PROBLEM TO BE SOLVED: To provide a system and method for forming a composite filler.SOLUTION: A method comprises applying a pressure to a first portion of a composite material blank with a pair of forming dies of a composite filler forming apparatus, the pair of forming dies having a pair of convex radii, where each forming die of the pair of forming dies has a corresponding convex radius of the pair of convex radii. The method also comprises repeating the applying step to a subsequent portion of the composite material blank to incrementally form the composite material blank into a desired cross-section along its length.SELECTED DRAWING: Figure 3
【課題】複合充填材を成形するためのシステム及び方法を提供すること。【解決手段】方法は、複合充填材成形装置の一対の成形型を用いて複合材料素材の第1の部分に圧力を印加するステップであって、一対の成形型が一対の凸湾曲部を有し、一対の成形型の各成形型が一対の凸湾曲部のそれぞれの凸湾曲部を有する、印加するステップを含む。方法はまた、複合材料素材をその長さに沿って所望の断面に徐々に成形するために、複合材料素材の後続部分に対して印加するステップを繰り返す。【選択図】図3
COMPOSITE FILLER FORMING APPARATUS
複合充填材成形装置
2016-04-07
Patent
Electronic Resource
Japanese
IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
LAMINATED COMPOSITE RADIUS FILLER WITH GEOMETRIC SHAPED FILLER ELEMENT AND METHOD OF FORMING SAME
European Patent Office | 2019
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