1991
DOI: 10.1109/20.133592
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Strain energy minimization in SSC magnet winding

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1991
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Cited by 34 publications
(20 citation statements)
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“…A coil end design that is useful for saddle, block and cos θ coils using thin tape conductors was also proposed in [11]. The constant-perimeter method was extended to model the bending of Rutherford cables [12]. The method was also implemented in ROXIE, a software package that is widely used for accelerator magnet design [13].…”
Section: Introductionmentioning
confidence: 99%
“…A coil end design that is useful for saddle, block and cos θ coils using thin tape conductors was also proposed in [11]. The constant-perimeter method was extended to model the bending of Rutherford cables [12]. The method was also implemented in ROXIE, a software package that is widely used for accelerator magnet design [13].…”
Section: Introductionmentioning
confidence: 99%
“…A "developable surface/grouped" configuration was chosen. 5,12,13,14 Conductor placement on the ends was generally very good. The end parts did not lilt from the mandrel surface during winding by more than 1/16 inch as shown in Fig.…”
Section: Dsa321 Assembly Historymentioning
confidence: 99%
“…This surface is based on the rectifying developable, and is by definition the least-strain surface definable within the given constraints [4,5]. The radially outer edge of the guiding strip lies on the outer surface of the tube and is called the base curve.…”
Section: Group Definitionsmentioning
confidence: 99%
“…The grouped end design approach treats each current block as a group of conductors that originate at the end of the coil straight section and maintain conductor-to-conductor contact as they wind around and over the mandrel. The group is a mathematically determined configuration that attempts to minimize the strain energy of individual conductors within the group, and is created by a computer program, BEND, written by Joe Cook [4,5]. This program is the heart of a complete coil end design system which consists of using BEND to create and optimize the groups, combining the group boundary surface files into files which represent the coil end parts, and reading these files into a CAD package to produce the part geometry.…”
Section: Introductionmentioning
confidence: 99%