首页> 外国专利> PREFORMED FOR STRENGTHENING A COMPOSITE STRUCTURE, THREE-DIMENSIONAL COMPOSITE STRUCTURE REINFORCED WITH A PREFORM, A PRE-SHAPED MANUFACTURING METHOD FOR STRENGTHENING A COMPOSITE STRUCTURE AND METHOD FOR MANUFACTURING A COMPREHENSIVE THREE-DIMENSIONAL STRUCTURE

PREFORMED FOR STRENGTHENING A COMPOSITE STRUCTURE, THREE-DIMENSIONAL COMPOSITE STRUCTURE REINFORCED WITH A PREFORM, A PRE-SHAPED MANUFACTURING METHOD FOR STRENGTHENING A COMPOSITE STRUCTURE AND METHOD FOR MANUFACTURING A COMPREHENSIVE THREE-DIMENSIONAL STRUCTURE

机译:为加强复合结构而预成型,由预成型件加强的三维复合结构,用于加强复合结构的预成形制造方法以及用于制造综合三维结构的方法

摘要

Pre -form used to reinforce a composite structure, enhanced three -dimensional composite structure with a pre -shape, method of manufacture of a pre -shape used to reinforce a composite 5 structure and method of manufacturing a three -dimensional composite structure at this time This relates to multidirectionally reinforced fibre preforms that easily fit complex curvatures, such a s composites of turbine blades, jet engine restraint rings, aircraft fuselage frames,Aircraft window frames and flanked rings to attach nacelle (barstools) to aircraft engines. The present invention provides multidirely enhanced preforms woven with improved resistance to composite structures that are axissimetric in nature as well as non -axissimetric. The invention is a pre -form used to reinforce a composite (matching) structure that includes a part of intertwined contour fabric, Bi -axially woven,Triaxially woven or part of bias fabric and /or a part of bias entertained fabric and a method of doing the same. The pre -form may optionally include a three -dimensional woven part. The combination of different tissue forms allows the pre -form to be produced without cutting and suturing the individual folds. The elimination of these cuts and sutures improves the resistance and performance of the resulting structure.
机译:此时用于增强复合结构的预成型件,具有预成型形状的增强型三维复合结构,用于增强复合材料5结构的预成型件的制造方法以及此时制造三维复合结构的方法这涉及容易适应复杂曲率的多向增强纤维预成型件,例如涡轮叶片,喷气发动机约束环,飞机机身框架,飞机窗框和侧翼环的复合物,以将机舱(脚凳)连接到飞机发动机。本发明提供了经多向增强的预成型件,该预成型件具有对复合结构的抵抗力,该复合结构本质上是轴对称的以及非轴对称的。本发明是用于增强复合(匹配)结构的预成型件,该预成型件包括交织的轮廓织物,双轴编织,三轴编织的一部分或斜交织物的一部分和/或斜交娱乐织物的一部分,以及做同样的事情。该预成型件可任选地包括三维机织部分。不同组织形式的组合允许在不切割和缝合单个折叠的情况下生产预成型件。消除这些切口和缝合线可提高所得结构的抵抗力和性能。

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