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Insulation materials, thermal limiting temperatures

The only procedure to have been standardised generally is application of the Arrhenius relation (see below). IEC 21662 is a guide to evaluating the thermal endurance of electrical insulating materials and ISO 257863 applies the same principle to determining time/temperature limits to plastics. In both cases, the accent is more on finding maximum service temperatures rather than extrapolating to normal ambient temperature. Use of the same... [Pg.306]

An essential point considering e-motors is their thermal behaviour. For the simple case of permanent operation at rated power, the windings shall exceed neither the temperature limit of the corresponding temperature class (T1. .. T6) nor the limiting temperature due to the thermal class of insulating material given in Table 6.13, Part A. [Pg.201]

The absorption of impurity centres is observed in the transparency domains of semiconductors and insulators, which are limited by their intrinsic electronic and vibrational absorptions. Further, a brief account of the relevant physical processes and an overview of the intrinsic optical properties of these materials and of their dependence on temperature, pressure and magnetic field is given in this chapter. Some semiconductors have been or are now synthesized in quasi-monoisotopic (qmi) forms because of improvements in their physical properties like thermal conductivity. A comparison of their intrinsic optical properties with those of the crystals of natural isotopic composition is also given. The absorption related to free carriers, due mostly to doping is also discussed at the end of this chapter. A detailed account of the optical properties of semiconductors can be found in the books by Yu and Cardona [107] and by Balkanski and Wallis [4]. [Pg.45]

Although in refractory practice there are hundreds of heat insulation materials, the list of heat insulation materials for the lining of reduction cells is rather limited. For one thing, economic considerations add some limitations, but for another, the heat insulation materials in reduction cells should withstand mechanical compression loads without deformation at temperatures up to 900 °C for a long time, and numerous inexpensive fiber heat insulation materials don t correspond to this requirement. In the Hall-Heroult reduction cell, the heat insulation materials should withstand the pressure of the layer of the electrolyte, the layer of molten aluminium, cathode carbon blocks (taking into account collector bars), and the refractory layer. Currently, only four or five heat insulation materials are used in the lining of reduction cells diatomaceous (moler) and perlite bricks, vermiculite and calcium silicate blocks (slabs), and sometimes lightweight fireclay bricks (but their thermal conductivity is relatively big, while the cost is not small) and fiber fireclay bricks. [Pg.190]

Efficient insulation materials for rocket tanks should be light and strong, and have low thermal-conductivity factors at low temperatures. On liquid-hydrogen tanks, insulation layers will experience mean temperatures (near their midpoints) as low as -300 F. Because only limited data were available in the literature on thermal conductivities of common insulation materials in this low-temperature range, an experimental investigation was conducted to obtain such data. [Pg.131]

Thermal Management Subsystem - Provides the heat rejection, thermal isolation, and supplemental heating needed to keep the different Reactor Module elements within temperature limits. The thermal management subsystem would include insulating materials (insulation, multi-layer blankets, spacers), surface thermo-optical materials (paints, coatings, treatments, etc), conductive and isolating materials, and probably more active elements such as heaters, temperature sensors and heat pipes. [Pg.28]

The goal of thermal control within the control drive mechanism region would be to limit CDM temperatures to 400 K maximum to satisfy the material requirements and to maximize the reliability of the CDMs. This goal may require the addition of thermal insulation or supplemental heat rejection. Insulation materials, if needed, would require development to insulate properly above 500 K. Near 600 K the permanent magnets may begin to degrade and would require further study. [Pg.552]

The ATR is carried out in the presence of a catalyst, which controls the reaction pathways and thereby determines the relative extents of the oxidation and SR reactions. The SR reaction absorbs part of the heat generated by the oxidation reaction, limiting the maximum temperature in the reactor. The net result is a slightly exothermic process. However, in order to achieve the desired conversion and product selectivity, an appropriate catalyst is essential. The lower temperature provides many benefits such as less thermal integration, less fuel consumed during the start-up phase, wider choice of materials, which reduces the manufacturing costs, and reduced reactor size and cost due to a minor need for insulation [22]. [Pg.293]

It is usual to operate an aqueous-medium fuel cell under pressure at temperatures well in excess of the normal boiling point, as this gives higher reactant activities and lower kinetic barriers (overpotential and reactant diffusion rates). An alternative to reliance on catalytic reduction of overpotential is use of molten salt or solid electrolytes that can operate at much higher temperatures than can be reached with aqueous cells. The ultimate limitations of any fuel cell are the thermal and electrochemical stabilities of the electrode materials. Metals tend to dissolve in the electrolyte or to form electrically insulating oxide layers on the anode. Platinum is a good choice for aqueous acidic media, but it is expensive and subject to poisoning. [Pg.313]


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Limiting temperatures

Temperature limitations

Temperature limiter

Thermal insulating materials

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Thermal limited

Thermal limits

Thermal limits temperatures

Thermal materials

Thermal temperature

Thermalization temperature

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