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Blanket

The blanket is a component installed to surround the plasma in a fusion reactor, serving three critical functions: producing tritium fuel, converting fusion energy into heat, and shielding against neutrons. For fusion reactors using the D-T reaction, the blanket is one of the most important and technically challenging components, and its design determines the overall performance, economics, and safety of the reactor.

The term “blanket” derives from the fact that it “wraps around the plasma like a blanket.” Most of the high-energy neutrons (14.1 MeV) generated by fusion reactions are slowed and absorbed in this blanket, and their kinetic energy is converted to heat. Simultaneously, nuclear reactions between lithium in the blanket and neutrons produce tritium, enabling fuel self-sufficiency for the fusion reactor.

The blanket must simultaneously fulfill three essential functions in a fusion reactor. These functions are interrelated, and design optimization must consider trade-offs among them.

In D-T fusion reactions, one tritium atom is consumed per reaction. Tritium exists in negligible quantities in nature (only trace amounts are produced by cosmic ray reactions with the atmosphere), and with a relatively short half-life of 12.32 years, continuous external supply is impractical. Therefore, the fusion reactor must have the capability to produce its own tritium.

By loading lithium-containing materials in the blanket, tritium is generated through nuclear reactions between neutrons produced by fusion reactions. This “tritium breeding” function allows the fusion reactor to produce more tritium than it consumes, achieving fuel self-sufficiency.

Approximately 80% of the energy released in D-T fusion reactions is carried by neutrons with kinetic energy of 14.1 MeV. Converting this neutron energy efficiently to heat for power generation is a crucial role of the blanket.

2D+3T4He (3.5 MeV)+n (14.1 MeV){}^{2}\text{D} + {}^{3}\text{T} \rightarrow {}^{4}\text{He}\ (3.5\ \text{MeV}) + n\ (14.1\ \text{MeV})

Of the total 17.6 MeV energy, the 3.5 MeV carried by alpha particles (helium-4) is used for plasma self-heating, while the 14.1 MeV carried by neutrons is recovered in the blanket. Neutrons are slowed through elastic and inelastic scattering with nuclei within the blanket, ultimately transferring thermal energy to the coolant.

High-energy neutrons and accompanying gamma rays cause severe damage to equipment and structures outside the blanket. Superconducting coils are particularly vulnerable to neutron irradiation and require strict dose limits. Sufficient shielding performance is also needed to reduce worker exposure during maintenance operations.

The blanket protects external equipment by slowing, absorbing neutrons, and shielding gamma rays. Inadequate shielding performance leads to serious problems such as reduced superconducting coil lifetime, increased vacuum vessel activation, and difficulties in remote maintenance.

The specific performance requirements for blankets are summarized below.

Function CategoryRequirementDesign TargetNotes
Tritium ProductionTritium Breeding Ratio (TBR)1.05\geq 1.05Margin for losses
Tritium ProductionTritium Recovery Rate>99%> 99\%Extraction efficiency from breeder
Heat ExtractionEnergy Multiplication Factor1.1 - 1.5Additional energy from nuclear reactions
Heat ExtractionCoolant Outlet Temperature300 - 700 CDirectly affects power generation efficiency
ShieldingSuperconducting Coil Neutron Flux<109< 10^{9} n/cm2^2/sTo ensure coil lifetime
ShieldingCoil Nuclear Heating<1< 1 mW/cm3^3To reduce cryogenic load
Structural IntegrityNeutron Wall Load Tolerance1 - 2 MW/m2^2DEMO conditions
Structural IntegrityDesign Lifetime>5> 5 yearsTo reduce replacement frequency
MaintainabilityModule Removal Time<1< 1 week/moduleBy remote operation
SafetyTritium ContainmentMultiple barriersBelow public exposure limits

Tritium (hydrogen-3, 3H{}^{3}\text{H} or T) is a radioactive isotope of hydrogen consisting of one proton and two neutrons. It undergoes beta decay with a half-life of 12.32 years, transforming into helium-3.

3T3He+e+νˉe+18.6 keV{}^{3}\text{T} \rightarrow {}^{3}\text{He} + e^{-} + \bar{\nu}_e + 18.6\ \text{keV}

The amount of tritium on Earth is extremely small; in nature, only about 4 kg is produced annually through spallation reactions between cosmic rays and atmospheric nuclei. In contrast, a 1 GW fusion power plant is estimated to consume approximately 56 kg of tritium per year.

m˙T=PfusionEfusion×mT×t\dot{m}_T = \frac{P_{\text{fusion}}}{E_{\text{fusion}}} \times m_T \times t

Here, PfusionP_{\text{fusion}} is the fusion power output, Efusion=17.6E_{\text{fusion}} = 17.6 MeV is the energy per reaction, and mTm_T is the mass of a tritium atom. For 1 GW of fusion power, the tritium consumption rate is approximately 1.8×1061.8 \times 10^{-6} g per second, reaching about 56 kg annually.

Therefore, “tritium breeding” that produces more tritium than consumed within the reactor is essential for sustained fusion reactor operation.

The reaction between lithium-6 (6Li{}^{6}\text{Li}) and neutrons is the primary pathway for tritium breeding.

6Li+n4He (2.05 MeV)+T (2.73 MeV){}^{6}\text{Li} + n \rightarrow {}^{4}\text{He}\ (2.05\ \text{MeV}) + T\ (2.73\ \text{MeV})

Characteristics of this reaction:

  • Q-value: +4.78 MeV (exothermic reaction)
  • Reaction threshold: None (can occur with thermal neutrons)
  • Cross-section: Approximately 940 barns at thermal energy (0.025 eV), follows 1/v law

The energy dependence of the reaction cross-section is approximated by:

σ(E)σ0E0E(low energy region)\sigma(E) \approx \sigma_0 \sqrt{\frac{E_0}{E}} \quad (\text{low energy region})

Here, σ0=940\sigma_0 = 940 barns and E0=0.025E_0 = 0.025 eV.

Due to this 1/v law, 6Li{}^{6}\text{Li} has a higher reaction probability with low-energy neutrons (thermal neutrons). Therefore, it is efficient to first slow down fusion neutrons (14.1 MeV) before reacting them with 6Li{}^{6}\text{Li}.

The natural abundance of 6Li{}^{6}\text{Li} in lithium is 7.59%, and enriched lithium-6 materials may be used to enhance tritium breeding efficiency.

The reaction between lithium-7 (7Li{}^{7}\text{Li}) and neutrons proceeds only with high-energy neutrons.

7Li+n4He+T+n{}^{7}\text{Li} + n \rightarrow {}^{4}\text{He} + T + n'

Characteristics of this reaction:

  • Q-value: -2.47 MeV (endothermic reaction)
  • Reaction threshold: 2.47 MeV (effectively about 4 MeV or higher)
  • Cross-section: Approximately 0.3 barns at 10 MeV

Being an endothermic reaction, the incident neutron energy must exceed the threshold. Fusion neutrons at 14.1 MeV satisfy this condition, and a neutron remains after the reaction. This “surplus neutron” effectively multiplies neutrons.

The natural abundance of 7Li{}^{7}\text{Li} is 92.41%, comprising most of lithium, but its contribution to tritium production is limited due to its smaller cross-section compared to 6Li{}^{6}\text{Li}. However, the neutron multiplication effect by high-energy neutrons cannot be ignored.

Let us examine the kinematics of the 6Li(n,α)T{}^{6}\text{Li}(n,\alpha)T reaction in detail. Consider the reaction in the center-of-mass frame.

With incident neutron energy EnE_n and reaction Q-value Q=4.78Q = 4.78 MeV, the total energy in the center-of-mass frame is:

Ecm=En×mLimn+mLi+QE_{\text{cm}} = E_n \times \frac{m_{\text{Li}}}{m_n + m_{\text{Li}}} + Q

The energy distribution of product particles (alpha particle and triton) follows from momentum conservation:

Eα=mTmα+mT×(EcmQ)2.05 MeVE_\alpha = \frac{m_T}{m_\alpha + m_T} \times (E_{\text{cm}} - Q') \approx 2.05\ \text{MeV} ET=mαmα+mT×(EcmQ)2.73 MeVE_T = \frac{m_\alpha}{m_\alpha + m_T} \times (E_{\text{cm}} - Q') \approx 2.73\ \text{MeV}

For thermal neutron incidence (En0.025E_n \approx 0.025 eV), the triton produced has an energy of approximately 2.73 MeV, which is rapidly slowed down within the blanket and converted to thermal energy.

To achieve TBR >1> 1 in a fusion reactor, detailed examination of neutron balance is necessary. One neutron is generated per D-T reaction, but the effective number of neutrons is reduced by the following factors:

  1. Neutron absorption by structural materials
  2. Neutron leakage through blanket openings (ports, plasma heating devices, etc.)
  3. Neutron capture reactions (parasitic absorption)
  4. Leakage to vacuum vessel and shielding

To compensate for these losses, neutron multiplier materials that undergo (n,2n)(n,2n) reactions are used. The neutron balance is expressed as:

TBR=V[σ6(E)N6+σ7(E)N7]ϕ(E)dEdV\text{TBR} = \int_V \left[ \sigma_6(E) N_6 + \sigma_7(E) N_7 \right] \phi(E) \, dE \, dV

Here, σ6\sigma_6 and σ7\sigma_7 are the reaction cross-sections for 6Li{}^{6}\text{Li} and 7Li{}^{7}\text{Li} respectively, N6N_6 and N7N_7 are nuclear densities, and ϕ(E)\phi(E) is the neutron flux spectrum.

Beryllium (9Be{}^{9}\text{Be}) is the most efficient neutron multiplier.

9Be+n24He+2n1.57 MeV{}^{9}\text{Be} + n \rightarrow 2{}^{4}\text{He} + 2n - 1.57\ \text{MeV}

Or more precisely:

9Be+n8Be+n24He+2n{}^{9}\text{Be} + n \rightarrow {}^{8}\text{Be}^* + n' \rightarrow 2{}^{4}\text{He} + 2n

Characteristics of the beryllium (n,2n)(n,2n) reaction:

PropertyValue
Reaction threshold1.85 MeV
Maximum cross-sectionApproximately 0.6 barns (3-4 MeV)
Average multiplication factorApproximately 1.8 (for 14 MeV neutron incidence)
Melting point1287 C
Density1.85 g/cm3^3

Advantages of beryllium:

  • Low reaction threshold (1.85 MeV) enables multiplication even with moderated neutrons
  • Being a light element, it also functions as a neutron moderator
  • High melting point allows high-temperature operation

Challenges with beryllium:

  • Limited resources (global confirmed reserves of approximately 100,000 tons)
  • Toxic dust (risk of chronic beryllium disease)
  • Helium embrittlement and swelling due to irradiation

Lead (Pb) is also used as a neutron multiplier that undergoes (n,2n)(n,2n) reactions. Natural lead is a mixture of four stable isotopes (204Pb{}^{204}\text{Pb}, 206Pb{}^{206}\text{Pb}, 207Pb{}^{207}\text{Pb}, 208Pb{}^{208}\text{Pb}).

APb+nA1Pb+2nQ{}^{A}\text{Pb} + n \rightarrow {}^{A-1}\text{Pb} + 2n - Q

(n,2n)(n,2n) reaction thresholds and cross-sections for each isotope:

IsotopeAbundanceReaction ThresholdCross-section (14 MeV)
204Pb{}^{204}\text{Pb}1.4%8.4 MeVApproximately 2.1 barns
206Pb{}^{206}\text{Pb}24.1%8.1 MeVApproximately 2.2 barns
207Pb{}^{207}\text{Pb}22.1%6.7 MeVApproximately 2.3 barns
208Pb{}^{208}\text{Pb}52.4%7.4 MeVApproximately 2.2 barns

Advantages of lead:

  • Abundant and inexpensive resources
  • Low melting point (327 C) facilitates use in liquid state
  • Lithium-lead alloy (Li-Pb) can serve as both breeder and multiplier

Challenges with lead:

  • High reaction threshold (6.7-8.4 MeV), multiplication only with high-energy neutrons
  • Being a high-Z element, has limited neutron moderation effect
  • 210Po{}^{210}\text{Po} production from activation (from 209Bi{}^{209}\text{Bi} impurities)

Optimization of Neutron Multiplier Placement

Section titled “Optimization of Neutron Multiplier Placement”

The placement of neutron multipliers must be optimized to maximize TBR. The basic principles are:

  1. Position multipliers close to the plasma (to utilize high-energy neutrons)
  2. Position breeder material (lithium) behind the multiplier (to utilize moderated neutrons)
  3. Alternate breeder and multiplier placement (multi-layer structure)

Optimization by one-dimensional transport calculation yields a typical arrangement:

PlasmaFirst WallBe LayerLi LayerBe LayerLi LayerShielding Layer\text{Plasma} \rightarrow \text{First Wall} \rightarrow \text{Be Layer} \rightarrow \text{Li Layer} \rightarrow \text{Be Layer} \rightarrow \text{Li Layer} \rightarrow \cdots \rightarrow \text{Shielding Layer}

Such multi-layer structures can achieve TBR = 1.1 - 1.4.

The Tritium Breeding Ratio (TBR) is a crucial indicator that quantitatively represents the tritium self-sufficiency capability of a fusion reactor.

TBR=Tritium production rate per unit timeTritium consumption rate per unit time\text{TBR} = \frac{\text{Tritium production rate per unit time}}{\text{Tritium consumption rate per unit time}}

More precisely, it is obtained by integrating the tritium production rate from 6Li{}^{6}\text{Li} and 7Li{}^{7}\text{Li} reactions within the blanket.

TBR=1Sn0V[σ6(E)N6(r)+σ7(E)N7(r)]ϕ(r,E)dVdE\text{TBR} = \frac{1}{S_n} \int_0^\infty \int_V \left[ \sigma_6(E) N_6(\mathbf{r}) + \sigma_7(E) N_7(\mathbf{r}) \right] \phi(\mathbf{r}, E) \, dV \, dE

Here, SnS_n is the fusion neutron source strength (neutrons/second), and ϕ(r,E)\phi(\mathbf{r}, E) is the neutron flux at position r\mathbf{r} and energy EE.

While TBR 1\geq 1 is necessary for a fusion reactor to be self-sufficient in tritium, actual designs require margins accounting for the following factors.

  1. Loss due to radioactive decay
dNTdt=λNT,λ=ln2t1/2=0.69312.32 years\frac{dN_T}{dt} = -\lambda N_T, \quad \lambda = \frac{\ln 2}{t_{1/2}} = \frac{0.693}{12.32\ \text{years}}

Approximately 5.5% of tritium is lost to decay annually.

  1. Losses in fuel processing systems

Small losses occur at each stage of tritium recovery, purification, and fuel supply. Typical loss rates are:

  • Recovery efficiency from breeder: 99% (1% loss)
  • Processing system loss: 0.1-0.5%
  • Fuel supply system loss: 0.1%
  1. Tritium inventory

“Inventory” tritium present in fuel processing systems, inside the vacuum vessel, and in structural materials is not available during reactor operation. Tritium accumulation in plasma-facing materials (tungsten, beryllium) is particularly problematic.

  1. Fuel supply for future reactors

During the deployment phase of fusion power, tritium must be supplied for initial fuel loading of new reactors. Approximately 1-2 kg of tritium is needed for initial loading of a 1 GW reactor.

The required TBR considering these factors is estimated by:

TBRrequired=1+ϵdecay+ϵprocess+ϵmargin\text{TBR}_{\text{required}} = 1 + \epsilon_{\text{decay}} + \epsilon_{\text{process}} + \epsilon_{\text{margin}}

Typical values are:

  • ϵdecay0.01\epsilon_{\text{decay}} \approx 0.01 (decay loss component)
  • ϵprocess0.02\epsilon_{\text{process}} \approx 0.02 (processing loss component)
  • ϵmargin0.02\epsilon_{\text{margin}} \approx 0.02 (design margin)

Therefore, TBR 1.05\geq 1.05 is the design target. More conservative targets of TBR 1.10\geq 1.10 may be adopted for DEMO reactor designs.

The major design parameters determining TBR are shown below.

ParameterEffect on TBROptimization Direction
Blanket coverageHigher coverage increases TBRMinimize port area
Breeder lithium densityHigher density increases TBRUse Li2_2O, liquid Li
6Li{}^{6}\text{Li} enrichmentOptimization at moderate enrichment30-90% (concept dependent)
Neutron multiplier amountOptimal amount maximizes TBRBe volume fraction 60-80%
Structural material volume fractionLower fraction increases TBRThin walls, low-absorption materials
Blanket thicknessThicker increases TBR50-80 cm (concept dependent)

Monte Carlo neutron transport calculations are used for precise TBR calculations. Representative calculation codes include MCNP, Serpent, and TRIPOLI.

Calculation procedure:

  1. Construction of 3D geometric model (conversion from CAD data)
  2. Setting material compositions and nuclear cross-section libraries
  3. Setting neutron source distribution (toroidal plasma distribution)
  4. Execution of neutron transport calculation
  5. Integration of 6Li(n,α)T{}^{6}\text{Li}(n,\alpha)T and 7Li(n,nα)T{}^{7}\text{Li}(n,n'\alpha)T reaction rates
  6. Statistical error evaluation

For ITER TBM design calculations, 10810^8 - 10910^9 neutron histories are tracked to keep TBR statistical error below 1%.

In the blanket, not only is the kinetic energy of fusion neutrons converted to heat, but energy is also generated or absorbed by various nuclear reactions. The energy multiplication factor MM represents the overall energy balance.

M=EtotalEn=En+EreactionEnM = \frac{E_{\text{total}}}{E_n} = \frac{E_n + E_{\text{reaction}}}{E_n}

Here, En=14.1E_n = 14.1 MeV is the fusion neutron energy, and EreactionE_{\text{reaction}} is the net energy generation (exothermic reaction) or absorption (endothermic reaction) from nuclear reactions.

Major reactions and energy balance:

ReactionEnergy BalanceTypical Contribution
6Li(n,α)T{}^{6}\text{Li}(n,\alpha)T+4.78 MeV+0.3 - 0.4
7Li(n,nα)T{}^{7}\text{Li}(n,n'\alpha)T-2.47 MeV-0.02
9Be(n,2n){}^{9}\text{Be}(n,2n)-1.57 MeV-0.05 - 0.1
Structural material (n,γ)(n,\gamma) reactions+several MeV+0.1 - 0.2
Neutron elastic scattering0 (kinetic energy transfer only)-

Typical solid breeder blankets yield M1.15M \approx 1.15 - 1.25, while liquid metal blankets yield M1.10M \approx 1.10 - 1.20.

The blanket thermal power of a fusion reactor is calculated as:

Pblanket=Pfusion×EnEfusion×M=Pfusion×14.117.6×MP_{\text{blanket}} = P_{\text{fusion}} \times \frac{E_n}{E_{\text{fusion}}} \times M = P_{\text{fusion}} \times \frac{14.1}{17.6} \times M

For 1 GW fusion power output with M=1.2M = 1.2:

Pblanket=1000 MW×0.80×1.2=960 MWP_{\text{blanket}} = 1000\ \text{MW} \times 0.80 \times 1.2 = 960\ \text{MW}

Power generation is performed from the total thermal output including this plus heat recovery at the divertor (a portion of alpha particle energy).

Higher blanket coolant temperatures improve power generation efficiency (Carnot efficiency constraint). Thermodynamic efficiency is expressed as:

ηCarnot=1TcoldThot\eta_{\text{Carnot}} = 1 - \frac{T_{\text{cold}}}{T_{\text{hot}}}

Actual power generation efficiency, considering turbine and generator efficiencies:

ηplant=ηCarnot×ηturbine×ηgenerator×(1ϵaux)\eta_{\text{plant}} = \eta_{\text{Carnot}} \times \eta_{\text{turbine}} \times \eta_{\text{generator}} \times (1 - \epsilon_{\text{aux}})

Here, ηturbine0.85\eta_{\text{turbine}} \approx 0.85 - 0.90, ηgenerator0.98\eta_{\text{generator}} \approx 0.98, and ϵaux\epsilon_{\text{aux}} is the auxiliary power ratio.

Cooling MethodOutlet TemperatureTheoretical EfficiencyEffective Efficiency
Pressurized water325 C40%33%
Helium500 C52%42%
Liquid Li600 C55%45%
Li-Pb500 C52%40%

Helium (He) is chemically inert and has minimal reactions with neutrons, making it an excellent coolant for fusion reactors.

PropertyValue/Characteristic
Chemical stabilityCompletely inert, no corrosion
Neutron absorptionExtremely small (minimal effect on TBR)
Induced radioactivityNone (does not activate)
Phase changeNone (single-phase flow)
Operating pressure8 - 10 MPa (typical)
Operating temperature350 - 550 C (outlet)

Helium heat transfer depends on Reynolds and Prandtl numbers. Heat transfer coefficient in the turbulent regime is estimated by the Dittus-Boelter correlation.

Nu=0.023×Re0.8×Pr0.4\text{Nu} = 0.023 \times \text{Re}^{0.8} \times \text{Pr}^{0.4} h=Nu×kDhh = \frac{\text{Nu} \times k}{D_h}

Due to helium’s low density and low heat transfer coefficient, high flow velocities (50-100 m/s) are required for adequate heat removal, resulting in large pressure drops.

ΔP=f×LDh×ρv22\Delta P = f \times \frac{L}{D_h} \times \frac{\rho v^2}{2}

Here, ff is the friction factor (Blasius equation), LL is the flow path length, and DhD_h is the hydraulic diameter.

  • Structural loading from high-pressure operation (8-10 MPa)
  • Coolant tube surface temperature rise due to low heat transfer coefficient
  • Increased pumping power (auxiliary power) due to high flow rates
  • Larger piping and equipment

Water (pressurized water) is a reliable coolant with extensive experience in nuclear power generation.

PropertyValue/Characteristic
Heat transfer coefficientHigh (approximately 10 times that of helium)
Technology maturityAccumulated LWR technology
Operating pressure15 - 15.5 MPa
Operating temperature280 - 325 C (inlet/outlet)
Phase changeNone (subcooled water)
  • Low coolant temperature limits power generation efficiency
  • TBR reduction due to neutron moderation effect (considered in design)
  • Hydrogen generation risk during loss of coolant (structural material reaction)
  • Tritium dissolution and permeation into water

In water-cooled blankets, tritium concentration management in coolant water is an important safety issue. Tritium water (HTO) concentration in primary coolant is limited considering biological effects.

This method uses liquid lithium or lithium-lead alloy (Li-Pb) as coolant. These can also serve as breeder material, enabling simplified blanket structures.

PropertyValue/Characteristic
Melting point180.5 C
Boiling point1342 C
Li densityMaximum (pure lithium)
Thermal conductivityHigh (approximately 50 W/m·K)
Electrical conductivityHigh (significant MHD effect)

Main challenges with liquid lithium are chemical reactivity (violent reactions with water and air) and MHD effects.

The eutectic composition Li17_{17}Pb83_{83} (17 at% Li) is primarily considered.

PropertyValue/Characteristic
Melting point235 C (eutectic)
Li densityApproximately 1/5 of pure Li
Neutron multiplication(n,2n)(n,2n) reaction by Pb
Vapor pressureLower than pure Li
MHD effectSmaller than pure Li

Advantages of Li-Pb include serving as both breeder and neutron multiplier, and lower chemical reactivity than pure lithium.

When liquid metals flow in strong magnetic fields, magnetohydrodynamic (MHD) effects cause large pressure drops. This is an important challenge unique to fusion reactors.

When conductive fluid flows across magnetic field lines, induced currents are generated, and Lorentz forces (braking forces) arise from their interaction with the magnetic field.

F=j×B\mathbf{F} = \mathbf{j} \times \mathbf{B} j=σ(E+v×B)\mathbf{j} = \sigma (\mathbf{E} + \mathbf{v} \times \mathbf{B})

MHD pressure drop is estimated by:

ΔPMHD=cσvB2L\Delta P_{\text{MHD}} = c \sigma v B^2 L

Here, cc is a coefficient depending on channel geometry, σ\sigma is the fluid electrical conductivity, vv is the flow velocity, BB is the magnetic field strength, and LL is the channel length.

Flowing liquid lithium at 1 m/s in a 10 T magnetic field can result in MHD pressure drops of several MPa, more than 100 times the normal fluid friction losses.

  • Insulating coatings on channel walls (alumina, aluminum nitride, etc.)
  • Flow channel geometry optimization (flow parallel to magnetic field)
  • Use of low electrical conductivity materials (SiC/SiC composites)
  • Low flow velocity design (challenge to balance with heat transfer)

HCPB (Helium Cooled Pebble Bed) is a solid breeder blanket concept developed in Europe.

ComponentMaterialSpecification
Structural materialEUROFER97 (reduced activation ferritic/martensitic steel)Thickness 4-6 mm
BreederLi4_4SiO4_4 pebblesDiameter 0.25-0.63 mm
MultiplierBe pebblesDiameter 1 mm
CoolantHe gas8 MPa, 300-500 C
Tritium purge gasHe + 0.1% H2_20.1 MPa
  1. Fusion neutrons enter the blanket
  2. Neutron multiplication in Be pebble layers
  3. Tritium production in Li4_4SiO4_4 pebble layers
  4. Heat recovery through helium cooling tubes
  5. Tritium recovery from pebbles by purge gas
  • TBR: Approximately 1.15 (considering port openings)
  • Energy multiplication factor MM: Approximately 1.20
  • Coolant outlet temperature: 500 C
  • Surface heat flux tolerance: 0.5 MW/m2^2
  • Neutron wall load tolerance: 2 MW/m2^2

HCLL (Helium Cooled Lithium Lead) is a liquid breeder blanket concept developed in Europe.

ComponentMaterialSpecification
Structural materialEUROFER97Thickness 4-6 mm
Breeder/MultiplierLi17_{17}Pb83_{83}Liquid state
CoolantHe gas8 MPa, 300-500 C
Insulating coatingAl2_2O3_3MHD countermeasure
  1. Fusion neutrons enter the blanket
  2. Neutron multiplication by Pb in Li-Pb
  3. Tritium production by Li in Li-Pb
  4. Circulating Li-Pb to recover tritium
  5. Heat recovery through helium cooling tubes
  • TBR: Approximately 1.10 (considering port openings)
  • Energy multiplication factor MM: Approximately 1.15
  • Coolant outlet temperature: 500 C
  • Li-Pb outlet temperature: 450 C

HCLL features a relatively simple internal blanket structure as Li-Pb serves as both breeder and multiplier. However, MHD effect countermeasures are a significant challenge.

WCLL (Water Cooled Lithium Lead) is a liquid breeder blanket concept developed in Europe using pressurized water as coolant.

ComponentMaterialSpecification
Structural materialEUROFER97Thickness 4-6 mm
Breeder/MultiplierLi17_{17}Pb83_{83}Liquid state
CoolantPressurized water15.5 MPa, 295-328 C
  • TBR: Approximately 1.10
  • Energy multiplication factor MM: Approximately 1.12
  • Cooling water outlet temperature: 328 C
  • Li-Pb outlet temperature: 328 C

WCLL has the advantage of utilizing mature LWR technology. However, power generation efficiency is limited by the low coolant temperature. Additionally, since structural material separates Li-Pb from water, design must consider Li-water reaction risks in case of cooling tube failure.

WCCB (Water Cooled Ceramic Breeder) is a solid breeder blanket concept developed in Japan.

ComponentMaterialSpecification
Structural materialF82H (reduced activation ferritic/martensitic steel)Thickness 5-7 mm
BreederLi2_2TiO3_3 pebblesDiameter 0.2-2 mm
MultiplierBe, Be12_{12}TiPebble/plate form
CoolantPressurized water15 MPa, 280-325 C
Tritium purge gasHe + H2_2Low pressure

Similar to HCPB but using pressurized water as coolant. Water’s excellent heat transfer characteristics simplify cooling system design.

  • TBR: Approximately 1.10
  • Energy multiplication factor MM: Approximately 1.18
  • Cooling water outlet temperature: 325 C

“Self-cooled” concepts using liquid breeder material (Li or Li-Pb) as coolant can significantly simplify blanket structures.

A concept developed in the United States using Li-Pb as breeder and coolant, with only the first wall and structural materials cooled by helium.

ComponentMaterialSpecification
Structural materialRAFM steel / SiC/SiC
Breeder/CoolantLi-PbTarget outlet 700 C
First wall coolingHe gas8 MPa
Flow channel insulationSiC insertMHD countermeasure

SiC/SiC composite Flow Channel Inserts (FCI) significantly reduce MHD pressure losses.

ΔPMHD1Rwall\Delta P_{\text{MHD}} \propto \frac{1}{R_{\text{wall}}}

Here, RwallR_{\text{wall}} is the wall resistance, which can be increased by insulating materials.

If high-temperature Li-Pb operation (700 C or higher) becomes possible, power generation efficiency exceeding 45% may be achievable.

At ITER, the Test Blanket Module (TBM) program is being advanced to demonstrate blanket technology for the prototype reactor (DEMO). The main blanket at ITER is a shielding blanket without tritium breeding function, but TBMs are installed in dedicated ports to verify breeding blanket performance in the fusion environment.

TBM testing will demonstrate the following:

  1. Tritium production in actual fusion neutron environment
  2. Operational verification of tritium recovery and measurement systems
  3. Irradiation behavior of breeder and multiplier materials
  4. Thermal-hydraulic performance of cooling systems
  5. Structural integrity (thermal stress, electromagnetic forces, irradiation damage)
  6. Remote handling for removal/maintenance

These data are extremely important as design basis for DEMO blankets.

Developed by Japan Atomic Energy Agency (JAEA) and National Institutes for Quantum Science and Technology (QST).

ItemSpecification
Structural materialF82H
BreederLi2_2TiO3_3 pebbles (enriched Li)
MultiplierBe pebbles, Be12_{12}Ti
CoolantPressurized water (15 MPa, 280-325 C)
Module dimensions680 mm x 1940 mm x 600 mm
Expected TBRApproximately 1.0 (TBM unit)

A feature of the Japanese TBM is the use of advanced beryllium compound (Be12_{12}Ti). This has smaller swelling under neutron irradiation than pure Be and superior mechanical properties.

Europe is developing two types of TBMs in parallel.

HCPB-TBM:

ItemSpecification
Structural materialEUROFER97
BreederLi4_4SiO4_4 pebbles
MultiplierBe pebbles
CoolantHe gas (8 MPa, 300-500 C)

WCLL-TBM:

ItemSpecification
Structural materialEUROFER97
Breeder/MultiplierLi-Pb alloy
CoolantPressurized water (15.5 MPa)

China is developing both solid breeder (HCCB) and liquid breeder (HCLB) types.

HCCB (Helium Cooled Ceramic Breeder):

  • Structural material: CLF-1 steel (Chinese-developed reduced activation ferritic/martensitic steel)
  • Breeder: Li4_4SiO4_4 pebbles
  • Coolant: He gas

HCLB (Helium Cooled Lithium-Lead Blanket):

  • Structural material: CLF-1 steel
  • Breeder/Multiplier: Li-Pb alloy
  • Coolant: He gas

HCSB (Helium Cooled Solid Breeder) TBM developed by Korea Atomic Energy Research Institute (KAERI).

  • Structural material: RAFM steel
  • Breeder: Li2_2TiO3_3 pebbles
  • Multiplier: Be pebbles
  • Coolant: He gas

India is developing both liquid breeder (LLCB) and solid breeder (HCCB) types.

TBMs are installed in three equatorial plane ports at ITER (Ports 16, 18, and 2). Two TBMs can be installed in parallel in each port.

TBMs will be installed in phases according to ITER operational phases.

PhasePeriodTBM Testing Content
Stage 1Hydrogen/Helium operationStructural integrity, cooling system performance
Stage 2D-D operationTritium production at low neutron flux
Stage 3D-T operationFull-scale tritium breeding tests

The prototype reactor (DEMO) blanket must meet the following stringent requirements based on demonstration results from ITER TBM.

ItemITER TBMDEMONotes
TBRReference value1.05\geq 1.05Self-sufficiency required
Neutron wall load0.78 MW/m2^21-2 MW/m2^22-3 times increase
Annual fluence0.1 MWa/m2^22-3 MWa/m2^220+ times increase
Operating timeHundreds of second pulsesContinuous operationSteady-state
LifetimeDemonstration test5+ yearsLimited replacements
Power generation efficiency-30-45%Economic requirement

European DEMO design (EU-DEMO) considers two concepts in parallel: HCPB and WCLL.

ItemDesign Value
BreederLi4_4SiO4_4 pebbles (enriched 6{}^{6}Li 60%)
MultiplierBe pebbles (70% volume fraction)
Structural materialEUROFER97
CoolantHe (8 MPa, 300-500 C)
TBR1.12
M1.25
First wall heat load1 MW/m2^2
Neutron wall load1.2 MW/m2^2
Design lifetime5 fpy (full power years)

fpy stands for “full power year,” expressing cumulative operating time at rated power in years. 5 fpy corresponds to 10 years of operation at 50% of rated power.

ItemDesign Value
Breeder/MultiplierLi-Pb (6{}^{6}Li enrichment 90%)
Structural materialEUROFER97
CoolantPressurized water (15.5 MPa, 295-328 C)
TBR1.09
M1.17
Power generation efficiency33%

WCLL can leverage mature LWR technology, but HCPB is considered more favorable economically due to lower power generation efficiency with WCLL.

Japanese prototype reactor design (JA-DEMO) is based on the WCCB concept, with advanced concepts using SiC/SiC composites for high-temperature blankets also being studied.

ItemDesign Value
BreederLi2_2TiO3_3 pebbles
MultiplierBe12_{12}Ti
Structural materialF82H
CoolantPressurized water (15 MPa)
TBR1.05 or higher
Neutron wall load1.5 MW/m2^2

For the long term, high-temperature blankets using SiC/SiC composites as structural material are being considered.

ItemTarget Value
Structural materialSiC/SiC composites
Coolant outlet temperature900-1000 C
Power generation efficiency50% or higher

SiC/SiC has advantages of excellent high-temperature strength and low activation under neutron irradiation. However, many technical challenges remain, including joining technology, hermeticity assurance, and large structure fabrication.

Blanket thermal design considers the following heat loads:

  1. Volumetric heating by neutrons
  2. Volumetric heating by gamma rays
  3. Surface heat load (radiation and particle flux from plasma)
  4. Heating from nuclear reactions

Heating density due to neutrons decays exponentially in the blanket depth direction.

q(x)=q0exp(xλ)q'''(x) = q'''_0 \exp\left(-\frac{x}{\lambda}\right)

Here, λ\lambda is the decay length (typically 5-10 cm).

In actual blankets, heating distribution becomes complex due to material combinations. 3D heating distributions are obtained by Monte Carlo calculations (MCNP, etc.) and input to CFD codes to calculate temperature distributions.

Steady-state heat conduction equation:

(kT)+q=0\nabla \cdot (k \nabla T) + q''' = 0

Forced convection in cooling tubes:

q=h(TwallTfluid)q'' = h (T_{\text{wall}} - T_{\text{fluid}})

Here, kk is thermal conductivity and hh is heat transfer coefficient.

CFD analysis models effective thermal conductivity of pebble bed layers using experimental correlations.

keff=kgas[(11ϵ)+1ϵf(ks/kg)]k_{\text{eff}} = k_{\text{gas}} \left[ (1 - \sqrt{1 - \epsilon}) + \sqrt{1 - \epsilon} \cdot f(k_s/k_g) \right]

Here, ϵ\epsilon is porosity, and ksk_s, kgk_g are solid and gas thermal conductivities.

The following loads act on blankets:

Thermal stress due to temperature gradients:

σthermal=EαΔT\sigma_{\text{thermal}} = E \alpha \Delta T

Here, EE is elastic modulus, α\alpha is linear expansion coefficient, and ΔT\Delta T is temperature difference.

Thermal stresses from transient temperature changes during cooling start-up or shutdown often dominate structural integrity.

Loads from coolant pressure:

  • Water cooling: 15-15.5 MPa
  • Helium cooling: 8-10 MPa

Cooling tube membrane stress:

σ=Prt\sigma = \frac{P r}{t}

Here, PP is internal pressure, rr is tube radius, and tt is wall thickness.

Large electromagnetic forces are generated in blanket structures due to rapid magnetic field changes during plasma disruptions.

Induced current density:

j=σBt\mathbf{j} = \sigma \frac{\partial \mathbf{B}}{\partial t}

Electromagnetic force density:

f=j×B\mathbf{f} = \mathbf{j} \times \mathbf{B}

Electromagnetic forces during disruptions can cause stresses of several hundred MPa in structural materials, making it an important design consideration.

The following damage accumulates in structural materials due to neutron irradiation:

  • Atomic displacements (dpa: displacement per atom)
  • Helium production (He/dpa)
  • Hydrogen production (H/dpa)
  • Swelling (volume expansion)
  • Irradiation hardening and embrittlement

Under DEMO conditions (1.5 MW/m2^2, 5 fpy), approximately 70-80 dpa of irradiation damage accumulates in structural materials near the first wall.

dpa=Φn×σdN\text{dpa} = \frac{\Phi_n \times \sigma_d}{N}

Here, Φn\Phi_n is neutron fluence, σd\sigma_d is displacement cross-section, and NN is atomic number density.

Finite element method (FEM) stress analysis is used for structural integrity evaluation. Commercial codes such as ANSYS, ABAQUS, and NASTRAN, as well as dedicated analysis systems for ITER, are used.

Design rules conforming to ASME/RCC-MR standards are applied as evaluation criteria.

  • Primary stress: σSm\sigma \leq S_m (allowable stress)
  • Secondary stress: σ3Sm\sigma \leq 3 S_m
  • Fatigue evaluation: Cumulative fatigue damage D1D \leq 1
  • Creep-fatigue: Time fraction rule

The following characteristics are required for blanket structural materials:

Required CharacteristicReason
High strengthResistance to thermal stress and pressure loads
High-temperature strengthMaintaining mechanical properties at operating temperature
Irradiation resistanceSuppression of degradation under neutron irradiation
Reduced activationWaste treatment, reduced worker exposure
WeldabilityEase of fabrication and repair
CompatibilityChemical compatibility with coolant and breeder

Reduced Activation Ferritic/Martensitic Steel (RAFM)

Section titled “Reduced Activation Ferritic/Martensitic Steel (RAFM)”

These are the primary candidate materials for current DEMO designs.

Material NameDeveloping CountryMain Composition
F82HJapan8Cr-2W-V-Ta
EUROFER97Europe9Cr-1W-V-Ta
CLAMChina9Cr-1.5W-V-Ta

These materials eliminate long-lived activation elements such as molybdenum (Mo) and niobium (Nb) from conventional ferritic steels, replacing them with tungsten (W) and tantalum (Ta).

The target is for radioactivity levels to decay to hands-on (manual handling possible) levels 100 years after irradiation.

A(t)=A0exp(ln2t1/2×t)A(t) = A_0 \exp\left(-\frac{\ln 2}{t_{1/2}} \times t\right)

The upper temperature limit for RAFM steels is around 550 C. This is due to reduced creep strength and ductility loss from irradiation embrittlement.

DBTT (Ductile-Brittle Transition Temperature) shift:

ΔDBTT=f(dpa,Tirr,He)\Delta \text{DBTT} = f(\text{dpa}, T_{\text{irr}}, \text{He})

Irradiation raises DBTT, increasing the risk of brittle fracture at low temperatures.

Ceramic breeders such as Li2_2TiO3_3 and Li4_4SiO4_4 face the following challenges:

  • Degradation of tritium release characteristics due to irradiation
  • TBR reduction due to lithium burn-up (Li consumption)
  • Crystal structure changes
  • Swelling

Tritium release strongly depends on temperature and is described by Arrhenius-type diffusion-limited kinetics.

D=D0exp(EaRT)D = D_0 \exp\left(-\frac{E_a}{RT}\right)

Here, D0D_0 is the frequency factor and EaE_a is the activation energy.

Challenges with Li-Pb alloy:

  • Compatibility with structural materials (corrosion)
  • Low tritium solubility (difficult recovery)
  • 210Po{}^{210}\text{Po} production (from Bi impurities)

Tritium solubility in Li-Pb is extremely low (ppb order), requiring permeation extraction or gas bubbling methods for efficient recovery.

ST=S0exp(ΔHsRT)S_T = S_0 \exp\left(-\frac{\Delta H_s}{RT}\right)
  • Swelling due to irradiation (He production)
  • Mechanical property degradation
  • Tritium accumulation
  • Resource constraints

He is produced by (n,α)(n,\alpha) reactions in Be, causing irradiation swelling.

9Be+n24He+2n{}^{9}\text{Be} + n \rightarrow 2 {}^{4}\text{He} + 2n

Swelling rate depends on temperature and irradiation dose, increasing sharply above 500 C.

ΔVV=f(T,ϕnt)\frac{\Delta V}{V} = f(T, \phi_n t)

Be12_{12}Ti (beryllium titanide) has smaller swelling than pure Be and superior mechanical properties. Japan is developing it for ITER TBM and DEMO.

PropertyBeBe12_{12}Ti
Be density100%Approximately 90%
Swelling (600 C, 10 dpa)Approximately 10%Approximately 3%
Strength (room temperature)300 MPa400 MPa

DEMO blankets consist of hundreds of modules. Each module has a surface area of approximately 1-2 m2^2 and weighs several tons.

Manufacturing process:

  1. First wall panel fabrication (HIP method, forging, machining)
  2. Cooling tube fabrication and joining (welding, brazing)
  3. Side wall and back wall fabrication
  4. Module assembly (electron beam welding, diffusion bonding)
  5. Breeder and multiplier loading
  6. Leak testing, pressure testing
  7. Non-destructive examination (UT, RT, PT)

The following techniques are used for welding RAFM steels:

Welding MethodApplicationFeatures
TIG weldingCooling tube joiningPrecision welding, thin wall
Electron beam weldingModule assemblyDeep penetration, low heat input
Laser weldingFirst wall panelsHigh speed, low distortion
Diffusion bondingFirst wall/cooling tubeDissimilar material joining

Welding of RAFM steels requires preheating (150-200 C) and post-weld heat treatment (750 C x 2h).

Strict quality control conforming to nuclear quality assurance programs (NQA-1, RCC-MR) is applied to blanket module manufacturing.

Main inspection items:

  • Non-destructive examination of welds (100%)
  • Leak testing (He leak inspection)
  • Hydrostatic testing (design pressure x 1.25-1.5)
  • Dimensional inspection
  • Material testing (mechanical properties, chemical composition)

Tritium produced in blankets must be properly contained and recovered. The multiple barrier concept prevents release to the environment.

Barrier hierarchy:

  1. Breeder material matrix
  2. Cooling tubes and structural materials
  3. Blanket module outer shell
  4. Vacuum vessel
  5. Building (containment area)

Tritium permeation follows Sieverts’ law.

J=PTd(p1p2)J = \frac{P_T}{d} \left( \sqrt{p_1} - \sqrt{p_2} \right)

Here, PTP_T is the permeation coefficient, dd is wall thickness, and p1p_1, p2p_2 are tritium partial pressures on both sides.

To reduce permeation, techniques for forming oxide layers of alumina (Al2_2O3_3) or chromia (Cr2_2O3_3) on structural material surfaces are being developed.

Blanket materials are activated by neutron irradiation and become radioactive waste after operation. The use of reduced activation materials alleviates waste treatment burden.

Waste classification targets:

Time PeriodRadioactivity LevelDisposal Classification
Immediately after operationHigh levelShielded storage
50 years after operationIntermediate levelNear-surface disposal
100 years after operationLow level to clearanceRecyclable

Contact dose rate of RAFM steel decays to approximately 1 μSv/h after 100 years of irradiation, enabling hands-on maintenance.

Safety during Loss of Coolant Accident (LOCA) is also an important design consideration.

Decay heat removal:

Qdecay(t)=Q0×0.066×[(tts1 s)0.2(t1 s)0.2]Q_{\text{decay}}(t) = Q_0 \times 0.066 \times \left[ \left(\frac{t - t_s}{1\ \text{s}}\right)^{-0.2} - \left(\frac{t}{1\ \text{s}}\right)^{-0.2} \right]

Fusion reactors have smaller decay heat than fission reactors (approximately 1% of rated power), enabling designs where passive cooling (natural convection, radiation) can provide removal.

To realize blanket technology, the following challenges must be addressed with priority:

  1. TBR achievement demonstration (ITER TBM testing)
  2. Establishment of tritium recovery technology
  3. Confirmation of material integrity under long-term irradiation
  4. Establishment of large module manufacturing technology
  5. Demonstration of remote maintenance technology
  6. Improved power generation efficiency (high-temperature operation)

Based on results from ITER TBM testing (scheduled to begin around 2035), DEMO blanket design and manufacturing will proceed.

StagePeriodMain Activities
ITER TBM Testing2035-2045Breeding function demonstration
DEMO Engineering Design2040-2050Detailed design and prototyping
DEMO Construction2050-2060Module manufacturing and installation
DEMO Operation2060-Power generation demonstration

For the long term, the following advanced concepts are being considered:

  • SiC/SiC composite blankets (high-temperature operation, 50%+ power generation efficiency)
  • Molten salt blankets (FLiBe, etc.)
  • Advanced dual coolant concepts
  • Application of self-healing materials

If these technologies are realized, the economics of fusion power could be significantly improved.