Download presentation
Presentation is loading. Please wait.
Published byRudolf Burke Modified over 9 years ago
1
ASIPP Development of a new liquid lithium limiter with a re-filling system in HT-7 G. Z. Zuo, J. S. Hu, Z.S, J. G. Li,HT-7 team July 19-20, 2011 Institute of Plasma Physics, Chinese Academy of Sciences, China 1 HT-7 Data Meeting and Workshop. Hefei, China July 19-20, 2011
2
ASIPP Outline Introduction Design of the new lithium limiter Main results Test of re-filling system Influence on plasma performance Discussion: Discussion: Li emission and plasma disruption Li erosion and deposition Summary 2
3
ASIPP Introduction Li is Li is developed as an potential alternative PFM for future fusion devices Liquid lithium is a self-recovery and renewable PFC material if surface damages due to erosions Best way to control recycling and H content, also suppress impurities; Enhance plasma performance. Main motivation of liquid lithium limiter ( LLL) experiment in HT-7 is to provide technical support and data accumulation for future design: Flowing LLL for HT-7 Flowing liquid lithium divertor (LLD ) after 2014 for EAST Accumulate data for its application in future fusion reactor. 3
4
ASIPP Graphite PFCs: Serious H retention and recycling. Serious erosion and co-deposition with T in future devices. Reaction between Li and C, reduce H, D trapping. Li surface should be confined by CPS to avoid splashing due to MHD. Heater should be reliable. It required a re-filling system for lithium: If lithium plates installed before experiment, it would possible lead to contamination. No available again, once lithium was used up. 4 Lessons from previous Li experiments
5
ASIPP Design of the new lithium limiter Full metal walls: Change all C tiles to Mo Using new type SS mesh Upgrade heater strips with armored structure. Design a re-filling system outside of HT-7. Same position, similar area (~400cm 2 ) and same movable system as previous experiment. 5 Re-filling system Sketch of the new designed LLL system with Re-filling system Mo limiters
6
ASIPP Structure of LLL 6 New SS mesh With 285*145*2.5 (mm) and pore radius~100 μm SS tray with channels for Li reservoir(50cm 3 ) Pipe and heater SS mesh and SS tray
7
ASIPP Outline Introduction Design of the new lithium limiter Main results Test of re-filling system Influence on plasma performance Li emission and plasma disruption Li erosion and deposition Summary 7
8
ASIPP Liquid Li flow could be driven: In a pipe with 10mm inner diameter At a low temperature ~250 ℃ Only by gravity force without pushing by a planed high pressure Ar. Main problems Hard to control flow velocity and the amount of injected Li. Hard to control position of lithium injection So many lithium flow onto the top of SS mesh Successfully test re-filling system 8 After 1 st Exp., a lot of liquid lithium was still remained on the top of SS mesh.
9
ASIPP Influence on plasma performance With LLL, High retention (with the same Ne, required more gas puffing). Reduce recycling. Reduce total impurities radiations. 9 ICRF OH
10
ASIPP Influence on plasma performance Compare some parameters of plasmas before and after using LLL ( r=27cm ) 10 After 17 th lithium coating, total using ~173g lithium
11
ASIPP Li emission and plasma disruption Plasma performance related with LLL position( Mo limiters at r=0.27m). While LLL at r=0.26m, with the same fueling, low density and V loop than it at r=0.275m. However, lots of disruptions if LLL at r=27cm and 26cm. –at r=27.5cm, Normal plasmas; –at r=27cm, ~ 2/3 plasmas disrupted ; –at r=26cm, ~9/10 plasmas disrupted. 11
12
ASIPP Li emission and plasma disruption Possibly due to strong Li emission intensity, there are lots of disruptive plasmas if LLL as main limiter at r=27cm and 26cm. 12 Increased lithium emission intensity Disruption Stronger Lithium Ejection
13
ASIPP Possible reasons for Li emission Sputtering (sputtering yield 0.5-1) Evaporation ~10 17 s -1 (r=260cm,t~0.8s, OH plasma, calculated Max Temp. of LLL surface in creased to ~360 ºC ) Splashing J×B force (Induced J by plasma, TEMHD, TCMHD, Other MHD instability.) Possible LLL vibrations during plasma discharge (Lots of Li on top of mesh). 13 Large-scale Droplets Before disruption, Li emission intensity increased and plasma and LLL interaction became strong, then plasma disrupted.
14
ASIPP Initial Temp. 220ºC(#112357). P OH ~200kW, t~1s; If half power loads on LLL, Q 0 ~6.7MW/m2. Plasma disruption analysis —Heat flux analysis 14 Li SS mesh T1 J 1TE T2 J 2TE V B R Force (J 2TE ×B)along radial direction. Force (J 1TE ×B)was possible to splash lithium. SS tray
15
ASIPP Lithium radial flow observed by fast CCD Observed by fast CCD, Liquid lithium flew along radial direction seemed corresponding to the direction of force (J 2TE xB). The estimated velocity along radial direction ~0.5m/s 0.27s 0.29s0.32s High temp. B 15
16
ASIPP
17
ASIPP
18
ASIPP
19
ASIPP
20
ASIPP
21
ASIPP
22
ASIPP
23
ASIPP
24
ASIPP
25
ASIPP
26
ASIPP
27
ASIPP
28
ASIPP
29
ASIPP
30
ASIPP
31
ASIPP
32
ASIPP
33
ASIPP
34
ASIPP
35
ASIPP
36
ASIPP
37
ASIPP
38
ASIPP
39
ASIPP
40
ASIPP
41
ASIPP
42
ASIPP
43
ASIPP
44
ASIPP
45
ASIPP
46
ASIPP
47
ASIPP
48
ASIPP
49
ASIPP
50
ASIPP
51
ASIPP
52
ASIPP
53
ASIPP
54
ASIPP
55
ASIPP
56
ASIPP
57
ASIPP
58
ASIPP
59
ASIPP
60
ASIPP
61
ASIPP
62
ASIPP
63
ASIPP
64
ASIPP
65
ASIPP
66
ASIPP
67
ASIPP
68
ASIPP
69
ASIPP
70
ASIPP
71
ASIPP
72
ASIPP
73
ASIPP
74
ASIPP
75
ASIPP
76
ASIPP
77
ASIPP
78
ASIPP
79
ASIPP
80
ASIPP
81
ASIPP
82
ASIPP
83
ASIPP
84
ASIPP
85
ASIPP
86
ASIPP
87
ASIPP
88
ASIPP
89
ASIPP
90
ASIPP
91
ASIPP
92
ASIPP
93
ASIPP
94
ASIPP
95
ASIPP
96
ASIPP
97
ASIPP
98
ASIPP
99
ASIPP
100
ASIPP
101
ASIPP
102
ASIPP
103
ASIPP
104
ASIPP
105
ASIPP
106
ASIPP
107
ASIPP
108
ASIPP
109
ASIPP
110
ASIPP
111
ASIPP
112
ASIPP
113
ASIPP
114
ASIPP
115
ASIPP
116
ASIPP
117
ASIPP
118
ASIPP
119
ASIPP
120
ASIPP
121
ASIPP
122
ASIPP
123
ASIPP
124
ASIPP
125
ASIPP
126
ASIPP
127
ASIPP
128
ASIPP
129
ASIPP
130
ASIPP
131
ASIPP
132
ASIPP
133
ASIPP
134
ASIPP
135
ASIPP
136
ASIPP
137
ASIPP
138
ASIPP
139
ASIPP
140
ASIPP
141
ASIPP
142
ASIPP
143
ASIPP
144
ASIPP
145
ASIPP
146
ASIPP
147
ASIPP
148
ASIPP
149
ASIPP
150
ASIPP
151
ASIPP
152
ASIPP
153
ASIPP
154
ASIPP
155
ASIPP
156
ASIPP
157
ASIPP
158
ASIPP
159
ASIPP
160
ASIPP
161
ASIPP
162
ASIPP
163
ASIPP
164
ASIPP
165
ASIPP
166
ASIPP
167
ASIPP
168
ASIPP
169
ASIPP
170
ASIPP
171
ASIPP
172
ASIPP
173
ASIPP
174
ASIPP
175
ASIPP
176
ASIPP After vent, we have found 1, lots of Li was floated out directly from LLL, possibly due to too much Li filling. 2, Lots of Li droplets around LLL, possibly strong JXB force. 3, SS mesh had no any damage and full of Li, indicating new SS mesh is good for CPS system. Li erosion and deposition 176 After 3rd Exp., thin Li film on mesh, and Li was effectively confined by the CPS.
177
ASIPP Outline Introduction Design of the new lithium limiter Main results Test of re-filling system Influence on plasma performance Li emission and plasma disruption Li erosion and deposition Summary 177
178
ASIPP Liquid lithium was successfully and easily injected into LLL from outside of HT- 7 by re-filling system. Ø10mm pipe, low Temp.~250 C, driven only by gravity. Plasma with a lower recycling and a lower radiation was obtained by using LLL. The new SS mesh was good for CPS system. SS mesh kept no any damage in spite of some disruption shots during LLL Exp. Due to Li emission intensity increase by various reasons, many plasmas was disrupted while as LLL served as main limiter. In alternative, disruption enhanced Li erosion, specially Li ejection directly from LLL. To control Li injection speed and Li splashing during plasma discharge should be considered. Summary and Discussion 178
179
ASIPP Thanks for your attention! 179 Acknowledgement This research is funded by National Magnetic confinement Fusion Science Program under contract 2010GB104002 and the National Nature Science Foundation of China under contract 11075185.
Similar presentations
© 2024 SlidePlayer.com. Inc.
All rights reserved.