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Void Entrapment into Air Pathways in Partially Impregnated Prepregs in the Out-of-Autoclave Process

机译:在室外浸渍的预浸料坯中的空气途径中的空气途径在室外灭弧过程中

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Out-of-Autoclave (OOA) thermoset prepreg manufacturing of aerospace quality parts is performed under low pressures, which makes it more susceptible to void formation and growth as compared to high pressure autoclave processing. Thus, OOA prepregs are intentionally partially impregnated with resin, with the goal to distribute the resin such that a completely connected network of empty channels is formed in the initial material. This network serves as pathways for evacuation of gases entrapped in the laminate before consolidation and cure. This work investigates how mechanically entrapped air can be removed from partially impregnated OOA prepreg laminates before oven curing. First, a model of void evacuation time is derived to estimate the time necessary to apply vacuum to remove air from within the laminate before placing it in the oven. Next, a flow visualization technique is presented where the resin film of the partially impregnated OOA prepreg is pressed into the fabric, while recording the resin flow on the dry side. This quantifies the degree of resin impregnation with processing time. A relationship between degree of resin impregnation and gas permeability is presented which influences the evacuation time necessary to remove air from the system. A large panel (~1.2m long) was fabricated in which low and high evacuation times were employed based on the model physics. The void content was quantified along the length via sectioning/polishing/image analysis and shown to have a void content of ~1%. The results of this study should prove useful to develop optimal vacuum application times and temperature and pressure cycles for void reduction and removal during processing of prepregs.The entrapment of voids is one of the most significant challenges of composites processing; a small percentage of voids will degrade mechanical properties by 10-15% [1]. The aerospace industry is motivated to replace aluminum and titanium structures with composites because of the additional weight benefits; however, composite structures of less than 1% void content are difficult to achieve outside the autoclave processing method. The elevated atmospheric pressure inside the autoclave compacts prepreg laminates to high fiber volume fraction and reduces void size. The drawback is that the autoclave process has high capital costs, which become prohibitively exorbitant as the size of the structure becomes larger. To counter these cost challenges, the Out-of-Autoclave (OOA) process is becoming attractive as it can process under vacuum pressure only in an oven to produce low void content large composite structures. OOA prepregs differ from autoclave prepregs in that resin only partially impregnates the fiber architecture - leaving dry, unimpregnated cross-sections to serve as ‘air pathways’ for removing air from the laminate, which if not removed will be entrapped between plies during cure and increase the void content in the composite. Additionally, any entrapped gases have a chance to migrate into air pathways during the application of vacuum, where they can be evacuated from the laminate easily. Some examples of partially impregnated prepregs are schematically shown in Figure 1. The initial architecture of these prepregs will play an important role in the formation of air and gas evacuation pathways which will influence the final void content in the fabricated composites by OAA process.The resin configuration has been shown to play an important role in air evacuation from partially impregnated prepreg laminates. Prepregs with low initial resin impregnation have less resistance to gas flow [2], making them suitable for evacuating gas from large structures. When fabricating sandwich structures with OOA prepregs, air pathways through the thickness have been shown to be highly beneficial for extracting air from the core [3,4]. This constraint makes UD prepregs (with no through thickness pathways) difficult t
机译:在低压下进行航空航天质量部件的高压釜(OOA)热固性预浸料制造,这使得与高压高压灭菌加工相比,使其更容易存在空隙形成和生长。因此,OOA预浸料具是有意地部分地用树脂浸渍,其目的是分配树脂,使得在初始材料中形成完全连接的空通道网络。该网络充当途径,用于在固结和固化前捕获层压板中捕获的气体的途径。该工作调查了在烘箱固化之前可以从部分浸渍的OOA预浸料层压物中取出机械捕获的空气。首先,推导出空隙疏散时间的模型,以估计在将其在烘箱中放置之前施加真空以从层压板中除去空气所需的时间。接下来,提出了一种流动可视化技术,其中将部分浸渍的OOA预浸料坯的树脂膜压入织物中,同时记录干侧的树脂流动。这量化了使用加工时间的树脂浸渍程度。提出了树脂浸渍程度和透气性之间的关系,其影响从系统中除去空气所需的抽空时间。制造了大面板(〜1.2米长),其中基于模型物理学采用低疏散时间。通过截面/抛光/图像分析沿长度量化空隙含量,并显示出具有〜1%的空隙含量。该研究的结果应证明是有用的,可用于开发最佳的真空施用时间和温度和压力循环,以便在预浸料的加工过程中减少和去除。空隙的扣留是复合材料加工的最重要挑战之一;小百分比的空隙将通过10-15%降低机械性能[1]。由于额外的重量效益,航空航天工业有动力用复合材料取代铝和钛结构;然而,难以在高压釜处理方法外部难以实现少于1%空隙含量的复合结构。高压釜压块内部的大气压升高,Preprege层压物到高纤维体积分数并降低空隙尺寸。缺点是高压灭菌过程具有高资本成本,因为结构的大小变大,这变得过高。为了抵消这些成本挑战,自动灭菌(OOA)过程变得具有吸引力,因为它只能在真空压力下处理,仅在烘箱中产生低空隙含量大的复合结构。 OOA预浸料不同于该树脂的高压釜预浸料,仅部分地浸渍纤维架构 - 离开干燥的未浸渍的横截面,以用作从层压板中除去空气的“空气途径”,如果未移除,那么如果未移除,则在固化过程中夹在层之间并增加复合材料中的空隙内容。另外,任何捕获的气体都有机会在施加真空期间迁移到空气途径中,在那里它们可以容易地从层压板抽空。部分浸渍的预浸料坯的一些示例在图1中示意性地示出。这些预浸料坯的初始架构将在形成空气和气体抽空途径中发挥重要作用,这将通过OAA方法影响制造的复合材料中的最终空隙含量。树脂已经显示出在部分浸渍的预浸料层压物中发挥着一种重要作用。具有低初始树脂浸渍的预浸料坯对气体流动的耐抗性较低,使得它们适合于从大结构中抽出气体。当用OOA预浸料坯制造夹层结构时,通过厚度的空气途径已经显示为从芯中提取空气的高有益,[3,4]。该约束使UD预浸料(没有通过厚度途径)困难

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