Noncontact Laser Ultrasonic Inspection of Ceramic Matrix Composites (CMCs)

dc.contributor.author Quintero, R.
dc.contributor.author Simonetti, F.
dc.contributor.author Howard, P.
dc.contributor.author Friedl, J.
dc.contributor.author Sellinger, A.
dc.date 2018-02-17T22:00:24.000
dc.date.accessioned 2020-06-30T06:54:10Z
dc.date.available 2020-06-30T06:54:10Z
dc.date.issued 2016-01-01
dc.description.abstract <p>Ceramic matrix composites (CMCs) are poised to revolutionize jet engine technology by enabling operation temperatures well beyond those possible with current superalloys, while reducing active cooling requirements and engine weight. Manufacturing of parts formed by silicon-carbide (SiC) fibers in a SiC matrix is now well advanced, with the first non-structural static components entering service in 2017 with the CFM Leap® engine that features SiC/SiC turbine shrouds. In order to expand the scope of application of CMCs to rotating parts, such as turbine blades, much work is being conducted to understand and characterize the modes of failure of these materials at temperatures beyond 1,000 °C. In this context, the ability of nondestructively monitoring the formation and progression of damage in CMCs specimens during high-temperature mechanical testing is critical. However, the elevated temperature precludes the possibility of using sensors placed in direct contact with the specimen and therefore severely restricts the range of available NDE techniques. This paper provides the first experimental assessment of the feasibility of noncontact laser ultrasonic inspection of SiC/SiC flat coupons. An Nd:Yag laser is used to excite ultrasonic waves on one side of the specimen while a Michelson interferometer detects the signals emerging on the other side at the epicenter position. The lasers are mounted on synchronized linear stages to form C-scans as in conventional immersion ultrasonics while ablation damage to the surface of the specimen is prevented by operating the lasers at low power density. Despite the complex microstructure of the SiC/SiC material it is found that the measured waveforms are remarkably similar to those observed when conducting the same tests in aluminum specimens. Moreover, it is shown that it is possible to: a) image interlaminar defects caused by impacts, and b) monitor crack opening under tensile load. Finally, very good signal stability is observed when temperature is increased from 25 to 1,250 °C which confirms the feasibility of laser monitoring at high temperature and is consistent with the excellent thermal stability of CMC mechanical properties.</p>
dc.format.mimetype application/pdf
dc.identifier archive/lib.dr.iastate.edu/qnde/2016/abstracts/315/
dc.identifier.articleid 4838
dc.identifier.contextkey 9060520
dc.identifier.s3bucket isulib-bepress-aws-west
dc.identifier.submissionpath qnde/2016/abstracts/315
dc.identifier.uri https://dr.lib.iastate.edu/handle/20.500.12876/62078
dc.language.iso en
dc.relation.ispartofseries Review of Progress in Quantitative Nondestructive Evaluation
dc.source.bitstream archive/lib.dr.iastate.edu/qnde/2016/abstracts/315/042.pdf|||Fri Jan 14 23:32:11 UTC 2022
dc.subject.disciplines Materials Science and Engineering
dc.subject.disciplines Structures and Materials
dc.title Noncontact Laser Ultrasonic Inspection of Ceramic Matrix Composites (CMCs)
dc.type event
dc.type.genre event
dspace.entity.type Publication
relation.isSeriesOfPublication 289a28b5-887e-4ddb-8c51-a88d07ebc3f3
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