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EU DEMO Conceptual Design Work Status
Gianfranco Federici
Power Plant Physics and Technology
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 2
Outline
• Background
• Organisation of design and R&D activities
• Definition of plant requirements
Lesson learned from GEN-IV
DEMO Stakeholder meetings
• Concept design approach
Physics basis and design drivers
Preliminary design choices under evaluation
• DEMO Design and physics integration challenges
Key interdependencies and trade-off studies
Results of selected studies no results of R&D reported in this talk
• Conclusions
See talk M. Shannon given by C. Waldon
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 3
Background
Outstanding Technical Challenges with Gaps beyond ITER
Tritium breeding blanket Exhaust
Remote Maintenance
Structural and HHF Materials
• For any further fusion step, safety, breeding, power exhaust, RH, component lifetime
and plant availability, are important design driver and CANNOT be compromised
- most important/novel parts of
DEMO
-
TBR >1 marginally achievable
but with thin PFCs/few
penetrations
- Feasibility concerns/
performance uncertainties with
all concepts
- Selection now is premature
- Peak heat fluxes near
technological limits (5-10 MW/m2)
- ITER solution may be marginal for
DEMO
-
Advanced divertor solutions may
be needed but integration is very
challenging
- Also exploring DN as a serious
option
- Strong impact on IVC design
-
Significant differences with ITER
RM approach for blanket
- RH schemes affects plant design
and layout
- Large size Hot Cell required
-
Service Joining Technology R&D is
needed.
- Embrittlement of EUROFER and Cu-alloys at low temp.
and loss of mechanical strength at ~ high temp. are
important design issues.
- Development needs of design rules for structural
materials
- Progressive blanket operation strategy (1st blanket 20
dpa; 2nd blanket 50 dpa).
- Technical down selection of options for DT n-sources
has been made in Europe M. Mittwollen (KIT)
L. Boccaccini (KIT)/ Y. Poitevin (F4E) R. Albanese (CREATE), H. Reimerdes (CRPP),
C. Linsmeier (FZJ), I. Mazul (Efremov)
J. Aktaa (KIT)
H. Tanigawa (JAEA)
S. O’hira (JAEA)
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 4
Emphasis on: Central role of ITER
assu ptio i ‘oad ap ITE‘ co es i operatio i early 2020 s
DEMO as a single step to commercial fusion power plants
DEMO construction starting early in the 2030s
• An ambitious roadmap implemented by a Consortium of Fusion Labs (EUROfusion)
• Distribution of resources based on priorities and on the quality of deliverables.
• Support to facilities based on the joint exploitation.
• Focus around 8 Missions
DEMO
IPH
IPH
1. Plasma Operation
2. Heat Exhaust
3. Neutron resistant Materials
4. Tritium-self sufficiency
5. Safety
6. Integrated DEMO Design
7. Competitive Cost of Electricity
8. Stellarator
Background
EU Fusion Roadmap to Fusion Electricity
See talk M. Gasparotto
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 5
Organisation of Design and R&D Activities
Each WP has a Project Board
Safety PMU & PMI
Activities
Materials
Remote
Maintenance
Diagnostics and
Control
Breeding
Blanket Magnets Divertor
H & CD
Systems
Tritium
Fuelling &
Vacuum
PHTS &
BoP
Contain
Structures
• A project-oriented
structure set-up
• Distributed Project
Teams aiming at the
design and R&D of
components
• Project Control and
Design Integration Unit
• Project coord. and
control
• Physics & Design
Integration
General Assembly ( GA )
Programme Management Unit
PPPT
Programme Manager
IPH / JET Admin Communications
PPPT Expert
Group
DEMO
Stakeholder
Group
STAC
Bureau
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 6
Organisation of Design and R&D Activities
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 7
Concept Design Approach
Time Plan and Scope
new
• EU Roadmap to fusion electricity
• Work-Plan 2014-18, AWPs
• List of Grant deliverables
• Scope, Schedule and Resource-
loaded Projects
• Project Management Plans
EFDA PPPT
2011-2013
EUROFusion
PPPT
2014-2017
EUROFusion
PPPT
2018-2022
• Identify DEMO pre-requisites
• Identify main design and technical challenges
(physics/ technology)
• Preliminary assessment technical solutions
• Prioritization of R&D to be included in the
Roadmap
new
• PRDs, SRDs, OCD, PBS,
Interface Process
• Trade-Off studies
• States & Modes Diagrams
• Functional Flow Block
Diagrams (FFBD)
• Design Description Docs
• 3D CAD model of Plant
• Cost Analysis
• Preliminary Safety Analysis
Report
• Plant RAMI Report
• Prel. Manufacturing Plans
• Preliminary Assembly &
Maintenance Plan
• Programme Management
Plan (for EDA phase)
• Select design options from leading technologies
• Select coolants
• Select divertor layout concept
• Finalise Plant System Architecture / down-select
variants in: BoP, BB, H&CD e.t.c.
• Safety Analysis report
• Engage DEMO Stakeholders and define DEMO HLRs
• Study machine configurations and key parameters.
• Optimisation / trade-off studies
• SE approach to solve design integration issues
• Resolve Plant System Architecture with variants
• Address key technology R&D needs (mainly PoP,
fabrication feasibility, performance tests)
• Develop and qualify materials and fill database gaps
Pre
pa
rato
ry P
ha
se
Pre
-Co
nce
ptu
al D
esi
gn
Ph
ase
C
on
cep
tua
l De
sig
n
Documents Scope
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 8
• In 2014 a traceable design process with SE approach was started to explore available
design/ operation space for DEMO to understand implications on technology requirements
Main challenges
• Integration of
design drivers
across different
projects.
Concept Design Approach
Basic Process Flow for Conceptual Design Work
Typical example is the selection of coolants. Technical issues include:
thermal power conversion efficiency;
pumping power requirements;
power handling requirements;
inner blanket thickness (n-shielding and streaming);
achievable tritium breeding ratio;
breeder tritium extraction;
T permeation/ coolant T purification & control;
chemical reactivity, coolant leakage;
design integration and feasibility of BoP.
• Design dealing with uncertainties
(physics and technology)
• High degree of system integration/
complexity/ system Interdependencies
• Trade-off studies/ sensitivity studies
with multi-criteria optimisations,
including engineering assessments.
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 9
Concept Design Approach
DEMO physics basis / uncertainties
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 10
Concept Design Approach
DEMO physics basis / uncertainties
Pel
tburn
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 11
Concept Design Approach
Main size drivers: Divertor and H-mode
• Power transported by electrons and
ions across separatrix:
Psep=Pα+Padd-Prad,core
• Physics/ Material limit condition for
divertor
Psep/‘ 20MW/m
• Boundary condition to access and
operate in H-mode with good
confinement:
Psep fLH PLH
Results of PROCESS Analysis:
• For low Psep/PLH major radius is
determined by the divertor protection
constraint (Psep/R)
• From a certain Psep/PLH onwards this in
combination with Psep/R is driving the
major radius
Main problem: • Extreme uncertainty on PLH is passed on to the major radius
Objective: Protect divertor and operate in H-mode
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 12
Concept Design Approach
Preliminary DEMO design features
• 2000 MWth~500 Mwe
• Pulses > 2 hrs
• SN water cooled divertor
• PFC armour: W
• LTSC magnets Nb3Sn (grading)
• Bmax conductor ~12 T (depends on A)
• RAFM (EUROFER) as blanket structure
• VV made of AISI 316
• Blanket vertical RH / divertor cassettes
• Lifetime: starter blanket: 20 dpa (200 appm
He); 2nd blanket 50 dpa; divertor: 5 dpa (Cu)
Open Choices:
• Operating scenario
• Breeding blanket design concept selection
• Primary Blanket Coolant/ BoP
• Protection strategy first wall (e.g., limiters)
• Advanced divertor configurations
• Number of coils
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 13
ITER
DEMO1
(2015)
A=2.6
DEMO1
(2015)
A=3.1
DEMO2
(2015)
A (m2) 680 1428 1428 1253
Volume (m3) 830 2502 2502 2217
Pfus (MW) 400 2037 2037 3255
tburn (hrs) 0.1 2 2 ss
IP (MW) 15 19.6 20 22
BT (T) 5.3 5.7 5.7 5.6
βN,total 1.8 2.6 2.6 3.8
βα/βth 8% 14% 14% 17%
βf/βth 12% 16% 16% 25%
Te0 (keV) 11.5 27.4 25.9 34.7
ne0 (1020 m-3) 1.25 1.0 1.7 1.2
Prad,core (MW) 47 303 306 634
Prad,core/Pheat 40% 66% 67% 81%
PCD (MW) 70 50 50 s 133
-6
-4
-2
0
2
4
6
3 5 7 9 11 13
Z (
m)
R (m)
ITERDEMO1 (A=2.6)DEMO1 2015 (A=3.1)DEMO2 2015
Concept Design Approach
Sensitivity study: Aspect Ratio
Courtesy R. Kemp (CCFE)
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 14
DEMO design and physics integration challenges
• Investigate impact of increasing plasma elongation, k, constrained by vertical stability,
through optimising for example PF coils layouts and current distributions (see next slide).
• Investigate divertor configurations with a lower X-point height and larger flux
expansion as they may provide a more favourable compromise between pumping and
power exhaust for DEMO than the vertical target divertor chosen for ITER.
• Improve power handling capabilities near the upper secondary null point in a SN
DEMO and assess impact of design and maintainability of the solutions proposed.
• Explore a Double Null (DN) Configuration: higher plasma performance with improved
vertical position control, and an accompanying reduced machine size. The impact on
blanket vertical RH should be investigated together with impact on T- breeding.
• Investigate divertor strike point sweeping, including technology issues such as thermal
fatigue of the HHFCs, AC losses of the adjacent PF coils, etc.
• Investigate magnetic field ripple: trade-off between RH access, coil size, and NBI
access.
• Estimate dwell time and evaluate impact of trade-offs on CS, BoP, pumping, etc.
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 15
Design and physics integration challenges
Optimisation of baseline divertor configuration
Options 1) SN deep divertor (ITER) 2) Shallow SN divertor 3) Shallow DN divertor
Advantages Compatible with BB vertical RH Compatible with BB vert. RH
improved T breeding
higher plasma performance
with improved vertical
position control
Shortcomings Elongation constrained by VS
Marginal T breeding
Limited power handling near
upper secondary null
Elong. constrained by VS
Problems of heat loads near
upper secondary null?
T breeding to be assessed
compatibility with BB vertical
maintenance scheme
questionable. Requires study.
Plasma VS is an
important design driver.
A variation of Beta or li
(e.g., due to loss of NBI,
RF, or impurity influx) or
loss of H-mode would
lead to a V moment that
in the case of an
asymmetric
configuration (SN)
would challenge control
requirements.
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 16
Design and physics integration challenges
Results of Selected Studies
• Sensitivity to plasma elongation
• Optimisation of the Upper Null
• Divertor Geometry optimisation studies
• Neutronic / TBR sensitivity analysis divertor size
• Strike point sweeping parametric scan (not shown
here)
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 17
Design and physics integration challenges
Increasing k,d (~20%) has large impact on machine layout
7
7,5
8
8,5
9
9,5
10
1,6 1,8 2 2,2
R0
(m
)
Elongation (k)
d = 0.5, q95 = 3.0
d = 0.75, q95 = 3.0
Single null baseline
19,5
20
20,5
21
21,5
22
22,5
1,6 1,8 2 2,2
Ip (
MA
)
Elongation (k)
d = 0.5, q95 = 3.0
d = 0.75, q95 = 3.0
Single null baseline
0
1
2
3
4
5
6
7
1,6 1,8 2 2,2
Bt
(T)
Elongation (k)
d = 0.5, q95 = 3.0
d = 0.75, q95 = 3.0
Single null baseline
0
0,05
0,1
0,15
0,2
0,25
0,3
0,35
0,4
0,45
0,5
1,6 1,8 2 2,2
f_b
s
Elongation (k)
d = 0.5, q95 = 3.0
d = 0.75, q95 = 3.0
Single null baseline
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 18
Design and physics integration challenges
Results of selected analysis: Optimisation of upper null Upper null position optimization
x
Inward-outward upper null position movement, while
preserving plasma shape
Intersection of upper-null isoflux curve with first wall larger
with null outward: less peaked heat loads expected (TBC)
Ongoing evaluation of q|| portion incident on upper wall
Upper null closer
to plasma
Upper null farther
from plasma
x
x
x upper null
— isoflux upper null
— plasma boundary
—FW-isoflux upper null
intersection x
�∥ = �0 ∙ �− ���
�0
Portion intersecting
upper FW
Courtesy R. Ambrosino (CREATE))
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 19
Results of selected studies
Optimisation of divertor geometry
Comparison previous (red) & new (dashed
blue) geometry with increased B.B. area
(dashed green)
• Exlcude divertor dome as the necessity is
not obvious —> Effect of the dome will be
investigated with SOLPS.
• Divertor area decreased and breeding area
increased in favour of meeting the DEMO
unique tritium breeding requirement.
Investigation on moving strike-
point closer to x-point: I estigatio o shallo divertor:
Wetted area increases linearly
with flux expansion fexp,t
However: Higher flux fexp,t also reduces the grazing angles g between
the field lines and the target plate, which cannot be arbitrarily small
Toroidal incidence angle
Connection length
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 20
Results of selected studies
TBR sensitivity analysis
Neutron wall load: Potential Tritium breeding contributions: Total TBR:
• Significant improvement of TBR due to reduction of divertor size.
• DN configuration with two small divertors seems possible regarding TBR.
P. Pereslavtsev, U. Fischer (KIT)
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 21
Conclusions
• The demonstration of electricity production ~2050 in a DEMO Fusion Power Plant is
a priority for the EU fusion program
• ITER is the key facility in this strategy and the DEMO design/R&D will benefit largely
from the experience gained with ITER construction
• There are outstanding gaps requiring a vigorous integrated design and technology
R&D (e.g., breeding blanket, divertor, Remote Handling, materials)
• DEMO reactor design suffers from high degree of system integration/ complexity/
system Interdependencies. Trade-off studies/ sensitivity studies with multi-criteria
optimisations, including engineering assessments
• In 2014 a traceable design process with SE approach was started to explore DEMO
design/ operation space to understand implications on technology requirements
• Main difficulty with designing is dealing with uncertainty.
• One of the greatest difficulties is the definition of a sufficiently flexible design /
analysis framework and approach to start a coherent iterative design process and
technology development in the projects.
• We are also keeping some flexibility in exploring options in parallel.
See talk M. Gasparotto
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 22
Highlights of Achievements
• WPBB: 4 designs studied: HCPB. HCLL, WCLL, DCLL. Key technology R&D work in progress.
• WPBOP: modelling work is underway for systems using water and He as coolant. Feasibility
issues are being identified and proposals for solutions examined.
• WPDIV: several target candidate concepts developed and fabrication trials performed. Design
integration of several divertor layout configurations are analysed.
• WPHCD: systems studies are exploring options for NBs, EC and IC Heating. System efficiencies
and feasible launch positions for these technologies are investigated.
• WPMAG Basic coil layouts defined. Samples of optimised design of LTSCs with improved
performance were manufactured and will be tested in 2015. HTSC samples fabricated /tested.
• WPMAT: two 80 kg batches of low temp. optimised EUROFER material were produced, + nine
80 kg of high temp optimised material. 23 lab-scale batches (250 – 550 g each) of ODS steel
were produced. Development of Codes and Design Criteria has been started.
• WPRM: consolidate the requirements for RH systems. Blanket extraction and installation
processes have been developed.
• WPSAE: S&E philosophies and approaches have been prepared, together with the high-level
principles, requirements. Initial safety studies are in progress.
• WPTFV: define system block diagrams and requirements for Tritium, Fuelling and Vacuum
systems. Direct Pumping concept further developed.
• WPDC/ WPENS: Being implemented. Definition of activities and establish working teams.
G. Federici & PPPT Team | 3rd IAEA DEMO Progr. Workshop|HEFEI| 11-14/05/2015| Page 23
Acknowledgements
The PPPT PMU Team:
M. Shannon, C. Morlock, R. Wenninger, F. Maviglia, C. Bachmann, M. Coleman, B.
Meszaros, T. Franke, S. Ciattaglia, E. Diegele, F. Cismondi, H. Hurzlmeyer.
PPPT Project leaders:
L. Boccaccini (KIT), M. Rieth (KIT), C. Day (KIT), W. Biel (FZJ), J-H. You (IPP), N. Taylor
(CCFE), T. Loving (CCFE), L. Zani (CEA), A. Ibarra (CIEMAT), M.Q. Tran (CRPP), M.
Grattarola (ENEA).
PPPT Work Programme Collaborators on this talk
(in particular): R. Kemp (CCFE), G. Giruzzi (CEA), M. Gilbert (CCFE), U. Fischer (KIT),
P. Pereslavtsev (KIT), R. Albanese (ENEA/Create), R. Ambrosino (ENEA/Create)
PPPT Expert Group:
H. Zohm, W. Morris, B. Saoutic, C. Waldon, P. Sonato, T. Mull, K. Hesch, S.
Chiocchio, P. Barabaschi.