Abstract
Advanced structural composites reinforced with boron, graphite, or aramid fibers have unique mechanical, thermal, and electrical properties that make them attractive alternatives for metals in many cryogenic applications. A most promising application is the structure of the central solenoid of the poloidal field system in Tokamak magnetic fusion energy (MFE) devices.1 Depending on the flux rise time of a particular design, energy loss due to generation of eddy currents in metallic structures might place an excessive burden on the refrigeration system. Here, a replacement of the metallic structure with advanced composites could suppress eddy currents while providing strength and stiffness equal to that, of steel. The low thermal conductivity of graphite-reinforced epoxy laminates in the 77–4 K range combined with high strength and modulus suggests the possibility of fabricating more efficient thermal isolation supports than heretofore available.
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References
C. J. Long, “Application of Advanced Composites in Tokamak Magnet Systems,” ORNL/TM-6047, Oak Ridge National Laboratory, Oak Ridge, Tennessee (1977).
R. E. Schramm and M. B. Kasen, Cryogenic mechanical properties of boron-, graphite-, and glass-reinforced composites, Mater. Sci. 30; 197 (1977).
M. B. Kasen, Cryogenic properties of filamentary-reinforced composites: An update, Cryogenics 21: 323 (1981).
H. M. Ledbetter, Dynamic elastic modulus and internal friction in fibrous composites, in: “Nonmetallic Materials and Composites at Low Temperatures,” A. F. Clark, R. P. Reed, and G. Hartwig, eds., Plenum Press, New York (1979), p. 267.
M. B. Kasen, Mechanical and thermal properties of filamentary- reinforced structural composites at cryogenic temperatures- 2: Advanced composites, Cryogenics 15: 701 (1975).
“Advanced Composite Design Guide: IV-Materials,” Wright-Patterson Air Force Base, Ohio (1973).
“Plastics for Aerospace Vehicles; Part 1. Reinforced Plastics,” MIL-HDBK-17A, Department of Defense, Washington, D.C. (1971).
F. J. Jelenik and E. W. Collings, Low-temperature thermal expansion and specific heat properties of structural materials, in: “Materials Research for Superconducting Machinery,” Vol. VI, R. P. Reed, H. M. Ledbetter, and E. C. Van Reuth, eds., ADA 036919, National Bureau of Standards, Boulder, Colorado (1976).
J. G. Hust, Thermal conductivity, in: “Materials Research for Superconducting Machinery,” Vol. VI, R. P. Reed, H. M. Ledbetter, and E. C. Van Reuth, eds., ADA 036919, National Bureau of Standards, Boulder, Colorado (1976).
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© 1982 Plenum Press, New York
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Kasen, M.B. (1982). Mechanical Performance of Graphite- and Aramid-Reinforced Composites at Cryogenic Temperatures. In: Reed, R.P., Clark, A.F. (eds) Advances in Cryogenic Engineering Materials . Advances in Cryogenic Engineering Materials , vol 28. Springer, Boston, MA. https://doi.org/10.1007/978-1-4613-3542-9_16
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DOI: https://doi.org/10.1007/978-1-4613-3542-9_16
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