首页> 外文会议>SAMPE Conference;Society for the Advancement of Material and Process Engineering >DESIGN OF AN AUTOMATED ULTRASONIC SCANNING SYSTEM FOR IN-SITU COMPOSITE CURE MONITORING AND DEFECT DETECTION
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DESIGN OF AN AUTOMATED ULTRASONIC SCANNING SYSTEM FOR IN-SITU COMPOSITE CURE MONITORING AND DEFECT DETECTION

机译:原位复合固化监测与缺陷自动超声扫描系统设计

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The preliminary design and development of an automated ultrasonic scanning system for in-situ composite cure monitoring and defect detection in the high temperature environment of an oven was completed. This preliminary design is a stepping stone to deployment in the high temperature and high pressure environment of an autoclave, the primary cure method of aerospace grade thermoset composites. Cure monitoring with real-time defect detection during the process could determine when defects form and how they move. In addition, real-time defect detection during cure could assist validating physics-based process models for predicting defects at all stages of the cure cycle. A physics-based process model for predicting porosity and fiber waviness originating during cure is currently under development by the NASA Advanced Composites Project (ACP).For the design, an ultrasonic contact scanner is enclosed in an insulating box that is placed inside an oven during cure. Throughout the cure cycle, the box is nitrogen-cooled to approximately room temperature to maintain a standard operating environment for the scanner. The composite part is mounted on the outside of the box in a vacuum bag on the build/tool plate. The build plate is attached to the bottom surface of the box. The scanner inspects the composite panel through the build plate, tracking the movement of defects introduced during layup and searching for new defects that may form during cure. The focus of this paper is the evaluation and selection of the build plate material and thickness. The selection was based on the required operating temperature of the scanner, the cure temperature of the composite material, thermal conductivity models of the candidate build plates, and a series of ultrasonic attenuation tests. This analysis led to the determination that a 63.5 mm thick build plate of borosilicate glass would be utilized for the system. The borosilicate glass plate was selected as the build plate material due to the low ultrasonic attenuation it demonstrated, its ability to efficiently insulate the scanner while supporting an elevated temperature on the part side of the plate, and the availability of a 63.5 mm thick plate without the need for lamination.
机译:完成了自动超声扫描系统的初步设计和开发,该系统用于在烤箱的高温环境中进行原位复合材料固化监测和缺陷检测。该初步设计是部署在高压灭菌器的高温和高压环境中的垫脚石,高压灭菌器是航空级热固性复合材料的主要固化方法。在过程中使用实时缺陷检测进行固化监控可以确定缺陷何时形成以及如何移动。此外,在固化过程中的实时缺陷检测可以帮助验证基于物理的过程模型,以预测固化周期所有阶段的缺陷。 NASA高级复合材料项目(ACP)目前正在开发一种基于物理的过程模型,用于预测固化过程中产生的孔隙率和纤维波纹度。 对于设计,超声波接触式扫描仪被封闭在一个绝缘盒中,该绝缘盒在固化过程中被放置在烤箱内。在整个固化周期中,将盒子氮气冷却至大约室温,以保持扫描仪的标准操作环境。复合部件安装在机箱的外部,该机箱位于构建/工具板上的真空袋中。盖板固定在盒子的底面上。扫描仪通过构建板检查复合板,跟踪在铺网过程中引入的缺陷的运动,并寻找在固化过程中可能形成的新缺陷。本文的重点是对底板材料和厚度的评估和选择。选择的依据是扫描仪所需的工作温度,复合材料的固化温度,候选构建板的导热系数模型以及一系列超声衰减测试。该分析导致确定该系统将使用63.5 mm厚的硼硅酸盐玻璃构建板。硼硅酸盐玻璃板之所以被选作构建板材料,是因为它显示出低的超声衰减,能够有效隔离扫描仪,同时在板的部分侧面上支持高温的能力以及可获得的63.5 mm厚的板而没有这种材料。需要层压。

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