TESTING OF CFRP SPECIMENS WITH IMPACT DAMAGE USING THE ACOUSTIC EMISSION METHOD AND TENSOMETRY

Author:

Seryeznov A. N.,Stepanova L. N.,Kabanov S. I.,Ramazanov I. S.,Kuznetsov A. B.,Chernova V. V.

Abstract

Samples of carbon fiber T 700 were researched. They were subjected to impact damage, after which they were loaded with a static load until failure. Registration of defects was carried out using the method of acoustic emission (AE) and tensometry. In the process of loading the samples, the deformation and load were determined, at which the AE signals were located. An antenna consisting of piezoelectric acoustic emission transducers (PAE) and fiber optic sensors (FOS) was used to monitor defects. When the load changed from 80 to 100 kN, a jump in mechanical stresses was observed in the samples from 338 to 432 MPa, registered by the certified microprocessor-based high-speed tensometic system “Dynamics-3”. In this case, the average amplitude of the AE signals significantly decreased, starting from the load P = 80 kN, after which it increased at the load P = 110 kN. For sensors PAE 3 and VOD 2, located on the opposite side of the sample, where impact damage was absent, these changes in the amplitudes of the AE signals were less pronounced.

Publisher

Izdatel'skii dom Spektr, LLC

Subject

General Medicine

Reference25 articles.

1. Feygenbaum Yu. M., Mikolaychuk Yu. A., Metelkin E. S., Batov G. P. (2015). Place and role of non-destructive testing in the airworthiness maintenance system of composite structures. Nauchniy vestnik GosNII GA, (9), pp. 71 – 82. [in Russian language]

2. Ahmethanov R. S., Dubinin E. F. (2020). Method for the analysis of acoustic signals in the diagnosis of composite materials. Problemy mashinostroeniya i nadezhnosti mashin, (2), pp. 106 – 112. [in Russian language]

3. Smotrova S. A., Smotrov A. V. (2016). Features of damage to aircraft structures made of PCM. Results of fundamental research in applied problems of aircraft engineering: collection of articles, pp. 418 – 429. Moscow: Nauka. [in Russian language]

4. Chernyshev S. L., Zichenkov M. Ch., Smotrova S. A. et al. (2018). Technology for detecting subtle impact damage to power elements of aircraft structures made of polymer composite materials using shock-sensitive polymer coatings with optical properties. Konstruktsii iz kompozitsionnyh materialov, (4), pp. 48 – 53. [in Russian language]

5. Feygenbaum Yu. M., Dubinskiy S. V. (2013). The influence of accidental operational damage on the strength and service life of aircraft structures. Nauchniy vestnik MGTU GA, 187, pp. 83 – 91. [in Russian language]

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3