Thermal properties of
Low temperature thermal properties of composite insulation systems
โ Scribed by P.E. Fabian; T.S. Bauer-McDaniel; R.P. Reed
- Publisher
- Elsevier Science
- Year
- 1995
- Tongue
- English
- Weight
- 412 KB
- Volume
- 35
- Category
- Article
- ISSN
- 0011-2275
No coin nor oath required. For personal study only.
โฆ Synopsis
The thermal contraction and thermal conductivity of candidate composite insulation systems for the International Thermonuclear
Experimental Reactor toroidal field coils were measured from 295 to 4 K. Matrix materials consisted of a diglycidyl ether of bisphenol-A epoxy suitable for vacuum impregnation, a tetrafunctional epoxy suitable for pre-impregnation, a polyimide system produced by a high-pressure laminating process, and a bismaleimide system. These matrix materials were combined with S-2 glass fabric and various barrier systems, such as ceramic and organic coatings, polyimide film and mica/glass. Thermal contraction was measured by the strain gauge method in which strain gauges are attached directly to the specimen. The thermal contraction in the through-thickness direction was different at 4 K for each resin system and changed slightly with the addition of electrical barriers. The thermal conductivity of the materials, with and without the electrical barriers, was similar at 4 K, but more distinctive at higher temperatures. The systems with the ceramic coatings exhibited the highest thermal conductivities at all temperatures.
๐ SIMILAR VOLUMES
## Shear/compression tests were performed at 76 and 4 K on candidate composite insulation systems for the International Thermonuclear Experimental Reactor (ITER) toroidal field coils. The insulation systems tested consisted of vacuum-pressure impregnated, pre-impregnated, and high-pressure laminat
Thermal conductivity data are presented for several samples: Gd2 (SO4) 3 8H2 0 pressed powders with and without copper fibres, pressed powders of NaCI and KCI, cloth base phenolic sheet, epoxy resin-bonded glass fibre laminate, and AGO T graphite in the presance of helium gas. Measurements on all sa
Fatigue tests under combined compression and shear loading were conducted at 76 K on four types of insulation system fabricated by vacuum-pressure impregnation and pre-impregnation. Fixtures developed for static tests with loading angles of 15", 45", 75", 84" and 90" were used to apply cyclic loads