Autoclave curing has historically been utilised in the production of composite aerospace and aircraft components to achieve the necessary fibre content (resin-to-fiber ratio) and the absence of resin voids to make light weight and strong components. This is accomplished by vacuum-sealing the component in an autoclave before pressurising it during the hot cure cycle. To reduce resin voids and obtain the desired resin/fiber ratio, the part is subjected to high pressure within a pressurised autoclave. Visit website to learn more on autoclave composites. Prepregs are composite materials made by pre-impregnating a reinforcement fibre with a thermoplastic or thermoset resin matrix in a specific ratio. Due of the tremendous temperatures and pressures used to cure them, pregnancies have special characteristics. Browse website to know more on prepreg composites.
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