Large-Scale Laser Ultrasonic Facility for Aerospace Applications

dc.contributor.author Yawn, Kenneth
dc.contributor.author Drake, Thomas
dc.contributor.author Osterkamp, Mark
dc.contributor.author Chaung, S. Y.
dc.contributor.author Acres, Paul
dc.contributor.author Thomas, Mike
dc.contributor.author Kaiser, David
dc.contributor.author Marquardt, Chris
dc.contributor.author Filkins, Bob
dc.contributor.author Lorraine, Peter
dc.contributor.author Martin, Ken
dc.contributor.author Miller, Jim
dc.date 2018-02-14T08:49:27.000
dc.date.accessioned 2020-06-30T06:51:59Z
dc.date.available 2020-06-30T06:51:59Z
dc.date.copyright Fri Jan 01 00:00:00 UTC 1999
dc.date.issued 1999
dc.description.abstract <p>The use of composite materials for aerospace applications has markedly increased over the past two decades. Typically, a large percentage of composite aircraft components are fatigue and fracture critical, necessitating 100% inspection coverage. For composite materials, ultrasonic testing is the method of choice for detecting manufacturing defects which could lead to catastrophic failure during flight. As composite usage and part complexity increase, greater demands are placed on ultrasonic inspection systems. Projections of future composite usage (e.g. Joint Strike Fighter (JSF) program) show that the inspection workload may push current conventional automated ultrasonic inspection systems beyond practical limits. Conventional systems are typically slow, require significant setup time for highly contoured parts, and are generally inappropriate for in-service inspections where access is limited to a single side. Laser ultrasonic testing (Laser UT™) on the other hand offers many advantages over conventional automated ultrasonic systems: (1) the method is non-contact, requiring no couplants, (2) it can rapidly scan large areas, (3) it is able to inspect at angles far off normal, (4) it does not require expensive part fixtures, and (5) prior knowledge of the surface contour is not required. The optical scanning techniques used in make it capable of testing complex composite structures at speeds that cannot be matched by conventional mechanical scanning systems. These advantages in turn will reduce inspection costs and increase production throughput by as much as a factor of 10. Figure 1 illustrates the time savings of Laser UT™ over conventional UT as a function of part complexity.</p>
dc.format.mimetype application/pdf
dc.identifier archive/lib.dr.iastate.edu/qnde/1999/allcontent/48/
dc.identifier.articleid 3911
dc.identifier.contextkey 5820148
dc.identifier.s3bucket isulib-bepress-aws-west
dc.identifier.submissionpath qnde/1999/allcontent/48
dc.identifier.uri https://dr.lib.iastate.edu/handle/20.500.12876/61766
dc.language.iso en
dc.relation.ispartofseries Review of Progress in Quantitative Nondestructive Evaluation
dc.source.uri 10.1007/978-1-4615-4791-4_48
dc.title Large-Scale Laser Ultrasonic Facility for Aerospace Applications
dc.type event
dc.type.genre article
dspace.entity.type Publication
relation.isSeriesOfPublication 289a28b5-887e-4ddb-8c51-a88d07ebc3f3
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