DFEM在氧化-氧化陶瓷基复合材料烧结变形分析中的应用:数字孪生

Baber Saleem, Ran He, Peter Polak, James Lander, Ian M. Edmonds, Xiaoxia Yu, Jingzhe Pan
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引用次数: 0

摘要

由于高温环境的影响,对陶瓷零件的烧结性能进行校准是费时且昂贵的。基于密度的有限元法(DFEM)用于计算陶瓷零件的烧结变形,而不需要详细了解其本构规律(如粘度和烧结势)。鉴于这一优势,本研究提出了DFEM在由氧化物-氧化物陶瓷基复合材料(Ox-Ox CMCs)制成的全尺寸隔热板(FSHS)中预测和减轻烧结变形的应用。DFEM用于开发数字孪生,该数字孪生可以准确识别容易变形的几何区域,并量化实验测量和有限元预测之间的偏差。通过应用边界条件来评估抑制策略,显示目标区域的失真显著减少。研究结果强调DFEM是一种近似但计算效率高的方法,能够消除对大量材料表征的需要,例如纤维取向、层数、基体成分和烧结剖面。相反,这些信息固有地反映在测量的烧结变形中,包括变形。该研究为进一步研究解决变形原因和优化烧结工艺以提高航空航天应用的可制造性奠定了基础。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

Application of DFEM in Sintering Distortion Analysis of Oxide–Oxide Ceramic Matrix Composite: Digital Twin

Application of DFEM in Sintering Distortion Analysis of Oxide–Oxide Ceramic Matrix Composite: Digital Twin

Application of DFEM in Sintering Distortion Analysis of Oxide–Oxide Ceramic Matrix Composite: Digital Twin

Application of DFEM in Sintering Distortion Analysis of Oxide–Oxide Ceramic Matrix Composite: Digital Twin

Application of DFEM in Sintering Distortion Analysis of Oxide–Oxide Ceramic Matrix Composite: Digital Twin

It is time-consuming and expensive to calibrate the sintering behavior of a ceramic part because of the elevated temperature environment. A Densification-Based Finite Element Method (DFEM) was developed for calculating the sintering distortion of ceramic parts without detailed knowledge of their constitutive law (such as viscosities and sintering potential). Given this advantage, this study presents the application of a DFEM for predicting and mitigating sintering distortion in a Full-Scale Heat Shield (FSHS) made of oxide–oxide ceramic matrix composites (Ox-Ox CMCs). DFEM was used to develop a digital twin that accurately identified geometric regions prone to distortion and quantified deviations between experimental measurements and finite element predictions. Suppression strategies were evaluated by applying boundary conditions, demonstrating a significant reduction in distortion in targeted regions. The findings highlight DFEM as an approximate yet computationally efficient approach, capable of eliminating the need for extensive material characterization, such as fiber orientations, ply numbers, matrix compositions, and sintering profiles. Instead, this information is inherently reflected in the measured sintering deformation, including distortion. This study establishes a foundation for further research into addressing distortion causes and optimizing sintering processes for improved manufacturability in aerospace applications.

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