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首页> 外文期刊>SAMPE Journal >Evolution in Composite Injection Moulding Processes for Wing Control Surfaces
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Evolution in Composite Injection Moulding Processes for Wing Control Surfaces

机译:机翼操纵面复合注射成型工艺的发展

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摘要

Since 2010, Sonaca is engaged in R&D projects, with the support of Radius Engineering and Coexpair, aiming to design, develop, manufacture and test monolithic CFRP flap structures made from the conventional 8552 resin prepreg system and the newest SQRTM process ('Same Qualified Resin Transfer Moulding) in order to assess several additional benefits of this process over the conventional RTM process, amongst which the use of already qualified tough prepreg materials and the ease combination with automatic deposition and preforming techniques of UD-tapes. Following advantages were also considered during the initial trade-off analysis for the technology selection of such wing control surface structure having very stringent requirements in terms of structural performance, weight optimisation, aerodynamic quality and cost:
机译:自2010年以来,Sonaca在Radius Engineering和Coexpair的支持下从事研发项目,旨在设计,开发,制造和测试由传统的8552树脂预浸料系统和最新的SQRTM工艺制成的整体CFRP翻板结构(“合格树脂”)。为了评估该工艺相对于传统RTM工艺的其他优点,其中包括使用已经合格的高强度预浸料,以及与UD胶带的自动沉积和预成型技术的轻松组合。在最初的权衡分析中,还考虑了以下优势,这些机翼控制表面结构的技术选择在结构性能,重量优化,空气动力学质量和成本方面有非常严格的要求:

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