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Optimizing Vacuum Assisted Resin Transfer Moulding (VARTM) Processing Parameters to Improve Part Quality.

机译:优化真空辅助树脂传递成型(VARTM)工艺参数以提高零件质量。

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摘要

The Low Cost Composites (LCC) group at Carleton University is studying out-of-autoclave composite manufacturing processes such as Vacuum Assisted Resin Transfer Moulding (VARTM) and Closed Cavity Bag Moulding (CCBM). These processes are used to produce inexpensive and high performance components for the GeoSurv II, an Unmanned Aerial Vehicle (UAV) being developed at Carleton University. This research has focused on optimizing VARTM processing parameters to reduce the weight and improve the strength and surface finish of GeoSurv II composite components.;An experimental study of the effects of the presence of a corner on composite thickness, void content, and strength was conducted. It was found that inside corners result in local increases in thickness and void content due to poor preform compaction. A novel bagging technique was developed to improve corner compaction, and this technique was shown to reduce thickness variability and void content. The strength, void content, and thickness variation were found to be heavily dependent on corner radius, with corner radii greater than 6.4 mm displaying the greatest improvement in performance for the layups considered. The design of the empennage and hatch mould incorporated the results of this study to improve the quality of these components.;A simulation was developed to model resin flow through in VARTM infusions and was used to simulate mould filling and resin emptying of the GeoSurv II inverted V-empennage and mission avionics hatch. The resin infusion schemes of these parts were designed to ensure full preform resin saturation, and minimize thickness variations.
机译:卡尔顿大学的低成本复合材料(LCC)小组正在研究高压灭菌的复合材料制造工艺,例如真空辅助树脂传递成型(VARTM)和密闭腔袋成型(CCBM)。这些工艺用于生产GeoSurv II的廉价,高性能组件,GeoSurv II是由卡尔顿大学开发的无人机(UAV)。这项研究的重点是优化VARTM工艺参数,以减轻重量并提高GeoSurv II复合材料组件的强度和表面光洁度。;进行了转角存在对复合材料厚度,空隙率和强度影响的实验研究。已经发现,由于不良的预型件压实,内角导致厚度和空隙含量的局部增加。已开发出一种新颖的装袋技术来改善边角压实,并且该技术已显示出可减少厚度变化和空隙含量。发现强度,空隙含量和厚度变化在很大程度上取决于拐角半径,拐角半径大于6.4 mm表现出所考虑的铺层的最大性能改进。尾盖和舱口模具的设计结合了这项研究的结果,以提高这些组件的质量。;开发了一个模拟模型,以模拟VARTM输注中树脂流经,并用于模拟GeoSurv II倒置模具的填充和树脂排空。 V型尾翼和任务航空电子舱口。这些部件的树脂注入方案旨在确保完全的瓶坯树脂饱和,并最大程度地减少厚度变化。

著录项

  • 作者

    Polowick, Christopher.;

  • 作者单位

    Carleton University (Canada).;

  • 授予单位 Carleton University (Canada).;
  • 学科 Engineering Aerospace.;Engineering Materials Science.;Engineering Mechanical.
  • 学位 M.A.Sc.
  • 年度 2013
  • 页码 164 p.
  • 总页数 164
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:40:49

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