发明名称 Laminated composite radius filler with geometric shaped filler element and method of forming the same
摘要 LAMINATED COMPOSITE RADIUS FILLER WITH GEOMETRIC SHAPED FILLER ELEMENT AND METHOD OF FORMING THE SAME A laminated composite radius filler (70) for a composite structure (28) has a stacked ply assembly (108) having a plurality of stacks (110) of laminate radius filler plies (1 10a, 1 Ob, 1 Oc, 1 Od) cut to a desired width (132) and having a desired ply orientation (134). The laminated composite radius filler (70) further has a geometric shaped filler element (100) positioned at a desired location (120) on a first portion (108a) of the stacked ply assembly (108). The geometric shaped filler element (100) deforms a second portion (108b) of the stacked ply assembly (108) stacked over the geometric shaped filler element (100), such that the laminate radius filler plies (1 Ob, 1 Oc, 1 Od) of the second portion (108b) of the stacked ply assembly (108) change direction and have a component of direction (116) including a horizontal direction (1 18a) and a vertical direction (118b). The laminated composite radius filler (70) having a shape substantially corresponding to a radius filler region (72) of the composite structure (28). CIO= coc 0 o N
申请公布号 AU2014203585(A1) 申请公布日期 2015.05.21
申请号 AU20140203585 申请日期 2014.06.30
申请人 THE BOEING COMPANY 发明人 KAJITA, KIRK B.;FRISCH, DOUGLAS A.
分类号 B32B5/12;B32B37/02;B64C1/12;B64C3/20 主分类号 B32B5/12
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