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Peel Ply and Grinding for CFRP Adhesive Bonding - a never ending Story in Aerospace?

机译:Peel Ply和磨削CFRP粘合剂粘合 - 航空航天中永无止境的故事?

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After more than 30 years in aerospace manual grinding of CFRP laminate surfaces after peel ply removal is still state-of-the-art for adhesive bonding. Manual grinding is very difficult to control, particularly in case of shaped and curved parts, is very time consuming and creates a lot of grinding dust in the bond shop. With the upcoming introduction of automated adhesive bonding processes alternative surface treatment processes are needed to keep a high, reproducible quality standard. Treatments like automated grit blasting have been developed [2] and promising alternatives like pre-impregnated peel plies [4,8,9], laser treatments [6] ultrasonic agitation [7], corona and atmospheric plasma methods are under investigation. The focus of this paper concentrates on the characterization of different peel ply fabrics and ply fabric treatments (release agents) as well as on the investigation of corona and atmospheric plasma treatment as alternatives for CFRP grinding. The quantity of peel plies for aerospace applications is increasing. Nevertheless peel plies are only a minor market for filament producers and for the industrial weavers. Currently it is not state-of-the-art in aerospace to qualify and purchase peel plies in the same manner as it is done for structural materials like pregregs and adhesives. Physical / chemical methods (e.g. IR, DSC, TGA, XPS) have been applied to characterize peel plies and release coatings. These methods can be adopted in material qualification of peel plies. The efficiency of corona and atmospheric plasma treatment was tested on a CFRP surface after removal of two different PA peel plies. Corona is restricted to flat parts and exhibited good bonding results only for one peel ply, which was coated with a hydrocarbon based release agent. Atmospheric plasma performed excellent for the examined peel plies, even when a siloxane release coating was on the peel ply. Further, the application on CFRP showed a very time stable activity of the plasma treatment on the CFRP surface before bonding and reproducible mechanical bonding performance after bonding.
机译:在Peel Ply去除后,在航空航天手工制作CFRP层压表面的手动研磨后,粘合剂粘合仍然是最先进的。手动磨削非常难以控制,特别是在成形和弯曲部件的情况下,非常耗时,在粘合店里创造了很多磨削灰尘。随着即将推出的自动粘合剂粘合工艺,需要替代的表面处理过程以保持高,可重复的质量标准。已经开发了自动砂砾喷射等处理[2],并且有前途的替代品如预浸渍的剥离层[4,8,9],激光处理[6]超声搅拌[7],电晕和大气等离子体方法都在调查。本文的重点浓缩了不同剥离织物和层织物处理(脱模剂)的表征,以及对CORON和大气等离子体处理的研究作为CFRP研磨的替代品。用于航空航天应用的剥离层数正在增加。然而,剥离层只有丝状生产者和工业编织者的轻微市场。目前,在航空航天中不是最先进的,以便以与Pregrogs和粘合剂等结构材料所做的相同方式获得剥离层。已经应用了物理/化学方法(例如IR,DSC,TGA,XPS),以表征剥离层和剥离涂层。这些方法可以采用剥离层的材料资格。在去除两种不同PA剥离层后,在CFRP表面上测试了电晕和大气等离子体处理的效率。电晕限制为平坦的部件,并且仅呈现一个剥离的粘合结果,其涂覆有烃基的脱模剂。即使硅氧烷释放涂层在剥离层上,也适用于检查剥离层的大气等离子体。此外,CFRP上的应用在粘接后粘接和可再现的机械键合性能之前,对CFRP表面的等离子体处理的施用非常稳定。

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