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Автор Scoville, A. N.
Автор Reagan, P.
Автор Huffman, F. N.
Дата выпуска 1988
dc.description AbstractSiC matrix composite components have been fabricated by infiltrating and overcoating fiber preforms of graphite, alumina, and SiC via chemical vapor deposition (CVD). The degree of CVD densification could be controlled to yield vacuum tight components as well as porous open mesh structures where only the fiber was coated. These components have been fabricated in a wide variety of shapes including baskets, tubes and corrugated panels. The CVD process has been successfully scaled up to produce panels 80 cm by 80 cm. The morphology, chemistry, and geometry of the fiber was found to have a significant effect on the deposition process. Thus, process conditions had to be modified based on the fiber being infiltrated. These components were subjected to 1400 C temperature treatments including operation in gas-fired furnaces. After 2000 hours of testing in a gas-fired furnace at 1300 C, the SiC composite tubes have remained intact and un cracked. This suggests that the monolithic SiC coating is the controlling material and not the fibers. Hence, in light-load applications these structures still have useful lifetimes.
Формат application.pdf
Издатель Taylor & Francis Group
Копирайт Copyright Taylor and Francis Group, LLC
Название EVALUATION OF SIC MATRIX COMPOSITES FOR HIGH TEMPERATURE APPLICATIONS
Тип research-article
DOI 10.1080/10426918808953222
Print ISSN 0898-2090
Журнал Advanced Materials and Manufacturing Processes
Том 3
Первая страница 643
Последняя страница 668
Аффилиация Scoville, A. N.; Thermo Electron Technologies Corporation
Аффилиация Reagan, P.; Thermo Electron Technologies Corporation
Аффилиация Huffman, F. N.; Thermo Electron Technologies Corporation
Выпуск 4

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