METHOD AND ARRANGEMENT FOR PRODUCTION OF AN INTEGRAL HOLLOW-PROFILED COMPONENT WITH FIBRE COMPOSITE MATERIAL
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app pub date -
Feb 18, 2011
filing date -
Feb 19, 2010
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Abandoned
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Abstract
Method for production of an integral hollow-profiled component with fibre composite material comprising at least the following steps: a) providing at least one inner tool core, b) covering the at least one inner tool core with at least one layer of fibre composite material, c) curing the at least one layer of fibre composite material, and d) removing the at least one inner tool core. This makes it possible to produce particularly dimensionally accurate aircraft components, which have an integral hollow-profiled component with a tapering cross section and a plurality of longitudinally running stringers.
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