发明名称 SYSTEM AND METHOD OF MANUFACTURING COMPOSITE MODULES
摘要 PROBLEM TO BE SOLVED: To provide a new system and method of manufacturing modules from a fiber-reinforced composite material for an aircraft or spacecraft which may enable a faster and/or more automated production procedure.SOLUTION: A system 1 includes: a form core assembly station to constitute at least one stiffening element of the integrated stiffening structure; a form core placement station 6 which receives assembled form cores from the assembly station for placing or depositing the form cores in or on a molding tool; and a turning station 9 for rotating or inverting the assembled form cores. The turning station 9 is configured to convey or transport the assembled form cores from the assembly station to the placement station 6. The turning station 9 defines a path I which is configured to rotate or invert the form cores as they are conveyed or moved to the placement station 6.
申请公布号 JP2015086074(A) 申请公布日期 2015.05.07
申请号 JP20140219551 申请日期 2014.10.28
申请人 AIRBUS OPERATION GMBH 发明人 ALEXANDER ENGELS;PIERRE ZAHLEN;LARS MEYER
分类号 B65G47/252;B23P21/00;B64C1/12;B64F5/00;B65G7/08 主分类号 B65G47/252
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