2007
DOI: 10.1016/j.fusengdes.2007.05.023
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Engineering challenges in designing an attractive compact stellarator power plant

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Cited by 5 publications
(3 citation statements)
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References 11 publications
(14 reference statements)
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“…This inboard shielding assumption is supported by 1D neutronics analysis described in section 4. Here, 'skeleton ring' [22] refers to an integrated support and shielding structure comprised of shield modules and manifolds to which blanket modules are attached. The skeleton-ring structure is utilized to mechanically and thermally separate the elevated-temperature core components from the colder vacuum vessel in order to withstand large loads caused by gravity, plasma disruptions and thermal expansion.…”
Section: Assessment Of Device Sizementioning
confidence: 99%
“…This inboard shielding assumption is supported by 1D neutronics analysis described in section 4. Here, 'skeleton ring' [22] refers to an integrated support and shielding structure comprised of shield modules and manifolds to which blanket modules are attached. The skeleton-ring structure is utilized to mechanically and thermally separate the elevated-temperature core components from the colder vacuum vessel in order to withstand large loads caused by gravity, plasma disruptions and thermal expansion.…”
Section: Assessment Of Device Sizementioning
confidence: 99%
“…These algorithms generally focus on the magnetic őeld optimization, and don't address the later stages of design. These later stages include winding pack design, cooling system, and vacuum chamber design [Raf+07] . As these all have different functions: the winding pack must reinforce the coils, the cooling system must regulate temperature at cryogenic levels, and the vacuum chamber must be airtight and resistant to the plasma, they are generally modeled with separate codes [Raf+07].…”
Section: Introductionmentioning
confidence: 99%
“…These later stages include winding pack design, cooling system, and vacuum chamber design [Raf+07] . As these all have different functions: the winding pack must reinforce the coils, the cooling system must regulate temperature at cryogenic levels, and the vacuum chamber must be airtight and resistant to the plasma, they are generally modeled with separate codes [Raf+07]. However, an integrated design workŕow is essential because the system is space-constrained and highly interconnected.…”
Section: Introductionmentioning
confidence: 99%