Title: TF Coils
1(No Transcript)
2The FIRE Design effort has addressed all major
subsystems issues
- TF Coils Global Structure
- Central Solenoid Poloidal Field Coils
- Vacuum Vessel
- Plasma Facing Components
- Thermal Shield
- Ion Cyclotron Heating
- Fueling Pumping
- Tritium Systems
- Neutronics Shielding
- Activation, Decay Heat Radiation Exposure
- Remote Maintenance
- Magnet Power Systems
- Cryoplant
- Facilities Siting
- Safety
-Design goals have been met or exceeded for the
baseline. -Several options issues have been
identified. -Initial cost estimates have been
prepared. -Peer reviews have been done on
some major systems.
3FY01 Meetings and Milestones
item where date
FY01 Kick-off Meeting ANS, Park City Oct 18, 00
Design Point Subgroup PPPL Nov 29-30, 00
Cost Subgroup PPPL Dec 1, 00
Review of Physics Engineering Status NSO PAC, MIT Jan 17-18, 01
Project Peer Reviews
TF/PF/Structures PPPL June 5-7, 01
VV, PFCs, Fueling Pumping PPPL June 5-7, 01
Nuclear Effects and Activation By mail (phone TBD) June, 01
Facilities Siting By mail phone June, 01
Power Supplies TBD FY02
ICRF Systems TBD FY02
Remote Handling Tritium TBD FY02
Final FY01 Engineering Report ------ Sept, 01
4June 5-7, 01 Review Committee Membership
C. Bushnell, Chairman Independent
J. Irby MIT
S. Majumdar ANL
P. Mioduszewski ORNL
R. Parker MIT
A. Pizzuto ENEA, Frascati
F. Puhn GA
Note Committee review report to C. Baker is on
web.
5FIRE Wedged Baseline Operation Summaryc-June 5-7,
01
Configuration TF Coilsa Flat-top time, s CS Coils Max Temp, K PF Coils Max Temp, K
Baseline 10T 6.44 MA DT Power 200 MW 18.5 s with DT 26 s with DD 152 173
Higher B mode 12T, 7.7 MA DT Power 250 MW 12 s with DT 15 s with DD 161 183
TPX mode 4T 2 MA DD Power 5 MW 214 s 144 169
AT/BP mode 8T 5 MA DT Power 150 MW 31 s with DTb 46 s with DD TBD TBD
Note a) BeCu for TF coil inner leg OFHC for
balance of TF coils, CS and PF coils b)
AT mode pulse length with DT may be limited by VV
or PFC thermal limits c) meets or
exceeds engineering requirements
6Bucked and Wedged TF Coil Study
- An all OFHC, Bucked and Wedged, TF configuration
is an option - Max Field is lt12T to remain within the OFHC
copper allowable stress limit - Longer pulses are possible at a given field level
- Lower power requirements may increase number of
possible sites - TF material processing costs will be reduced
- RD for a BeCu to OFHC joint in TF plates will
not be required - TF fabrication assembly will be more complex to
assure proper bucking wedging
7POWER REQUIREMENTS FOR FIRE, June 5-7, 01
BeCu TF Inner Legs
All Cu TF Coils
Field Flat-top 10T 20s 10T 20s 12T 12s 12T 12s 10T 31s 10T 31s 12T 23s 12T 23s
Peak Power (MW) Peak Energy (GJ) Peak Power (MW) Peak Energy (GJ) Peak Power (MW) Peak Energy (GJ) Peak Power (MW) Peak Energy (GJ)
TF 490 11.5 815 11.5 267 12.6 345 13.2
PF 250 2.2 360 3.7 250 5 360 4.6
RF 60 1 60 0.6 60 2.3 60 1.3
Sum 800 14.7 1235 15.8 577 19.9 765 19.1
Grid 550 12.5 600 10.9 577 19.9 404 14.5
MG 250 2.2 635 4.9 0 0 360 4.6
Significantly lower power for all Cu TF coils
reduces capital operating costs and expands the
list of candidate sites.
8FIRE Design Review Variations-June 5-7, 01
FIRE baseline FIRE FIRE FIRE
Wedged B W Wedged B W
Inner Leg Matl BeCu OFHC BeCu OFHC
Radii R(m), a(m) 2.0, 0.525 2.0, 0.525 2.14, 0.595 2.14, 0.595
Field Bt at R, (T) 10 (12) 10 (12) 10 (12) 10 (12)
Plasma Current Ip, (MPa) 6.44 (7.7) 6.44 (7.7) 7.7 (8.25) 7.7 (8.25)
Flat-top time, (sec) 20 (12) 31 (23) 20 (12) 31 (23)
TF Allowable Stress, MPa 700 300 700 300
TF VM Stress, MPa 466 (666) 230 (326) 529 (762) 230 (326)
Allowable/Actual Stress 1.5 (1.05) 1.3 (0.92) 1.3 (0.92) 1.3 (0.92)
Questions
- What is a suitable margin for Pre-conceptual
design? - What can the machines do at comparable stress
margins?
9External Review of FIRE Design Point--
Conclusion Summary for Magnet Systems
- Critical Design Issues
- Focus on 2 designs near Q10 that have, at the
Pre-conceptual Design level, an Engineering
Margin of 1.2-1.3 - Then focus on 1 device, either wedged or bucked
and wedged (to be selected by the design team) - Incorporate design attention to the details of
leads, both TF and CS, associated cooling systems
design of all other critical systems that are
lacking detail at the Pre-conceptual level - Critical RD Issues
- Qualification of the properties of BeCu for the
wedged design and OFHC copper for the bucked and
wedged design in sizes and thicknesses needed for
fabrication - Qualification of materials for the insulation
systems
10Estimated Machine Variations at Margins of 1.0-1.3
Wedged B W Wedged B W B W
Inner Leg Matl BeCu OFHC BeCu OFHC OFHC
Major Radius, R, m 2.0 2.0 2.14 2.14 1.86
Minor radius, m 0.525 0.525 0.595 0.595 0.488
allowable stress Max TF stress 1.0 1.3 1.5 1.0 1.2 1.3 1.0 1.2 1.3 1.0 1.2 1.3 1.0 1.2 1.3
Plasma, Current, MA 7.89 6.93 6.44 7.34 6.70 6.44 8.78 8.01 7.70 8.78 8.01 7.70 6.82 6.23 5.99
Field at R, Tesla 12.3 10.8 10.0 11.4 10.4 10.0 11.4 10.4 10.0 11.4 10.4 10.0 11.4 10.4 10.0
Flat-top, s 11.7 14.8 18.5 23.9 28.7 31.0 15.4 18.5 20.0 23.9 28.7 31.0 20.7 24.8 26.8
Question What is an appropriate margin at this
stage? June Review recommends 1.2 to
1.3
11Preliminary B W Risk Assessment
- Can a BW machine be assembled?..yes
- Is it robust wrt assembly tolerances?yes
- Issues to be resolved
- Need for a bucking cylinder
- Cooling of the Central Solenoid
- Material properties for TF conductor
12Two B W Assembly Options That Work
- High Tolerance Machining
- Machine wedge faces and nose of TF coils
- Machine the CS to a known OD
- Assemble TF array apply ring preload
- Machine TF bore
- Back-off TF coils insert CS reset TF coils
- Epoxy filled bladders and shims
- Assemble TF coils and CS with radial gap
- Use machined wedge faces or epoxy filled bladders
at TF wedge faces - Use epoxy filled bladders in radial gap
- (as in ITER CS Model Coil)
- Remove a shim if a gap is desired
13BW Assembly is Robust wrt Tolerances
- Elastic/Plastic Analysis Summary for 11.5 T
- Fractional mm fit-up tolerances are OK
- Off-normal fit, up to 2.5 mm, produces small
plastic strains within the capacity of the
conductor and insulation materials -
14Wedged vs Bucked and Wedged
issue Wedged Bucked Wedged
TF/CS interaction uncoupled operation, but no mutual support has coupled operation with mutual support
Material processing costs BeCu is more expensive than OFHC
Conductor mechanical properties Require validation for thick plates Require validation for thick plates
Conductor joints Require more development Require development
TF/CS Assembly Assembly is more difficult
Power required Substantially more
15External Review of FIRE Design Point--
Conclusion Summary for VV, PFCs, Fueling
Pumping
- Critical Design Issues
- The design divertor heat load of 25 MW/m2 for the
outer divertor is at the limit of engineering
feasibility - Develop a complete description of
disruption/loads/stresses - Consider active cooling for the inner divertor
- Determine diagnostic design RD required
- Critical RD Issues
- Determine behavior of W rods in divertor plates
under disruption conditions (loss of melt layer,
effects on neighboring rods, etc.) - Optimization Issues
- Adopt the ITER Design Criteria expand as needed
- Require 104 l/s pumping speed
- Determine Cu-ss bonding method for in vessel use
16FIRE Engineering RD
- State-of-the-art materials and manufacturing
processes will allow the highest performance to
be achieved cost effectively. - Several RD areas have been identified to
- -complete the material property data base to
assure consistency with design criteria for
materials procured in the size required for the
device, - -test design concepts for component manufacture
or assembly to assure processes are sufficiently
developed and specified, or - -validate the design of prototype components
through fabrication and test to assure that
performance, cost or remote handling features
have been adequately considered.
17Engineering RD Lists Initial Cost Estimates
- TF Conductor and Design Criteria
- TF Conductor Joints
- Radiation Resistant Electrical Insulation
- High and Low Friction Materials
- High Force, High Reliability Jacking System for
TF coils - First Wall and Divertor Components
- Vacuum Vessel
- Remote Handling
- Fueling and Pumping
- ICRH Antenna
- Power Supply System-tbd
Note red specifically mentioned in June
reviewers report
181. Copper Conductor and Design Criteria
- Background
- The data base requires assessment and extension
for plates of the size to be procured for the
full scale TF and CS conductor. The properties
assumed require validation for both designs. - Inner Leg of the Wedged TF baseline design-
- C17510 BeCu (68 IACS) in thick plate (36mm) form
is used in the inner leg. The principal stresses
are primarily axial tension and azimuthal
compression. Required UTS 800 MPa min. yield
724 MPa. - Bucked and Wedged TF alternate design-
- Design uses OFHC copper in thick plate form.
Required 60 cold work for 300 MPa - Central Solenoid Coil Both Wedged and Bucked and
Wedged Alternate Design - Both concepts use C10200 copper in thick plate
(38mm) form. Rolled or forged copper discs are
required to meet strength requirements. (350 MPa
UTS 300 MPa min. yield) - RD Task
- Obtain samples from full size plate stock and
carry out a mechanical testing program to assure
that static and crack growth properties at room
and LN2 temperatures are adequate.
192. Conductor Joint Development
- Background Both the baseline and alternate TF
coil designs require a high strength joining
process which does not result in an annealed
zone. - Baseline wedged design
- The baseline design uses C17510 BeCu for the
inboard leg of the TF coils and C10200 copper for
the balance of the coils. A cost effective,
reliable high strength joining method for the
material transition is essential. - Bucked and wedged alternate design
- The bucked and wedged alternate TF design uses
OFHC copper throughout the TF coil. In principal
the turns for the latter could be cut from large
thick plates, from which, the centers would be
scrap. A cost effective joining method for
joining plate segments would allow the TF legs
to be fabricated from readily available plate
sizes and eliminate the need to procure
specially sized plates. - RD Task
- Develop manufacturing processes and carry out a
mechanical testing program to assure adequate
mechanical properties and to validate design
criteria for the joints. Potential candidate
processes include friction stir welding and
e-beam welding.
203. Radiation Resistant Insulating Materials
- Background
- Data from the BPX insulation test program
indicates that there are several glass/epoxy
formulations (CTD-101 Shikazima) which can meet
FIREs requirement for radiation exposure
capability of 1.5 x 1010 rads. - This is a high leverage RD item, since it has
the potential to permit more full power D-T shots
and may permit the experimental program to be
expanded with possibly only a minor impact on
costs. - RD Task
- Develop high radiation resistant insulating
materials with good processing characteristics
for coil fabrication. (note several SBIRs are
underway in this area)
21RD List for PFCs
22Conclusions
- A FIRE Wedged baseline is a reasonable choice
- A FIRE Bucked Wedged machine is a suitable
back-up - It can be assembled with adequate tolerances
- It is robust wrt assembly tolerances
- BW Design Issues to be resolved
- Need for a bucking cylinder
- Cooling for the CS
- RD items have been identified
- Critical Items as per review
- Material properties for conductor and insulation
- Behavior of W rods in divertor
- RD tasks require a budget and time frame!
23Back-up viewgraphsOther Engineering RD Needs
244a. Low Friction Insulation Characterization
- Background The design of the TF and CS coil
systems require that selected interface areas
retain a desired level of either low or high
friction during operation. - Segmented Central Solenoid in both Wedged and
Bucked Wedged Designs- - FIRE employs a segmented CS with a variation of
currents among the 5 coils in the stack during a
pulse. - Adjacent coils in the CS operate with different
temperature and electromagnetic load profiles
during a pulse. - Adjacent coils will strain differently and
relative radial motion between coils in the CS
will occur. - Interface must lock the coils azimuthally,
maintain the coils co-axial, and allow relative
radial motion with low friction. - RD Tasks
- Prototypes of the interface areas will be
fabricated and tested under simulated operating
conditions to verify operation and adequate life.
- .
254b. Low Friction Insulating Material for the
TF/CS Interface in Bucked Designs
- Background The CS tends to expand radially and
compress axially during operation. The inboard
legs of the TF coils tend to stretch vertically
due to their in-plane loads and shift azimuthally
due to their out-of-plane loads. In a bucked
design a low friction interface between the TF
and CS is desirable to limit - the CS vertical tension imposed by the TF,
- transmission of torsional shear into the CS, and
- radial-vertical traction shear imposed on the CS
by the TF. - RD Task
- Select candidate materials and processes for
application to the identified interfaces in the
FIRE design. - Apply low friction materials to substrates on a
scale consistent with fabrication methods for
FIRE. - Perform mechanical tests to assure that expected
surface friction performance is consistent with
design criteria and reliable for the lifetime of
the machine.
264c. High Friction Insulation Characterization
- Background
- TF Coils in both Wedged and Bucked Wedged
Designs- - Overturning moments on the TF coils are reacted
by wedging action at the inboard legs and by
shear between interfaces of the outer intercoil
structures on the TF cases. - A friction coefficient of 0.3 is needed
between TF inboard legs to limit torsional
motions and between cases on the outboard side to
reduce shear pin and bolting requirements - RD Task
- Testing is required to verify friction
coefficients and adequate life.
275. Ring Preload Jacking System
- Background Both the Wedged and the Bucked and
Wedged TF coil designs use large steel rings
outboard of the TF coils. The rings are
pre-loaded at assembly using radial jacks to
augment the wedge compression at the inboard
faces of the TF coils and provide compression
between the faces of the outboard intercoil
structures during operation. The space available
is very limited. Three jack concepts have been
identified - A mechanical system (proposed for IGNITOR)
consisting of opposing wedges - Stainless steel bladders with hydraulic fluid
- Commercial Enerpac jacks
- RD Task Select one primary concept plus one
back-up. Mock-up and test under expected
operating conditions simulating assembly,
cooldown, operational pressures, and temperatures.
28Vacuum Vessel
299.Remote Handling RD Background Remote
handling of components is a key issue because of
activation. Verification of designs and component
maintenance tasks should be completed prior to
final design completion, or at least prior to
fabrication of components. The goal is to reduce
cost and times for replacement, repair and
maintenance tasks. RD tasks 1. In-vessel
transporter (articulated boom) component
handling end effectors 2. In-vessel inspection
systems (laser metrology and video systems and
deployment mechanisms) 3. Midplane and
auxiliary port handling vehicles and dexterous
manipulator 4. YAG laser based divertor pipe
port lip seal cutting, welding, and inspection
tools, and power fastener wrench 5. Midplane
port cask and air cushion transport vehicle 6.
Hot cell remote repair stations fixtures for
midplane port assembly, divertor modules, and
cryopump
30Vacuum Vessel Remote Handling RD
31Vacuum Vessel Remote Maintenance RD
329.Fueling and Pumping Background A new, twin
screw, extruder concept has the potential to run
steady state with reduced hydrogen ice
inventories compared to existing linear piston
extruders. In parallel, a cooling concept based
on a Gifford-McMahon cryocooler could be
developed to simplify operation of the pellet
injector by removing the need for liquid helium.
The design of cryopumps for the divertor
relies on helium compression in the pump entrance
region to allow a compact, in-vessel
system. RD Tasks Design, build and test a
prototype twin screw extruder with the goal of
minimizing tritium inventory for safety and
siting flexibility. Demonstrate extruder cooling
without LHe by using a G-M cryocooler. Design,
build and test a single cryopump module to
validate the expected inlet He compression which
permits a compact in-vessel pumping system.
33ICRH Antenna Mockup RD Background
Calculations for the two current strap antenna
show good performance, but the model requires
validation with an electrical mock-up of the
antenna. RD Task Build and test a mock-up
that uses a sheet metal antenna cavity current
straps, an uncooled Faraday shield, and is not
vacuum compatible. Measure electrical
characteristics at operating frequencies, refine
electrical models, and modify the design as
results indicate to improve performance.