)
Poisson Ratio 0.3 0.298 0.24
Young’s modulus 206GPa 207GPa ~95GPa
Thermal conductivity 25.9W/moC 11.2 W/moC ~2 W/moC
radius ∞ ∞0.1125 mm(Reimann
et al., 2006)
s Pebble-
T91 steel
Pebble-
Inconel 718
3 700.482 640.012
4 578.235 528.318
5 498.308 455.291
6 441.276 403.182
7 398.180 363.806
1/3gh d p h= +
Material properties at room temperature
The values of d in Pebble packing topology:(111)-surface of FCC: 3.464(001)-surface of SC: 4(001)-surface of FCC: 4(001)-surface of BCC: 16/3
• Dependent on both local temperature and pressure (initial pressure).•
First simulation, pressure dependent TCC model, using RT parameters. (Aquaro, 2006)
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Prediction of present model and compared with experiments:Abou-Sena, Ying and Abdou
(2003) Fusion Science and Technology
Validation of TCC model
Lack of experimental data of ceramic breeder pebble-wall interaction.
Using other materials’ data sets (Beryllium-SiC), in the same framework of TCC model for validation purpose.
Validated with existing beryllium pebble-wall experiments, well-consist with experimental data while concerning the “initial pressure” (i.e. gravity…).
0.0 0.5 1.0 1.5 2.0 2.5500
1000
1500
2000
2500
3000
3500
4000
4500
Inte
rface
Con
duct
ance
Coe
ffici
ent
(W/m
2 K)
External Applied Load (MPa)
TCC model Experiments
(Abou-Sena et al. 2003)
1/33000( 0.1)Be SiCh p− = +
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• Materials:T91 steel; AISI 316L; Inconel
718; Kathal; Gasket;Li4
SiO4 (Fokkens 2005; Reimann et al. 2006)• FE model:Extracted from IGES file from ENEA BrasimoneModel symmetry2D generalized plane strain element: 3664• Pebble-wall interactionThermal contact conductance modelFriction (0.02/0.05)
HELICA Mock-up
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Results
• Temperature FieldProfiles at different heating steps
• FEM results vs. ExperimentsComparison between FEM model and thermal couples, LVDTs
• Stress-strain fieldhydrostatic pressure, von-Mises
stress, volumetric inelastic strains• Thermal conductivity profiles
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Temperature profiles
Heat flux step-428 kW/m2
Heat flux step-535 kW/m2
Heat flux step-642 kW/m2
CPU time: 4 hours for whole analysis. Convenient for studying the variations of model parameters,
i.e. surface interactions, and physical meaning.
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0 60 120 180 240 300 360 420 480
200
300
400
500
600
700
800FEM Experiments
TE211D (°C) TE306S (°C) TE222D (°C) TE351D (°C)
Tem
pera
ture
(o C)
Time (min)
TC 150mm
0 60 120 180 240 300 360 420 480
200
300
400
500
600
700
800
Tem
pera
ture
(o C)
Time (min)
FEM Experiments TE223D (°C) TE304S (°C) TE105D (°C) TE306D (°C)
TC 55mmThermal couplesCassette
Pebble
Heater
Pebble
Experimental data from A. Tincani, ENEA Brasimone
0 60 120 180 240 300 360 420 480
200
300
400
500
600
700
800FEM Experiments
TE231D (°C) TE305S (°C) TE212D (°C) TE305D (°C)
Tem
pera
ture
(o C)
Time (min)
TC 100mm
Surface heat flux is not uniform in experiments.
55mm100mm150mm
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1 2 3 4 5 660
70
80
90
100
110
120
130
60
70
80
90
100
110
120
130
Tem
pera
ture
Incr
emen
t (0 C
)
Step Number
Experiment FEM Position 55mm 100mm 155mm
55/100/150 mmPressure-dependent TCC modelIncrement of temperature at each step
•
Increment of temperature decreases due to the contact pressure increasing.
• The maximum decrement
(25% of maximum increment) in the experimental observation.•
The trends predicted by FEM compared well with the experiments.•
The initial TCC value is higher in experiments, due to the initial pressure.
; ;p h T↑ ↑ Δ ↓
0( ) 26.5i jMax T T CΔ −Δ =
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0 60 120 180 240 300 360 420 480-0.35
-0.30
-0.25
-0.20
-0.15
-0.10
-0.05
0.00
LVD
T (m
m)
Time (min)
LVDT 01-03 LVDT 04-06 Average value FEM
Displacement vs. LVDTs
0.000 0.005 0.010 0.015 0.020 0.025
400
450
500
550
600
650
700
750
800
Tem
pera
ture
(0 C)
Distance (m)
FEM Experiment 55mm 100mm 150mm
Heater Cassette
Temperature distribution at 42kW/m2
Temperature distribution along the transversal direction
55mm100mm150mm
Experimental data from A. Tincani, ENEA Brasimone
Y
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Hydrostatic Pressure (Pa) at heat flux step-6
von Mises
stress (Pa) at heat flux step-6
• Maximum hydrostatic pressure: 4.28 MPa (average <2 MPa)• Locally distributed at the end of pebble layers• Related to the pebble-wall friction
• Shear region
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0 60 120 180 240 300 360 420 4800.0
0.2
0.4
0.6
0.8
1.0
1.2
1.4
1.6
von
Mis
es S
tress
(MP
a)
Time (min)
55mm 100mm 150mm
0 60 120 180 240 300 360 420 4800.0
0.2
0.4
0.6
0.8
1.0
1.2
1.4
1.6
1.8
2.0
55mm 100mm 150mm
Hyd
rost
atic
Pre
ssur
e (M
Pa)
Time (min)
Stresses along symmetric axis vs. Time
• von Mises
and hydrostatic stresses • Decrease by creep effects• non-positive stresses after unloading.
55/100/150 mm
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Volumetric plastic strain
Volumetric creep strain
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Plastic strain magnitude
Creep strain magnitude
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Thermal Conductivity
• Thermal conductivity depends on both temperature and strain values.• Different values while loading and unloading, decreasing value after unloading.
0.83~1.08W/moC step-6
0.77~0.79 W/moC after unloading
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Conclusion
• Continuum approach for modelling of pebble bedNonlinear elastic law (Coube, 1998)Drucker-Prager-Cap theory (yielding, hardening and creep law)Volumetric strain dependent conductivity (Reimann et al. 2006)Thermo-mechanical interaction (thermal expansion)Identification of material parameters (Gan and Kamlah, 2006)
• Pebble-wall interactionPebble-wall frictionThermal contact conductance
• Simulation of HELICA mock-up2D generilized plane strain modelFully coupled thermal-mechanical analysis
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Dank u zeer!
Thank you!