Carbon-carbon composites have been made using PAN-and pitch-based carbon fibers as reinforcement, and the carbon matrix has been derived from phenolic resin (R) and coal tar pitch (P) and a mixture of the two. The temperature of initiation of oxidation in the case of carbonized composites is about l
Oxidation behavior of carbon-carbon composites
β Scribed by Chang Heh-Won; Robert M. Rusnak
- Publisher
- Elsevier Science
- Year
- 1979
- Tongue
- English
- Weight
- 426 KB
- Volume
- 17
- Category
- Article
- ISSN
- 0008-6223
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β¦ Synopsis
This study investigates the oxidation mechanisms of carbon-carbon composite materials of the type used for aircraft brakes. The rate-controlling steps for oxidation at temperatures ranging between 450 and 750Β°C were determined by measuring activation energies of composite samples in bulk form and in ground form and by measuring oxidation rates as a function of reaction gas flow. Below 65O"C, the two forms of carbon samples showed considerably different activation energies, which suggests that in bulk samples, oxidation is controlled by diffusion through pores, and that as grinding reduces pore length, activation energy increases. At 75O"C, the ratio of oxidation rates was the same as the square root of the ratio of reactant flow rates. It was therefore concluded that the dominant oxidation mechanism at 750Β°C is diffusion of oxygen through a film of gaseous reaction products at the sample surface. The oxidation mechanism of carbon-carbon composite samples at temperatures between 450 and 650Β°C is primarily controlled by the diffusion of oxygen into pores. Between 650 and 750Β°C. the rate-controlling mechanism undergoes a transition from diffusion through pores to diffusion through stagnant gas film.
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