发明名称 NANO-REINFORCED RADIUS FILLER FOR AN AIRCRAFT STRUCTURE AND A METHOD OF PRODUCING AN AIRCRAFT STRUCTURE COMPRISING SUCH FILLER
摘要 The present invention relates to a composite radius filler for use in an aircraft structure (2), which comprises structural composite parts (7) assembled together to form the aircraft structure (2). The composite radius filler (3) is arranged between rounded sections (5', 5") of the structural composite parts (7) for filling a gap (4) formed between the structural composite parts (7). The composite radius filler (3) is made structural by a nanostructure (23) arranged within the composite radius filler (3) for the reinforcement of the interface between the radius filler (3) and the structural composite part (7). The invention also relates to a method for producing an aircraft structure comprising said nano-reinforced radius filler.
申请公布号 CA2765138(A1) 申请公布日期 2010.12.16
申请号 CA20092765138 申请日期 2009.06.11
申请人 SAAB AB 发明人 HALLANDER, PER;PETERSSON, MIKAEL;WEIDMANN, BJOERN;GRANKAELL, TOMMY;STRINDBERG, GOETE;NORDIN, PONTUS
分类号 B29C70/14;B29C65/00;B64C1/06 主分类号 B29C70/14
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