Design of an Automated Ultrasonic Scanning System for In-situ Composite Cure Monitoring and Defect Detection

T. Hudson, F. Palmieri, T. Abbott, Jeffrey P. Seebo, E. Burke
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引用次数: 3

Abstract

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.
复合材料原位固化监测与缺陷检测自动超声扫描系统的设计
完成了高温环境下复合材料原位固化监测与缺陷检测的超声自动扫描系统的初步设计与研制。该初步设计是在高压灭菌器的高温高压环境中部署的踏脚石,高压灭菌器是航空级热固性复合材料的主要固化方法。在过程中进行实时缺陷检测的缺陷监测可以确定缺陷何时形成以及它们如何移动。此外,在修复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,以预测修复周期所有阶段的缺陷。目前,NASA先进复合材料项目(ACP)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度和纤维波纹度。在设计中,超声波接触式扫描仪被封装在一个绝缘盒中,在固化过程中放置在烤箱内。在整个固化周期中,盒子被氮气冷却到大约室温,以保持扫描仪的标准操作环境。复合件装在构建/工具板上的真空袋中,安装在箱体外侧。构建板附着在箱体的底面上。扫描仪通过构建板检查复合板,跟踪在铺设过程中引入的缺陷的运动,并搜索在固化过程中可能形成的新缺陷。本文的研究重点是构建板的材料和厚度的评价和选择。根据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波衰减测试进行选择。这一分析导致确定63.5毫米厚的硼硅酸盐玻璃构建板将用于该系统。之所以选择硼硅玻璃板作为构建板材料,是因为它具有较低的超声波衰减,能够有效地隔离扫描仪,同时支持板部分侧的高温,并且可以使用63.5毫米厚的板而无需层压。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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