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Third PRC-US Magnetic Fusion Collaboration Workshop 18-19 May 2006. Plans and Results of the Texas Collaboration with ASIPP. K.W. Gentle Fusion Research Center University of Texas. Plans and Results of the Texas Collaboration with ASIPP. - PowerPoint PPT Presentation
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Third PRC-US Magnetic Fusion Collaboration Third PRC-US Magnetic Fusion Collaboration Workshop 18-19 May 2006Workshop 18-19 May 2006
Plans and Results of the Texas
Collaboration with ASIPPLong history of collaboration between
the Fusion Research Center, Texas and the Institute of Plasma Physics, Hefei
Plans for HT-7 and EAST ECE -- Electron Cyclotron Emission radiometer for Te
CXRS -- Charge Exchange Recombination Spectroscopy for Ti and rotation
Expanded divertor
Results of Helimak project
Spatial Coverage of ECE System on HT-7
Schematic of the ECE diagnostic on HT-7
Lo Freq(GHz)
98.5 100.433
102.336
104.299
106.232
108.165
110.098
112.031
Hi Freq(GHz)
112 114 116 118 120 122 124 126
ECE Data with position shift to obtain a
relative calibration.
Te Profile (ECE)
• Relative calibration from shift is position position
• Absolute calibration form Thomson Scattering (central temperature)
ECE Temperature Profile
• Shot 81535:
EAST ECE System
Proposed ECE Antenna for EAST• Diffraction limited spatial
resolution • Integrated hot calibration source
• Possible test of ITER prototype calibration source
CXRS on HT-7 and EASTW. L. Rowan,1 Yuejiang Shi,2 June Huang,2
Huang He1, and B. N. Wan2
1Fusion Research Center, The University of Texas at Austin2Institute of Plasma Physics, Chinese Academy of Sciences
• DNB transferred to ASIPP and brought back into operation through common effort
• CXRS spectrometer and optics installed• Plans
–Develop CXRS analysis codes–Conduct transport experiments on HT-7–Transfer DNB to EAST–Transfer CXRS to EAST
DNB, Component Mix, and
CXRS Viewing Range
€
0.25 ≤ r ≤ −0.07
0.93 ≤ ρ ≤ −0.26
CXRS view range
DNBHT-7
The beam has operated for one campaign with an useful density component mix E:E/2:E/3:E/18 = 10:26:49:15
The CXRS diagnostic is installed for the current campaign and is expected to provide Ti, v over the LFS of the plasma
Divertor Projections
• Although ITER divertor may handle heat loads adequately, the divertor heat loads for the next-step reactor will exceed material limits: This is a show-stopper
• Other divertor configurations including radiating mantle and swept divertor will not scale to ITER or to a reactor
• Need an expanded divertor or other configuration
M. Kotschenreuther, P. M. Valanju, S. M. Mahajan, J. C. Wiley, M. Pekker Sherwood Fusion Theory Conference,
April, 2006
Expanded Divertor for EAST
• A new configuration to reduce the heat load on the divertor plates
• Axisymmetric coils near the divertor plates expand the footprint of the intersection of the field lines with the divertor plates
• Divertor coil currents are comparable to other PF coil currents
• The first test of this idea is proposed for EAST. Use reduced plasma current and pulsed divertor coils as a proof of concept
• A concept could be presented in August at ASIPP
An Experiment for EAST
• Energize coils in blue to yield flux expansion
• To prove the concept, use a set of coils with pulsed current just large enough to observe the expansion effect easily
An Experiment for EAST
• Energize coils in blue to expand the green flux at the divertor plate (in the circle)
Flux Expansion Versus Divertor Coil Current
I = 0 kAexpansion = 2.2
I = 40 kAexpansion = 4.3
I = 80 kAexpansion = 10.3
Helimak
Unique concept for a basic plasma experiment
Simple sheared cylindrical slab geometry
Device large compared with all scale lengths
Designed, engineered, and built by ASIPP
Operating successfully at Texas
Helimak
Dimensionless test of drift-wave turbulence
Simple, but physical geometry (curvature)
Open field lines, but long ( up to ~1 km)
Test of flow shear stabilization of turbulence
Dimensionless model of SOL
Helimak
Probe connections
Vacuum Vessel
Toroidal field coils
Vertical field coils
Microwave feed
Magnetron
Amplifiers and A/D
Helimak
Helimak
Helimak Dimensions and ParametersA Sheared Cylindrical Slab
<R> = 1.1 m ∆R = 1 mh = 2 mBT = 0.1 T Bv ≤ 0.01 TPulse ≤ 60 sPlasma source and heating: 6 kW ECH @ 2.45 GHzn ≤ 1011 cm-3 Te ~ 10 eVArgon, Heliumcs = 3 x 104 m/s (Argon) Vdrift = 100 m/s Vdiamagnetic = 103 m/sdrift-wave ~ 1 kHzConnection length: 10 m < L < 1000 m p (parallel loss) > 1 msProbe arrays in end plates provide vertical and full radial profilesIsolated end plates may apply radial electric fields: Vp ≤ ±100 Volts
Helimak
0.6 0.7 0.8 0.9 1 1.1 1.2 1.3 1.4 1.5 1.6
Bias plate
0.77
0.82
0.87
0.92
ECH resonance radius
R (m)
Density Profiles for various ECH Resonant Radii
Argon (shot# 402100062: 1 kW, 700 A, 15 ohms) U profile
-12
-7
-2
3
8
0 10 20 30 40 50 60 70 80 90
R - R inner [cm]
Te [eV], Vfl [V], n [10^16 m^-3] electron temperaturefloating potentialdensity
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Typical Density, Temperature, and Floating Potential Profiles
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0
0.5
1
0.6 0.8 1 1.2 1.4 1.6
Radial Profiles of Fluctuation Amplitude
∆n/n
R
(Various ECHResonant radii)
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0
20
40
60
80
100
120
0 2000 4000
Frequency Spectra
R=1.2Drift waves
in LFSgradient
R=1Coherent modeat density peak
(Hz)
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-5 -3 -1 1 3 5
Density PDF R=1.4 -- Low DensityLow median density with "blobs"
of high densityMaximum of density, coherent modeBimodal PDF typical of
harmonic oscillator
Helimak
0
1
2
3
0 1000 2000 3000 4000
Phase
(Hz)
VPH=400 m/s
kρs~0.5
=1.2R
( - )Vertical Propagation Drift wave
Helimak
Helimak
Major Points
The Helimak provides a good example of a turbulence bifurcation (shear stabilization)
The stabilization is caused by j (not E)
The transition is binary, not gradual -- no intermediate states as threshold approached from either direction
12341234BBhRiRoBRzφProbe
Helimak
Cross-section
Field lines terminate on isolated end plates
Biasing #2 plates with respect to others imposes radial electric field, current
Helimak
Response to Negative BiasProbe n(t) across radial profile
Bias Reduced ∆n Reduced ∆n; increased <n>
Helimak
Response to Positive BiasProbe n(t) across radial profile
Bias Reduced ∆nReduced ∆n; increased <n> Increased <n>
Helimak
Response to Negative BiasProbe n(t) across radial profile
Bias Reduced ∆nIncreased <n>Helium
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Time History of a Bifurcation
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Negative Bias Positive Bias
Isat(t)
BiasVoltageCurrent
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Profile Changes at Bifurcation
-50 V
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0
0.2
0.4
0.6
0.8
1
1.2
1.4
0.6 0.8 1 1.2 1.4 1.6R (m)
Profile of ∆n/n Reduction
Positive Bias
Negative Bias
Bias Plate(Various resonance radii)
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0 2000 4000 6000 8000
Γo = 1Γ- = 0.33
Γ+ = 0.53
( )Hz
Frequency-Resolved Particle Transport
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High Field Side
Low Field Side
Phase Velocity
Change with Bias
Larger changes for positive bias Equilibrium flow reversed by positive bias Negative bias adds to equilibrium flow
Helimak
Inferred Velocity Shear Same |∂Vz/∂z| for ± bias ~104 s-1
Equilibrium V from potential profile
∆V with bias from ∆Vphase of turbulence
Rn(r)E x B equilibrium∆V for + Bias∆V for - Bias01100 700 m/s1400 1200 m/s4000 m/s200 m/sVz(-)Vz(+)
Helimak
Velocity Shear vs.
Velocity shear ~104 s-1 comparable with shortest turbulence autocorrelation time
-0.2
0
0.2
0.4
0.6
0.8
1
0 0.0002 0.0004 0.0006 0.0008 0.001 0.0012 0.0014 0.0016
Autocorrelation
Low field side c = 0.14 ms
High field side c = 0.7 msDensity
max c = 0.4 ms
Helimak
Drive for Velocity Shear:E x B or j x B?
Plasma floating potentials and Er decrease at bifurcation,
despite large bias
Threshold voltages for positive and negative bias different
Threshold currents for positive and negative bias similar
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0
20
40
60
50 1000
5
10
15
Connection Length
Threshold Conditions -- Argon
-V
+V
-I
+I
No Transition
(V) (A)
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0
5
10
15
20
25
0.75 0.8 0.85 0.9 0.95 10
5
10
+V
-V
+I
-I
Threshold Conditions -- Helium
RECH
No Transition
(V)(A)
12341234Rzφ Flow of Bias Current , From plates j||jr across field drives sheared
vz flow
++------
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Biasing drives current from+ plates into plasma along field lines, across the field lines, and back out alongfield lines to the - plates.
For typical threshold currents,<jr> ~ 0.1 A/m2
j X B = dp/dt ~ p/p
p = mnVz
For p ~ 1 ms, Vzmax ~ 2 km/sShear, ∂vz/∂r ~ 104 s-1
Helimak
Drive for Velocity Shear:E x B or j x B?
Plasma floating potentials and Er decrease at bifurcation
Threshold voltages for positive and negative bias different
Threshold currents for positive and negative bias similar
Symmetric current flow essential to bifurcation; if one plate isolated to stop current flow, transition absent.
Observations favor j(Shear flow driven by radial shear in j x B)
Helimak
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Normal, Fast Bifurcation
Bias
Isat(t) at various radii
Jump between two steady states
Simultaneous at all radii
No hysteresis; bias directly controls instability
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Isat(t) at various radii
Bias
Slow Sweep Through Threshold Bias always near threshold
Jump between two steady states; sharp threshold, no graded transition
No hysteresis
Helimak
Conclusions
• The Helimak offers a simple, controlled model of shear-flow driven turbulence bifurcations – bifurcation without hysteresis through equilibrium profile
• The shear flows are driven by current ( jxB ) ⇒ momentum transport key
• The bifurcation is a step-function in shearin g rate – no intermediate regimes near threshold