ornl is managed by ut-battelle for the us department of energy effects of neutron irradiation in...
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ORNL is managed by UT-Battelle for the US Department of Energy
Effects of Neutron Irradiation in IG-110
Y. Katoh, M. Snead, A.A. CampbellOak Ridge National Laboratory
E. Kunimoto, M. Yamaji, T. KonishiToyo Tanso Co., Ltd.
Presented at the 15th International Nuclear Graphite Specialist Meeting (INGSM-15), September 15-18, 2014, Hangzhou, China
DisclaimerAll data included in this presentation are preliminary and are subject to revision after further analysis and
certification processes are complete.
2 Toyo Program Update
Acknowledgements
• Research sponsored by Toyo Tanso Co., Ltd. under contract NFE-10-02974 with UT-Battelle, LLC.
• Use of HFIR sponsored by Office of Basic Energy Science, U.S. Department of Energy.
• Patricia Tedder, William Comings, Stephanie Curlin, Michael McAllister, Daniel Lewis, Brian Eckhart, Chunghao Shih, Wallace Porter, Marie Williams for their work in LAMDA to obtain the presented results. Nesrin Cetiner and Joel McDuffee for irradiation engineering. Additional ORNL people for irradiation management, hot cell work, radiological protection, etc.
3 Toyo Program Update
Program Summary
• Temperature range significant for gas cooled reactors (300°C-1000°C)
• Dose range from 7 – 40 n/m2 (x1025 [E>0.1MeV])(5 – 30 dpa)
• Acquire comprehensive design properties by rabbit and target creep irradiations
• Rabbit program– PIE-1 is complete – early results reported here
– PIE-2 is in process
– PIE-3 planned after spring 2015
• Creep program– PIE-1 in late 2014 through 2015
– PIE-2 in ~2017
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Pre-Irradiation Material Properties
IG-110a IG-110 ORNL IG-430a IG-430 ORNL
Density (g/cm3) 1.77 1.77 1.82 1.81
Young’s Modulus (GPa) 9.8 9.10 AX9.69 TR 10.8 10.61 AX
11.24 TR
Young’s (Sonic Velocity) 8.94 AX9.75 TR
9.80 AX10.56 TR
CTEmean (x10-6/°C) 4.5b 4.305 Axc
4.069 TRc 4.8b 4.277 AXc
4.079 TRc
Thermal Conductivity (W/m/K) 120 129.04 AX
130.39 TR 140 161.01 AX162.81 TR
Compressive Strength (MPa) 78 79.16 AX
77.71 TR 90 84.93 AX87.32 TR
Tensile Strength (MPa) 25 37
Flexural Strength (MPa) 39d 33.55 AXe
35.87 TRe 54d 46.94 AXe
50.50 TRe
a: Catalog valueb: The measurement temperature range for the CTE is 350 to 450℃c: The measurement temperature range for the CTE is RT to 400℃d: 3 point loadinge: 4 point loading
5 Toyo Program Update
Definition of Orientations for Iso-molded Graphite
X = (~with grain) = against gravity = transverse (TR)
Y = (~with grain) = against gravity = transverse (TR)
Z = (~against grain) = with gravity = axial (AX)
6 Toyo Program Update
Specimen Shapes and Orientations
+Z(AX)
+Y(TR)
-X(TR)
25=L
3=W
2.9=T
MB (TR)
Y=8
Z=X=6
CRS (TR)
Y=4
Z=X=6
TD4 (TR)
25=L
3=W
2.9=
T
MB (AX)
CRS (AX)
Z=8
X=Y=6
TD4 (AX)
4=Z
X=Y=6
TD3 (AX)
3=Z
X=Y=6
Y=3
Z=X=6
TD3 (TR)
Validation of small specimen testing in Y. Katoh et al., ASTM STP1578 (in press)
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Specimen Arrangement in Rabbits
• Two capsule types
• 25 capsules with 8 modulus beam specimens in each capsule
• 9 capsules with a combination of compression strength and thermal diffusivity specimens
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Irradiation Envelope
5 10 15 20 25 30 35 400
200
400
600
800
1000
1200 TTB PIE-1
TTB PIE-2
TTB PIE-3
TTR PIE-2
TTR PIE-3
Neutron Fluence (x1025 n/m2 [E>0.1MeV])
Irra
dia
tion
Tem
per
atu
re (
°C)
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Creep Capsule Specimens
+Z(AX)
+Y(TR)
-X(TR)
CRS (AX) TD3 (AX)
Z=83=Z
X=Y=6
X=Y=6
Y=8 Y=3
Z=X=6Z=X=6
CRS (TR) TD3 (TR)
CRP (AX)
Z=8
X=Y=6
Y=8
Z=X=6
CRP (TR)
1.25 mm hole down center
1.25 mm hole down center
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Creep Capsule Design
• Loaded region has 4 CRP specimens and 1 CRS specimen in each temperature zone
• Lower unloaded region has 1 CRS specimen, 2 CRP specimens, and 8 TD3 specimens in each temperature zone
Upper stressedregion
Lowerunstressedregion
300°C
450°C
600°C
600°C
450°C
300°C
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5 10 15 20 25 30 35 400
200
400
600
800
1000
1200 TTB PIE-1
TTB PIE-2
TTB PIE-3
TTR PIE-2
TTR PIE-3
Neutron Fluence (x1025 n/m2 [E>0.1MeV])
Irra
dia
tion
Tem
per
atu
re (
°C)
Irradiation Envelope
12 Toyo Program Update
Data Analysis Notes
• In the following plots a consistent color and plotting scheme is used:– Filled data points and solid lines are AX direction– Open data points and dotted lines are TR direction– Error bars are one standard deviation (data points without
error bars are measurements from one specimen)– In plot legends the IG-110 is only listed by average
temperature, which IG-430 has the material label included– Data point shapes and color family were kept the same
for IG-110 and IG-430 (i.e. 319°C IG-110 red circles and IG-430 are pink circles)
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Dimensional Change
Burchell, HTK-7 Experiment
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Volume Change
Ishiyama et al. (1996)
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Young’s Modulus Change
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Compressive Strength IG-110
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Thermal Conductivity
650°C
1021.0~,
11
,
1 KmWTKKTK RDunirrirr
Ishiyama et al. (1996)
18 Toyo Program Update
CTE of Irradiated IG-110
Mean CTE referenced to Room Temperature
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CTE Changes with Neutron Fluence
Mean CTE referenced to Room TemperatureCTE values at irradiation temperature
20 Toyo Program Update
Irradiated Young’s Modulus Change Correlates with Density Change
28.4
00
EE
• Irradiated Young’s modulus correlates very well with density (and electrical conductivity).
• Density exponent for irradiation-induced modulus changes appears significantly greater than that for oxidation-induced modulus decrease.
• Large (>> 1) density exponent indicates that pores responsible for modulus variations are extremely non-spherical.
Yoda et al. (1985)
Kunimoto et al. (2009)
Schulz (1981)
Field
EllipsoidalPore
FF
p
2
cos
1
cos1
122
Transfer efficiency factor:
a
F 0 F = 1/3 F 1
21 Toyo Program Update
Major Change in Structural Factor Requires Refinement of Defect Thermal Resistivity Model
0
0 ,,,
unirrunirrunirr
irrirrirr
KK
TKTTK
e : transport efficiency factor in porous medium
000irr
irr
irr
irr
irr
irrirr E
E
K
K
K0 : thermal conductivity of pore-free bulk
unirr
unirr
irr
irr
unirrirrRD KTKKTKTK
,
1
,
1
,
1000
1/K0RD : intrinsic radiation defect thermal resistivity
= better measure of matrix defect accumulation
unirrirrRD KTKTK
1
,
1
,
1
1/KRD : radiation defect thermal resistivity in conventional model
22 Toyo Program Update
Summary
• PIE-1 campaign is in progress
• Initial results show expected trends– All observations consistent with each other and known trends in
early contraction regime– Observed difference in dimensional behavior depending on axial or
transverse relation to gravity during molding
• Findings / implications from additional analyses– Structural term dominates in modulus change in this dose range
• Source mainly from crack closure
– Decrease in intrinsic thermal conductivity more significant than in apparent conductivity
• More PIE-1 and PIE-2 results to come– Higher fluence– Higher temperatures