Numerical Optimization of Vacuum Assisted Manufacturing of Aircraft Composite Parts Using the Predictive Assessment of Objectives

S. Shevtsov, I. Zhilyaev, Jyun-Ping Huang, N. Snezhina
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Abstract

The vacuum assisted technologies of composite parts manufacturing are becoming very popular owing to their relative simplicity and inexpensive equipment. They are implemented in the production of aircrafts, rotorcrafts, ships, cars and wind turbine blades. Unfortunately, in many cases this technology does not provide sufficient repeatability and quality due to very high process sensitivity to its layout (number, dimensions and positions of the resin gates and vacuum vents) and the temperature. Due to the fact that process testing is very expensive and time-consuming, the use of vacuum infusion process simulation is relevant. Such modeling tools must be able to correctly predict resin spreading in the preform and identify potential defects. In contrast to the well-known software tools, we propose to use the phase field equation as the leading one and providing a more accurate reconstruction of the front of the moving resin. To describe the pressure distribution in an incompletely saturated porous preform, we use the Richards equation, and the state of the moving resin is modeled by the convection-diffusion equation with a source controlled by the autocatalytic equation. The formulation of a forward coupled modeling problem also includes modified relationships for the dependence of the resin viscosity on the degree of cure and temperature, as well as for the diffusion coefficient of the degree of cure when mixing streams of liquid resin. The article presents the results of modeling the vacuum infusion of a 3D preform at varying positions of the vacuum vent, high-permeability medium (HPM) tape and temperature. It is shown that the indicators of the quality and performance of the process at the moment of stopping of the resin spreading due to beginning of its gelation can be predicted at an early stage of simulation, which is very important for using the developed CAE model for the process optimization. The validity and reliability of such predictive estimate using the objectives and their combination, which are determined at an early stage of simulation, are discussed.
基于目标预测评估的飞机复合材料零件真空辅助制造数值优化
真空辅助复合材料零件制造技术由于其相对简单和廉价的设备而变得非常流行。它们被应用于飞机、旋翼飞机、船舶、汽车和风力涡轮机叶片的生产中。不幸的是,在许多情况下,由于对其布局(树脂浇口和真空通风口的数量、尺寸和位置)和温度的非常高的工艺敏感性,该技术不能提供足够的可重复性和质量。由于工艺测试是非常昂贵和耗时的,使用真空输液过程模拟是相关的。这种建模工具必须能够正确预测树脂在预成型中的扩散,并识别潜在的缺陷。与已知的软件工具相比,我们建议使用相场方程作为主导方程,并提供更准确的移动树脂前部重建。为了描述不完全饱和多孔预制件中的压力分布,我们使用Richards方程,并且用自催化方程控制源的对流扩散方程来模拟树脂的运动状态。前向耦合建模问题的公式还包括树脂粘度对固化程度和温度的依赖关系的修正关系,以及混合液体树脂流时固化程度的扩散系数。本文介绍了三维预制体在不同真空出口位置、高磁导率介质(HPM)带和温度下的真空注入建模结果。结果表明,在模拟的早期阶段,可以预测树脂开始凝胶化而停止扩散时刻的工艺质量和性能指标,这对利用所建立的CAE模型进行工艺优化具有重要意义。讨论了在仿真初期确定的目标及其组合的预测估计的有效性和可靠性。
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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