METHOD FOR MANUFACTURING A FIBRE COMPOSITE COMPONENT, FIBRE COMPOSITE COMPONENT, AND STRUCTURAL COMPONENT FOR AN AIRCRAFT OR SPACECRAFT
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United States of America Patent
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app pub date -
Sep 12, 2014
filing date -
Sep 16, 2013
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Abstract
A method for manufacturing a fibre composite component is disclosed. A single-piece foam body or the parts of a multi-part foam body having at least one recess which is open towards a first side of the foam body are prepared and positioned. A rigidifying element for the backing structure or a preform or first semi-finished product for forming the rigidifying element is arranged in the recess at least in portions. A skin portion or a second semi-finished product for forming the skin portion is provided, and brought into contact, in regions, with the foam body on the first side thereof and with the rigidifying element. The skin portion or second semi-finished product and the rigidifying element or preform or first semi-finished product in contact therewith are processed further in such a way that a fibre composite component is obtained in which the skin portion and the rigidifying element are interconnected.
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