基于单元微分法的编织陶瓷纤维绳封结构多物理场耦合分析

Yong-Tong Zheng, Xiaowei Gao, Sheng Liu, Yan-Jing Man, Kai Yang
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引用次数: 1

摘要

近年来,随着高超声速飞行器的快速发展,高温密封技术变得越来越重要。最近,一种编织陶瓷纤维的绳密封结构被设计用于高超音速飞行器。结构中的陶瓷纤维具有高温强度的特性,使密封结构适合在高温下工作。同时,当受到外力作用时,编织纤维可以在陶瓷界面处产生缓冲力,从而保持整个密封结构的良好性能。但到目前为止,对这种结构的研究还很少。本文提出了一种简化的热-力耦合模型来模拟这类结构复杂的物理过程。同时,由于单元微分法(EDM)在求解多物理场耦合问题方面具有很大的优势,因此采用了一种新的数值方法来计算耦合问题。并对密封结构在使用过程中的泄漏量进行了试验研究。最后,结合实验结果,建立了密封结构的一系列材料参数关系,验证了所提出的多物理场耦合模型的合理性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Multi-physics coupling analysis of rope-sealed structures with braided ceramic fibres by element differential method
With the rapid development of hypersonic vehicles in recent years, high-temperature seal technology has become more and more essential. Recently, a rope-sealed structure with braided ceramic fibres has been designed for hypersonic vehicles. The ceramic fibres in the structure have the characteristics of high temperature strength, so that they make the sealed structure suitable for working under a high temperature. Meanwhile, when subjected to an external force, braided fibres can produce a buffer force at the ceramic interface, so that it can maintain the good performance of the whole sealed structure. But up to now, only a few researches have been conducted on this kind of structures. In this paper, a simplified thermal–mechanical seepage coupling model is proposed to simulate the complicated physical process for this kind of structures. Meanwhile, a new numerical method called element differential method (EDM) is used to calculate the coupling problem because it has great advantages in solving multiphysics coupling problems. What is more, some experiments are used to obtain the leakages when the sealed structure is under service. And finally, by referring the experimental results, the authors establish a series of material parameter relationships for the sealed structure and also verify the reasonability of the proposed multi-physics coupling model.
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