slide 1 12-15 nov 2006, efda pwi meeting, ljubljanai.s. landman, fz-karlsruhe modelling on wall...
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12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 1
Modelling on Wall Surfaces and Tokamak Plasma
Consequences of ITER Transient Events
1 Forschungszentrum Karlsruhe (FZK), Germany2 Troitsk Institute for Innovation and Fusion Research (TRINITI), Russia
Contents
• Surface melting of W divertor armour and Be main chamber wall
• Brittle destruction of Carbon Fibre Composites (CFC) and cracking of W
• Contamination of the SOL and core plasma after ELMs
Forschungszentrum Karlsruhein der Helmholtz-Gemeinschaft
FUSION-PL
FZK – EURATOM FUSION ASSOCIATION
I. Landman1, B. Bazylev1, S. Pestchanyi1
with contributions from
A. Zhitluckhin2, V. Podkovyrov2 N. Klimov2 and V. Safronov2
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 2
Introductory comments:• Available tokamaks cannot provide required transient loads Q up to 15 MJ/m2
• Therefore we develop own codes to apply to ITER predictions
-- behavior of candidate materials for fusion (Be, C, W) -- tolerable sizes of off-normal events (ELMs and disruptions)
• For validation, “tokamak simulators” – pulsed plasma guns are engaged ( up to 0.5 ms)
The objectives of our EFDA tasks running in 2006:
TW3-TPP/ MATDAM (finished Jun), TW5-TPP/ ITERTRAN, TW5-TPP/ BEDAM• Modelling support for plasma gun experiments with ITER divertor materials of EU
trademark (TRINITI facilities QSPA-T and MK-200UG)
• Modelling of damage to ITER divertor and main chamber after transients
• Modelling of tokamak plasma contamination following ITER ELMs
• The codes MEMOS, PHEMOBRID, PEGASUS, FOREV and TOKES are engaged
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 3
MEMOS calculates melt motion at heated metallic surfaces (Be, W) accounting formelting, resolidification and evaporation.Melt motion is due to 1) p, 2) surface tension, 3) JB force
It was validated against electron beam- and plasma gun experiments (e-beams: JUDITH, plasma guns: QSPA-Kh50 (Kharkov), QSPA-T, MK-200UG)
The code MEMOS: earlier validations
Qmelt works wellMEMOS validations by plasma guns
MEMOS validations by e-beam at 5 MJ/m2 on the depth of resolidification crater
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 4
Simulation of W-brushe with MEMOS
Validation by QSPA-T
The 2D profile of W-brushes is implemented
Main conclusion: the depth of W melting and resolidification profile are rather similar to that of bulk W target.
However, melt velocity in W-brushes is less by a factor 0.3 - 0.5
Validation by QSPA-T is carried out
Relevance of QSPA to ITER:
Q ~ 0.5 – 1.5 MJ/m2 and = 0.5 ms as in ITER
QSPA: plasma velocity V is 105m/s, in ITER ~ 106
Pressure at the target: p ~ nEi
Density n follows from Q=EinV p 1/Ei
Ei is ion kinetic energy, in QSPA 100 eV only
Thus in ITER the pressure should be much lower.
(Particular figures significantly depend on the size of transient event)
ITER transients Kind of damage
Disruption
(10 MJ/m2, 3 ms)
ELM
(3 MJ/m2 0.5 ms)
W vaporization loss
1 m 0.1 m
W melt roughness 5-10 m 1 m
Single ELMs and disruptions
Therefore, the QSPA experiments should result in much more pronounced melt motion
Therefore the MEMOS was engaged for ITER predictions
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 5
MEMOS (in 2006): simulation of Be melting under radiation impact
Bulk temperature at 0.5 ms.Radiation load duration 0.5 msFull resolidification after 1.1 ms
Radiation heat load distribution over Be target surface
Melt depth vs. heat load duration (T0 = 300 K)
Evaporation depth vs. heat load duration
Melting and evaporation thresholds vs. heat load duration
Resolidification profileon Be target surfaceunder plasma action
Validation by radiation load experiments is required
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 6
PHEMOBRID validation against the QSPA
PHEMOBRID calculates evaporation and BD of CFCbased on BD threshold 10 kJ/g (as GOL-3 results)
The recent QSPA experiments (ELM relevant loads with 0.5 ms):• Mass losses appear at the impact energy density W0 > 1.4 MJ/m2• The rate of CFC erosion exceeds 1 μm/shot (evaporation at T0 = 500 C)
Numerical simulations:
• The heat flux at the surface was calculated as W(t) = W0exp(-h(t)/h0), h(t) calculated thickness of evaporated material, h0 = 1.5 μm (vapour shield).
• Plasma impact was assumed under 30 deg
CFC target layout Evaporation rate of CFC NB31 vs. absorbed energy
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 7
PEGASUS simulation for CFC with inclined fibres versus MK-200UG testsIt calculates BD of CFC and cracking on W surface
The last idea was to incline the PAN fibres under 45 deg to the pitch fibres
In PEGASUS simulations, BD erosion rate under ELM-like loads has decreased by ~5 times
Experiments at MK-200UG to proof this qualitative prediction are performed
The experiments have not confirmed the modelling results:
CFC erosion rate does not depend on orientation of CFC sample
PEGASUS: standard (a) and inclined (b) CFC fibres
a) b)
It seems that the CFC surface was so damaged that the CFC properties became isotropic, and at the large temperature the pitch- and PAN fibres acquire equal thermoconductivities.
PEGASUS: BD damage to improved CFC structure
(The PEGASUS is an abbreviation of “Particle Ensemble for Grain Aggregate Simulation ”)
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 8
PEGASUS modelling of cracks on W target surface
• A model of W surface cracking is developed by S. Pestchanyi to explain experimental crack patterns with crack depth scales of 500 and 50 µm
• A thermostress that appears in the thin resolidified layer after fast cooling causes the cracks through the bulk
Typical W parameters:
Young’s modulus E 3102 GPaThe Poisson ratio 0.3 (shear modulus/E)Tensile strength T < 1 GPaThermal expansion coeff. 10-5 K-1
Melt layer thickness h ~ 10 mTypical thermostress c ~TmeltE ~ 10 GPa
At c >> T cracking should occur
W cross-section with the cracks:QSPA results versus PEGASUS simulation.Q = 0.9 MJ/m2, = 0.5 ms
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 9
PEGASUS simulation of cracks on W target
PEGASUS simulation of cracks on W surface
W surface (QSPA, 100 shots of 0.9 MJ/m2, 0.5 ms. Primary cracks depth ~500 µmSecondary meshes sizes and depth ~102 µm
Typical thermostress F applied to the cracks on W surface (hmelt << L)
A formula for crack depth(F relates with ET )
Cracking scenario:
W surface is fast heated, higher than Tmelt.
Thus pre-surface bulk gets stressed, but in melt c = 0 even just after resolidification
The surface temperature decreases and after c exceeded T, large cracks appear, which decreases c.
Further cooling increases thermostress, and again c exceeded T cracks of small size
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 10
Main features of FOREV:
• Magnetic toroidal geometry of ITER and JET
• SOL multi-fluid plasma description (D+, T+, He+2, C+ to C+6)
• Radiation transport in toroidal geometry for C
ELM scenario as calculated by FOREV:
1. Due to a short large increase of cross-diffusion coefficient Ddiff in the pedestal and the SOL, the pedestal plasma fills the SOL.
2. SOL DT-He plasma hits in both divertor surfaces.
3. At the targets, heat flux and plasma pressure cause evaporation, with account of heat transport into carbon material
4. Eroded material propagates back into the SOL.
Comments on the simulations:
• Experimental DT plasma flux was reproduced approximating Ddiff by suitable dependencies from existing tokamaks.
• The calculations had been performed at WELM = 3.5 to 12 MJ.
ITER layoutin FOREV
RMHD code FOREV: applications for ELM simulations
targets maximum heat fluxes and behaviour of Ddiff during an ELM
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 11
FOREV modelling for heat flux and plasma pressure at ITER divertor surfaces
In this example ELM size isQ = 0.8 MJ/m2, = 0.5 ms
Distributions of impacting DT heat flux and pressure over inner divertor surface.
Those load profiles at different times are used by MEMOS, PHEMOBRID and PEGASUS.
along separatrix, 1.1 ms
SOL contamination as calculated by FOREV
• The vaporization threshold is obtained at WELM = 4.0 MJ (Q = 0.4 MJ/m2).
• During 0.5 ms a significant carbon plasma density in SOL can occur, up to 1021 m-1.
• Carbon ions occupy SOL for a few ms, with their temperature dropping down to 1-2 eV (due to radiative cooling)
• Further ELM consequences are simulated with the code TOKES using the FOREV data on carbon influx into the pedestal
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 12
Newly available features: wall and neutrals
• Heat transport in the wall, surface evaporation
• Underground triangle meshes
• Propagation of neutrals (atoms, photons and neutrons) in the vessel volume as random (Monte-Carlo) beams
• Ionization of atoms by plasma (immediately to Post’s Z)
• The magnetic surfaces are chains of segments through the triangle meshes, which provides optimal plasma-neutral coupling
• Vessel surface of arbitrary poloidal cross-section
• The algorthm of TOKES allows magnetic islands
The TOKES is still under development
(ITER preliminary layout)
Features of TOKES on plasma
• The Grad-Shafranov equation
• Pfirsch-Schlüter transport
• Multi-fluid plasma, (from D to C, and W ions)
• D- and T-beams heat and feed, radiation cools (by Post)
• D+T He + n fusion reaction
• Coil currents feedback upon plasma shape
ITER layout in TOKES
a
b
w
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 13
Contamination of ITER core by carbon after ELMs using the FOREV data
Whole ITER discharge of 400 s was simulated
Carbon ions of FOREV were injected into plasma edge
Power losses have been calculated: radiation losses and fusion power decrease
Q from 0.8 to 1.4 MJ/m2. Magnetic field was fixed.
Main result:
Tolerable ELM size 1 MJ/m2 for ELM frequency ~1Hz
Carbon impurity propagationinto the core after ELM
Benchmark scenario:
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 14
Conclusions and further objectives
MEMOS• Validations for W under plasma impact and Be under e-beams are done
• Validation for Be under radiation load experiments is required (experimental activity on Be using plasma guns is assumed in Kurchatov’s and TRINITI)
PEGASUS and PHEMOBRID• In the modelling the CFC erosion develops mainly due to cracking of PAN fibres
• At the validation of PHEMOBRID the account for vapor shield became necessary
• PEGASUS should be validated extrapolating pitch fibre thermoconductivity down to PAN fibre’s at ~ 4103 K
• PEGASUS modelling on W cracking seems successful. Further development is needed (cracking below the melting threshold: implementation of plasticity).
FOREV and TOKES• The tolerable 1 MJ/m2 obtained is at the minimum of expected ITER ELM sizes.
• In FOREV, Be and W plasma species should be implemented
• In TOKES, at first the radiation transport and the ionization modelling should be improved (now Post’s data are used)
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 15
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 16
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 17
Additional informations
Main results from MK-200UG and QSPA-T at large Q
CFC NB31 and NS31 were exposed to 200 shots 15 MJ/m2
Both CFC behaved similarly (regime with vapour shield)
Maximum erosion rate is proportional to pulse duration
PAN fibres max. erosion rate is of 20 m/ms
Pitch fibres max. erosion rate is of 3 m/ms (evaporation)
Graphite particles of sizes of 1 to 102 m are collected
• Start of vaporization: Qmin=0.3 MJ/m2 for 0.05 ms (MK-200UG) (Qmin: at 0.5 ms would be Qmin = 1 MJ/m2)
Matrix Tow
Direction to axis || to axis
radial axial
10-2k [W/m/K] 2 - 5 0.4 - 0.8 0.5 10 - 20
106 [1/K] 1 ~30 ~10 1
10-2E [GPa] 3 – 7 0.3-0.80.1-0.2
4-8
CFC properties (T < 2103 K)W melt damage after single ELM:
Melting threshold 1.0 MJ/m2 ( = 0.3 ms)
Vaporization threshold: 2.5 MJ/m2
Melt velocity less than 0.5 m/s
Maximum crater depths ~ 0.5 m
Vaporization thickness ~ 0.1 m
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 18
Additional informations (continued)
Damage to the dome gapsand the divertor cassette gaps
• the melting of copper at the W-Cu adjoins is significant
• protective tungsten aprons of the gaps may be necessary
PEGASUS features:• 3106 cells of 1 m represent 3D
material structure• Thermal- and mechanical bonds
between the grains• Anisotropic (for CFC) heat transport
through grain boundaries• Stress due to anisotropy and (c)
temperature gradients• Cracking of the bonds above
elasticity threshold (T)
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 19
Transient energy fluxes expected at the ITER divertor target
ITER Event Repetition Duration Target load Impact energy
Disruption seldom 1 .. 10 ms 10..30 MJ/m2 up to 10 keV
Type I ELMs 1-10 Hz 0.3..0.6 ms 0.5..4 MJ/m2 1..3 keV
Normal tokamak operation 500 s 10 MJ/ m2/s 1..3 keV
Main parameters of plasma guns
Facility MK-200UG QSPA
Pulse duration [ ms ] 0.05 0.2-0.5
Target load [ MJ/m2 ] 0.3 - 15 0.6 - 30
Load spot size [ cm ] 6 – 7 4-5
Magnetic field [ T ] 2 0.5
Impact energy [ keV ]
1.5 (ions) 0.2 (ions)
Plasma gun QSPA
Plasma gun MK200UG schematically
12-15 Nov 2006, EFDA PWI meeting, Ljubljana I.S. Landman, FZ-Karlsruhe Slide 20
FZK codes for consequences of ITER off-normal events
Material surface modelling
MEMOS-1.5D (fluid dynamics)• Melt motion at heated metallic surface• (W and Be targets)
PEGASUS-3D (thermomechanics)• Brittle destruction of graphite and CFC• Cracking on W surface
PHEMOBRID-3D (BD threshold model)• Brittle destruction of graphite and CFC
Plasma modelling
FOREV-2D (radiation MHD)• Pulse transient loads at targets• Plasma shield (disruptions, Type I ELMs)• SOL contamination (C, W, Be)
TOKES-2D (equilibrium MHD)• Confined plasma equilibrium• Core contamination (by C so far)• Core plasma wall coupling effects