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Describes the development of a low‐cost tooling system for the manufacture of composite aircraft parts. The ability to withstand a high temperature autoclave process and provide a…
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Describes the development of a low‐cost tooling system for the manufacture of composite aircraft parts. The ability to withstand a high temperature autoclave process and provide a high tolerance life expectancy in excess of ten prototype units were key factors in the development of the system. The process uses a syntactic epoxy moulded over an aluminium core to form the tool.
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