Strength analysis method of CMCs tip shroud structure considering random distribution of preform properties

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-07-04 DOI:10.1016/j.ast.2024.109374
Yue Zhou , Sheng Zhang , Huajun Zhang , Chengqian Dong , Xiguang Gao , Yingdong Song , Fang Wang
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Abstract

This paper considers the impact of the random distribution of yarn properties on the mechanical and failure behavior of ceramic matrix composites (CMCs) structures and proposes an integrated analysis method based on preform-structure. Tensile tests of CMCs tip shroud specimens were carried out, and the digital image correlation technique was used to record the deformation of the specimens in real-time during loading. Based on the actual structure, a preform model of the CMCs tip shroud was established, and the kernel density estimation method was used to obtain the distribution of the yarn cross-sectional area. The random distribution of the cross-sectional area is equivalent to material properties, simulating the dispersion of the performance of CMCs. The progressive damage method simulates the failure mode during the specimen's loading process. The peak load error is 1.5 %, and the failure modes such as transverse shear damage, stitching yarn fracture, and interlaminar separation were successfully predicted.

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考虑预成型性能随机分布的 CMC 尖端护罩结构强度分析方法
本文探讨了纱线性能的随机分布对陶瓷基复合材料(CMCs)结构的力学和失效行为的影响,并提出了一种基于预成型结构的综合分析方法。对 CMCs 尖端护罩试样进行了拉伸试验,并利用数字图像相关技术实时记录了加载过程中试样的变形情况。在实际结构的基础上,建立了 CMCs 尖端护罩的预成型模型,并利用核密度估计方法获得了纱线截面积的分布。截面积的随机分布相当于材料特性,模拟了 CMC 性能的分散性。渐进损伤法模拟试样加载过程中的破坏模式。峰值载荷误差为 1.5%,并成功预测了横向剪切破坏、缝合纱断裂和层间分离等破坏模式。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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