Reflections on Fusion Chamber Technology and SiC/SiC Applications - - PowerPoint PPT Presentation

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Reflections on Fusion Chamber Technology and SiC/SiC Applications - - PowerPoint PPT Presentation

Reflections on Fusion Chamber Technology and SiC/SiC Applications Mohamed Abdou UCLA Presented at CREST Conference, Kyoto, Japan, May 21, 2002 The Region Immediately Surrounding the Plasma Divertor / First Wall / Blanket / Vacuum Vessel /


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SLIDE 1

Reflections on Fusion Chamber Technology and SiC/SiC Applications

Mohamed Abdou UCLA

Presented at CREST Conference, Kyoto, Japan, May 21, 2002

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SLIDE 2

The Region Immediately Surrounding the Plasma Divertor / First Wall / Blanket / Vacuum Vessel / Shield

Names

Fusion Nuclear Technology (FNT) Fusion Power Technology Reactor Core Plasma Exterior In-Vessel System (components)

  • FNT embodies a majority of the most challenging issues in development of an

attractive fusion energy source

  • Despite Meager Resources for FNT R&D, remarkable progress has been

made (witness this conference)

What Have We Learned? What Have We Learned?

Realizing the fusion promise of an attractive energy source for future generations requires, among other top priorities, advances in engineering sciences and innovative research to develop advanced fusion nuclear technology

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SLIDE 3

Functional Requirements of Chamber Technology

1) Provision of VACUUM environment 2) EXHAUST of plasma burn products 3) POWER EXTRACTION from plasma particles and radiation (surface heat loads) 4) POWER EXTRACTION from energy deposition of neutrons and secondary gamma rays 5) TRITIUM BREEDING at the rate required to satisfy tritium self sufficiency 6) TRITIUM EXTRACTION and processing 7) RADIATION PROTECTION

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SLIDE 4

General Criteria for Attractiveness of (Fusion) Energy System

1. ECONOMICS 2. SAFETY 3. ENVIRONMENTAL

a) Cost per unit thermal power b) Thermal conversion efficiency c) Mean time between failure (MTBF) d) Mean time to repair (MTTR) e) Lifetime a) Chemical reactivity b) Decay heat c) Tritium inventory and tritium permeation d) Off-site dose e) Biological hazard potential f) Radioactive inventory of volatile materials g) Etc. a) Waste disposal b) Routine releases (e.g. tritium) c) Material resources utilization d) Etc.

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SLIDE 5

Economics Principles motivated our Chamber Technology Goals

t time replacemen rate failure / 1 ) rate failure / 1 ( +

  • Need Low Failure Rate:
  • Innovative Chamber Technology
  • Need Short Maintenance Time:
  • Simple Configuration Confinement
  • Easier to Maintain Chamber Technology

Need Low Failure Rate Energy Multiplication Need High Temp. Energy Extraction Need High Power Density/Physics-Technology Partnership

  • High-Performance Plasma
  • Chamber Technology Capabilities

th fusion

M P M O i C COE η ⋅ ⋅ ⋅ + + ⋅ = Availability & replacement cost

Need High Availability / Simpler Technological and Material Constraints

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SLIDE 6

Power Density and Heat Flux in Fission Reactors Compared to Fusion with Traditional Evolutionary Concepts

50 1.43 12.8 2.6 2.8

1.2 240 9 56 96

30 15 2.1 0.9 8.4 6.3 4.6 3.8 3.6 3.8

ITER- Type LMFBR HTGR BWR PWR

Peak-to-Average Heat Flux at Coolant Average Core Power Density (MW/m3)

Equivalent Core Diameter (m) Core Length (m)

Need Revolutionary Concepts with High Power Density Capability

i.e. concepts capable of handling both high plasma heat flux and neutron wall load

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SLIDE 7

200 400 600 800

MTBF per Blanket Segment(FPY)

5 10

MTBF per Blanket System(FPY)

1 2 3

MTTR (Months) N e e d e d ( R ) Expected A C

Current FW/B Design Concepts are NOT Capable of Meeting the Challenging Reliability Requirements

R = Required A = Expected with extensive R&D (based on mature technology and no fusion-specific failure modes) C = Potential improvements with aggressive R&D

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SLIDE 8

Challenging Fusion Nuclear Technology Issues

  • 1. Heat Removal at High Temperature and Power
  • 1. Heat Removal at High Temperature and Power

Density Density

  • 2. Tritium Fuel Self
  • 2. Tritium Fuel Self-
  • Sufficiency

Sufficiency

  • 3. Failure Rate
  • 3. Failure Rate
  • 4. Time to Recover from a Failure
  • 4. Time to Recover from a Failure
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SLIDE 9

Heat Extraction Issue Suggested Future Directions

Aggressively Promote Creativity and Innovation to Stimulate NEW DESIGN CONCEPTS for First Wall / Blanket / Divertor / Shield (In-Vessel System) that Have

  • Less Constraints
  • Higher Power Density Capability
  • Larger Design Margin
  • Better Breeding Capability
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SLIDE 10

SiC/SiC for Fusion Applications

Major Advantages Applications in Fusion

  • Low Long-Term Radioactivity
  • “Potentially” High Temperature Capability
  • Enhances the environmental attractiveness of fusion energy
  • Strong interest in using SiC composites in fusion first wall /

blankets started in the early 80’s in the US.

  • Several reactor design studies have explored the utilization
  • f SiC/SiC. These studies served to understand the benefits

and identify the issues in the use of SiC.

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SLIDE 11

Challenges in Utilization of SiC/SiC in Fusion Applications

  • Low Thermal Conductivity

Limits High Power Density Capability

  • Typical Problems of Ceramics

(e.g. embrittlement/fracture toughness, particularly when they are irradiated, joining, hermiticity, etc.)

  • Do Not know yet how to design first wall/structure with

SiC/SiC (e.g. no design criteria exists yet in the fusion environment)

How to Resolve These Challenges? How to Resolve These Challenges?

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SLIDE 12

Key Points as Elements in a Strategy for Enhancing the Potential of SiC/SiC in Fusion Applications Near-Term Applications Long-Term Applications

  • Focus on utilizing SiC for suitable applications such as inserts (for

electric insulation), and deeper regions of the blanket.

  • Explore fusion designs that can keep the “surface heat flux” away

from a SiC/SiC first wall.

  • 1-2 cm liquid on the plasma side of SiC first wall will remove the

surface heat flux.

  • mitigates problems of low thermal conductivity, high stresses, etc.
  • allows SiC to be considered for high density, high temperature

attractive fusion applications

Example: Thin Liquid Wall

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SLIDE 13

THIN Liquid Wall

a) Provide High Power Density Capability b) Make the structural wall thermomechanics & other material issues more tractable c) Tolerate Disruptions d) Realize almost all the potential benefits of LM’s in improving plasma performance

CLiFF - Convective Liquid Flow Firstwall

Use thin (1-2 cm) liquid layer to remove surface heat flux and peak nuclear heating in First Wall & Divertor

  • eliminate thermal stress and erosion as limiting

factors in the first wall and divertor

  • results in smaller and lower cost system
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Potential Benefits if w e can develop good liquid w alls:

  • Improvements in Plasma Stability and Confinement
  • Enable high ß, stable physics regimes if liquid metals are used
  • High Power Density Capability
  • Eliminate thermal stress and erosion as limiting

factors in the first wall and divertor

  • Results in smaller and lower cost components
  • Increased Potential for Disruption Survivability
  • Reduced Volume of Radioactive Waste
  • Reduced Radiation Damage in Structural Materials
  • Makes difficult structural materials problems more tractable
  • Potential for Higher Availability

No single LW concept may simultaneously realize all these benefits, but realizing even a subset will be remarkable progress for fusion

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Complete Sector Liquid Wall Components

Thin Liquid Wall Concept Thin Liquid Wall Concept

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HYLIFE-II ALPS/APEX NSTX Li module

Liquid Wall Science & Technology are being Advanced in Several MFE & IFE Research Programs

IFMIF APEX CLiFF DNS Free Surface Simulation Collaboration with non-fusion scientists US-Japan Collaboration

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SLIDE 17

Remarkable Progress on Liquid Wall Research in the Past 3 years

  • New Design Ideas for Liquid Walls in MFE Have Evolved
  • Key Technical Issues Identified & Characterized

(Elaborate Liquid Wall Designs for IFE have long existed)

  • R&D Effort on Top Issues Initiated: Significant Progress

Modeling

  • Plasma Physics Edge & Core
  • Fluid Mechanics, MHD, Heat Transfer

Experiments

  • Laboratory Experiments on Thermofluids (w/ & w/o MHD)
  • Laboratory Experiments on Sputtering & Particle Trapping, etc.
  • Tokamak Experiments: Liquid Lithium in Actual Plasma Devices
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SLIDE 18

Best CDX-U Plasmas Achieved w ith Liquid Lithium Limiter

I Bare SS tray limiter L Cold lithium limiter G Liquid lithium limiter (250o C)

  • 0.5

0.5 1 1.5 2 2.5 10 20 30 40 50 60 70 80 90 Tray O-II (4416A) (arb. units) Plasma current (kA)

O-II 4416Å

  • Highest plasma currents and lowest impurity emission ever
  • btained in CDX-U were achieved with liquid lithium in the tray

limiter

  • Plasma recycling is very low on liquid lithium

– Possible that the recycling coefficient is zero

  • 0.5

0.5 1 1.5 2 2.5 3 20 30 40 50 60 70 80 90 Tray D-alpha (arb. units) Plasma current (kA)

Dα 6561Å

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SLIDE 19

Utilization of Liquid Metals for a Conducting Shell May Allow Higher Power Density Tokamak Plasma

  • Initial results from new WALLCODE resistive MHD code: Stable highly

elongated plasmas possible with appropriately shaped conducting shell

  • Liquid metals may be used for the conducting shell
  • Implications for fusion:
  • High power density plasma (plus power extraction capability)
  • Overcome physics-engineering conflicting requirements that reactor

designers have struggled with for decades

Relative growth rate of n=0 resitive wall mode for different % coverages (with a divertor hole)

1 2 3 4 5 6 7 1.5 2 2.5 3 3.5 4 4.5 Elongation 35% shell, d/a = .28 (ARIES) 84% shell, d/a = .28 84% shell, d/a=.15

γ / γ0

box

Beta Limits for high elongation (example of initial results)

κ β*

2 3 4 7.6 % 15.8 % 21.8 %

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SLIDE 20

Magnetic TOROIDAL Facility (MTOR) has been constructed

Multiple MHD experiments currently underw ay

  • 24 electromagnets:

600KW, 130 KJ stored energy

  • Bmax= 0.6 T ( >1.0 T with magnetic

flux concentrators)

  • 15L room-temp Ga-alloy flowloop
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SLIDE 21

Flinabe

  • Melting Point = 240 - 310 C

Inlet T ~ 350 C

  • From Plasma-edge modeling

T (allowable) = 480 C - FW = 700 C - Divertor

  • Turbulent FLINABE layer

can tolerate high heat fluxes: FW: 1.4 MW/m2 (averaged) Divertor: 30 MW/m2 (peak) (accounting for B effect with no flow mixing)

  • Further improvements are

possible through, for example, mixing the liquid right before the divertor inlet

HEAT TRANSFER - EDGE PLASMA MODELING FOR FLINABE FW SHOWS HIGH HEAT LOAD CAPABILITIES T allowable, divertor = 700 C T allowable, FW = 480 C

FW: qav = 1.4MW/m2 Divertor

2 4 6 8 10

DISTANCE, m

300 400 500 600 700

SURFACE TEMPERATURE, degree C 30 MW/m2 20 MW/m2 10MW/m2 Turbulent FLINABE flow: U=10 m/s, h=2.3 cm B=10 T