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Investigation of a Moire Based Crack Detection Technique for Propulsion Health MonitoringThe development of techniques for the health monitoring of the rotating components in gas turbine engines is of major interest to NASA s Aviation Safety Program. As part of this on-going effort several experiments utilizing a novel optical Moir based concept along with external blade tip clearance and shaft displacement instrumentation were conducted on a simulated turbine engine disk as a means of demonstrating a potential optical crack detection technique. A Moir pattern results from the overlap of two repetitive patterns with slightly different periods. With this technique, it is possible to detect very small differences in spacing and hence radial growth in a rotating disk due to a flaw such as a crack. The experiment involved etching a circular reference pattern on a subscale engine disk that had a 50.8 mm (2 in.) long notch machined into it to simulate a crack. The disk was operated at speeds up to 12 000 rpm and the Moir pattern due to the shift with respect to the reference pattern was monitored as a means of detecting the radial growth of the disk due to the defect. In addition, blade displacement data were acquired using external blade tip clearance and shaft displacement sensors as a means of confirming the data obtained from the optical technique. The results of the crack detection experiments and its associated analysis are presented in this paper.
Document ID
20120012546
Document Type
Technical Memorandum (TM)
Authors
Woike, Mark R.
(NASA Glenn Research Center Cleveland, OH, United States)
Abudl-Aziz, Ali
(NASA Glenn Research Center Cleveland, OH, United States)
Fralick, Gustave C.
(NASA Glenn Research Center Cleveland, OH, United States)
Wrbanek, John D.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 26, 2013
Publication Date
June 1, 2012
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-18210
NASA/TM-2012-217622
Meeting Information
Meeting: SMART Structures and Materials and Nondestructive Evaluation and Health Monitoring 2012
Location: San Diego, CA
Country: United States
Start Date: March 11, 2012
End Date: March 15, 2012
Sponsors: International Society for Optical Engineering
Funding Number(s)
WBS: WBS284848,02,03,03.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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