发明名称 CORE FOR PRODUCING AN FIBER REINFORCED COMPOSITE PART
摘要 <p>The method involves producing removable cores (26-29) into core molds, and applying bar-preforms (30-32) formed with reinforcing carbon fibers on the cores for forming reinforcing elements and arranging the cores at a common structure (23). The cores are supplied with web-like semi-finished products for creating an external shell (33). The common structure is inserted into a closed molding tool and filtered with hardenable plastic material. A fiber composite part is hardened by utilizing pressure and/or temperature, and the cores are removed. An independent claim is also included for a core mold for executing a method for producing an integral fiber composite part.</p>
申请公布号 EP2254749(A1) 申请公布日期 2010.12.01
申请号 EP20090720371 申请日期 2009.02.12
申请人 AIRBUS OPERATIONS GMBH 发明人 ENDER, TOBIAS
分类号 B29C70/48;B29C33/00;B29C33/52;B29C33/76 主分类号 B29C70/48
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