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Construction of Aerospace Bracket Manufactured from Short-Reinforced Composite

机译:用短增强复合材料制造的航空航天支架的构造

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The article describes the question of the production of aerospace bracket from short-reinforced composite material by injection molding. A technique for constructing structured computational meshes for modeling the molding of ultra-viscous multiphase anisotropic environments containing short high-strength fibers in the Moldex3D using the joint use of the ANSYS Meshing and Rhinoceros was developed. The article describes the research of influence of the shape, dimensions, location of the runner system and parameters of the molding of spatial brackets from short-reinforced composites on the manufacturing quality of aerospace structures. The calculation results allowed to design and manufacture the tool for molding bracket. Five brackets were manufactured of UPA 6 20M and five brackets of UPA 30M by an injection-molding machine the Negri Bossi VE210-1700. Tests manufactured brackets confirm the calculations of the melt front, the location of the weld lines and orientation of reinforcing fibers.
机译:该文章描述了由短增强复合材料通过注塑成型生产航空航天支架的问题。开发了一种用于构造结构化计算网格的技术,该技术使用ANSYS Meshing和Rhinoceros的联合使用,在Moldex3D中对包含短高强度纤维的超粘多相各向异性环境的成型进行建模。本文描述了短强化复合材料的形状,尺寸,流道系统的位置以及空间支架成型参数对航空航天结构制造质量的影响的研究。计算结果允许设计和制造用于模制托架的工具。用注塑机Negri Bossi VE210-1700制造了5个UPA 6 20M支架和5个UPA 30M支架。通过测试制造的支架,可以确定熔体前沿,熔合线位置和增强纤维方向的计算结果。

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