• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

用于航空航天应用的陶瓷基复合材料的无损损伤评估。

Nondestructive damage evaluation in ceramic matrix composites for aerospace applications.

作者信息

Dassios Konstantinos G, Kordatos Evangelos Z, Aggelis Dimitrios G, Matikas Theodore E

机构信息

Department of Materials Science & Engineering, University of Ioannina, 45110 Ioannina, Greece.

出版信息

ScientificWorldJournal. 2013 Jul 11;2013:715945. doi: 10.1155/2013/715945. Print 2013.

DOI:10.1155/2013/715945
PMID:23935428
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC3725719/
Abstract

Infrared thermography (IRT) and acoustic emission (AE) are the two major nondestructive methodologies for evaluating damage in ceramic matrix composites (CMCs) for aerospace applications. The two techniques are applied herein to assess and monitor damage formation and evolution in a SiC-fiber reinforced CMC loaded under cyclic and fatigue loading. The paper explains how IRT and AE can be used for the assessment of the material's performance under fatigue. IRT and AE parameters are specifically used for the characterization of the complex damage mechanisms that occur during CMC fracture, and they enable the identification of the micromechanical processes that control material failure, mainly crack formation and propagation. Additionally, these nondestructive parameters help in early prediction of the residual life of the material and in establishing the fatigue limit of materials rapidly and accurately.

摘要

红外热成像(IRT)和声发射(AE)是评估用于航空航天应用的陶瓷基复合材料(CMC)损伤的两种主要无损检测方法。本文将这两种技术应用于评估和监测在循环和疲劳载荷作用下的碳化硅纤维增强CMC中的损伤形成和演变。本文阐述了IRT和AE如何用于评估材料在疲劳状态下的性能。IRT和AE参数专门用于表征CMC断裂过程中发生的复杂损伤机制,并且能够识别控制材料失效的微观力学过程,主要是裂纹的形成和扩展。此外,这些无损参数有助于早期预测材料的剩余寿命,并能快速、准确地确定材料的疲劳极限。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/31d6b32431ce/TSWJ2013-715945.015.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/fe383664d115/TSWJ2013-715945.001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/b25eee29e099/TSWJ2013-715945.002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/e5667d4c29d0/TSWJ2013-715945.003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/ba83a57420e6/TSWJ2013-715945.004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/d128f9710be5/TSWJ2013-715945.005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/df08295dc5eb/TSWJ2013-715945.006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/564f23cc340a/TSWJ2013-715945.007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/c806908b34a0/TSWJ2013-715945.008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/bc16d79238c6/TSWJ2013-715945.009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/eea0c5ccea94/TSWJ2013-715945.010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/27d779c3d993/TSWJ2013-715945.011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/ae7fa20be7af/TSWJ2013-715945.012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/18de3c996cfc/TSWJ2013-715945.013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/840bb42b6ea9/TSWJ2013-715945.014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/31d6b32431ce/TSWJ2013-715945.015.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/fe383664d115/TSWJ2013-715945.001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/b25eee29e099/TSWJ2013-715945.002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/e5667d4c29d0/TSWJ2013-715945.003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/ba83a57420e6/TSWJ2013-715945.004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/d128f9710be5/TSWJ2013-715945.005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/df08295dc5eb/TSWJ2013-715945.006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/564f23cc340a/TSWJ2013-715945.007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/c806908b34a0/TSWJ2013-715945.008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/bc16d79238c6/TSWJ2013-715945.009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/eea0c5ccea94/TSWJ2013-715945.010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/27d779c3d993/TSWJ2013-715945.011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/ae7fa20be7af/TSWJ2013-715945.012.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/18de3c996cfc/TSWJ2013-715945.013.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/840bb42b6ea9/TSWJ2013-715945.014.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/9f63/3725719/31d6b32431ce/TSWJ2013-715945.015.jpg

相似文献

1
Nondestructive damage evaluation in ceramic matrix composites for aerospace applications.用于航空航天应用的陶瓷基复合材料的无损损伤评估。
ScientificWorldJournal. 2013 Jul 11;2013:715945. doi: 10.1155/2013/715945. Print 2013.
2
A Micromechanical Fatigue Limit Stress Model of Fiber-Reinforced Ceramic-Matrix Composites under Stochastic Overloading Stress.随机过载应力作用下纤维增强陶瓷基复合材料的微观力学疲劳极限应力模型
Materials (Basel). 2020 Jul 24;13(15):3304. doi: 10.3390/ma13153304.
3
Damage Determination in Ceramic Composites Subject to Tensile Fatigue Using Acoustic Emission.使用声发射技术对承受拉伸疲劳的陶瓷复合材料进行损伤判定
Materials (Basel). 2018 Dec 6;11(12):2477. doi: 10.3390/ma11122477.
4
Fatigue Damage and Lifetime of SiC/SiC Ceramic-Matrix Composite under Cyclic Loading at Elevated Temperatures.高温循环载荷下SiC/SiC陶瓷基复合材料的疲劳损伤与寿命
Materials (Basel). 2017 Mar 31;10(4):371. doi: 10.3390/ma10040371.
5
Effect of Stochastic Loading on Tensile Damage and Fracture of Fiber-Reinforced Ceramic-Matrix Composites.随机载荷对纤维增强陶瓷基复合材料拉伸损伤与断裂的影响
Materials (Basel). 2020 May 28;13(11):2469. doi: 10.3390/ma13112469.
6
Comparisons of Damage Evolution between 2D C/SiC and SiC/SiC Ceramic-Matrix Composites under Tension-Tension Cyclic Fatigue Loading at Room and Elevated Temperatures.2D C/SiC和SiC/SiC陶瓷基复合材料在室温和高温下的拉-拉循环疲劳载荷作用下损伤演化的比较
Materials (Basel). 2016 Oct 19;9(10):844. doi: 10.3390/ma9100844.
7
Damage accumulation in cyclically-loaded glass-ceramic matrix composites monitored by acoustic emission.通过声发射监测循环加载的玻璃陶瓷基复合材料中的损伤累积。
ScientificWorldJournal. 2013 Nov 28;2013:869467. doi: 10.1155/2013/869467. eCollection 2013.
8
Modeling Tensile Damage and Fracture Behavior of Fiber-Reinforced Ceramic-Matrix Minicomposites.纤维增强陶瓷基微型复合材料拉伸损伤与断裂行为的建模
Materials (Basel). 2020 Sep 27;13(19):4313. doi: 10.3390/ma13194313.
9
Modeling Temperature-Dependent Vibration Damping in C/SiC Fiber-Reinforced Ceramic-Matrix Composites.C/SiC纤维增强陶瓷基复合材料中温度依赖型减振的建模
Materials (Basel). 2020 Apr 1;13(7):1633. doi: 10.3390/ma13071633.
10
Cyclic-Dependent Damage Evolution in Self-Healing Woven SiC/[Si-B-C] Ceramic-Matrix Composites at Elevated Temperatures.高温下自愈合编织 SiC/[Si-B-C] 陶瓷基复合材料中循环依赖损伤演化
Materials (Basel). 2020 Mar 24;13(6):1478. doi: 10.3390/ma13061478.