Lay-up arrangement and structural arrangement and method for producing a component for aerospace
A structural and structural technology, applied in the field of laminated structures, can solve problems such as time-consuming, high production costs, and positioning errors, and achieve the effects of easy positioning accuracy, cost savings, and cost advantages
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[0041] figure 1 The laminated structure 1 according to the first exemplary embodiment of the present invention is shown in a perspective view.
[0042] The laminated structure 1 is provided in the form of a bundle 3 coiled around a mandrel 2 . The fabric-like end that has been unfolded is indicated with reference numeral 4 . The broken lines schematically show the fiber directions of the glass fibers 5 in the laminated structure 1 . Preferably, the glass fibers 5 extend in the unfolding direction, ie along the fabric-like end 4 .
[0043] figure 2 display edge figure 1 Sectional view of the section line I-I in.
[0044] Preferably, the laminated structure 1 comprises a backing layer 6 , a glass fiber laminate 8 and a protective film 9 . Preferably, the backing layer 6 is designed in the form of a paper layer. Arranged on top of the backing layer is a glass fiber layer 5 extending perpendicular to the cross-sectional plane. Located between the glass fibers 5 is a resin...
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