An Alternative SCWR Design Based on Vertical Power Channels and Hexagonal Fuel Assemblies - PowerPoint PPT Presentation

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An Alternative SCWR Design Based on Vertical Power Channels and Hexagonal Fuel Assemblies

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Title: An Alternative SCWR Design Based on Vertical Power Channels and Hexagonal Fuel Assemblies


1
An Alternative SCWR Design Based on Vertical
Power Channels and Hexagonal Fuel Assemblies
  • Jacopo Buongiorno

April 29, 2003 Madison, Wisconsin
2
Concept Description
Moderation is provided by the feedwater flowing
downward in the inter-assembly gap
3
Concept Description (2)
4
Concept Evaluation
  • Advantages
  • Simple mechanical design of the fuel assembly
    with no water rods. Wire wrapping can be used as
    spacer.
  • The amount of vessel internals above the core is
    minimal, which should simplify refueling
    operation.
  • A favorable neutron economy due to the use of
    the zirconium-based alloy for the power channels.
  •  Specific Challenges
  • High local peaking due to the distance of the
    inner fuel rods from the moderator in the
    inter-power-channel gap.
  • The moderator temperature rises roughly 58ºC,
    therefore the RPV lower head operates at higher
    temperature than the rest of the vessel.
  • A durable insulation material for the power
    channels needs to be selected/developed.

5
Thermal-Hydraulics
Temperature and density distributions in the
nominal channel appear acceptable


6
Neutronics (1)
The MCNP model




BOL analysis
7
Neutronics (2)
Average spectrum




Thermal tail in the fuel rods
8
Neutronics (3)
Doppler and coolant reactivity coefficients
similar to LWRs.




9
Neutronics (5)
Local peaking
Power skewing




Axial peaking (1.4 with uniform enrichment)
10
Conclusions
  • A new SCWR concept with no water rods is
    introduced.
  • Moderation is provided by the feedwater in the
    inter-assembly gap.
  • The fuel assembly design is simple with
    hexagonal lattice and zircaloy ducting.
  • The power density is much higher than for the
    water rod design.
  • The estimated fuel-cycle cost is comparable with
    that of the PWR the temperature and power
    distributions seem acceptable the Doppler and
    coolant reactivity feedbacks are both negative
    and within LWR range.
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