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Out-of-Autoclave Manufacturing of Aerospace Representative Parts.

机译:航空航天代表性零件的高压灭菌器制造。

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摘要

The use of carbon fibre reinforced composites for aerospace structures has seen a high increase in recent years, and is still growing. The high stiffness-to-weight ratio of these materials makes them ideal for primary structures on airplanes, satellites, and spacecrafts. Nevertheless, the manufacturing of composites remains very costly since it requires equipment investment such as an autoclave, and very qualified workers. Out-of-autoclave manufacturing technology is very promising since it only requires a traditional oven, while still aiming at similar part quality. However, the absence of positive pressure compared with an autoclave makes it more difficult to achieve low porosity parts.;This research investigates the manufacturing of complex features with out-of autoclave prepreg technology. The features studied are tight-radius corners with a curvature change, and ply drop-offs. Ply drop-offs tests were conducted to identify if porosity is higher at ply terminations. In corners, the bagging arrangement was modified to achieve the most uniform thickness in areas of curvature change, even with small radii. The conclusions from these studies provided us with guidelines to manufacture larger representative parts, which included these features. The representative parts were tested for porosity, thickness uniformity, mechanical performance, and glass transition temperature (Tg). A total of four representative parts were manufactured with out-of-autoclave technology, and one more was manufactured with an autoclave to allow for a proper comparison between the two processes. The materials used were MTM45-1 5 harness satin and CYCOM5320 plain weave for the out-of-autoclave parts, and CYCOM5276-1 plain weave for the autoclave part. The effect of ply drop-offs on porosity was found to be negligible. Thickness deviation in corners was attributed to a combination of consumable bridging, prepreg's bulk factor and inter-ply shear. Overall, out-of-autoclave prepregs showed performance similar to autoclave prepregs.
机译:近年来,碳纤维增强复合材料在航空航天结构中的使用已大大增加,并且仍在不断增长。这些材料的高刚度/重量比使其非常适合飞机,卫星和航天器的主要结构。然而,复合材料的制造仍然非常昂贵,因为它需要高压釜等设备投资以及非常合格的工人。高压灭菌器制造技术非常有前途,因为它仅需要传统的烤箱,同时仍致力于达到相似的零件质量。然而,与高压釜相比,由于没有正压,因此很难获得低孔隙率的零件。该研究调查了采用高压釜预浸料技术制造复杂特征的情况。研究的特征是具有曲率变化的紧密半径拐角和帘布层脱落。进行了层脱落测试,以确定在层末端处的孔隙率是否更高。在拐角处,对套袋布置进行了修改,即使在半径较小的情况下,也可以在曲率变化区域获得最均匀的厚度。这些研究的结论为我们提供了制造包括这些特征的较大代表性零件的指南。测试了代表性零件的孔隙率,厚度均匀性,机械性能和玻璃化转变温度(Tg)。总共用高压釜技术制造了四个有代表性的零件,并用高压釜制造了另外四个零件,以便对这两个过程进行适当的比较。所用的材料是MTM45-1 5线束缎和CYCOM5320平纹用于高压灭菌器零件,以及CYCOM5276-1平纹用于高压灭菌器零件。发现层脱落对孔隙率的影响可以忽略不计。拐角处的厚度偏差归因于消耗性桥接,预浸料的体积系数和层间剪切的组合。总体而言,高压灭菌预浸料的性能与高压灭菌预浸料相似。

著录项

  • 作者

    Cauberghs, Julien.;

  • 作者单位

    McGill University (Canada).;

  • 授予单位 McGill University (Canada).;
  • 学科 Engineering Aerospace.;Engineering Materials Science.
  • 学位 M.Eng.
  • 年度 2012
  • 页码 105 p.
  • 总页数 105
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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