Journal
FIRE AND MATERIALS
Volume 41, Issue 7, Pages 808-816Publisher
WILEY
DOI: 10.1002/fam.2423
Keywords
carbon fiber; epoxy; flame retardant; polymer matrix composite
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Fundamental aspects for the thermal decomposition and formation of respirable fragments of carbon fibers are investigated to assess the health hazard of carbon fiber reinforced plastic material after a fire. The influence of temperature (600 degrees C-900 degrees C)/heat flux (30-80 kW/m(2)), time of thermal load (up to 20 minutes), and oxygen exposure is analyzed by means of mass loss and fiber diameter of intermediate modulus and high tenacity fibers with initial diameters of 5 to 7 mu m. Various types and concentrations of flame retardants were tested with respect to fiber protection. Epoxy-based composite specimens (RTM6/G0939) additionally containing aluminum or magnesium hydroxide and/or zinc borate (1-25 wt% per resin) were analyzed by cone calorimetry. Carbon fiber decomposition increases with combustion/irradiation time and temperature/heat flux, after a threshold temperature (ca 600 degrees C) is exceeded. Critical fiber diameters below 3 mu m are reached within minutes and are predominantly observed close to the panel surface in contact with air. Effective fiber protection is achieved by flame retardants acting beyond 600 degrees C, forming thermally resistant layers such as zinc borate. A new field of research is opened identifying flame retardants, which protect carbon fibers in carbon fiber reinforced plastic.
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