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ASIPP
Concept Design of VV of CFETR
Presented by Yuntao,SONG
Vacuum Vessel Design Team
31st May 2012, USTC·Hefei
ASIPPOutline
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Introduction
Concept Design of VV
Thermal requirement
Ongoing design plans
Material for VV
Next-step plan and Optimization
Summary
ASIPP
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Main Parameters for the CFETR VV Design
Main parameters for Tokamak machine
Major radius R 5.5m
Minor radius a 1.6m
Toroidal field Bt 4.5/[email protected]
Elongation 1.8
Triangularity 0.4
Thickness of blanket 0.8-1.0m
VV design parameters
Torus outer radius 8.6m
Torus inner radius 2.6m
Torus height 9.7m
Shell thickness 50mm
D shape (vertical direction) Symmetry
Ports (average in one sector) 3
Introduction
ASIPP
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Basic Functions
Provide the first confinement barrier for radioactive materials.
Remove decay heat of all in-vessel components, even in conditions when the other
cooling systems are not functioning.
Provide a boundary consistent with the generation and maintenance of a high quality
vacuum.
Mount in-vessel components and support electromagnetic loads during plasma
disruptions and vertical displacement events.
Together with the first wall and blanket, maintain a specified toroidal electrical
resistance and contribute to plasma stability.
Together with the first wall, blanket, divertor, and ancillary equipment in ports,
provide adequate radiation shielding for the superconducting coils.
Provide access ports for in-vessel components maintenance equipment, diagnostics
and plasma heating methods, and blanket test modules.
……
Introduction
ASIPP
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Introduction
Basic Layout
ASIPP
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Concept Design
The design core of VV:
Inner shell ~ 500℃
Outer shell ~ 100℃
VV D-shape(Inner shell) configuration
The basic D-shape
5 arcs and 1 straight line
Max size (Horizontal direction) ~5205mm
Max size (Vertical direction) ~8880mm
ITER VV D-shape : 7 arcs and 3 lines for Inner shell; 6 arcs and 2
lines for out shell; The D-shape is not symmetrical in vertical
direction. CFETR VV D-shape is symmetrical in vertical direction for
all shells.
CFETR VV is easier to design, manufacture and maintenance
ASIPP
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Concept Design
Ports Description
The quantity of upper and lower ports
are both 12.
The equatorial ports include two kinds:
Normal (10) and Full-scale port (2).
Port Type Quantity Function
Upper 12 Diagnostics (5) , Divertors(5), VV/Blanket piping(2)
Equatorial
8 LHCD(1), ECRH(1), Diagnostics(3-4), VV/Blanket piping(2)
2 Neutral Beam Injection
2 full-scale port Sector assembly and maintainance
Lower 12 Diagnostics (5) , Divertors(5), VV/Blanket piping(2)
ASIPP
The basic structure for CFETR VV
Concept Design
ASIPP
The basic structure for removable VV sector
The VV has double-shell structure to increase bending resistance and provide
active cooling channel, meanwhile the neutron shielding blocks are placed in
this channel; for different VV design strategy, the double-shell configuration
could have modifications.
Concept Design
ASIPP
The basic structure for Two full-sector ports
Two full-scale ports are designed to ease the assembly modularization of the inner
components. The inner components are inserted into this port and rotated to the correct
location.
Concept Design
ASIPP
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General sector structure
• The symmetrical in vertical direction for the D-shape
• Supporting rib without housing
• Simplify the triangular support to supporting keys
• Coolant channel inside the double-shell
VV supporting rib New VV blanket support
Concept Design
ASIPPThermal requirement
A obvious character of the CFETR VV is its designed for hot wall
operation, 3 candidate designs are proposed, they can be classified into
two types:
Water-cooled VV: works at 100℃.
Gas-cooled VV: works at 500℃.
Critical thermal environment includes the nuclear heat on the VV, the
coolant effect and the radiation to the VVTS.
Boundary conditions
Typical temperature
distribution
ASIPP
Gas-cooled
double-shell
Water-cooled
double-shell
Water-cooled double-shell
Inner insulation
Gas-cooled double-
shell
Outer insulation
Inner thermal
resistance design(20mm insulation layer)
Double cooling system design
Outer thermal
resistance design(20mm insulation layer)
Ongoing design plans
ASIPPOngoing design plans
Design type Temperature contour Advantage Disadvantage
Inner thermal
resistance
1. Existing experience
on water-cooled VV,
2. No need of high
temperature
structural material,
3. Compact.
1. Insulation material
needs R&D under
neutron radiation,
2. Difficult to control
inner wall temperature.
Outer thermal
resistance
1. Lower radiation
resistance
requirement to
insulation material,
2. Easy to control inner
wall temperature.
1. Structural material has
to have good
performance at high
temperature,
2. Insulation material has
to have very low
conductivity .
Double cooling
system
1. Easy to control both
inner and outer
surface temperature,
2. Insulation material
need not, only
between the two
double-shells.
1. High space
requirement,
2. Difficult to
manufacture,
3. High temperature
structural material
required.
4. Complicated cooling
system
VVTS (80K)
Water-cooled double-shell(100C)
Insulation(500C)
Blanket(600C+)
VVTS(80K)
Insulation (100C)
Gas-cooled double-shell(500C)
Blanket(600C+)
VVTS(80K)
Water-cooled double-shell(100C)
Gas-cooled double-shell(500C)
Blanket (600C+)
ASIPPMaterial
For the water-cooled designs, the structural material could be stainless steel like
SS316L.
For the gas-cooled designs, the insulation material is inorganic material which could
survive at high temperature, the coolant gas could be N2 or He.
The mechanical material should be a high temperature metal, has good creep strength
and erosion resistance. Candidate types are listed:
Stainless steel, like SS310S and SS30815.
Nicket alloy, like Inconel 718 and x-750.
Titanium alloy, like Ti-6Al-4V
. . . . .
At present SS is preferred to make a balance at performance, manufacture
convenience and cost.
ASIPPNext step plan
Design: optimize the port and space use, make corresponding arrangement for
blanket, divertor, heating, cooling, power supply, diagnostic and other systems.
Material related R&D:
Neutron radiation test for structural and insulation materials.
High performance thermal insulation material development.
Gas cooling system development.
Analysis plays an important role in the next step work, the list of main
analyses concludes:
EM analysis;
Thermal analysis;
Mechanical analysis (including static, seismic and buckling analysis…)
ASIPP
真空室分析
Electromagnetic analysis
MD (Major Disruption)
VDE (Vertical Displacement Event)
TFCFD (TF Coil Fast Discharge)
The EM scenarios cause huge eddy current and
strong Lorentz force. Plasma current during MD 36ms linear decay and Eddy current on the VV
Seismic analysis
The VV response under seismic loads needs to
be checked, which will also have impact to the
components attached to it. X and Y directions
Reference spectrum for seismic analysis and acceleration result
Analysis Plan
ASIPP
Structural analysisTo evaluate the strength of the conceptual design of VV,
structure analysis will follow the process below:
Single load (like gravity)
Combined loads (EM loads, thermal loads, SL)
Critical combined loads (Normal/Off-normal)
This load consideration covers all possible and unlikely cases,
to find out the most important load issue and the limit of the
structure design.
Thermal analysisThe aim of thermal analysis is to calculate the thermal stress
caused by temperature difference under the combined load
conditions of nuclear heating and water cooling. The heat
load of the neutron deposition and the radiation from the VV
to the VVTS are concerned, too.
Inner shell
Outer shell
Temperature distribution of two shells of VV
Stress distribution of two shells of VV
Model of structure analysis Stress distribution of 40deg of VV
Analysis Plan
ASIPPSummary
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1. Function and requirement of the VV is proposed.
2. Basic outline of the VV is generated, as well as the space holders.
3. 3 kinds of Thermal designs are proposed and compared .
4. Material candidates are proposed.
5. The design, R&D and analysis work in the next-step are proposed.
ASIPP
Thanks for your attention!
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