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Thermoplastic tape placement process - in situ consolidation is reachable

机译:热塑性胶带的放置过程-可以原位固结

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摘要

The aerospace industry is looking for highly efficient and fully automated processes to manufacture large structural components. Placement processes are fulfilling these requirements. Furthermore, they allow to lay up the structure with the highest degree of fibre orientation and well defined fibre position. Already in service are thermoset tape based placement processes. Main disadvantage is the need to have a consolidation process after structure lay-up has finished. Additionally, the required autoclave limits the component size. The thermoplastic tape placement process offers new possibilities. Fully impregnated fibre reinforced thermoplastic tapes are laid onto a mould to build up curved or flat structures step by step. Each tape is melted by a heat source, welded to the layer below, compressed by e.g. a roller, and cooled down below melting temperature. If this is done properly, an in situ consolidation can be achieved, which means no additional consolidation process is needed. The paper is giving an overview about thermoplastic tape placement process and elaborates the requirements to reach in situ consolidation.
机译:航空航天工业正在寻找高效且全自动的工艺来制造大型结构部件。安置过程正在满足这些要求。此外,它们允许以最高程度的纤维取向和良好定义的纤维位置铺放结构。基于热固性胶带的贴装工艺已经投入使用。主要缺点是在结构布局完成后需要进行合并过程。此外,所需的高压釜会限制组件的尺寸。热塑性胶带的放置过程提供了新的可能性。将完全浸渍的纤维增强热塑性胶带铺设在模具上,以逐步形成弯曲或平坦的结构。每个带通过热源熔化,焊接到下面的层,通过例如热压缩。辊,并冷却至低于熔化温度。如果正确执行此操作,则可以实现原位合并,这意味着不需要其他合并过程。本文概述了热塑性胶带的放置过程,并详细说明了实现现场固结的要求。

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