2019
DOI: 10.1016/j.cryogenics.2019.04.011
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Thermal and electrical stabilities of GdBCO magnets impregnated with epoxy composites using surface-treated carbon nanotube fillers

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Cited by 9 publications
(1 citation statement)
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“…Because the tensile radial stress is mainly caused by the thermal expansion coefficient (CTE) mismatch between the REBCO CC and the epoxy resin layer in the epoxy impregnated REBCO pancake coil. In this regard, the investigation showed that the thermal stress can be reduced by modifying the CTE of the epoxy resin by adding fillers to the epoxy resin [38][39][40][41]. Meanwhile, the overband fabrication technology is also widely used in the epoxy impregnated REBCO pancake coil or no-insulation REBCO coil to reduce the radial and hoop stresses [42][43][44].…”
Section: Introductionmentioning
confidence: 99%
“…Because the tensile radial stress is mainly caused by the thermal expansion coefficient (CTE) mismatch between the REBCO CC and the epoxy resin layer in the epoxy impregnated REBCO pancake coil. In this regard, the investigation showed that the thermal stress can be reduced by modifying the CTE of the epoxy resin by adding fillers to the epoxy resin [38][39][40][41]. Meanwhile, the overband fabrication technology is also widely used in the epoxy impregnated REBCO pancake coil or no-insulation REBCO coil to reduce the radial and hoop stresses [42][43][44].…”
Section: Introductionmentioning
confidence: 99%