Published June 28, 2010 | Version v1
Journal article

Effects of Slip Planes on Stresses in MICE Coupling Solenoid Coil Assembly

Description

The MICE superconducting coupling solenoid magnet is made from copper matrix Nb-Ti conductors with inner radius of 750 mm, length of 285 mm and thickness of 110.4 mm at room temperature. The coil is to be wound on a mandrel made of aluminum. The peak magnetic field on the conductor is about 7.3 T when fully charged at 210 A. High magnetic field and large size make the stress inside the coupling coil assembly relatively high during cool down and full energizing. The shear stress between coil winding and aluminum casing may cause premature quench. To avoid quench potential induced by stress, slip planes were designed for the coil assembly. In this paper, FE models with and without slip planes for it have been developed to simulate the stresses during the process including winding, cooling down and charging. The stress distribution in the coil assembly with and without slip planes was investigated. The results show that slip planes with low friction coefficients can improve the stress condition in the coil, especially reduce the shear stress largely so that improve the stability.

Availability note (English)

Available from OSTI as DE00984364; PURL: https://www.osti.gov/servlets/purl/984364-1MeOSv/

Additional details

Publishing Information

Journal Title
IEEE Transactions on Applied Superconductivity (Print)
Journal Volume
20
Journal Issue
3
Journal Page Range
vp.
ISSN
1051-8223

INIS

Country of Publication
United States
Country of Input or Organization
United States
INIS RN
41108360
Subject category
S36: MATERIALS SCIENCE;
Descriptors DEI
ALUMINIUM; COPPER; DISTRIBUTION; FRICTION; MAGNETIC FIELDS; MAGNETS; SHEAR; SLIP; SOLENOIDS; STABILITY; STRESSES; THICKNESS
Descriptors DEC
DIMENSIONS; ELECTRIC COILS; ELECTRICAL EQUIPMENT; ELEMENTS; EQUIPMENT; METALS; TRANSITION ELEMENTS

Optional Information

Contract/Grant/Project number
AC02-05CH11231
Notes
4 pages; Journal Publication Date: June 2010
Funding organization
Accelerator and Fusion Research Division (United States); Engineering Division (United States)
Secondary number(s)
LBNL--3571E