A shell segment of an aircraft and a production method
Shell segment (1), and method to produce it, in particular for an aircraft, having a skin field (2) and a stiffening structure (4) for purposes of stiffening the skin field (2), wherein the skin field (2) and the stiffening structure (4) are made from fibre-reinforced plastic materials, and wherein...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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Zusammenfassung: | Shell segment (1), and method to produce it, in particular for an aircraft, having a skin field (2) and a stiffening structure (4) for purposes of stiffening the skin field (2), wherein the skin field (2) and the stiffening structure (4) are made from fibre-reinforced plastic materials, and wherein the stiffening structure (4)is bonded to an inner surface (6) of the skin field (2) and comprises a multiplicity of first stiffeners (8) and a multiplicity of mounts (12) which are formed integrally with the first stiffeners (8) and which extend in the transverse of the first stiffeners (8) for the connection of second stiffeners to form an integral lattice structure, wherein a multiplicity of reinforcement elements (28, 36) for fixing the mounts (12) mechanically to the skin field (2), each reinforcement element (28, 36) has a connection section (30, 40) and a blocking section (32, 38) having an extension in a direction inclined to the connection section (30, 40), the connection section (30, 40) penetrates the skin field (2) and the mounts (12), and the blocking section (32, 38) is in contact with an outer surface of the skin field (2). |
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